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AU2001500A - Rotary turbine engine of the reaction type - Google Patents

Rotary turbine engine of the reaction type

Info

Publication number
AU2001500A
AU2001500A AU20015/00A AU2001500A AU2001500A AU 2001500 A AU2001500 A AU 2001500A AU 20015/00 A AU20015/00 A AU 20015/00A AU 2001500 A AU2001500 A AU 2001500A AU 2001500 A AU2001500 A AU 2001500A
Authority
AU
Australia
Prior art keywords
turbine engine
reaction type
rotary turbine
rotary
reaction
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.)
Abandoned
Application number
AU20015/00A
Inventor
Giovanbattista Greco
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU2001500A publication Critical patent/AU2001500A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU20015/00A 1998-12-28 1999-12-27 Rotary turbine engine of the reaction type Abandoned AU2001500A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITRM98A0804 1998-12-28
IT1998RM000804A IT1302949B1 (en) 1998-12-28 1998-12-28 INTERNAL COMBUSTION ENDOTHERMAL ENGINE WITH REACTIVE "CIRCULAR" EMOTO PROPULSION.
PCT/IT1999/000424 WO2000039440A1 (en) 1998-12-28 1999-12-27 Rotary turbine engine of the reaction type

Publications (1)

Publication Number Publication Date
AU2001500A true AU2001500A (en) 2000-07-31

Family

ID=11406275

Family Applications (1)

Application Number Title Priority Date Filing Date
AU20015/00A Abandoned AU2001500A (en) 1998-12-28 1999-12-27 Rotary turbine engine of the reaction type

Country Status (3)

Country Link
AU (1) AU2001500A (en)
IT (1) IT1302949B1 (en)
WO (1) WO2000039440A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10033653A1 (en) * 2000-06-16 2002-03-07 Sandor Nagy Drive system for e.g. aircraft, is formed multistage with drives units such that the drive system is combined with at least one negative pressure system
DE10126632A1 (en) * 2000-08-08 2002-09-12 Sandor Nagy Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines
US8333060B2 (en) 2003-02-28 2012-12-18 Micro Turbine Technology B.V. Micro reaction turbine with integrated combustion chamber and rotor
NL1022803C2 (en) * 2003-02-28 2004-08-31 Micro Turbine Technology B V Micro reaction turbine with integrated combustion chamber and rotor.
NL1030744C2 (en) * 2005-12-22 2007-06-25 Micro Turbine Technology B V Reaction turbine.
WO2008140433A2 (en) * 2007-05-15 2008-11-20 Ahmet Kaan Onay Turbo cyclic integral impulsion motor
GB2451704A (en) * 2007-08-10 2009-02-11 Keven Chappell Gas turbine engine with compressor formed from a plurality of stacked surfaces

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR999958A (en) * 1946-02-07 1952-02-06 Improvements to reaction turbines
US2670597A (en) * 1946-10-14 1954-03-02 Villemejane Jacques Rotating jet motor with regulation of power output
FR934755A (en) * 1946-10-14 1948-06-01 Thermal engine with rotating nozzles
US3727401A (en) * 1971-03-19 1973-04-17 J Fincher Rotary turbine engine
GB1581050A (en) * 1976-12-23 1980-12-10 Rolls Royce Combustion equipment for gas turbine engines
GB2064666A (en) * 1979-05-29 1981-06-17 Weir Group Ltd Rotary Fluid-flow Machines
CA1191702A (en) * 1981-10-22 1985-08-13 Gaston Lavoie Engine
US5185541A (en) * 1991-12-02 1993-02-09 21St Century Power & Light Corporation Gas turbine for converting fuel to electrical and mechanical energy
US5306116A (en) * 1992-04-10 1994-04-26 Ingersoll-Rand Company Surge control and recovery for a centrifugal compressor
US5282356A (en) * 1993-01-07 1994-02-01 Abell Irwin R Flywheel engine

Also Published As

Publication number Publication date
IT1302949B1 (en) 2000-10-10
ITRM980804A1 (en) 2000-06-28
ITRM980804A0 (en) 1998-12-28
WO2000039440A1 (en) 2000-07-06

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase