FR1131310A - Gas turbine - Google Patents

Gas turbine

Info

Publication number
FR1131310A
FR1131310A FR1131310DA FR1131310A FR 1131310 A FR1131310 A FR 1131310A FR 1131310D A FR1131310D A FR 1131310DA FR 1131310 A FR1131310 A FR 1131310A
Authority
FR
France
Prior art keywords
gas turbine
turbine
gas
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
Application number
Other languages
French (fr)
Inventor
Pierre Canarelli
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 filed Critical
Application granted granted Critical
Publication of FR1131310A publication Critical patent/FR1131310A/en
Expired 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1131310D 1955-09-19 1955-09-19 Gas turbine Expired FR1131310A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1131310T 1955-09-19

Publications (1)

Publication Number Publication Date
FR1131310A true FR1131310A (en) 1957-02-20

Family

ID=9637835

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1131310D Expired FR1131310A (en) 1955-09-19 1955-09-19 Gas turbine

Country Status (1)

Country Link
FR (1) FR1131310A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3503563A1 (en) * 1984-02-21 1985-08-29 Hans G. 5441 Hirten Albrecht EXPLOSION TURBINE ENGINE
US4693075A (en) * 1984-10-31 1987-09-15 Andrew Sabatiuk Gas turbine engines employing fixed volume combustion
FR2825753A1 (en) * 2001-06-06 2002-12-13 Gerard Andre Machine using internal combustion to produce rotary motion has combustion chambers connected to shaft between compressor and turbine blades
WO2003004846A1 (en) * 2001-07-06 2003-01-16 Hubert Michael Benians Compound gas turbine engines and methods of operation thereof
FR2829528A1 (en) * 2001-09-07 2003-03-14 Bernard Gilbert Macarez Pulse motor-turbine engine for aircraft has air fed from compressor to turbine through combustors with opening and closing flap valves operated by electromagnets with numerical control system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3503563A1 (en) * 1984-02-21 1985-08-29 Hans G. 5441 Hirten Albrecht EXPLOSION TURBINE ENGINE
US4693075A (en) * 1984-10-31 1987-09-15 Andrew Sabatiuk Gas turbine engines employing fixed volume combustion
FR2825753A1 (en) * 2001-06-06 2002-12-13 Gerard Andre Machine using internal combustion to produce rotary motion has combustion chambers connected to shaft between compressor and turbine blades
WO2003004846A1 (en) * 2001-07-06 2003-01-16 Hubert Michael Benians Compound gas turbine engines and methods of operation thereof
US7000402B2 (en) 2001-07-06 2006-02-21 Hubert Michael Benians Compound gas turbine engines and methods of operation thereof
FR2829528A1 (en) * 2001-09-07 2003-03-14 Bernard Gilbert Macarez Pulse motor-turbine engine for aircraft has air fed from compressor to turbine through combustors with opening and closing flap valves operated by electromagnets with numerical control system
WO2003023206A1 (en) * 2001-09-07 2003-03-20 Bernard Macarez Gas turbine with intermittent combustion

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