FR2664329B1 - Turbine a reaction a compresseur. - Google Patents

Turbine a reaction a compresseur.

Info

Publication number
FR2664329B1
FR2664329B1 FR9008714A FR9008714A FR2664329B1 FR 2664329 B1 FR2664329 B1 FR 2664329B1 FR 9008714 A FR9008714 A FR 9008714A FR 9008714 A FR9008714 A FR 9008714A FR 2664329 B1 FR2664329 B1 FR 2664329B1
Authority
FR
France
Prior art keywords
reaction turbine
compressor reaction
compressor
turbine
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.)
Expired - Fee Related
Application number
FR9008714A
Other languages
English (en)
Other versions
FR2664329A1 (fr
Inventor
Henri Coutzac
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
Priority to FR9008714A priority Critical patent/FR2664329B1/fr
Publication of FR2664329A1 publication Critical patent/FR2664329A1/fr
Application granted granted Critical
Publication of FR2664329B1 publication Critical patent/FR2664329B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00—Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/08—Engines with star-shaped cylinder arrangements
    • 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
    • F02C3/055—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor being of the positive-displacement type
    • 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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18—Multi-cylinder engines
    • F02B2075/1804—Number of cylinders
    • F02B2075/1816—Number of cylinders four

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9008714A 1990-07-04 1990-07-04 Turbine a reaction a compresseur. Expired - Fee Related FR2664329B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9008714A FR2664329B1 (fr) 1990-07-04 1990-07-04 Turbine a reaction a compresseur.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9008714A FR2664329B1 (fr) 1990-07-04 1990-07-04 Turbine a reaction a compresseur.

Publications (2)

Publication Number Publication Date
FR2664329A1 FR2664329A1 (fr) 1992-01-10
FR2664329B1 true FR2664329B1 (fr) 1994-09-23

Family

ID=9398520

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9008714A Expired - Fee Related FR2664329B1 (fr) 1990-07-04 1990-07-04 Turbine a reaction a compresseur.

Country Status (1)

Country Link
FR (1) FR2664329B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107076022A (zh) * 2013-12-17 2017-08-18 迭戈·奥雷利亚纳乌尔塔多 圆形推进喷射式压缩发动机

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2773846A1 (fr) 1998-01-22 1999-07-23 Pierre Claude Marie Moreau Moteur tambour a reaction ou gyroreacteur
ES2315053B1 (es) * 2005-06-30 2010-01-21 Daniel Corbacho Arranz Motor rotativo de tres tiempos turboalimentado.

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE139650C (fr) *
DE230289C (fr) * 1910-05-06
FR1294053A (fr) * 1961-07-05 1962-05-18 Porsche Kg Moteur à combustion interne avec cylindres rotatifs
US3541787A (en) * 1967-10-30 1970-11-24 Mario Romoli Self-compressed continuous circular internal combustion engine
US4304095A (en) * 1980-09-24 1981-12-08 Rasanen Kaarlo E Internal combustion steam power unit
FR2496759A1 (fr) * 1980-12-22 1982-06-25 Power D Inc Moteur rotatif a combustion interne

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107076022A (zh) * 2013-12-17 2017-08-18 迭戈·奥雷利亚纳乌尔塔多 圆形推进喷射式压缩发动机
CN107076022B (zh) * 2013-12-17 2021-01-08 迭戈·奥雷利亚纳乌尔塔多 圆形推进喷射式压缩发动机

Also Published As

Publication number Publication date
FR2664329A1 (fr) 1992-01-10

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Legal Events

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ST Notification of lapse
ST Notification of lapse
ST Notification of lapse