DE1206660C2 - - Google Patents

Info

Publication number
DE1206660C2
DE1206660C2 DE1961N0020315 DEN0020315A DE1206660C2 DE 1206660 C2 DE1206660 C2 DE 1206660C2 DE 1961N0020315 DE1961N0020315 DE 1961N0020315 DE N0020315 A DEN0020315 A DE N0020315A DE 1206660 C2 DE1206660 C2 DE 1206660C2
Authority
DE
Germany
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
DE1961N0020315
Other languages
German (de)
Other versions
DE1206660B (en
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 filed Critical
Publication of DE1206660B publication Critical patent/DE1206660B/en
Application granted granted Critical
Publication of DE1206660C2 publication Critical patent/DE1206660C2/de
Granted 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Engines (AREA)
  • Control Of Turbines (AREA)
  • Jet Pumps And Other Pumps (AREA)
DEN20315A 1960-07-11 1961-07-11 Combined turbo ramjet engine Granted DE1206660B (en)

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 (2)

Publication Number Publication Date
DE1206660B DE1206660B (en) 1965-12-09
DE1206660C2 true DE1206660C2 (en) 1966-06-23

Family

ID=26186739

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN20315A Granted DE1206660B (en) 1960-07-11 1961-07-11 Combined turbo ramjet engine

Country Status (3)

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

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB971222A (en) * 1962-12-17 1964-09-30 Rolls Royce Gas turbine power plant
US3273345A (en) * 1963-09-10 1966-09-20 Gen Motors Corp Gas turbine engine
US4069661A (en) * 1975-06-02 1978-01-24 The United States Of America As Represented By The United States National Aeronautics And Space Administration Variable mixer propulsion cycle
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.

Also Published As

Publication number Publication date
FR79090E (en) 1962-10-19
DE1206660B (en) 1965-12-09
GB924331A (en) 1963-04-24

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