FR2284042A1 - Perfectionnements apportes aux groupes turbopropulseurs - Google Patents

Perfectionnements apportes aux groupes turbopropulseurs

Info

Publication number
FR2284042A1
FR2284042A1 FR7527158A FR7527158A FR2284042A1 FR 2284042 A1 FR2284042 A1 FR 2284042A1 FR 7527158 A FR7527158 A FR 7527158A FR 7527158 A FR7527158 A FR 7527158A FR 2284042 A1 FR2284042 A1 FR 2284042A1
Authority
FR
France
Prior art keywords
turbopropeller
units
turbopropeller units
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.)
Withdrawn
Application number
FR7527158A
Other languages
English (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.)
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 FR2284042A1 publication Critical patent/FR2284042A1/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Withdrawn legal-status Critical Current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
    • 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
FR7527158A 1974-09-07 1975-09-04 Perfectionnements apportes aux groupes turbopropulseurs Withdrawn FR2284042A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3917174A GB1473543A (en) 1974-09-07 1974-09-07 Gas turbine powerplants

Publications (1)

Publication Number Publication Date
FR2284042A1 true FR2284042A1 (fr) 1976-04-02

Family

ID=10408070

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7527158A Withdrawn FR2284042A1 (fr) 1974-09-07 1975-09-04 Perfectionnements apportes aux groupes turbopropulseurs

Country Status (6)

Country Link
US (1) US4102499A (fr)
JP (1) JPS5153112A (fr)
DE (1) DE2539052A1 (fr)
FR (1) FR2284042A1 (fr)
GB (1) GB1473543A (fr)
IT (1) IT1042169B (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8715844D0 (en) * 1987-07-06 1987-08-12 Mcculloch M L Propulsion device
US7762374B2 (en) * 2006-11-22 2010-07-27 Honeywell International Inc. Turbine engine diffusing exhaust muffler
US8128037B2 (en) * 2009-01-19 2012-03-06 The Boeing Company Apparatus and method for passive purging of micro-perforated aerodynamic surfaces
US8245976B2 (en) * 2009-01-19 2012-08-21 The Boeing Company Door assembly for laminar flow control system
US8245966B2 (en) 2009-02-04 2012-08-21 21St Century Airship Technologies Inc. Airship and vectored propeller drive therefor
US9487288B2 (en) 2013-06-04 2016-11-08 The Boeing Company Apparatus and methods for extending hybrid laminar flow control

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510506A (en) * 1944-07-15 1950-06-06 Jarvis C Marble Turbojet power plant with controllable primary and secondary outlets
US2680948A (en) * 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
DE1100385B (de) * 1958-12-10 1961-02-23 Entwicklungsbau Pirna Veb Vorrichtung zur Laermbekaempfung des Abgasstrahles eines Strahltriebwerkes durch Zumischen von Frischluft und zur AEnderung der Ausstroemrichtung des Abgasstrahles mittels stellbarer Umlenkplatten
GB895331A (en) * 1960-03-04 1962-05-02 Rolls Royce Improvements in or relating to jet propulsion nozzles
US3248878A (en) * 1963-09-18 1966-05-03 Gen Electric Thrust deflector and reverser
FR1401425A (fr) * 1964-04-24 1965-06-04 Aviation Louis Breguet Sa Dispositif de tuyère d'éjection pour avions à réaction
US3486698A (en) * 1966-07-13 1969-12-30 Thiokol Chemical Corp Roll and directional control apparatus for rocket motors
US3558058A (en) * 1969-03-14 1971-01-26 Us Air Force Thrust vectorable supersonic nozzle
US3650348A (en) * 1970-02-19 1972-03-21 Boeing Co Supersonic noise suppressor
US3739582A (en) * 1972-04-13 1973-06-19 Rohr Industries Inc Thrust reversing apparatus

Also Published As

Publication number Publication date
US4102499A (en) 1978-07-25
JPS5153112A (en) 1976-05-11
IT1042169B (it) 1980-01-30
GB1473543A (en) 1977-05-11
DE2539052A1 (de) 1976-03-25

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Legal Events

Date Code Title Description
CA Change of address
CD Change of name or company name
ST Notification of lapse