BR9403763A - Unidade motopropulsora de uma aeronave - Google Patents

Unidade motopropulsora de uma aeronave

Info

Publication number
BR9403763A
BR9403763A BR9403763A BR9403763A BR9403763A BR 9403763 A BR9403763 A BR 9403763A BR 9403763 A BR9403763 A BR 9403763A BR 9403763 A BR9403763 A BR 9403763A BR 9403763 A BR9403763 A BR 9403763A
Authority
BR
Brazil
Prior art keywords
aircraft
power unit
power
unit
Prior art date
Application number
BR9403763A
Other languages
English (en)
Inventor
Derek Cole
Philip David Sherry
Alan John Blair
Original Assignee
Short Brothers 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 Short Brothers Plc filed Critical Short Brothers Plc
Publication of BR9403763A publication Critical patent/BR9403763A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/08—Inspection panels for power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Emergency Protection Circuit Devices (AREA)
  • Retarders (AREA)
BR9403763A 1993-01-26 1994-01-24 Unidade motopropulsora de uma aeronave BR9403763A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB939301457A GB9301457D0 (en) 1993-01-26 1993-01-26 An aircraft propulsuve power unit
PCT/GB1994/000131 WO1994016945A1 (en) 1993-01-26 1994-01-24 An aircraft propulsive power unit

Publications (1)

Publication Number Publication Date
BR9403763A true BR9403763A (pt) 1999-06-15

Family

ID=10729304

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9403763A BR9403763A (pt) 1993-01-26 1994-01-24 Unidade motopropulsora de uma aeronave

Country Status (9)

