DE1476755B2 - Cooled blade - Google Patents
Cooled bladeInfo
- Publication number
- DE1476755B2 DE1476755B2 DE1476755A DE1476755A DE1476755B2 DE 1476755 B2 DE1476755 B2 DE 1476755B2 DE 1476755 A DE1476755 A DE 1476755A DE 1476755 A DE1476755 A DE 1476755A DE 1476755 B2 DE1476755 B2 DE 1476755B2
- Authority
- DE
- Germany
- Prior art keywords
- shovel
- blade
- skirt
- coolant
- rotor
- 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.)
- Pending
Links
- 239000002826 coolant Substances 0.000 claims description 10
- 230000035699 permeability Effects 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims 10
- 238000004519 manufacturing process Methods 0.000 claims 4
- 239000000463 material Substances 0.000 claims 3
- 241000251133 Sphyrna tiburo Species 0.000 claims 1
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 239000002800 charge carrier Substances 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 claims 1
- 238000010894 electron beam technology Methods 0.000 claims 1
- 239000004744 fabric Substances 0.000 claims 1
- 230000035515 penetration Effects 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 238000005507 spraying Methods 0.000 claims 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Am wurzelseitigen Ende des Schaufelhemdes 13 ist eine Randfläche W vorgesehen, die ebenfalls keine Austrittsöffnungen aufweist.At the root end of the shovel skirt 13, an edge surface W is provided, which likewise has no outlet openings.
Der Anordnung der Stege 11 am Schaufelinnenkörper 10 entsprechend sind im Schaufelhemd 13 die Randflächen K und W verbindende Flächenstreifen S vorgesehen, die von der Einbringung von Austrittsöffnungen ausgenommen sind. Corresponding to the arrangement of the webs 11 on the inner blade body 10, surface strips S connecting the edge surfaces K and W are provided in the shovel skirt 13 and are excluded from the introduction of outlet openings.
Die noch verbleibende Restfläche des Schaufelhemdes 13 ist mit kleineren Durchtrittsöffnungen, beispielsweise im Durchmesser von 0,040 mm, vorgesehen. Diese Restfläche besitzt dann eine Durchlässigkeit von 15%.The remaining area of the shovel skirt 13 is provided with smaller passage openings, for example, with a diameter of 0.040 mm. This remaining area then has a permeability of 15%.
Durch die beschriebene Verteilung von größeren, mittleren und kleineren Durchtrittsöffnungen im Schaufelhemd 13 treten an diesem keine unterschiedlichen Betriebstemperaturen auf, da der Kühlmittel-Durchsatz durch die angegebene Verteilung der Austrittsöffnungen auf die örtlich abzuführendenDue to the distribution of larger, medium and smaller passage openings in the Shovel skirt 13 does not occur at this different operating temperatures, since the coolant throughput by the specified distribution of the outlet openings on the locally to be discharged
ίο Wärmemengen abgestimmt ist.ίο the amount of heat is coordinated.
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (1)
kannten Laufschaufel besteht das Schaufelhemd aus 35 Für den Austritt des Kühlmittels aus der Laufporösem Metallgewebe, auf das ein Zusatzwerkstoff schaufel ist das Schaufelhemd 13 mit Austrittsöffaufgespritzt wird, um die Durchlässigkeit des Gewe- nungen versehen. Das in F i g. 3 in abgewickelter bes für das" Kühlmittel entsprechend der Temperatur- Form dargestellte Schaufelhemd 13 weist einen mittverteilung an der Schaufelblattoberfläche örtlich zu leren, strichpunktiert umrissenen Flächenbereich A verändern. Derartige Laufschaufeln mit Metallge- 4° auf, innerhalb dessen größere Durchtrittsbohrungen, webe verursachen hohe Materialkosten und sind beispielsweise mit 0,065 mm Durchmesser, in das schwierig herzustellen, Das Aufspritzen von Zusatz- Schaufelhemd eingebracht sind. Der Flächenbewerkstoff muß für jede einzelne Laufschaufel geson- reicht kann eine Durchlässigkeit von 25% aufweidert im individuellen Versuch durchgeführt werden. sen, d. h. 25 % einer Flächeneinheit dieses Bereichs Es liegt die Aufgabe vor, eine Laufschaufel der 45 sind freier Durchtrittsquerschnitt. Die Austrittsöffeingangs genannten Art derart zu verbessern, daß nungen selbst sind infolge des gewählten Zeichnungseine aufwendige Herstellung des Schaufelhemdes maßstabes für das gezeigte Ausführungsbeispiel einer vermieden wird. erfindungsgemäßen Laufschaufel bei der zeichneri-At its surface facing away from the blade head 14, and at the lower temperature end, the inner blade body 10 protrudes a bit from the surface of the airfoil through an arrangement that takes this temperature distribution into account ° Way a blade root 16 for fastening the opening and / or formation of the outlet openings in the rotor blade on its associated turbine rotor. The scoop shirt are essentially balanced. When the rotor blade is inserted into the turbine rotor, such a cooled rotor blade is out of the set, the root ends 17 of the Ka-USA. Patent 3,067,982 known. There are 12 inlet openings for the coolant,
