FR2068798A1 - - Google Patents

Info

Publication number
FR2068798A1
FR2068798A1 FR7041150A FR7041150A FR2068798A1 FR 2068798 A1 FR2068798 A1 FR 2068798A1 FR 7041150 A FR7041150 A FR 7041150A FR 7041150 A FR7041150 A FR 7041150A FR 2068798 A1 FR2068798 A1 FR 2068798A1
Authority
FR
France
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
FR7041150A
Other languages
French (fr)
Other versions
FR2068798B1 (en
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 DE19691961999 external-priority patent/DE1961999C3/en
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2068798A1 publication Critical patent/FR2068798A1/fr
Application granted granted Critical
Publication of FR2068798B1 publication Critical patent/FR2068798B1/fr
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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/10—Varying effective area of jet pipe or nozzle by distorting the jet pipe or nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Nozzles (AREA)
FR7041150A 1969-12-10 1970-11-17 Expired FR2068798B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691961999 DE1961999C3 (en) 1969-12-10 Thrust nozzle for aircraft jet engines

Publications (2)

Publication Number Publication Date
FR2068798A1 true FR2068798A1 (en) 1971-09-03
FR2068798B1 FR2068798B1 (en) 1975-01-10

Family

ID=5753486

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7041150A Expired FR2068798B1 (en) 1969-12-10 1970-11-17

Country Status (2)

Country Link
FR (1) FR2068798B1 (en)
GB (1) GB1276965A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706946A1 (en) * 1993-06-23 1994-12-30 Snecma Pseudo-two-dimensional tail pipe

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6183837B2 (en) * 2013-08-19 2017-08-23 国立研究開発法人宇宙航空研究開発機構 Exhaust nozzle
CN114109644A (en) * 2021-10-09 2022-03-01 中国航发贵阳发动机设计研究所 Method for adjusting area of exit throat of special-shaped fixed spray pipe of aircraft engine

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1380382A (en) * 1963-02-08 1964-11-27 Rolls Royce Shutter device for regulating the flow in a gas turbo-reactor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1380382A (en) * 1963-02-08 1964-11-27 Rolls Royce Shutter device for regulating the flow in a gas turbo-reactor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706946A1 (en) * 1993-06-23 1994-12-30 Snecma Pseudo-two-dimensional tail pipe
US5437412A (en) * 1993-06-23 1995-08-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.) Variable geometry jet engine exhaust nozzle

Also Published As

Publication number Publication date
GB1276965A (en) 1972-06-07
DE1961999B2 (en) 1975-07-03
FR2068798B1 (en) 1975-01-10
DE1961999A1 (en) 1971-06-16

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Legal Events

Date Code Title Description
ST Notification of lapse