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EP1163451B1 - Rotary helical screw-type compressor - Google Patents

Rotary helical screw-type compressor Download PDF

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Publication number
EP1163451B1
EP1163451B1 EP00916927A EP00916927A EP1163451B1 EP 1163451 B1 EP1163451 B1 EP 1163451B1 EP 00916927 A EP00916927 A EP 00916927A EP 00916927 A EP00916927 A EP 00916927A EP 1163451 B1 EP1163451 B1 EP 1163451B1
Authority
EP
European Patent Office
Prior art keywords
housing
rotors
shaft journal
rotor
rotor housing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP00916927A
Other languages
German (de)
French (fr)
Other versions
EP1163451A1 (en
Inventor
Carsten Achtelik
Karl-Heinz Gilfert
Arno Heinz
Walter MÜRMANN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GHH Rand Schraubenkompressoren GmbH
Original Assignee
GHH Rand Schraubenkompressoren GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GHH Rand Schraubenkompressoren GmbH filed Critical GHH Rand Schraubenkompressoren GmbH
Publication of EP1163451A1 publication Critical patent/EP1163451A1/en
Application granted granted Critical
Publication of EP1163451B1 publication Critical patent/EP1163451B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/12Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/02Arrangements of bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/12Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C18/14Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C18/16Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0092Removing solid or liquid contaminants from the gas under pumping, e.g. by filtering or deposition; Purging; Scrubbing; Cleaning
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/04Heating; Cooling; Heat insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/06Silencing
    • F04C29/065Noise dampening volumes, e.g. muffler chambers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/06Silencing
    • F04C29/068Silencing the silencing means being arranged inside the pump housing

Definitions

  • the invention relates to a screw compressor in the Preamble of claim 1 mentioned type.
  • the invention is preferred, but not exclusively applicable to a screw compressor for generating a compressed air flow for the pneumatic transport of bulk goods, and especially one for attachment to one Silo vehicle trained screw processor.
  • Screw compressors work on the displacement principle Air compressors compared to other types of compressors have beneficial properties they especially for the pneumatic transport of bulk goods make suitable. This applies in particular to so-called dry running screw compressors, where the by a synchronous gear synchronized screw rotors no contact with each other and with the surrounding housing parts to have. There is therefore no lubrication in the compression chamber required so that they are kept oil-free can and therefore any contamination of the compressed air with oil is avoided. Due to the contact-free running of the rotors there is no wear in this area either the lifespan is reduced and there is no abrasion the contaminated air can contaminate.
  • screw compressors are due to their operating characteristics especially suitable for realizing high pressure ratios and are insensitive to short-term pressure increases, caused by the blockage of the compressed air Pipeline could be caused. Finally have they lighter weight and small size, what makes them special for mobile use e.g. B. suitable for silo vehicles makes.
  • GB-A-2 299 622 discloses a screw compressor according to the preamble Claim 1.
  • this screw compressor can be oil lubricated at the suction end of the rotor housing to be dispensed with.
  • the suction side Shaft journal of the rotors and their bearing arrangement surrounding Area of the suction-side housing cover directly for the inflow of air into the compressor room can be used.
  • a suction filter and / or Intake silencer is not available, however.
  • the invention has for its object by an improved Construction of the screw compressor in the area a simplified of the suction end of the compressor housing and improved air intake with filtering and / or sound absorption and a compact design of the compressor.
  • the intake filter and / or the intake housing containing the intake silencer directly attached to the suction end of the compressor housing resulting in a compact, space-saving and particularly robust construction for mobile use.
  • the housing of the compressor shown in Figs. 1-4 is composed of the following main parts: one Gear housing 1, a rotor housing 3, an inflow housing 4, a suction housing 5 and an oil tank 7.
  • the rotor housing 3 are two rotors, namely a main rotor 9 (profile teeth) and a secondary runner 11 (profile gaps) rotatably mounted with their helical teeth and interlock tooth gaps while sealing Form chambers, which are in the rotation of the rotor Move and reduce the axial direction and thereby the suctioned Compress air.
  • the rotors so driven that the right end in Figs. 1-3 Suction side is.
  • air gets through at the front of the Rotor housing 3 provided intake openings 13 sucked.
  • the air is from the interlocking teeth and tooth gaps of the rotor pair is conveyed to the left in the axial direction and occurs as compressed air at the pressure end the rotors at an upward pressure outlet 15 out.
  • the principle of operation of a screw compressor is known and will not be explained here.
  • the gear housing 1 has the shape of a disk-like Stand. In it, the drive shaft 17 is in bearings 16, 18 of the compressor, whose from the housing cover 49th protruding shaft journal 17a to a not shown Rotary drive is connected.
  • the gearbox 1 also contains a drive gear consisting of a on the drive shaft 17 fixed gear 19 and a fastened on the shaft journal 23 of the secondary rotor 11 Gear 21 through which the rotation of the drive shaft 17th with a suitable gear ratio to the secondary runner 11 is transmitted. Furthermore, in the gear housing 1, d. H.
  • the overall stator or disc-shaped gear housing 1 has on both sides at its lower base cantilevered mounting feet 31 with holes 33 for Fastening screws that secure the entire compressor a suitable pad, e.g. B. a vehicle attached can be.
  • the rotor housing 3 on the gear housing 1 by means of a flange connection 37 attached so that it projects freely from the gear housing 1.
  • the oil container 7, which has a flat box shape, is also attached to the gear housing 1 so that it is free of this cantilevered, approximately parallel to the rotor housing 3 and below it.
  • the side walls of the oil container 7 are provided with cooling fins 39.
  • Between the oil tank 7 and the bottom of the rotor housing 3 is a relatively wide air gap 41.
  • an oil pump 45 For the circulation of the oil inside the gearbox 1, or for generating an oil mist, an oil pump 45 is used, which surrounds and is driven by the drive shaft 17 becomes.
  • the housing of the oil pump 45 has a protruding outward Flange 47, which is used to center the gearbox housing 1 attached housing cover 49 is used.
  • the oil pump 45 is with 4 screws 51 (Fig. 3) and associated threaded holes attached to the gear housing 1.
  • Inlet openings that close the rotor housing 3 on the suction side 13 inflow housing 4 is at a distance surrounded by a large-volume intake housing 5 (in Fig. 2 and Fig. 3 only indicated by dash-dotted lines), the means Screws attached to a flange 67 of the rotor housing 3 is.
  • Intake housing 5 is an intake filter for filtering the intake air and / or a damper for sound absorption.
  • a filter 6 made of a suitable porous or air-permeable filter material.
  • the filter lies in an air flow path between an outer suction slot 69 and one arranged in an inner partition 71 Passage slot 73, with suction slot 69 and passage slot are offset from each other so that a longest possible flow path for the air between the Slits 69, 73 is formed by the filter 6.
  • the intake housing 5 is a modified embodiment of the intake housing 5, in which the through the suction slot 69 sucked in and through the deflection wall 71 Passage slot 73 redirects air e.g. from suitable Flows through perforated plates trained muffler 75, before it gets into the space surrounding the housing cover 69 and through the inflow openings 13 into the interior of the rotor housing 3 flows. It is also possible to use the intake housing 5 so that it is both a filter and also contains a silencer.
  • An advantage of the direct attachment of a filter and / or a silencer-containing suction housing 5 on the rotor housing 3 such that it is the inflow housing 4 at a distance surrounds is that a separate arrangement of a Filters and / or silencers, and a connecting line between this and the suction side of the compressor can. This makes it particularly simple, compact and robust arrangement achieved.
  • Another advantage is there in that the air sucked into the suction housing 5 Outside of the inflow housing containing the shaft journal bearings 4 flows around and cools before passing through the Inflow openings 13 into the interior of the rotor housing 3 entry. This ensures effective cooling of the suction side Rotor bearing achieved.
  • Fig. 6 shows the storage in an enlarged sectional view and sealing the shaft journal 55 of the rotor 9 in the inflow housing 4.
  • the shaft journal 57 of the other rotor 11 is mounted and sealed in an analogous manner.
  • the shaft journals provided with tool engagement (flats 63) 57 is formed in the manner of a hub Middle part of the inflow housing 4 by means of a roller bearing 53 stored between a shoulder of the shaft journal 57 and one engaging in an annular groove of the shaft journal Circlip 83 is arranged. Because on the suction side the rotors 9, 11, as stated above, no oil lubrication Rolling bearing 53 is preferably to take place as an encapsulated bearing with a lifetime grease filling trained so that there is no subsequent lubrication needed.
  • the race 85 which e.g. a commercial one
  • the race for a rolling bearing can be made of steel specially hardened peripheral surface.
  • Lip seal ring 87 is between this and an inner shoulder 4a of the inflow housing 4, a protective ring 89 is arranged, the inner periphery of the outer surface of the race 85 with a very small gap, but faces without contact.
  • the protective ring 89 and the lip seal ring 87 are on each other and on the inner shoulder 4a of the inflow housing 4 attached in the bore of the housing, preferably glued.
  • the function of the guard ring 89 is as follows:
  • the compressor generated during operation by sucking in air on the Suction side and blowing out compressed air at the pressure port 15 a compressed air flow, e.g. for pneumatic transport of dusty goods can serve.
  • a compressed air flow e.g. for pneumatic transport of dusty goods
  • the guard ring protects 89 the lip seal 87 in front of that dust particles underneath the sealing lips of the lip seal ring 87 and impair the sealing effect.
  • suction-side bearing arrangement has the further advantage that it can be withdrawn from the shaft journal 57 without the rotor 9 or 11 removed or the precise setting the rotors must be changed to each other.
  • the Remove the bearing and seal assembly from the journal can be done in the following ways:
  • FIG. 7 shows in a sectional view corresponding to FIG. 3, but on a larger scale the storage and sealing of the pressure side shaft journal 29, 23 of the rotors 9, 11 am pressure-side end of the rotor housing 3.
  • the one for the shaft journal 23 the rotor 11 is completely analog.
  • the shaft journal 29 is in the pressure-side end wall of the Rotor housing 3 by two roller bearings arranged side by side 91, 93 stored, the so-called angular contact ball bearings are trained.
  • Angular contact ball bearings that are commercially available are ball bearings, the balls of which are from the outside and inner race only on one or the other side of the radial central plane are encompassed.
  • the two angular contact ball bearings 91, 93 are arranged side by side in mirror symmetry. Such an arrangement of angular contact ball bearings has the Property that it is completely free of play in the axial direction.
  • a shaft nut 95 arranged on the shaft journal 29 puts the angular contact ball bearings 91, 93 in the axial direction on the Shafts journal 29 firmly.
  • the outer race of the Angular contact ball bearing 93 lies against an inner shoulder 97 of the Rotor housing 3 on.
  • This race 101 is made just like the one previously described 6, made of steel with a special hardened peripheral surface. On the surface of the race 101 lie against the sealing lips of a lip sealing ring 103, which the compression space of the rotor housing 3 against the oil-loaded Seals gearbox and bearing area.
  • the hardened and extremely precisely machined, e.g. polished Outer surface of the race 25 results in a particularly wear-reducing Contact surface for the sealing lips of the lips sealing rings 103.
  • labyrinth sealing ring 105 on its inner circumference has several adjacent ring ribs, that of the outer surface of the race 101 with very little Face the gap, but without contact and with this form a labyrinth gap.
  • the race 101 normally no contact with the labyrinth sealing ring 105 , it is still advantageous that the Race 101 also over the area of the labyrinth seal 105 extends.
  • the labyrinth gap seal is normal a non-contact seal, but it can be under extreme operating conditions under certain circumstances between the ring ribs of the labyrinth sealing ring 105 and the Race 101 take place.
  • race 101 If the race 101 is not would be present, there would be grooves on the shaft journal 29 are generated so that it is damaged and the Rotor 9 becomes unusable. Thanks to the presence of the race 101 only needs the race 101 in such a case to be replaced, so that the rotor 9, otherwise Damage free, can be used again.
  • the opening of the lantern 109 lies at a distance from with the cooling fins 39 provided top of the oil container 7 opposite. A straight access path to the mouth of the lantern 109 from below is blocked by the oil container 7.
  • FIG. 4 shows a perspective view from below of the compressor with the oil container 7 removed, so that the screw holes 44 for the attachment of the oil container 7 and the large connecting opening 43, through which the oil container communicates with the transmission housing, are visible in the end wall of the transmission housing 1 , 4, the suction housing 5 is removed from the suction-side end of the rotor housing 3, so that there is a clear view of the inflow housing 4 with its supporting ribs 14 and the inflow openings 13 leading to the interior of the rotor housing 3.
  • FIG. 4 also shows the mouth of the lantern (ventilation duct) 109 on the underside of the rotor housing 3. As can be seen from Fig.
  • projections 111 are provided on the underside of the rotor housing 3, which the mouth of the lantern 109 against linear access from the Shield side.
  • These projections 111 can be formed by oil drain channels. The mouth of the lantern 109 is thus at a protected location, to which a straight-line access path is neither possible from below (because of the oil container 7) nor from the side (because of the projections 111).
  • the race 101 attached to the shaft journal 29 additionally serves as a spacing element, which is used to maintain a very precisely dimensioned gap between the pressure-side end face of the rotor 9 or 11 and the end face 113 of the rotor housing 3 facing it serves.
  • a spacing element which is used to maintain a very precisely dimensioned gap between the pressure-side end face of the rotor 9 or 11 and the end face 113 of the rotor housing 3 facing it serves.
  • this gap is set and maintained precisely in such a way that, when the rotor housing 3 is machined, the distance a between the end face 113 facing the rotor 9 and the contact shoulder 97 for the roller bearing 93 is manufactured with very narrow tolerances to a predetermined value ,
  • the length b of the race 101, which is used as a spacing element between the roller bearing 97 and the end face of the rotor 9, is also ground with correspondingly precise tolerances to a value which has an oversize compared to the distance a , which is exactly the width of the between Corresponds to rotor 9 and the rotor housing 3 gap to be set.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Supercharger (AREA)

