FR79090E - Combined turbojet-ramjet - Google Patents

Combined turbojet-ramjet

Info

Publication number
FR79090E
FR79090E FR851486A FR851486A FR79090E FR 79090 E FR79090 E FR 79090E FR 851486 A FR851486 A FR 851486A FR 851486 A FR851486 A FR 851486A FR 79090 E FR79090 E FR 79090E
Authority
FR
France
Prior art keywords
ramjet
turbojet
combined
combined turbojet
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
FR851486A
Other languages
French (fr)
Inventor
Pierre Sandre
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.)
Nord Aviation Societe Nationale de Constructions Aeronautiques
Original Assignee
Nord Aviation Societe Nationale de Constructions Aeronautiques
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
Priority claimed from FR832622A external-priority patent/FR1271544A/en
Application filed by Nord Aviation Societe Nationale de Constructions Aeronautiques filed Critical Nord Aviation Societe Nationale de Constructions Aeronautiques
Priority to FR851486A priority Critical patent/FR79090E/en
Priority to GB2412261A priority patent/GB924331A/en
Priority to DEN20315A priority patent/DE1206660B/en
Application granted granted Critical
Publication of FR79090E publication Critical patent/FR79090E/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/075Plants 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/10Plants 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
    • F02K7/16Composite ram-jet/turbo-jet engines

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)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Engines (AREA)
FR851486A 1960-07-11 1961-02-02 Combined turbojet-ramjet Expired FR79090E (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR851486A FR79090E (en) 1960-07-11 1961-02-02 Combined turbojet-ramjet
GB2412261A GB924331A (en) 1960-07-11 1961-07-04 Improved combined turbo-jet-ram-jet-engine
DEN20315A DE1206660B (en) 1960-07-11 1961-07-11 Combined turbo ramjet engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR832622A FR1271544A (en) 1960-07-11 1960-07-11 Combined turbojet-ramjet
FR851486A FR79090E (en) 1960-07-11 1961-02-02 Combined turbojet-ramjet

Publications (1)

Publication Number Publication Date
FR79090E true FR79090E (en) 1962-10-19

Family

ID=26186739

Family Applications (1)

Application Number Title Priority Date Filing Date
FR851486A Expired FR79090E (en) 1960-07-11 1961-02-02 Combined turbojet-ramjet

Country Status (3)

Country Link
DE (1) DE1206660B (en)
FR (1) FR79090E (en)
GB (1) GB924331A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231961B (en) * 1962-12-17 1967-01-05 Rolls Royce Combined turbojet and ramjet engine
FR2313565A1 (en) * 1975-06-02 1976-12-31 Gen Electric GAS TURBINE ENGINE WITH ADJUSTABLE BY-PASS AND PROCESS FOR CONTROL OF THIS ENGINE

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273345A (en) * 1963-09-10 1966-09-20 Gen Motors Corp Gas turbine engine
DE3738703A1 (en) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh COMBINED, SWITCHABLE JET ENGINE FOR DRIVING PLANES AND SPACES
DE3912330A1 (en) * 1989-04-14 1990-10-18 Mtu Muenchen Gmbh INTEGRATED TURBO JET ENGINE
US5307624A (en) * 1990-04-04 1994-05-03 General Electric Company Variable area bypass valve assembly
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
DE102004026367B4 (en) * 2004-05-29 2014-05-28 MTU Aero Engines AG turbomachinery
CN110529287B (en) * 2019-08-13 2022-08-26 中国航发贵阳发动机设计研究所 Shunt casing for tandem type combined stamping engine
CN111692013A (en) * 2020-07-03 2020-09-22 南京航空航天大学 Axisymmetric internal parallel turbine-based rotary detonation ramjet combined engine and control method
CN114704379A (en) * 2022-03-02 2022-07-05 南京航空航天大学 Wide-speed-range parallel combustion turbine engine
CN117738814B (en) * 2024-02-21 2024-05-17 中国航发四川燃气涡轮研究院 Variable flow path wide speed range engine with blade tip fan and series compressor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE865558C (en) * 1942-01-26 1953-02-02 Anxionnaz Rene Recoil drive
FR999953A (en) * 1945-02-07 1952-02-06 Rateau Soc Improvement of jet turboprop engines for aircraft
US2527732A (en) * 1946-02-07 1950-10-31 Rateau Soc Braking device for aircraft jet turbopropellers
DE1777113U (en) * 1958-08-08 1958-11-06 Ernst Heinkel Farhzeugbau G M ADJUSTABLE AIR INLET, IN PARTICULAR FOR JETS.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1231961B (en) * 1962-12-17 1967-01-05 Rolls Royce Combined turbojet and ramjet engine
FR2313565A1 (en) * 1975-06-02 1976-12-31 Gen Electric GAS TURBINE ENGINE WITH ADJUSTABLE BY-PASS AND PROCESS FOR CONTROL OF THIS ENGINE

Also Published As

Publication number Publication date
DE1206660B (en) 1965-12-09
GB924331A (en) 1963-04-24
DE1206660C2 (en) 1966-06-23

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