FR1377199A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
FR1377199A
FR1377199A FR957463A FR957463A FR1377199A FR 1377199 A FR1377199 A FR 1377199A FR 957463 A FR957463 A FR 957463A FR 957463 A FR957463 A FR 957463A FR 1377199 A FR1377199 A FR 1377199A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine
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
FR957463A
Other languages
French (fr)
Inventor
John Gregory Keenan
Jack Palereyman
John Bertram Holliday
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to FR957463A priority Critical patent/FR1377199A/en
Application granted granted Critical
Publication of FR1377199A publication Critical patent/FR1377199A/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
    • 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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR957463A 1963-12-17 1963-12-17 Gas turbine engine Expired FR1377199A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR957463A FR1377199A (en) 1963-12-17 1963-12-17 Gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR957463A FR1377199A (en) 1963-12-17 1963-12-17 Gas turbine engine

Publications (1)

Publication Number Publication Date
FR1377199A true FR1377199A (en) 1964-10-31

Family

ID=8819046

Family Applications (1)

Application Number Title Priority Date Filing Date
FR957463A Expired FR1377199A (en) 1963-12-17 1963-12-17 Gas turbine engine

Country Status (1)

Country Link
FR (1) FR1377199A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2085470A1 (en) * 1970-04-23 1971-12-24 Snecma
FR2313565A1 (en) * 1975-06-02 1976-12-31 Gen Electric GAS TURBINE ENGINE WITH ADJUSTABLE BY-PASS AND PROCESS FOR CONTROL OF THIS ENGINE
FR2313566A1 (en) * 1975-06-02 1976-12-31 Gen Electric VARIABLE CYCLE GAS TURBINE ENGINE
FR2399547A1 (en) * 1977-08-02 1979-03-02 Gen Electric MULTI-BYPASS VARIABLE CYCLE TURBO-BLOWER MOTOR
FR2550821A1 (en) * 1983-08-18 1985-02-22 Snecma DEVICE FOR VARIATING THE SECONDARY FLOW OF A MULTIFLUX TURBOREACTOR
FR2615906A1 (en) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh REACTOR COMBINED, SWITCHABLE, FOR THE TRAINING OF AIRCRAFT AND SPECIAL EQUIPMENT
CN109653899A (en) * 2018-12-10 2019-04-19 中国航发四川燃气涡轮研究院 A kind of adjustable throttling set for simulating aero-engine jet pipe
CN114278617A (en) * 2021-11-30 2022-04-05 清华大学 Compression device and runner system thereof

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2085470A1 (en) * 1970-04-23 1971-12-24 Snecma
FR2313565A1 (en) * 1975-06-02 1976-12-31 Gen Electric GAS TURBINE ENGINE WITH ADJUSTABLE BY-PASS AND PROCESS FOR CONTROL OF THIS ENGINE
FR2313566A1 (en) * 1975-06-02 1976-12-31 Gen Electric VARIABLE CYCLE GAS TURBINE ENGINE
FR2399547A1 (en) * 1977-08-02 1979-03-02 Gen Electric MULTI-BYPASS VARIABLE CYCLE TURBO-BLOWER MOTOR
FR2550821A1 (en) * 1983-08-18 1985-02-22 Snecma DEVICE FOR VARIATING THE SECONDARY FLOW OF A MULTIFLUX TURBOREACTOR
EP0135430A1 (en) * 1983-08-18 1985-03-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Apparatus for varying the secondary flow of a multiple-flow turbine engine
US4638631A (en) * 1983-08-18 1987-01-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Multiflow turbo jet engine secondary flow adjusting device
FR2615906A1 (en) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh REACTOR COMBINED, SWITCHABLE, FOR THE TRAINING OF AIRCRAFT AND SPECIAL EQUIPMENT
CN109653899A (en) * 2018-12-10 2019-04-19 中国航发四川燃气涡轮研究院 A kind of adjustable throttling set for simulating aero-engine jet pipe
CN109653899B (en) * 2018-12-10 2021-08-03 中国航发四川燃气涡轮研究院 Adjustable throttling device for simulating jet pipe of aircraft engine
CN114278617A (en) * 2021-11-30 2022-04-05 清华大学 Compression device and runner system thereof

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