DE1206660B - Kombiniertes Turbo-Staustrahltriebwerk - Google Patents

Kombiniertes Turbo-Staustrahltriebwerk

Info

Publication number
DE1206660B
DE1206660B DEN20315A DEN0020315A DE1206660B DE 1206660 B DE1206660 B DE 1206660B DE N20315 A DEN20315 A DE N20315A DE N0020315 A DEN0020315 A DE N0020315A DE 1206660 B DE1206660 B DE 1206660B
Authority
DE
Germany
Prior art keywords
engine
ramjet
ring
turbo
air
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.)
Granted
Application number
DEN20315A
Other languages
German (de)
English (en)
Other versions
DE1206660C2 (no
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 DE1206660B publication Critical patent/DE1206660B/de
Application granted granted Critical
Publication of DE1206660C2 publication Critical patent/DE1206660C2/de
Granted 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)
DEN20315A 1960-07-11 1961-07-11 Kombiniertes Turbo-Staustrahltriebwerk Granted DE1206660B (de)

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 (2)

Publication Number Publication Date
DE1206660B true DE1206660B (de) 1965-12-09
DE1206660C2 DE1206660C2 (no) 1966-06-23

Family

ID=26186739

Family Applications (1)

Application Number Title Priority Date Filing Date
DEN20315A Granted DE1206660B (de) 1960-07-11 1961-07-11 Kombiniertes Turbo-Staustrahltriebwerk

Country Status (3)

Country Link
DE (1) DE1206660B (no)
FR (1) FR79090E (no)
GB (1) GB924331A (no)

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 (de) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh Kombiniertes, umschaltbares strahltriebwerk zum antrieb von flugzeugen und raumfahrzeugen
DE3912330A1 (de) * 1989-04-14 1990-10-18 Mtu Muenchen 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
DE102004026367B4 (de) * 2004-05-29 2014-05-28 MTU Aero Engines AG Turbomaschine
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
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB622313A (en) * 1946-02-07 1949-04-29 Rateau Soc Improvements in jet propulsion plant for aircraft and the like
FR999953A (fr) * 1945-02-07 1952-02-06 Rateau Soc Perfectionnement aux turbopropulseurs à réaction pour aéronefs
DE865558C (de) * 1942-01-26 1953-02-02 Anxionnaz Rene Rueckstossantrieb
DE1777113U (de) * 1958-08-08 1958-11-06 Ernst Heinkel Farhzeugbau G M Regelbarer lufteinlauf, insbesondere fuer strahltriebwerke.

Patent Citations (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
GB622313A (en) * 1946-02-07 1949-04-29 Rateau Soc Improvements in jet propulsion plant for aircraft and the like
DE1777113U (de) * 1958-08-08 1958-11-06 Ernst Heinkel Farhzeugbau G M Regelbarer lufteinlauf, insbesondere fuer strahltriebwerke.

Also Published As

Publication number Publication date
DE1206660C2 (no) 1966-06-23
GB924331A (en) 1963-04-24
FR79090E (fr) 1962-10-19

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