Country Link
US (1) US5609313A (pt)
EP (1) EP0631554B1 (pt)
JP (1) JPH07508698A (pt)
AU (1) AU5888694A (pt)
BR (1) BR9403763A (pt)
CA (1) CA2131598A1 (pt)
DE (1) DE69401313D1 (pt)
GB (2) GB9301457D0 (pt)
WO (1) WO1994016945A1 (pt)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9407632D0 (en) * 1994-04-18 1994-06-08 Short Brothers Plc An aircraft propulsive power unit
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2767560B1 (fr) * 1997-08-19 1999-11-12 Aerospatiale Ensemble reducteur de bruit pour turboreacteur d'aeronef
GB9906621D0 (en) 1999-03-23 1999-05-19 British Aerospace Vehicle propulsion systems
GB9921935D0 (en) * 1999-09-17 1999-11-17 Rolls Royce A nacelle assembly for a gas turbine engine
US6340135B1 (en) * 2000-05-30 2002-01-22 Rohr, Inc. Translating independently mounted air inlet system for aircraft turbofan jet engine
GB2385382B (en) * 2002-02-13 2006-02-15 Rolls Royce Plc A cowl structure for a gas turbine engine
US20060145001A1 (en) * 2004-12-30 2006-07-06 Smith Matthew C Fan cowl door elimination
US20070220895A1 (en) * 2005-09-19 2007-09-27 General Electric Company Methods and apparatus for housing gas turbine engines
GB2436353B (en) * 2006-03-22 2008-04-23 Rolls Royce Plc Panel assembly including deformable seal
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2911372B1 (fr) * 2007-01-15 2009-02-27 Aircelle Sa Inverseur de poussee translatable pour moteur a reaction
FR2912378B1 (fr) 2007-02-14 2009-03-20 Aircelle Sa Nacelle de moteur a reaction pour un avion
FR2914363B1 (fr) * 2007-03-26 2012-07-27 Aircelle Sa Systeme de guidage verrouillable pour partie mobile d'une nacelle
US7966808B2 (en) * 2007-04-30 2011-06-28 General Electric Company Baffle seal for gas turbine engine thrust reverser
FR2916426B1 (fr) * 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
FR2920214B1 (fr) * 2007-08-20 2009-10-02 Aircelle Sa Joint d'etancheite double
FR2925607B1 (fr) * 2007-12-21 2013-05-10 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
FR2925877B1 (fr) * 2007-12-26 2009-12-04 Aircelle Sa Installation de systeme de guidage sur une nacelle d'aeronef.
FR2926537B1 (fr) 2008-01-18 2010-02-12 Aircelle Sa Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
FR2927061B1 (fr) * 2008-02-01 2010-02-12 Aircelle Sa Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur
FR2927609B1 (fr) * 2008-02-18 2010-06-25 Aircelle Sa Entree d'air pour nacelle d'aeronef, et nacelle equipee d'une telle entree d'air
FR2928681B1 (fr) * 2008-03-14 2013-11-22 Aircelle Sa Systeme d'actionnement et de controle d'un capot mobile de nacelle de turboreacteur
FR2931205B1 (fr) * 2008-05-16 2010-05-14 Aircelle Sa Ensemble propulsif pour aeronef, et structure d'entree d'air pour un tel ensemble
FR2935355B1 (fr) * 2008-09-02 2010-08-27 Aircelle Sa Dispositif de centrage d'une structure d'entree d'air sur une structure mediane d'une nacelle
FR2936492B1 (fr) * 2008-10-01 2011-04-01 Aircelle Sa Nacelle pour turboreacteur.
FR2936777B1 (fr) * 2008-10-08 2010-10-22 Aircelle Sa Structure d'entree d'air pour une nacelle pour turboreacteur
US8528176B2 (en) 2008-10-24 2013-09-10 Pratt & Whitney Canada Corp. Diffuser case removal apparatus and method
FR2938236B1 (fr) * 2008-11-13 2011-04-15 Aircelle Sa Nacelle pour turboreacteur
FR2938237B1 (fr) * 2008-11-13 2011-05-20 Aircelle Sa Nacelle pour turboreacteur a capot amont translatable
US7798285B2 (en) * 2008-11-14 2010-09-21 Rohr, Inc. Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
US9188025B2 (en) * 2008-11-26 2015-11-17 Mra Systems, Inc. Apparatus for facilitating access to a nacelle interior
US8220738B2 (en) * 2008-11-26 2012-07-17 Mra Systems, Inc. Nacelle and method of assembling the same
US9188026B2 (en) * 2008-11-26 2015-11-17 Mra Systems, Inc. Apparatus for facilitating access to a nacelle interior and method of assembling the same
US8181905B2 (en) * 2008-12-17 2012-05-22 Rohr, Inc. Aircraft engine nacelle with translating inlet cowl
FR2941674B1 (fr) * 2009-02-04 2011-02-11 Aircelle Sa Nacelle de turboreacteur.
ES2345808B1 (es) * 2009-03-31 2011-07-28 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil deslizante.
FR2946014B1 (fr) 2009-05-28 2011-05-20 Sagem Defense Securite Nacelle de moteur d'aeronef comportant un capot mobile mu par des moteurs electriques
FR2960216B1 (fr) * 2010-05-19 2013-02-15 Aircelle Sa Element d'aerodynamisme pour une nacelle d'aeronef
FR2961788B1 (fr) * 2010-06-29 2012-06-15 Aircelle Sa Nacelle de turboreacteur
US8549026B2 (en) * 2010-10-12 2013-10-01 Clinicomp International, Inc. Standardized database access system and method
FR2966433B1 (fr) * 2010-10-26 2012-12-07 Airbus Operations Sas Capot d'aeronef incorporant des moyens pour limiter les phenomenes d'ecope de type pneumatique
US9016042B2 (en) 2011-05-20 2015-04-28 Rohr, Inc. Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure
GB2492107B (en) 2011-06-22 2013-09-04 Rolls Royce Plc Mounting assembly
US9783315B2 (en) * 2012-02-24 2017-10-10 Rohr, Inc. Nacelle with longitudinal translating cowling and rotatable sleeves
FR2997725B1 (fr) * 2012-11-05 2018-03-02 Safran Aircraft Engines Carter de turbomachine
US9822734B2 (en) 2013-02-22 2017-11-21 United Technologies Corporation Tandem thrust reverser with multi-bar linkage
US9611048B2 (en) * 2013-02-22 2017-04-04 United Technologies Corporation ATR axial V-groove
FR3004750B1 (fr) * 2013-04-18 2017-08-11 Snecma Carter de turbomachine
FR3005100B1 (fr) 2013-04-26 2015-05-01 Snecma Carter de turbomachine
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
US9702375B2 (en) 2013-07-16 2017-07-11 United Technologies Corporation Liner attaching scheme
FR3020040B1 (fr) * 2014-04-17 2018-06-29 Societe Lorraine De Construction Aeronautique Ensemble propulsif pour aeronef
FR3020344B1 (fr) * 2014-04-24 2016-05-13 Airbus Operations Sas Assemblage pour un aeronef comportant un panneau d'acces mobile
FR3031341B1 (fr) * 2015-01-07 2017-07-14 Aircelle Sa Ensemble propulsif pour aeronef
JP6506069B2 (ja) * 2015-03-27 2019-04-24 株式会社Ｓｕｂａｒｕ 航空機の推力偏向装置及び航空機の推力偏向方法
US10471610B2 (en) * 2015-06-16 2019-11-12 Samsung Electronics Co., Ltd. Robot arm having weight compensation mechanism
US20170283081A1 (en) * 2016-04-05 2017-10-05 Rohr, Inc. Securing a translating fanlet for an aircraft propulsion system nacelle
FR3052809B1 (fr) * 2016-06-17 2019-05-03 Safran Nacelles Systeme de guidage axial pour des capots d'inverseur de poussee comprenant un doigt de securite
US10738737B2 (en) * 2016-11-18 2020-08-11 Rohr, Inc. Self-locking alignment at a nacelle interface
FR3060650B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Structure d'entree d'air pour une nacelle d'aeronef
FR3094698B1 (fr) * 2019-04-02 2022-09-09 Safran Aircraft Engines Manche d’entree d’air pour une nacelle d’un ensemble propulsif d’aeronef
US11441482B2 (en) * 2019-06-04 2022-09-13 Rohr, Inc. Single track translating inlet
FR3114849A1 (fr) * 2020-10-02 2022-04-08 Airbus Operations Turboreacteur double flux d’un aeronef comportant un capot articule en rotation et un systeme de deploiement dudit capot
FR3117170B1 (fr) * 2020-12-07 2022-11-04 Safran Nacelles Ensemble propulsif pour un aeronef et son procede de montage