Known rotor blades, the shovel skirt is made of 35. For the coolant to exit from the porous metal mesh, onto which an additional material is shovel, the shovel skirt 13 is sprayed with an outlet opening in order to provide the permeability of the thread. The in Fig. 3 in developed besides for the "coolant according to the temperature shape shown the shovel skirt 13 has a central distribution on the blade surface to be changed locally, dash-dotted outlined area A. Such blades with metal 4 °, within which larger through-holes, weave cause high material costs and are, for example, with a diameter of 0.065 mm, which is difficult to manufacture. The spraying-on of additional shovel skin is incorporated. The object is to provide a free passage cross-section for a rotor blade of 45. The type mentioned at the beginning of the discharge opening is to be improved in such a way that openings themselves are, as a result of the selected drawing, an elaborate production of the blade skirt to scale for the shown Aus Leadership example one is avoided. blade according to the invention in the drawing
strahlen. Hierbei ist es möglich, insbesondere Elek- 65 Am schaufelkopfseitigen Ende des Schaufelhemtronenstrahlen nach einem gespeicherten Programm des 13 ist eine Randfläche K angedeutet, mit der das — entsprechend der einmal ermittelten Temperatur- Schaufelhemd 13 am Schaufelkopf 14 angeschweißt verteilung an der Schaufelblattoberfläche — auf den und die von Austrittsöffnungen frei ist.from an easily destructible fabric. The agile spraying of additional metal onto the middle surface area A is also avoided by two surfaces. In particular, the outlet openings C 1 and C 2 can be provided , within which the blades for the coolant can be introduced into the blade skirt in a much simpler and more straightforward manner, likewise with central through-bores. The surface areas C 1 and C 2, for example due to the effect of charge carriers, also have a permeability of 20.
shine. At the end of the shovel head-side end of the shovel electron beam according to a stored program of 13, an edge surface K is indicated with which the shovel shroud 13 welded to the shovel head 14 on the surface of the shovel blade - in accordance with the once determined temperature - on the and which is free from outlet openings.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED0050302 | 1966-06-11 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE1476755A1 DE1476755A1 (en) | 1970-03-26 |
DE1476755B2 true DE1476755B2 (en) | 1974-01-17 |
Family
ID=7052546
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1476755A Pending DE1476755B2 (en) | 1966-06-11 | 1966-06-11 | Cooled blade |
Country Status (3)
Country | Link |
---|---|
US (1) | US3468513A (en) |
DE (1) | DE1476755B2 (en) |
GB (1) | GB1146790A (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1776015A1 (en) * | 1968-09-04 | 1971-09-16 | Daimler Benz Ag | Turbine blade |
DE1801475B2 (en) * | 1968-10-05 | 1971-08-12 | Daimler Benz Ag, 7000 Stuttgart | AIR-COOLED TURBINE BLADE |
US3656863A (en) * | 1970-07-27 | 1972-04-18 | Curtiss Wright Corp | Transpiration cooled turbine rotor blade |
US6565312B1 (en) * | 2001-12-19 | 2003-05-20 | The Boeing Company | Fluid-cooled turbine blades |
US6699015B2 (en) | 2002-02-19 | 2004-03-02 | The Boeing Company | Blades having coolant channels lined with a shape memory alloy and an associated fabrication method |
US7500828B2 (en) * | 2005-05-05 | 2009-03-10 | Florida Turbine Technologies, Inc. | Airfoil having porous metal filled cavities |
US20120067054A1 (en) | 2010-09-21 | 2012-03-22 | Palmer Labs, Llc | High efficiency power production methods, assemblies, and systems |
US10808547B2 (en) | 2016-02-08 | 2020-10-20 | General Electric Company | Turbine engine airfoil with cooling |
DE102017215940A1 (en) * | 2017-09-11 | 2019-03-14 | MTU Aero Engines AG | Blade of a turbomachine with a cooling channel and displacer arranged therein and method for the production thereof |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2787049A (en) * | 1952-05-23 | 1957-04-02 | Stalkcr Dev Company | Process of fabricating blades for turbines, compressors and the like |
BE529252A (en) * | 1953-06-01 | |||
US2851216A (en) * | 1954-01-13 | 1958-09-09 | Schwarzkopf Dev Co | Device adapted for respiration cooling and process of making same |
US2991973A (en) * | 1954-10-18 | 1961-07-11 | Parsons & Marine Eng Turbine | Cooling of bodies subject to a hot gas stream |
US3067982A (en) * | 1958-08-25 | 1962-12-11 | California Inst Res Found | Porous wall turbine blades and method of manufacture |
US3240468A (en) * | 1964-12-28 | 1966-03-15 | Curtiss Wright Corp | Transpiration cooled blades for turbines, compressors, and the like |
GB1070480A (en) * | 1966-02-01 | 1967-06-01 | Rolls Royce | Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine |
US3402291A (en) * | 1966-04-06 | 1968-09-17 | Gen Motors Corp | Method and apparatus of measuring residual stress in metals and the amount of a known constituent |
-
1966
- 1966-06-11 DE DE1476755A patent/DE1476755B2/en active Pending
-
1967
- 1967-06-08 US US644725A patent/US3468513A/en not_active Expired - Lifetime
- 1967-06-12 GB GB27020/67A patent/GB1146790A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE1476755A1 (en) | 1970-03-26 |
US3468513A (en) | 1969-09-23 |
GB1146790A (en) | 1969-03-26 |
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