FR2018120A1 - - Google Patents

Info

Publication number
FR2018120A1
FR2018120A1 FR6931064A FR6931064A FR2018120A1 FR 2018120 A1 FR2018120 A1 FR 2018120A1 FR 6931064 A FR6931064 A FR 6931064A FR 6931064 A FR6931064 A FR 6931064A FR 2018120 A1 FR2018120 A1 FR 2018120A1
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.)
Withdrawn
Application number
FR6931064A
Other languages
French (fr)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2018120A1 publication Critical patent/FR2018120A1/fr
Withdrawn legal-status Critical Current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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/58—Reversers mounted on the inner cone or the nozzle housing or the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Lift Valve (AREA)
FR6931064A 1968-09-14 1969-09-12 Withdrawn FR2018120A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4382468 1968-09-14

Publications (1)

Publication Number Publication Date
FR2018120A1 true FR2018120A1 (de) 1970-05-29

Family

ID=10430458

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6931064A Withdrawn FR2018120A1 (de) 1968-09-14 1969-09-12

Country Status (4)

Country Link
US (1) US3570247A (de)
DE (1) DE1946592B2 (de)
FR (1) FR2018120A1 (de)
GB (1) GB1253071A (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2123115B1 (de) * 1971-01-08 1975-01-17 Serap
US3824946A (en) * 1972-08-30 1974-07-23 D Macardy Water jet propulsion unit
US3774868A (en) * 1972-12-11 1973-11-27 G Goetz Integrated nozzle
US3831376A (en) * 1973-02-05 1974-08-27 Boeing Co Thrust reverser
US4037405A (en) * 1975-09-30 1977-07-26 United Technologies Corporation Two dimensional nozzle with rotating plug
US4050631A (en) * 1976-03-26 1977-09-27 The Boeing Company Jet engine nozzle for controlling the direction of thrust
US4088270A (en) * 1976-03-31 1978-05-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Two dimensional wedge/translating shroud nozzle
US4147027A (en) * 1976-04-06 1979-04-03 Grumman Aerospace Corporation Thrust reverser nozzle
US4175385A (en) * 1977-12-12 1979-11-27 General Electric Company Thrust reverser for an asymmetric aircraft exhaust nozzle
US5699966A (en) * 1980-03-31 1997-12-23 General Electric Company Exhaust nozzle of a gas turbine engine
FR2622928A1 (fr) * 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes,a section variable d'ejection
FR2766522B1 (fr) * 1997-07-24 1999-09-03 Hispano Suiza Sa Inverseur de poussee de turbosoufflante a obstacle a guidage axial lies au capot primaire
SE515379C2 (sv) * 1999-12-22 2001-07-23 Saab Ab Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning
US7568348B2 (en) * 2005-11-28 2009-08-04 Aerojet-General Corporation Nozzle assembly for rocket and ramjet applications
DE102008022289B4 (de) * 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
US9623976B2 (en) * 2012-07-25 2017-04-18 Rohr, Inc. Nacelle for a high bypass ratio engine with multiple flow paths
US10001080B2 (en) * 2014-08-19 2018-06-19 The Boeing Company Thrust reverse variable area fan nozzle
RU2758875C1 (ru) * 2020-07-23 2021-11-02 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Выходное устройство плоского реактивного сопла
RU2758867C1 (ru) * 2020-07-23 2021-11-02 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Выходное устройство плоского реактивного сопла

Also Published As

Publication number Publication date
US3570247A (en) 1971-03-16
DE1946592A1 (de) 1970-05-21
DE1946592B2 (de) 1977-02-24
GB1253071A (de) 1971-11-10

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Legal Events

Date Code Title Description
TP Transmission of property
TP Transmission of property
TP Transmission of property
ST Notification of lapse