Abstract

The drive gear 19, 21 and the synchronizing gear 25, 27 for the two rotors 9,11 of a screw compressor are both located at the pressurized end of the rotor housing 3. At the suction end of the rotor housing 3 is only the bearing 53 for the suction side shaft journal 55, 57 that is free of oil lubrication. Inlet openings 13 in a suction side inlet housing are located in such a way that the intake air cools the oil-free shaft bearing 53. Each shaft journal has a tool interface 63 accessible through the inlet housing on which to attach a rotating tool. The inlet housing 4 can be removed from the shaft journal 55, 57 together with the bearing 53 and seal 87, for example to exchange the bearing, without having to remove the rotors 9, 11 or without throwing off their adjustment.

Description

Die Erfindung betrifft einen Schraubenkompressor von der im Oberbegriff des Anspruchs 1 genannten Art. Die Erfindung ist vorzugsweise, aber nicht ausschließlich anwendbar bei einem Schraubenkompressor für die Erzeugung eines Druckluftstroms für den pneumatischen Transport von Schüttgütern, und insbesondere bei einem für die Anbringung an einem Silofahrzeug ausgebildeten Schraubenkompessor.The invention relates to a screw compressor in the Preamble of claim 1 mentioned type. The invention is preferred, but not exclusively applicable to a screw compressor for generating a compressed air flow for the pneumatic transport of bulk goods, and especially one for attachment to one Silo vehicle trained screw processor.

Schraubenkompressoren sind nach dem Verdrängerprinzip arbeitende Luftverdichter, die im Vergleich zu anderen Kompressortypen vorteilhafte Eigenschaften aufweisen, die sie besonders für den pneumatischen Transport von Schüttgütern geeignet machen. Dies gilt insbesondere für sogenannte trockenlaufende Schraubenkompressoren, bei denen die durch ein Gleichlaufgetriebe synchronisierten Schraubenrotoren keine Berührung miteinander und mit den umgebenden Gehäuseteilen haben. Im Kompressionsraum ist deshalb keine Schmierung erforderlich, so daß dieser ölfrei gehalten werden kann und somit jegliche Verunreinigung der Druckluft mit Öl vermieden wird. Durch den berührungsfreien Lauf der Rotoren findet auch in diesem Bereich kein Verschleiß statt, der die Lebensdauer reduziert, und es entsteht kein Abrieb, der die geförderte Luft verunreinigen kann. Schraubenkompressoren sind aufgrund ihrer Betriebscharakteristik vor allem zur Realisierung hoher Druckverhältnisse geeignet und sind unempfindlich gegen kurzfristige Drucksteigerungen, die durch Verstopfung der mit der Druckluft beaufschlagten Rohrleitung verursacht werden könnten. Schließlich haben sie geringeres Gewicht und geringe Abmessungen, was sie besonders für mobilen Einsatz z. B. an Silofahrzeugen geeignet macht.Screw compressors work on the displacement principle Air compressors compared to other types of compressors have beneficial properties they especially for the pneumatic transport of bulk goods make suitable. This applies in particular to so-called dry running screw compressors, where the by a synchronous gear synchronized screw rotors no contact with each other and with the surrounding housing parts to have. There is therefore no lubrication in the compression chamber required so that they are kept oil-free can and therefore any contamination of the compressed air with oil is avoided. Due to the contact-free running of the rotors there is no wear in this area either the lifespan is reduced and there is no abrasion the contaminated air can contaminate. screw compressors are due to their operating characteristics especially suitable for realizing high pressure ratios and are insensitive to short-term pressure increases, caused by the blockage of the compressed air Pipeline could be caused. Finally have they lighter weight and small size, what makes them special for mobile use e.g. B. suitable for silo vehicles makes.