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB750623A (en) * 1950-06-16 1956-06-20 Snecma Thrust reducing or reversing device for jet propelling nozzles
GB717760A (en) * 1951-10-10 1954-11-03 Boulton Aircraft Ltd Improvements in or relating to air intakes for jet propulsion engines
GB850691A (en) * 1957-05-14 1960-10-05 Power Jets Res & Dev Ltd Improvements in or relating to aircraft engine nacelle structures
GB883634A (en) * 1958-08-15 1961-12-06 Rolls Royce Improved gas turbine engine
GB950909A (en) * 1962-05-11 1964-02-26 Rolls Royce Improvements relating to the mounting of gas turbine engines
GB1077196A (en) * 1966-04-26 1967-07-26 Rolls Royce Air intake duct for a gas turbine engine
GB1120240A (en) * 1966-04-26 1968-07-17 Rolls Royce Air intake duct for a gas turbine engine
FR1588379A (pt) * 1967-11-27 1970-04-10
GB1375868A (pt) * 1972-09-22 1974-11-27
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
US4206893A (en) * 1978-09-27 1980-06-10 The Boeing Company Seal closure for slot in engine mounting strut
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
GB8822798D0 (en) * 1988-09-28 1988-11-02 Short Brothers Ltd Ducted fan turbine engine

Also Published As

Publication number Publication date
GB9301457D0 (en) 1993-03-17
GB2274490B (en) 1996-09-18
DE69401313D1 (de) 1997-02-13
EP0631554B1 (en) 1997-01-02
GB2274490A (en) 1994-07-27
US5609313A (en) 1997-03-11
CA2131598A1 (en) 1994-08-04
EP0631554A1 (en) 1995-01-04
GB9401269D0 (en) 1994-03-23
JPH07508698A (ja) 1995-09-28
WO1994016945A1 (en) 1994-08-04
AU5888694A (en) 1994-08-15

Similar Documents

Publication Publication Date Title
BR9403763A (pt) Unidade motopropulsora de uma aeronave
DE59405105D1 (de) Kombinations-luftfahrzeug
DE69315410D1 (de) Leistungsversorgungen
DE69403946D1 (de) Leistungskondensator
DE69326663D1 (de) Unterschneidungsverfahren
BR8605952A (pt) Tear e metodo de instalar pelo menos uma unidade de interruptor no tear
DE59403182D1 (de) Hochspannungsanlage
DE59307227D1 (de) Leistungs-Spannungsbegrenzungsschaltung
KR940020906U (ko) 축류팬의 날개구조
KR940020859U (ko) 케이스의 개폐장치
DE69408535D1 (de) Hochspannungsgenerator
KR970051679U (ko) 항공기의 동체
SE9202692D0 (sv) En flygmaskin
KR970011314U (ko) 전원공급장치의 접지 구조
KR940023748U (ko) 모니터 절전회로
FI933782A (fi) Voimayksikkö
KR950001939U (ko) 모터의 동력전달장치
KR950002484U (ko) 고압선 격리구
KR940021064U (ko) 냉장고의 전장부 조립구조
KR950011439U (ko) 자동차 동력 조향장치의 동체부
UA596S (uk) Агрегат силовий універсальний
KR940020710U (ko) 마그네트론의 에프(f)-세라믹 구조
KR950022034U (ko) 모니터의 모드콘트롤 회로
KR950022003U (ko) 모니터의 전원제어회로
KR970020144U (ko) 모니터의 고전압 출력 회로

Legal Events

Date Code Title Description
FA7 Application deemed withdrawn (art. 18 par. 1 of law 5772/71) - being contrary to morals, good customs and public security, order and health