FR1062016A - Gas turbine starter - Google Patents

Gas turbine starter

Info

Publication number
FR1062016A
FR1062016A FR1062016DA FR1062016A FR 1062016 A FR1062016 A FR 1062016A FR 1062016D A FR1062016D A FR 1062016DA FR 1062016 A FR1062016 A FR 1062016A
Authority
FR
France
Prior art keywords
gas turbine
turbine starter
starter
gas
turbine
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)
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston Co Ltd
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 British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Priority claimed from US291618A external-priority patent/US2775865A/en
Application granted granted Critical
Publication of FR1062016A publication Critical patent/FR1062016A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
FR1062016D 1952-06-04 1952-05-30 Gas turbine starter Expired FR1062016A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US291618A US2775865A (en) 1951-06-07 1952-06-04 Starters for prime movers such as gas turbines
US455316A US2775866A (en) 1952-06-04 1954-09-10 Starters for prime movers such as gas turbines

Publications (1)

Publication Number Publication Date
FR1062016A true FR1062016A (en) 1954-04-16

Family

ID=26966883

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1062016D Expired FR1062016A (en) 1952-06-04 1952-05-30 Gas turbine starter

Country Status (2)

Country Link
US (1) US2775866A (en)
FR (1) FR1062016A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2988430A (en) * 1958-02-11 1961-06-13 Thompson Ramo Wooldridge Inc Fuel dissociation chamber
US3149460A (en) * 1960-09-28 1964-09-22 Gen Electric Reaction propulsion system
US3533233A (en) * 1967-09-13 1970-10-13 Lockheed Aircraft Corp Hot gas generator utilizing a mono-propellant fuel
US3707074A (en) * 1970-09-30 1972-12-26 Westinghouse Electric Corp Spontaneous ignition of fuel in a combustion chamber
US4092824A (en) * 1974-05-28 1978-06-06 Vereinigte Flugtechnische Werke-Fokker Gmbh Method of operating a turbine
WO2009136389A1 (en) 2008-05-05 2009-11-12 Joshua Waldhorn Turbine driven by predetermined deflagration of anaerobic fuel and method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584803A (en) * 1946-08-07 1952-02-05 Borg Warner Mono-fuel
US2643511A (en) * 1949-10-07 1953-06-30 Avco Mfg Corp Engine starter having combustion chamber supplied with fuel and combustion supporting medium for constant ratio by weight
US2689454A (en) * 1950-05-13 1954-09-21 Soc Et Propulsion Par Reaction Rocket engine

Also Published As

Publication number Publication date
US2775866A (en) 1957-01-01

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