Bei vielen bisher bekannten Schraubenkompressoren, insbesondere für den Einsatz von Silofahrzeugen, ist das Antriebsgetriebe für die Rotoren an dem einem Ende und das Synchronisiergetriebe am anderen Ende der Rotoren angeordnet. Ölschmierung ist deshalb sowohl am druckseitigen als auch am saugseitigen Ende der Rotoren erforderlich. Das Ansaugen der Luft erfolgt über ein Filter und/oder einen Schalldämpfer, die als vom Kompressorgehäuse separate Einheiten ausgebildet und mit dem Kompressorgehäuse über eine Ansaugleitung verbunden sind, die unter Umgehung des Synchronisiergetriebes in der Nähe des saugseitigen Endes des Rotorgehäuses in dieses mündet. Das Vorhandensein von Ölschmierung an der Saugseite des Rotorgehäuses ist unerwünscht, weil es die Gefahr der Verunreinigung der Luft mit Öl erhöht. Die Ausbildung des Ansaugfilters und/oder Schalldämpfers getrennt vom eigentlichen Kompressorgehäuses läuft der Forderung nach kompakter, robuster und gewichtssparender Bauweise entgegen.In many previously known screw compressors, in particular for the use of silo vehicles is the drive gear for the rotors at one end and the synchronizing gear arranged at the other end of the rotors. oil lubrication is therefore on the pressure side as well as on the suction side End of the rotors required. Sucking the Air comes through a filter and / or a silencer, which are designed as separate units from the compressor housing and with the compressor housing via a suction line are connected, bypassing the synchronizing gear near the suction end of the rotor housing in this ends. The presence of oil lubrication on the Suction side of the rotor housing is undesirable because it is the Risk of air contamination with oil increases. Training of the intake filter and / or muffler separately the demand runs from the actual compressor housing after compact, robust and weight-saving construction opposite.

Das Dokument GB-A-2 299 622 offenbart einen Schraubenkompressor gemäß dem Oberbegriff Anspruch 1. Durch die Anordnung sowohl des Antriebs- als auch des Synchronisiergetriebes an der Druckseite des Rotorgehäuses dieses Schraubenkompressors kann am saugseitigen Ende des Rotorgehäuses auf Ölschmierung verzichtet werden. Ferner kann der die saugseitigen Wellenzapfen der Rotoren und deren Lageranordnung umgebende Bereich des saugseitigen Gehäusedeckels direkt für das Einströmen der Luft in den Kompressorraum genutzt werden. Ein Ansaugfilter und/oder Ansaugschalldämpfer ist jedoch nicht vorhanden. GB-A-2 299 622 discloses a screw compressor according to the preamble Claim 1. By arranging both the drive and the synchronizing gear on the pressure side of the rotor housing of this screw compressor can be oil lubricated at the suction end of the rotor housing to be dispensed with. Furthermore, the suction side Shaft journal of the rotors and their bearing arrangement surrounding Area of the suction-side housing cover directly for the inflow of air into the compressor room can be used. A suction filter and / or Intake silencer is not available, however.

Der Erfindung liegt die Aufgabe zugrunde, durch eine verbesserte Konstruktion des Schraubenkompressors im Bereich des saugseitigen Endes des Kompressorgehäuses eine vereinfachte und verbesserte Luftansaugung mit Filterung und/oder Schalldämpfung und eine kompakte Bauweise des Kompressors zu ermöglichen.The invention has for its object by an improved Construction of the screw compressor in the area a simplified of the suction end of the compressor housing and improved air intake with filtering and / or sound absorption and a compact design of the compressor.

Die erfindungsgemäße Lösung der Aufgabe ist im Anspruch 1 angegeben. Die Unteransprüche beziehen sich auf vorteilhafte weitere Ausgestaltungen der Erfindung. The achievement of the object is in claim 1 specified. The sub-claims relate to advantageous further refinements of the invention.

Erfindungsgemäß ist ein das Ansaugfilter und/oder den Ansaugschalldämpfer enthaltendes Ansauggehäuse direkt an das saugseitige Ende des Kompressorgehäuses angesetzt, wodurch sich eine kompakte, platzsparende und für mobilen Einsatz besonders robuste Konstruktion ergibt.According to the invention, the intake filter and / or the intake housing containing the intake silencer directly attached to the suction end of the compressor housing, resulting in a compact, space-saving and particularly robust construction for mobile use.

Eine Ausführungsform des erfindungsgemäßen Kompressors wird anhand der Zeichnungen näher erläutert. Es zeigt:

Fig. 1
eine perspektivische Ansicht des Kompressors mit Ansaugfilter, von der Seite gesehen;
Fig. 2
einen Vertikalschnitt durch den Kompressor von Fig. 1;
Fig. 3
einen horizontalen Schnitt durch den Kompressor in der die beiden Rotorachsen enthaltenden Ebene;
Fig. 4
eine weitere perspektivische Darstellung des Kompressors in Untersicht, vom saugseitigen Ende her gesehen, bei abgenommenem Ansauggehäuse und Ölbehälter;
Fig. 5
ein Detail der perspektivischen Ansicht gemäß Fig. 1, mit einer geänderten Ausführungsform des Ansauggehäuses;
Fig. 6
ein vergrößertes Detail der Schnittdarstellung von Fig. 2 im Bereich der saugseitigen Rotorlagerung.
Fig. 7
ein vergrößertes Detail der Schnittdarstellung von Fig. 3 im Bereich der druckseitigen Rotorlagerung.
An embodiment of the compressor according to the invention is explained in more detail with reference to the drawings. It shows:
Fig. 1
a perspective view of the compressor with suction filter, seen from the side;
Fig. 2
a vertical section through the compressor of Fig. 1;
Fig. 3
a horizontal section through the compressor in the plane containing the two rotor axes;
Fig. 4
a further perspective view of the compressor from below, seen from the suction end, with the suction housing and oil tank removed;
Fig. 5
a detail of the perspective view of Figure 1, with a modified embodiment of the suction housing.
Fig. 6
an enlarged detail of the sectional view of FIG. 2 in the area of the suction-side rotor bearing.
Fig. 7
an enlarged detail of the sectional view of Fig. 3 in the region of the pressure-side rotor bearing.

In allen Figuren sind gleiche oder einander entsprechende Teile mit gleichen Bezugszeichen bezeichnet.All figures are the same or correspond to each other Parts labeled with the same reference numerals.

Das Gehäuse des in Fig. 1 - 4 dargestellten Kompressors setzt sich aus den folgenden Hauptteilen zusammen: einem Getriebegehäuse 1, einem Rotorgehäuse 3, einem Einströmgehäuse 4, einem Ansauggehäuse 5 und einem Ölbehälter 7. In dem Rotorgehäuse 3 sind zwei Rotoren, nämlich ein Hauptläufer 9 (Profilzähne) und ein Nebenläufer 11 (Profillükken) drehbar gelagert, die mit ihren schraubenförmigen Zähnen und Zahnlücken ineinandergreifen und dabei abgedichtete Kammern bilden, die sich bei der Drehung des Rotors in Axialrichtung verschieben und verkleinern und dabei die angesaugte Luft komprimieren. Bei Betrieb werden die Rotoren so angetrieben, daß ihr in den Fig. 1 - 3 rechtes Ende die Saugseite ist. Hier wird Luft durch an der Stirnseite des Rotorgehäuses 3 vorgesehene Einströmöffnungen 13 angesaugt. Die Luft wird von den ineinandergreifenden Zähnen und Zahnlücken des Rotorpaares in Axialrichtung nach links gefördert und tritt als komprimierte Luft am druckseitigen Ende der Rotoren an einem nach oben gerichteten Druckauslaß 15 aus. Das Funktionsprinzip eines Schraubenkompressors ist bekannt und wird hier nicht näher erläutert. The housing of the compressor shown in Figs. 1-4 is composed of the following main parts: one Gear housing 1, a rotor housing 3, an inflow housing 4, a suction housing 5 and an oil tank 7. In the rotor housing 3 are two rotors, namely a main rotor 9 (profile teeth) and a secondary runner 11 (profile gaps) rotatably mounted with their helical teeth and interlock tooth gaps while sealing Form chambers, which are in the rotation of the rotor Move and reduce the axial direction and thereby the suctioned Compress air. In operation, the rotors so driven that the right end in Figs. 1-3 Suction side is. Here air gets through at the front of the Rotor housing 3 provided intake openings 13 sucked. The air is from the interlocking teeth and tooth gaps of the rotor pair is conveyed to the left in the axial direction and occurs as compressed air at the pressure end the rotors at an upward pressure outlet 15 out. The principle of operation of a screw compressor is known and will not be explained here.

