GB924331A - Improved combined turbo-jet-ram-jet-engine - Google Patents

Improved combined turbo-jet-ram-jet-engine

Info

Publication number
GB924331A
GB924331A GB2412261A GB2412261A GB924331A GB 924331 A GB924331 A GB 924331A GB 2412261 A GB2412261 A GB 2412261A GB 2412261 A GB2412261 A GB 2412261A GB 924331 A GB924331 A GB 924331A
Authority
GB
United Kingdom
Prior art keywords
jet
pass
engine
ram
duct
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
GB2412261A
Other languages
English (en)
Inventor
Pierre Yves Aimable Fer 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/fr
Application filed by Nord Aviation Societe Nationale de Constructions Aeronautiques filed Critical Nord Aviation Societe Nationale de Constructions Aeronautiques
Publication of GB924331A publication Critical patent/GB924331A/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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
GB2412261A 1960-07-11 1961-07-04 Improved combined turbo-jet-ram-jet-engine Expired GB924331A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR832622A FR1271544A (fr) 1960-07-11 1960-07-11 Combiné turboréacteur-statoréacteur
FR851486A FR79090E (fr) 1960-07-11 1961-02-02 Combiné turboréacteur-statoréacteur

Publications (1)

Publication Number Publication Date
GB924331A true GB924331A (en) 1963-04-24

Family

ID=26186739

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2412261A Expired GB924331A (en) 1960-07-11 1961-07-04 Improved combined turbo-jet-ram-jet-engine

Country Status (3)

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

Cited By (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
FR2615906A1 (fr) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh Reacteur combine, commutable, pour l'entrainement d'avions et d'engins speciaux
EP0392527A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Integriertes Turbo-Staustrahltriebwerk
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
US5307624A (en) * 1990-04-04 1994-05-03 General Electric Company Variable area bypass valve assembly
DE102004026367B4 (de) * 2004-05-29 2014-05-28 MTU Aero Engines AG Turbomaschine
CN110529287A (zh) * 2019-08-13 2019-12-03 中国航发贵阳发动机设计研究所 一种串联式组合冲压发动机用分流机匣
CN111692013A (zh) * 2020-07-03 2020-09-22 南京航空航天大学 一种轴对称内并联涡轮基旋转爆震冲压组合发动机及控制方法
CN114704379A (zh) * 2022-03-02 2022-07-05 南京航空航天大学 一种宽速域并联燃烧涡轮发动机
CN117738814A (zh) * 2024-02-21 2024-03-22 中国航发四川燃气涡轮研究院 带叶尖风扇及串联压气机的变流路宽速域发动机

Families Citing this family (2)

* 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
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

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE865558C (de) * 1942-01-26 1953-02-02 Anxionnaz Rene Rueckstossantrieb
FR999953A (fr) * 1945-02-07 1952-02-06 Rateau Soc Perfectionnement aux turbopropulseurs à réaction pour aéronefs
US2527732A (en) * 1946-02-07 1950-10-31 Rateau Soc Braking device for aircraft jet turbopropellers
DE1777113U (de) * 1958-08-08 1958-11-06 Ernst Heinkel Farhzeugbau G M Regelbarer lufteinlauf, insbesondere fuer strahltriebwerke.

Cited By (13)

* 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
FR2615906A1 (fr) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh Reacteur combine, commutable, pour l'entrainement d'avions et d'engins speciaux
EP0392527A1 (de) * 1989-04-14 1990-10-17 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Integriertes Turbo-Staustrahltriebwerk
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
US5343697A (en) * 1992-01-02 1994-09-06 General Electric Company Variable area bypass injector
DE102004026367B4 (de) * 2004-05-29 2014-05-28 MTU Aero Engines AG Turbomaschine
CN110529287A (zh) * 2019-08-13 2019-12-03 中国航发贵阳发动机设计研究所 一种串联式组合冲压发动机用分流机匣
CN110529287B (zh) * 2019-08-13 2022-08-26 中国航发贵阳发动机设计研究所 一种串联式组合冲压发动机用分流机匣
CN111692013A (zh) * 2020-07-03 2020-09-22 南京航空航天大学 一种轴对称内并联涡轮基旋转爆震冲压组合发动机及控制方法
CN114704379A (zh) * 2022-03-02 2022-07-05 南京航空航天大学 一种宽速域并联燃烧涡轮发动机
CN117738814A (zh) * 2024-02-21 2024-03-22 中国航发四川燃气涡轮研究院 带叶尖风扇及串联压气机的变流路宽速域发动机
CN117738814B (zh) * 2024-02-21 2024-05-17 中国航发四川燃气涡轮研究院 带叶尖风扇及串联压气机的变流路宽速域发动机

Also Published As

Publication number Publication date
DE1206660B (de) 1965-12-09
DE1206660C2 (de) 1966-06-23
FR79090E (fr) 1962-10-19

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