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WO2008140433A3 - Turbomoteur cyclique à impulsion intégrale - Google Patents

Turbomoteur cyclique à impulsion intégrale Download PDF

Info

Publication number
WO2008140433A3
WO2008140433A3 PCT/TR2008/000032 TR2008000032W WO2008140433A3 WO 2008140433 A3 WO2008140433 A3 WO 2008140433A3 TR 2008000032 W TR2008000032 W TR 2008000032W WO 2008140433 A3 WO2008140433 A3 WO 2008140433A3
Authority
WO
WIPO (PCT)
Prior art keywords
working power
impulsion
turbo
jet
obtaining
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.)
Ceased
Application number
PCT/TR2008/000032
Other languages
English (en)
Other versions
WO2008140433A2 (fr
Inventor
Ahmet Kaan Onay
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 WO2008140433A2 publication Critical patent/WO2008140433A2/fr
Publication of WO2008140433A3 publication Critical patent/WO2008140433A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)
  • Motor Or Generator Cooling System (AREA)

Abstract

Cette invention concerne en particulier des systèmes qui produisent de la ventilation, du refroidissement, de la chaleur, de la pression ou de l'espace vide (dépression) pour des systèmes d'énergie, en particulier pour une puissance utile de l'arbre, un moteur à impulsions, une alimentation en courant électrique, un moteur à réaction et des véhicules. Cette invention introduit de la diversité dans l'utilisation pratique en ce qu'elle porte l'échappement et la chambre de combustion jusqu'à la limite du cycle circulaire amplifié pour ainsi bénéficier de la force centrifuge et obtenir davantage de couple et de puissance utile dans ces moteurs à réaction dont les turbines reçoivent une puissance utile pure par écoulement linéaire ainsi qu'une impulsion.
PCT/TR2008/000032 2007-05-15 2008-04-02 Turbomoteur cyclique à impulsion intégrale Ceased WO2008140433A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR200703306 2007-05-15
TR2007/03306 2007-05-15

Publications (2)

Publication Number Publication Date
WO2008140433A2 WO2008140433A2 (fr) 2008-11-20
WO2008140433A3 true WO2008140433A3 (fr) 2008-12-31

Family

ID=39832537

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2008/000032 Ceased WO2008140433A2 (fr) 2007-05-15 2008-04-02 Turbomoteur cyclique à impulsion intégrale

Country Status (1)

Country Link
WO (1) WO2008140433A2 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20190101128A1 (en) * 2017-10-01 2019-04-04 Papa Abdoulaye MBODJ Wing or blade design for wingtip device, rotor, propeller, turbine, and compressor blades with energy regeneration

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541787A (en) * 1967-10-30 1970-11-24 Mario Romoli Self-compressed continuous circular internal combustion engine
GB2009855A (en) * 1977-08-16 1979-06-20 Lamb S Gas turbine plant
GB1581065A (en) * 1977-05-05 1980-12-10 Hedrick L W Gas turbine engine of the jet reaction type
WO1998016722A2 (fr) * 1996-10-01 1998-04-23 H.P.G. Promotion & Investment (1993) Ltd. Moteur orbital
WO2000039440A1 (fr) * 1998-12-28 2000-07-06 Giovanbattista Greco Moteur a turbine rotative du type a reaction

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3541787A (en) * 1967-10-30 1970-11-24 Mario Romoli Self-compressed continuous circular internal combustion engine
GB1581065A (en) * 1977-05-05 1980-12-10 Hedrick L W Gas turbine engine of the jet reaction type
GB2009855A (en) * 1977-08-16 1979-06-20 Lamb S Gas turbine plant
WO1998016722A2 (fr) * 1996-10-01 1998-04-23 H.P.G. Promotion & Investment (1993) Ltd. Moteur orbital
WO2000039440A1 (fr) * 1998-12-28 2000-07-06 Giovanbattista Greco Moteur a turbine rotative du type a reaction

Also Published As

Publication number Publication date
WO2008140433A2 (fr) 2008-11-20

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