Das Getriebegehäuse 1 hat die Form eines scheibenartigen Ständers. In ihm ist in Lagern 16, 18 die Antriebswelle 17 des Kompressors gelagert, deren aus dem Gehäusedeckel 49 herausragender Wellenzapfen 17a an einen nicht dargestellten Drehantrieb angeschlossen ist. Das Getriebegehäuse 1 enthält ferner ein Antriebsgetriebe, bestehend aus einem auf der Antriebswelle 17 befestigten Zahnrad 19 und einem auf dem Wellenzapfen 23 des Nebenläufers 11 befestigten Zahnrad 21, durch welches die Drehung der Antriebswelle 17 mit geeignetem Übersetzungsverhältnis auf den Nebenläufer 11 übertragen wird. Ferner ist im Getriebegehäuse 1, d. h. ebenfalls auf der Druckseite der Rotoren 9, 11, das für den Synchronlauf dieser Rotoren sorgende Synchronisiergetriebe untergebracht, bestehend aus den ineinandergreifenden Zahnrädern 25, 27, die auf dem Wellenzapfen 23 des Nebenläufers bzw. auf dem Wellenzapfen 29 des Hauptläufers 9 befestigt sind. Das Synchronisiergetriebe sorgt dafür, daß die Rotoren 9, 11 mit sehr geringem Spiel, aber berührungsfrei ineinander greifen. Hierdurch ist es möglich, ohne jede Ölschmierung zwischen den Rotoren 9, 11 auszukommen, d.h. einen trockenlaufenden Kompressor zu realisieren. Dies ist besonders wichtig, wenn der Kompressor einen von Ölrückständen absolut freien Luftstrom zur pneumatischen Förderung von empfindlichem Fördergut erzeugen soll.The gear housing 1 has the shape of a disk-like Stand. In it, the drive shaft 17 is in bearings 16, 18 of the compressor, whose from the housing cover 49th protruding shaft journal 17a to a not shown Rotary drive is connected. The gearbox 1 also contains a drive gear consisting of a on the drive shaft 17 fixed gear 19 and a fastened on the shaft journal 23 of the secondary rotor 11 Gear 21 through which the rotation of the drive shaft 17th with a suitable gear ratio to the secondary runner 11 is transmitted. Furthermore, in the gear housing 1, d. H. also on the pressure side of the rotors 9, 11, which for the Synchronization of these rotors ensures synchronizing gears housed, consisting of the intermeshing gears 25, 27 on the shaft journal 23 of the secondary rotor or attached to the shaft journal 29 of the main rotor 9 are. The synchronizing gear ensures that the rotors 9, 11 with very little play, but without contact to grab. This makes it possible without any Oil lubrication between the rotors 9, 11, i.e. to realize a dry running compressor. This is especially important if the compressor has any oil residue absolutely free air flow for pneumatic conveying of sensitive goods to be conveyed.

Das ingesamt ständer- oder scheibenförmig ausgebildete Getriebegehäuse 1 hat an seiner unteren Standfläche beiderseits vorkragende Befestigungsfüße 31 mit Löchern 33 für Befestigungsschrauben, mit denen der gesamte Kompressor an einer geeigneten Unterlage, z. B. einem Fahrzeug, befestigt werden kann. The overall stator or disc-shaped gear housing 1 has on both sides at its lower base cantilevered mounting feet 31 with holes 33 for Fastening screws that secure the entire compressor a suitable pad, e.g. B. a vehicle attached can be.

Zum Zweck der ständigen Schmierung des Antriebsgetriebes 19, 21 und des Synchronisiergetriebes 25, 27 wird in den Bereich des Verzahnungseingriffs beider Getriebe Schmieröl eingespritzt, das durch eine Ölpumpe 45 ständig umgewälzt wird. Ein erforderlicher Vorrat an Öl wird in dem Ölbehälter 7 vorrätig gehalten, der mit dem Innenraum des Getriebegehäuses 1 kommuniziert. Mit den Wellenzapfen 23, 29 der Rotoren 9, 11 wirken Dichtungsanordnungen 35 zusammen, die den Ölzutritt zu den Rotoren 9, 11 und damit zum Verdichtungsraum des Kompressors verhindern. Diese Dichtungsanordnungen werden noch im einzelnen erläutert. Da das Antriebsgetriebe 19, 21 und das Synchronisiergetriebe 25, 27 beide auf der Druckseite der Rotoren 9, 11 angeordnet sind und die saugseitigen Lager der Rotoren fettgefüllt sind, wie noch erläutert wird, wird an der Saugseite der Rotoren (in Fig. 1 - 3 rechts) keine Ölschmierung benötigt. Es sind deshalb auch keine Ölleitungen, wie bei der üblichen Bauart von Schraubenkompressoren, erforderlich, durch die Öl von der Druckseite zur Saugseite des Rotors und zurück zirkulieren kann.For the purpose of constant lubrication of the drive gear 19, 21 and the synchronizing gear 25, 27 is in the Gearing area of both gears Lube oil injected, which is constantly circulated by an oil pump 45 becomes. A required supply of oil is in the oil container 7 kept in stock with the interior of the gearbox 1 communicates. With the shaft journals 23, 29 the Rotors 9, 11 cooperate sealing arrangements 35 which the oil access to the rotors 9, 11 and thus to the compression chamber prevent the compressor. These sealing arrangements are explained in detail. Because the drive gear 19, 21 and the synchronizing gear 25, 27 both are arranged on the pressure side of the rotors 9, 11 and the suction side bearings of the rotors are filled with grease, as will be explained, is on the suction side of the rotors (in Fig. 1-3 right) no oil lubrication required. There are therefore no oil lines, as with the usual design of screw compressors, required by the oil of circulate the pressure side to the suction side of the rotor and back can.

Wie aus Fig. 1 und Fig. 3 ersichtlich, ist das Rotorgehäuse 3 am Getriebegehäuse 1 mittels einer Flanschverbindung 37 so befestigt, daß es vom Getriebegehäuse 1 frei auskragt. Auch der Ölbehälter 7, der eine flache Kastenform hat, ist am Getriebegehäuse 1 so befestigt, daß er von diesem frei auskragt, und zwar etwa parallel zum Rotorgehäuse 3 und unterhalb desselben. Die Seitenwände des Ölbehälters 7 sind mit Kühlrippen 39 versehen. Zwischen dem Ölbehälter 7 und der Unterseite des Rotorgehäuses 3 befindet sich ein relativ breiter Luftzwischenraum 41. Mit dieser Anordnung des Rotorgehäuses 3 und Ölbehälters 7 relativ zueinander und zum Getriebegehäuse 1 wird erreicht, daß die Wärmeübertragung, insbesondere Wärmeleitung, vom Rotorgehäuse 3 zum Ölbehälter 7 auf ein Minimum reduziert wird. Damit wird vermieden, daß die bei Betrieb des Kompressors im Rotorgehäuse 3 durch die Luftverdichtung erzeugte Wärme zu einer unerwünschten Aufheizung des Ölvorrats im Ölbehälter 7 führt, obwohl der Ölbehälter 7 direkt mit dem Getriebegehäuse verbunden ist. Durch die direkte Befestigung (Flanschverbindung) des Ölbehälters 7 an dem Getriebegehäuse 1 kann dieser mit dem Getriebegehäuse 1 über eine große Öffnung 43 kommunizieren. Gesonderte Ölleitungen entfallen.As can be seen from FIGS. 1 and 3, the rotor housing 3 on the gear housing 1 by means of a flange connection 37 attached so that it projects freely from the gear housing 1. The oil container 7, which has a flat box shape, is also attached to the gear housing 1 so that it is free of this cantilevered, approximately parallel to the rotor housing 3 and below it. The side walls of the oil container 7 are provided with cooling fins 39. Between the oil tank 7 and the bottom of the rotor housing 3 is a relatively wide air gap 41. With this arrangement of the rotor housing 3 and oil container 7 relative to each other and to the gear housing 1 it is achieved that the heat transfer, in particular heat conduction, from the rotor housing 3 to the oil tank 7 is reduced to a minimum. So that will avoided that when operating the compressor in the rotor housing 3 Heat generated by air compression into one undesired heating of the oil supply in the oil tank 7 leads, although the oil tank 7 directly with the gear housing connected is. Through direct attachment (Flange connection) of the oil tank 7 on the gear housing 1 can this with the gear housing 1 via a communicate large opening 43. There are no separate oil lines.

Für die Zirkulation des Öls im Inneren des Getriebegehäuses 1, bzw. zum Erzeugen eines Ölnebels, dient eine Ölpumpe 45, die die Antriebswelle 17 umgibt und von dieser angetrieben wird. Das Gehäuse der Ölpumpe 45 hat einen nach außen abstehenden Flansch 47, der zur Zentrierung des am Getriebegehäuse 1 befestigten Gehäusedeckels 49 dient. Die Ölpumpe 45 wird mit 4 Schrauben 51 (Fig. 3) und zugehörigen Gewindebohrungen am Getriebegehäuse 1 befestigt.For the circulation of the oil inside the gearbox 1, or for generating an oil mist, an oil pump 45 is used, which surrounds and is driven by the drive shaft 17 becomes. The housing of the oil pump 45 has a protruding outward Flange 47, which is used to center the gearbox housing 1 attached housing cover 49 is used. The oil pump 45 is with 4 screws 51 (Fig. 3) and associated threaded holes attached to the gear housing 1.

Aufgrund der Anordnung des Antriebsgetriebes 19, 21 und Synchronisiergetriebes 25, 27 auf der Druckseite der Rotoren 9, 11 befinden sich auf deren Saugseite lediglich die Lager 53 für die saugseitigen Wellenzapfen 55, 57 in einem das Rotorgehäuse 3 saugseitig abschließenden Einströmgehäuse 4, in dem zwischen Stützrippen 14 die zum Innenraum des Rotorgehäuses 3 führenden Einströmöffnungen 13 ausgebildet sind. Den Lagern 53 sind mit den wellenzapfen 55, 57 zusammenwirkende Dichtungsanordnungen 61 vorgelagert, die noch erläutert werden. Due to the arrangement of the drive gear 19, 21 and Synchronizing gear 25, 27 on the pressure side of the rotors 9, 11 are only on the suction side Bearing 53 for the suction-side shaft journal 55, 57 in one the rotor housing 3 closing inlet inlet 4, in which between the support ribs 14 to the interior of the rotor housing 3 leading inflow openings 13 are formed are. The bearings 53 are with the shaft journals 55, 57 cooperating sealing arrangements 61 upstream, the still to be explained.

Die über die Lager 53 vorstehenden Enden der saugseitigen Wellenzapfen 55, 57 der Rotoren 9, 11 sind mit einem Werkzeugeingriff für den Ansatz eines Drehwerkzeuges versehen. Bei dem in Fig. 6 gezeigten Ausführungsbeispiel besteht der Werkzeugeingriff aus zwei Abflachungen 63 für den Ansatz eines Maulschlüssels. Der Werkzeugeingriff kann aber auch die Form eines Vierkants, Sechskants, eines Innensechskants oder dergleichen aufweisen. Die mit dem Werkzeugeingriff versehenen Wellenzapfen 55, 57 sind durch Abnehmen eines auf dem Einströmgehäuse 4 mit Schrauben befestigten Gehäusedeckels 65 leicht zugänglich.The ends of the suction side projecting beyond the bearings 53 Shaft journals 55, 57 of the rotors 9, 11 are in tool engagement for the approach of a turning tool. In the embodiment shown in Fig. 6 there is Tool engagement from two flats 63 for the approach a wrench. Tool intervention can also the shape of a square, hexagon, an internal hexagon or the like. The one with the tool intervention provided shaft journals 55, 57 are by removing one on the inflow housing 4 with the housing cover fastened with screws 65 easily accessible.

Durch Ansetzen eines Drehwerkzeugs an einem oder beiden saugseitigen Wellenzapfen der Rotoren 9, 11 ist es möglich, diese von Hand zu drehen und dadurch eine Blockierung der Rotoren zu beseitigen, die auftreten kann, wenn staubförmiges Gut, das durch den vom Kompressor erzeugten Druckluftstrom gefördert werden soll, in Folge eines Materialrückschlages in das Innere des Rotorgehäuses 3 und zwischen die Rotoren 9, 11 gelangt. Durch Drehen des Antriebswellenzapfens 17a kann eine solche Blockierung in der Regel nicht beseitigt werden, da das Antriebsgetriebe 19, 21 eine zu hohe Übersetzung hat.By attaching a turning tool to one or both suction-side shaft journal of the rotors 9, 11 it is possible turning them by hand and thereby blocking the Eliminate rotors that can occur when dusty Well, that thanks to the compressed air flow generated by the compressor to be funded as a result of a material setback in the interior of the rotor housing 3 and between the Rotors 9, 11 arrives. By turning the drive shaft journal Such a block can usually not be eliminated since the drive gear 19, 21 a too has high translation.

Das das Rotorgehäuse 3 saugseitig abschließende, die Einströmöffnungen 13 aufweisende Einströmgehäuse 4 ist mit Abstand von einem großvolumigen Ansauggehäuse 5 umgeben (in Fig. 2 und Fig. 3 nur strichpunktiert angedeutet), das mittels Schrauben an einem Flansch 67 des Rotorgehäuses 3 befestigt ist. In diesem direkt am Rotorgehäuse 3 befestigten Ansauggehäuse 5 befindet sich ein Ansaugfilter zum Filtern der angesaugten Luft und/oder ein Dämpfer zur Schalldämpfung. Bei der in Fig. 1 gezeigten Ausführungsform enthält das Ansauggehäuse 5 ein Filter 6 aus einem geeigneten porösen bzw. luftdurchlässigen Filtermaterial. Das Filter liegt in einem Luftströmungsweg zwischen einem äußeren Ansaugschlitz 69 und einem in einer inneren Trennwand 71 angeordneten Durchlaßschlitz 73, wobei Ansaugschlitz 69 und Durchlaßschlitz so gegeneinander versetzt sind, daß ein möglichst langer Strömungsweg für die Luft zwischen den Schlitzen 69, 73 durch das Filter 6 gebildet wird.The inlet openings that close the rotor housing 3 on the suction side 13 inflow housing 4 is at a distance surrounded by a large-volume intake housing 5 (in Fig. 2 and Fig. 3 only indicated by dash-dotted lines), the means Screws attached to a flange 67 of the rotor housing 3 is. In this fastened directly to the rotor housing 3 Intake housing 5 is an intake filter for filtering the intake air and / or a damper for sound absorption. In the embodiment shown in Fig. 1 contains the suction housing 5 a filter 6 made of a suitable porous or air-permeable filter material. The filter lies in an air flow path between an outer suction slot 69 and one arranged in an inner partition 71 Passage slot 73, with suction slot 69 and passage slot are offset from each other so that a longest possible flow path for the air between the Slits 69, 73 is formed by the filter 6.

In Fig. 5 ist eine abgeänderte Ausführungsform des Ansauggehäuses 5 dargestellt, bei dem die durch den Ansaugschlitz 69 angesaugte und durch die Umlenkwand 71 mit Durchlaßschlitz 73 umgelenkte Luft einen z.B. aus geeigneten Lochblechen ausgebildeten Schalldämpfer 75 durchströmt, bevor sie in den den Gehäusedeckel 69 umgebenden Raum gelangt und durch die Einströmöffnungen 13 in den Innenraum des Rotorgehäuses 3 einströmt. Es ist auch möglich, das Ansauggehäuse 5 so auszubilden, daß es sowohl ein Filter als auch einen Schalldämpfer enthält.5 is a modified embodiment of the intake housing 5, in which the through the suction slot 69 sucked in and through the deflection wall 71 Passage slot 73 redirects air e.g. from suitable Flows through perforated plates trained muffler 75, before it gets into the space surrounding the housing cover 69 and through the inflow openings 13 into the interior of the rotor housing 3 flows. It is also possible to use the intake housing 5 so that it is both a filter and also contains a silencer.

Ein Vorteil der direkten Anbringung des ein Filter und/oder einen Schalldämpfer enthaltenden Ansauggehäuses 5 am Rotorgehäuse 3 derart, daß es das Einströmgehäuse 4 mit Abstand umgibt, besteht darin, daß eine separate Anordnung eines Filters und/oder Schalldämpfers, und eine Verbindungsleitung zwischen diesem und der Saugseite des Kompressors entfallen kann. Dadurch wird eine besonders einfache, kompakte und robuste Anordnung erzielt. Ein weiterer Vorteil besteht darin, daß die in das Ansauggehäuse 5 angesaugte Luft die Außenseite des die Wellenzapfenlager enthaltenden Einströmgehäuses 4 umströmt und kühlt, bevor sie durch die Einströmöffnungen 13 in das Innere des Rotorgehäuses 3 eintritt. Hierdurch wird eine wirksame Kühlung der saugseitigen Rotorlager erzielt.An advantage of the direct attachment of a filter and / or a silencer-containing suction housing 5 on the rotor housing 3 such that it is the inflow housing 4 at a distance surrounds is that a separate arrangement of a Filters and / or silencers, and a connecting line between this and the suction side of the compressor can. This makes it particularly simple, compact and robust arrangement achieved. Another advantage is there in that the air sucked into the suction housing 5 Outside of the inflow housing containing the shaft journal bearings 4 flows around and cools before passing through the Inflow openings 13 into the interior of the rotor housing 3 entry. This ensures effective cooling of the suction side Rotor bearing achieved.

Fig. 6 zeigt in vergrößerter Schnittdarstellung die Lagerung und Abdichtung des Wellenzapfens 55 des Rotors 9 in dem Einströmgehäuse 4. Der Wellenzapfen 57 des anderen Rotors 11 ist in analoger Weise gelagert und abgedichtet. Der mit dem Werkzeugeingriff (Abflachungen 63) versehene Wellenzapfen 57 ist in dem nach Art einer Nabe ausgebildeten Mittelteil des Einströmgehäuse 4 mittels eines Wälzlagers 53 gelagert, das zwischen einer Schulter des Wellenzapfens 57 und einem in einer Ringnut des Wellenzapfens eingreifenden Sicherungsring 83 angeordnet ist. Da auf der Saugseite der Rotoren 9, 11, wie oben ausgeführt, keinerlei Ölschmierung stattfinden soll, ist das Wälzlager 53 vorzugsweise als gekapseltes Lager mit einer Lebensdauer-Fettfüllung ausgebildet, so daß es keinerlei nachträgliche Schmierung benötigt. Anschließend an das Wälzlager 53 ist auf dem Wellenzapfen 57 ein Laufring 85 befestigt, vorzugsweise aufgeschrumpft. Der Laufring 85, der z.B. ein handelsüblicher Laufring für ein Wälzlager sein kann, besteht aus Stahl mit speziell gehärteter Umfangsfläche. Mit dieser wirken zwei Dichtlippen eines Lippen dichtrings 87 zusammen, der den Innenraum des Rotorgehäuses 3 gegen die Wälzlager 53 abdichtet. Auf der dem Rotorgehäuse 3 zugewandten Seite des Lippendichtrings 87 ist zwischen diesem und einer Innenschulter 4a des Einströmgehäuses 4 ein Schutzring 89 angeordnet, dessen Innenumfang der Außenfläche des Laufrings 85 mit einem sehr kleinen Spalt, aber berührungsfrei gegenübersteht. Der Schutzring 89 und der Lippendichtring 87 sind aneinander und an der Innenschulter 4a des Einströmgehäuses 4 anliegend in der Bohrung des Gehäuses festgelegt, vorzugsweise eingeklebt. Fig. 6 shows the storage in an enlarged sectional view and sealing the shaft journal 55 of the rotor 9 in the inflow housing 4. The shaft journal 57 of the other rotor 11 is mounted and sealed in an analogous manner. The shaft journals provided with tool engagement (flats 63) 57 is formed in the manner of a hub Middle part of the inflow housing 4 by means of a roller bearing 53 stored between a shoulder of the shaft journal 57 and one engaging in an annular groove of the shaft journal Circlip 83 is arranged. Because on the suction side the rotors 9, 11, as stated above, no oil lubrication Rolling bearing 53 is preferably to take place as an encapsulated bearing with a lifetime grease filling trained so that there is no subsequent lubrication needed. Following the roller bearing 53 is on the shaft journal 57 a race 85 attached, preferably shrunk. The race 85 which e.g. a commercial one The race for a rolling bearing can be made of steel specially hardened peripheral surface. Two work with this Sealing lips of a lip sealing ring 87 together, the Seals the interior of the rotor housing 3 against the roller bearings 53. On the side facing the rotor housing 3 Lip seal ring 87 is between this and an inner shoulder 4a of the inflow housing 4, a protective ring 89 is arranged, the inner periphery of the outer surface of the race 85 with a very small gap, but faces without contact. The protective ring 89 and the lip seal ring 87 are on each other and on the inner shoulder 4a of the inflow housing 4 attached in the bore of the housing, preferably glued.

Die Funktion des Schutzrings 89 ist die Folgende: Der Kompressor erzeugt bei Betrieb durch Ansaugen von Luft auf der Saugseite und Ausblasen verdichteter Luft am Druckstutzen 15 einen Druckluftstrom, der z.B. zum pneumatischen Transport von staubförmigen Gut dienen kann. Bei Betriebsstörungen kann es zu einem Rückschlag von komprimierter Luft von der Druckseite zur Saugseite der Rotoren kommen, wodurch die Gefahr besteht, daß von Luftstrom getragene Partikel des staubförmigen Materials in das Rotorgehäuse 3 und aus diesem bis zu den Wellenzapfen der Rotoren gelangen. Im Fall eines solchen Materialrückschlags schützt der Schutzring 89 den Lippendichtring 87 davor, daß Staubpartikel unter die Dichtlippen des Lippendichtrings 87 gelangen und die Dichtwirkung beeinträchtigen.The function of the guard ring 89 is as follows: The compressor generated during operation by sucking in air on the Suction side and blowing out compressed air at the pressure port 15 a compressed air flow, e.g. for pneumatic transport of dusty goods can serve. In the event of malfunctions there may be a backlash of compressed air from the pressure side to the suction side of the rotors, whereby there is a risk of airborne particles of the dusty material in the rotor housing 3 and out this up to the shaft journal of the rotors. in the In the event of such a material kickback, the guard ring protects 89 the lip seal 87 in front of that dust particles underneath the sealing lips of the lip seal ring 87 and impair the sealing effect.

Die in Fig. 6 dargestellte und vorstehend beschriebene saugseitige Lageranordnung hat den weiteren Vorteil, daß sie von dem Wellenzapfen 57 abgezogen werden kann, ohne daß dabei der Rotor 9 bzw. 11 ausgebaut oder die präzise Einstellung der Rotoren zueinander verändert werden muß. Das Abnehmen der Lager- und Dichtungsanordnung vom Wellenzapfen kann in folgender Weise durchgeführt werden:The one shown in Fig. 6 and described above suction-side bearing arrangement has the further advantage that it can be withdrawn from the shaft journal 57 without the rotor 9 or 11 removed or the precise setting the rotors must be changed to each other. The Remove the bearing and seal assembly from the journal can be done in the following ways:

Nach Abnehmen des Ansauggehäuses 5 wird der Gehäusedeckel 65 des Einströmgehäuses 4 abgenommen, so daß der Wellenzapfen 57 mit seinem Sicherungsring 83 zugänglich wird. Der Sicherungsring 83 wird entfernt. Anschließend werden die das Einströmgehäuse 4 mit dem Rotorgehäuse 3 verbindenden Schrauben gelöst. Nunmehr kann das gesamte Einströmgehäuse 4 mitsamt den darin enthaltenden Wälzlagern 53, Lippendichtringen 87 und Schutzringen 89 abgenommen werden. Dadurch können die saugseitigen Wälzlager 53, die diejenigen Teile sind, die aufgrund der begrenzten Standzeit ihrer Fettfüllung am ehesten ausgetauscht werden müssen, leicht ausgewechselt werden, ohne daß die Rotoren 9, 11 in ihrer Justage zueinander und zum Gehäuse geändert oder gar ausgebaut werden müßten.After removing the suction housing 5, the housing cover 65 of the inflow housing 4 removed, so that the shaft journal 57 is accessible with its locking ring 83. The Circlip 83 is removed. Then the connecting the inflow housing 4 to the rotor housing 3 Screws loosened. Now the entire inflow housing 4 together with the roller bearings 53 contained therein, lip seals 87 and protective rings 89 are removed. Thereby can the suction-side roller bearings 53, those Parts are due to the limited life of their Grease filling is most likely to need to be replaced, easily be replaced without the rotors 9, 11 in their Adjustment to each other and to the housing changed or even expanded should be.

Fig. 7 zeigt in einer Schnittdarstellung entsprechend Fig. 3, aber in größerem Maßstab die Lagerung und Abdichtung der druckseitigen Wellenzapfen 29, 23 der Rotoren 9, 11 am druckseitigen Ende des Rotorgehäuses 3. Im Folgenden wird die Lager- und Dichtungsanordnung für den Wellenzapfen 29 des Rotors 9 beschrieben. Diejenige für den Wellenzapfen 23 des Rotors 11 ist völlig analog ausgebildet.7 shows in a sectional view corresponding to FIG. 3, but on a larger scale the storage and sealing of the pressure side shaft journal 29, 23 of the rotors 9, 11 am pressure-side end of the rotor housing 3. In the following the bearing and sealing arrangement for the shaft journal 29 of the rotor 9 described. The one for the shaft journal 23 the rotor 11 is completely analog.

Der Wellenzapfen 29 ist in der druckseitigen Stirnwand des Rotorgehäuses 3 durch zwei nebeneinander geordnete Wälzlager 91, 93 gelagert, die als sogenannte Schrägkugellager ausgebildet sind. Schrägkugellager, die im Handel erhältlich sind, sind Kugellager, deren Kugeln vom äußeren und inneren Laufring nur auf der einen bzw. anderen Seite der radialen Mittelebene umgriffen werden. Die beiden Schrägkugellager 91, 93 sind spiegelsymmetrisch nebeneinander angeordnet. Eine solche Anordnung von Schrägkugellagern hat die Eigenschaft, daß sie in Axialrichtung völlig spielfrei ist. Eine auf dem Wellenzapfen 29 angeordnete Wellenmutter 95 legt die Schrägkugellager 91, 93 in Axialrichtung auf dem Wellen zapfen 29 fest. Der äußere Laufring des Schrägkugellagers 93 liegt gegen eine Innenschulter 97 des Rotorgehäuses 3 an.The shaft journal 29 is in the pressure-side end wall of the Rotor housing 3 by two roller bearings arranged side by side 91, 93 stored, the so-called angular contact ball bearings are trained. Angular contact ball bearings that are commercially available are ball bearings, the balls of which are from the outside and inner race only on one or the other side of the radial central plane are encompassed. The two angular contact ball bearings 91, 93 are arranged side by side in mirror symmetry. Such an arrangement of angular contact ball bearings has the Property that it is completely free of play in the axial direction. A shaft nut 95 arranged on the shaft journal 29 puts the angular contact ball bearings 91, 93 in the axial direction on the Shafts journal 29 firmly. The outer race of the Angular contact ball bearing 93 lies against an inner shoulder 97 of the Rotor housing 3 on.

Zwischen dem Schrägkugellager 93 und dem Rotor 9 befindet sich ein Abschnitt des Wellenzapfens 29, auf dem ein Laufring 101 befestigt, vorzugsweise aufgeschrumpft ist. Is located between the angular contact ball bearing 93 and the rotor 9 a section of the shaft journal 29 on which a Race 101 attached, preferably shrunk.

Dieser Laufring 101 besteht, ebenso wie der zuvor beschriebene Laufring 85 gemäß Fig. 6, aus Stahl mit einer speziell gehärteten Umfangsfläche. An der Oberfläche des Laufrings 101 liegen die Dichtlippen eines Lippendichtrings 103 an, der den Kompressionsraum des Rotorgehäuses 3 gegen den ölbeaufschlagten Getriebe- und Lagerungsbereich abdichtet. Die gehärtete und extrem präzise bearbeitete, z.B. polierte Außenfläche des Laufrings 25 ergibt eine besonders verschleißmindernde Anlagefläche für die Dichtlippen des Lippen dichtrings 103.This race 101 is made just like the one previously described 6, made of steel with a special hardened peripheral surface. On the surface of the race 101 lie against the sealing lips of a lip sealing ring 103, which the compression space of the rotor housing 3 against the oil-loaded Seals gearbox and bearing area. The hardened and extremely precisely machined, e.g. polished Outer surface of the race 25 results in a particularly wear-reducing Contact surface for the sealing lips of the lips sealing rings 103.

Zwischen dem Lippendichtring 103 und dem Rotor 9 befindet sich ferner ein Labyrinthdichtring 105, der an seinem Innenumfang mehrere nebeneinanderliegende Ringrippen aufweist, die der Außenfläche des Laufrings 101 mit sehr geringem Spalt, aber berührungsfrei gegenüberstehen und mit dieser einen Labyrinthspalt bilden. Obwohl der Laufring 101 mit dem Labyrinthdichtring 105 normalerweise keine Berührung hat, ist es trotzdem vorteilhaft, daß sich der Laufring 101 auch über dem Bereich des Labyrinthdichtrings 105 erstreckt. Die Labyrinthspaltdichtung ist zwar im Normalfall eine berührungslose Dichtung, es kann aber unter extremen Betriebsbedingungen unter Umständen eine Berührung zwischen den Ringrippen des Labyrinthdichtrings 105 und dem Laufring 101 erfolgen. Wenn der Laufring 101 nicht vorhanden wäre, würden hierbei Rillen auf den Wellenzapfen 29 erzeugt werden, so daß dieser beschädigt wird und der Rotor 9 unbrauchbar wird. Dank des Vorhandens des Laufrings 101 braucht in einem solchen Fall nur der Laufring 101 ausgewechselt zu werden, so daß der Rotor 9, bei sonstiger Schadensfreiheit, wieder benutzt werden kann. Is located between the lip seal ring 103 and the rotor 9 there is also a labyrinth sealing ring 105 on its inner circumference has several adjacent ring ribs, that of the outer surface of the race 101 with very little Face the gap, but without contact and with this form a labyrinth gap. Although the race 101 normally no contact with the labyrinth sealing ring 105 , it is still advantageous that the Race 101 also over the area of the labyrinth seal 105 extends. The labyrinth gap seal is normal a non-contact seal, but it can be under extreme operating conditions under certain circumstances between the ring ribs of the labyrinth sealing ring 105 and the Race 101 take place. If the race 101 is not would be present, there would be grooves on the shaft journal 29 are generated so that it is damaged and the Rotor 9 becomes unusable. Thanks to the presence of the race 101 only needs the race 101 in such a case to be replaced, so that the rotor 9, otherwise Damage free, can be used again.

Zwischen dem Labyrinthdichtring 105 und dem Lippendichtring 103 befindet sich ein ringförmiger Entlastungsraum 107, der über einen Lüftungskanal 109 (s. Fig. 7 und Fig. 2) mit der Atmosphäre verbunden ist. Der im Inneren des Rotorgehäuses 3 ausgebildete Lüftungskanal 109, die sogenannte Laterne, verläuft von einem Punkt zwischen den beiden Wellenzapfen 29, 23 der Rotoren 9, 11 nach unten und mündet an der Unterseite des Rotorgehäuses 3. Der Mündung der Laterne 109 liegt mit Abstand die mit den Kühlrippen 39 versehene Oberseite des Ölbehälters 7 gegenüber. Ein geradliniger Zugangsweg zu der Mündung der Laterne 109 von unter her wird durch den Ölbehälter 7 versperrt.
Fig. 4 zeigt eine perspektivische Ansicht von unten des Kompressors bei abgenommenem Ölbehälter 7, so daß in der Stirnwand des Getriebegehäuse 1 die Schraubenlöcher 44 für die Befestigung des Ölbehälters 7 und die große Verbindungsöffnung 43, über die der Ölbehälter mit dem Getriebegehäuse kommuniziert, sichtbar sind. Ferner ist in Fig. 4 das Ansauggehäuse 5 vom saugseitigen Ende des Rotorgehäuses 3 abgenommen, so daß der Blick frei ist auf das Einströmgehäuse 4 mit seinen Stütz-Rippen 14 und den zum Inneren des Rotorgehäuses 3 führenden Einströmöffnungen 13. Die Fig. 4 zeigt auch die Mündung der Laterne (Lüftungskanal) 109 an der Unterseite des Rotorgehäuses 3. Wie aus Fig. 4 ersichtlich, sind beiderseits der Mündung der Laterne 109 Vorsprünge 111 an der Unterseite des Rotorgehäuses 3 vorgesehen, die die Mündung der Laterne 109 gegen geradlinigen Zugang von der Seite her abschirmen. Diese Vorsprünge 111 können durch Ölablaufkanäle gebildet sein. Die Mündung der Laterne 109 befindet sich somit an einer geschützten Stelle, zu der ein geradliniger Zugangsweg weder von unten (wegen des Ölbehälters 7), noch von der Seite (wegen der Vorsprünge 111) möglich ist. Hierdurch wird verhindert, daß z.B. bei der Reinigung des Kompressors mittels eines Hochdruckspritzgerätes der Hochdruck-Wasserstrahl direkt auf die Mündung der Laterne 109 gerichtet werden kann, wodurch Wasser in den Ringraum 107 und damit in den Bereich des Lippendichtrings 103 und des Labyrinthdichtrings 105 gelangen könnte.
Between the labyrinth sealing ring 105 and the lip sealing ring 103 there is an annular relief space 107, which is connected to the atmosphere via a ventilation duct 109 (see FIGS. 7 and 2). The ventilation channel 109 formed in the interior of the rotor housing 3, the so-called lantern, runs downward from a point between the two shaft journals 29, 23 of the rotors 9, 11 and opens at the underside of the rotor housing 3. The opening of the lantern 109 lies at a distance from with the cooling fins 39 provided top of the oil container 7 opposite. A straight access path to the mouth of the lantern 109 from below is blocked by the oil container 7.
Fig. 4 shows a perspective view from below of the compressor with the oil container 7 removed, so that the screw holes 44 for the attachment of the oil container 7 and the large connecting opening 43, through which the oil container communicates with the transmission housing, are visible in the end wall of the transmission housing 1 , 4, the suction housing 5 is removed from the suction-side end of the rotor housing 3, so that there is a clear view of the inflow housing 4 with its supporting ribs 14 and the inflow openings 13 leading to the interior of the rotor housing 3. FIG. 4 also shows the mouth of the lantern (ventilation duct) 109 on the underside of the rotor housing 3. As can be seen from Fig. 4, on both sides of the mouth of the lantern 109 projections 111 are provided on the underside of the rotor housing 3, which the mouth of the lantern 109 against linear access from the Shield side. These projections 111 can be formed by oil drain channels. The mouth of the lantern 109 is thus at a protected location, to which a straight-line access path is neither possible from below (because of the oil container 7) nor from the side (because of the projections 111). This prevents that, for example, when cleaning the compressor by means of a high-pressure spraying device, the high-pressure water jet can be directed directly onto the mouth of the lantern 109, as a result of which water could get into the annular space 107 and thus into the area of the lip sealing ring 103 and the labyrinth sealing ring 105.

Wie anhand von Fig. 7 erläutert werden kann, dient der auf dem Wellenzapfen 29 angebrachte Laufring 101 zusätzlich als Abstandselement, welches für die Einhaltung eines sehr genau bemessenen Spaltes zwischen der druckseitigen Stirnfläche des Rotors 9 oder 11 und der dieser zugewandten Stirnfläche 113 des Rotorgehäuses 3 dient. Für den Wirkungsgrad des Kompressors kommt es entscheidend auf einen möglichst kleinen und exakt definierten Spalt an der druckseitigen Stirnfläche des Rotors 9 bzw. 11 an. Erfindungsgemäß erfolgt die präzise Einstellung und Einhaltung dieses Spalts in der Weise, daß zunächst bei der Bearbeitung des Rotorgehäuses 3 der Abstand a zwischen der dem Rotor 9 zugewandten Stirnfläche 113 und der Anlageschulter 97 für das Wälzlager 93 mit sehr engen Toleranzen auf einem vorgegebenen Wert gefertigt wird. Die Länge b des Laufrings 101, der als Abstandselement zwischen dem Wälzlager 97 und der Stirnfläche des Rotors 9 eingesetzt ist, wird ebenfalls mit entsprechend genauen Toleranzen auf einem Wert eingeschliffen, der gegenüber dem Abstand a ein Übermaß hat, welches exakt der Breite des zwischen dem Rotor 9 und dem Rotorgehäuse 3 einzustellenden Spaltes entspricht. Diese Einstellung des Spaltes aufgrund der Längendifferenz der Abstände a und b ist dadurch möglich, daß erfindungsgemäß Schrägkugellager 91, 93 in symmetrischer Anordnung verwendet werden, die, wie erwähnt, eine vom Axialspiel völlig freie Lageranordnung ergeben. Da somit die Berührungsflächen zwischen dem äußeren Lagerring und der Gehäuseschulter 97 einerseits und zwischen dem inneren Lagerring des Wälzlagers 93 und dem Laufring 101 andererseits als axial spielfreie Referenzflächen dienen, erhält man durch hinreichend genaue Bearbeitung des Abstandes a der Gehäuseschultern und der Länge b des Laufringes 101 eine entsprechend genaue Einstellung des Rotorstirnspaltes. Die einmal erzielte Einstellung des Rotorstirnspaltes bleibt auch bei Temperaturänderungen erhalten, da der Einfluß der unterschiedlichen Wärmedehnung von Rotorgehäuse 3 und Laufring 101 vernachlässigbar klein ist. Es entfällt die bisher bei Kompressoren dieser Art bei der Montage erforderliche Einstellung des Rotorstirnspaltes durch Einsetzen von Beilagringen unterschiedlicher Dicke entsprechend der Fertigungstoleranzschwankungen.As can be explained with reference to FIG. 7, the race 101 attached to the shaft journal 29 additionally serves as a spacing element, which is used to maintain a very precisely dimensioned gap between the pressure-side end face of the rotor 9 or 11 and the end face 113 of the rotor housing 3 facing it serves. For the efficiency of the compressor, what is crucial is the smallest possible and precisely defined gap on the pressure-side end face of the rotor 9 or 11. According to the invention, this gap is set and maintained precisely in such a way that, when the rotor housing 3 is machined, the distance a between the end face 113 facing the rotor 9 and the contact shoulder 97 for the roller bearing 93 is manufactured with very narrow tolerances to a predetermined value , The length b of the race 101, which is used as a spacing element between the roller bearing 97 and the end face of the rotor 9, is also ground with correspondingly precise tolerances to a value which has an oversize compared to the distance a , which is exactly the width of the between Corresponds to rotor 9 and the rotor housing 3 gap to be set. This adjustment of the gap due to the length difference of the distances a and b is possible in that angular contact ball bearings 91, 93 are used according to the invention in a symmetrical arrangement, which, as mentioned, result in a bearing arrangement that is completely free of axial play. Since the contact surfaces between the outer bearing ring and the housing shoulder 97 on the one hand and between the inner bearing ring of the roller bearing 93 and the race 101 on the other hand serve as axially backlash-free reference surfaces, the distance a between the housing shoulders and the length b of the race 101 can be obtained with sufficient precision a correspondingly precise setting of the rotor front gap. The setting of the rotor end gap once obtained is retained even with changes in temperature, since the influence of the different thermal expansion of the rotor housing 3 and the race 101 is negligible. There is no longer any need to adjust the rotor front gap when installing compressors of this type by inserting shims of different thicknesses in accordance with the fluctuations in the manufacturing tolerance.

Claims (5)

  1. A screw compressor comprising: two rotors mounted in a rotor housing (3) with parallel axes, that engage one another with screw-shaped teeth and tooth gaps, and that convey air during operation from a suction end toward a pressure end of the rotor housing (3) and thereby compress the air,
       a gear housing (1) located at one end of the rotor housing (3) in which a drive shaft (17) is mounted with drive gears (19, 21) for the rotors (9, 11) and in which oil lubrication is provided for the drive gears,
       and a synchronizing gear (25, 27) that couples the rotors (9, 11) to run together in opposite directions synchronously without touching,
       wherein the drive gear (19,21) and the synchronizing gear (25, 27) are both located in the gear housing (1) on the pressure end of the rotor housing (3), and wherein the bearings (53) for suction side shaft journals (55, 57) of the rotors (9, 11) are free of oil lubrication and are located in an inlet housing (4) that closes off the rotor housing (3) at the suction end and has inlet openings (13) for the air aspirated by the rotors (9, 11) such the section of the inlet housing (4) containing said bearings (55, 57) is cooled by means of the intake air,
       characterized in that that the inlet housing (4) is surrounded in spaced relationship by an intake housing (5) attached to the rotor housing (3) that has at least one intake opening (59) and in which there is located a filter (6) and/or a muffler insert (75) in the flow path of the air from the intake opening (69) to the inlet openings (13).
  2. A screw compressor according to claim 1, wherein each of the bearings (53) for the suction side shaft journal (55, 57) of the rotors (9, 11) is an encapsulated roller bearing with a lifetime grease filling.
  3. A screw compressor according to claim 1, wherein the inlet housing (4) has holes (66) through which the shaft journals (55, 57) of the rotors (9, 11) can be accessed, and that a tool interface (63) is designed into each shaft journal (53, 55) for engagement by a turning tool.
  4. A screw compressor according to claim 1 wherein the inlet housing (4) has holes (66) through which the shaft journals (53, 57) of the rotors (9, 11) can be accessed, and that a retaining ring (83) that secures the bearing (53) to the shaft journal (55, 57) can be accessed through the holes (66) in such a way that the retaining ring (83) can be removed from the shaft journal (55, 57) and then, after removing any attaching screws, the inlet housing (4) and the bearing (53) and any seals (87) can be removed from the shaft journal (55, 57).
  5. A screw compressor according to claim 1 wherein each suction side shaft journal (55, 57) is sealed in the inlet housing (4) by means of a lip seal ring (87) that sits against the shaft journal or a race (85) located on the shaft journal, and that between the lip seal ring (87) and the rotor housing is a guard ring (89) that sits opposite the perimeter surface of the shaft journal or race (85) with a minimal separation without touching it.
EP00916927A 1999-03-10 2000-03-10 Rotary helical screw-type compressor Expired - Lifetime EP1163451B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE29904410U 1999-03-10
DE29904410U DE29904410U1 (en) 1999-03-10 1999-03-10 Screw compressor
PCT/EP2000/002152 WO2000053930A1 (en) 1999-03-10 2000-03-10 Rotary helical screw-type compressor

Publications (2)

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EP1163451A1 EP1163451A1 (en) 2001-12-19
EP1163451B1 true EP1163451B1 (en) 2004-05-19

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EP00916927A Expired - Lifetime EP1163451B1 (en) 1999-03-10 2000-03-10 Rotary helical screw-type compressor

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US (1) US6488488B2 (en)
EP (1) EP1163451B1 (en)
AT (1) ATE267343T1 (en)
DE (2) DE29904410U1 (en)
WO (1) WO2000053930A1 (en)

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Also Published As

Publication number Publication date
DE29904410U1 (en) 2000-07-20
WO2000053930A1 (en) 2000-09-14
US6488488B2 (en) 2002-12-03
EP1163451A1 (en) 2001-12-19
DE50006495D1 (en) 2004-06-24
ATE267343T1 (en) 2004-06-15
US20020048521A1 (en) 2002-04-25

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