IL91811A0 - Ducted fan turbine engine - Google Patents

Ducted fan turbine engine

Info

Publication number
IL91811A0
IL91811A0 IL91811A IL9181189A IL91811A0 IL 91811 A0 IL91811 A0 IL 91811A0 IL 91811 A IL91811 A IL 91811A IL 9181189 A IL9181189 A IL 9181189A IL 91811 A0 IL91811 A0 IL 91811A0
Authority
IL
Israel
Prior art keywords
turbine engine
ducted fan
fan turbine
ducted
engine
Prior art date
Application number
IL91811A
Other languages
English (en)
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 IL91811A0 publication Critical patent/IL91811A0/xx

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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Catching Or Destruction (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IL91811A 1988-09-28 1989-09-27 Ducted fan turbine engine IL91811A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888822798A GB8822798D0 (en) 1988-09-28 1988-09-28 Ducted fan turbine engine

Publications (1)

Publication Number Publication Date
IL91811A0 true IL91811A0 (en) 1990-06-10

Family

ID=10644413

Family Applications (1)

Application Number Title Priority Date Filing Date
IL91811A IL91811A0 (en) 1988-09-28 1989-09-27 Ducted fan turbine engine

Country Status (11)

Country Link
US (1) US5136839A (xx)
EP (1) EP0361901B1 (xx)
JP (1) JPH03501835A (xx)
AU (1) AU633518B2 (xx)
BR (1) BR8907100A (xx)
CA (1) CA1334723C (xx)
DE (1) DE68908321T2 (xx)
ES (1) ES2043032T3 (xx)
GB (2) GB8822798D0 (xx)
IL (1) IL91811A0 (xx)
WO (1) WO1990003309A1 (xx)

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9120658D0 (en) * 1991-09-27 1991-11-06 Short Brothers Plc Ducted fan turbine engine
GB9123083D0 (en) * 1991-10-31 1991-12-18 Band David M Ion-selective polymeric electrodes
GB9301457D0 (en) * 1993-01-26 1993-03-17 Short Brothers Plc An aircraft propulsuve power unit
FR2755095B1 (fr) * 1996-10-24 1998-12-18 Conception Aeronautique Du Sud Nacelle longue pour moteur a reaction double flux d'aeronef
FR2764644B1 (fr) * 1997-06-12 1999-07-16 Hispano Suiza Sa Turboreacteur a double flux associe a un inverseur de poussee avec un carenage rapporte dans la veine fluide
FR2771330B1 (fr) * 1997-11-26 2004-02-27 Aerospatiale Procede de fabrication d'un panneau composite monolithique articule avec des moyens raidisseurs integres, panneau articule obtenu et capot articule dans un aeronef
FR2811716B1 (fr) * 2000-07-17 2002-10-04 Hurel Dubois Avions Perfectionnements aux arriere-corps de nacelle, a tuyere commune, de reacteur d'avion
US6887035B2 (en) 2002-10-23 2005-05-03 General Electric Company Tribologically improved design for variable stator vanes
FR2856379B1 (fr) * 2003-06-18 2006-11-24 Airbus France Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
US6971240B2 (en) * 2004-03-30 2005-12-06 General Electric Company Methods and apparatus for exhausting gases from gas turbine engines
ES2264625B1 (es) * 2004-12-15 2007-12-01 GAMESA INNOVATION & TECHNOLOGY, S.L. Procedimiento de retirada de la cubierta de un aerogenerador.
FR2896481B1 (fr) * 2006-01-23 2009-12-04 Aircelle Sa Systeme de fixation pour element constitutif d'une nacelle de turboreacteur
ES2316257B1 (es) * 2006-10-31 2010-01-12 Airbus España, S.L. Cono de cola para aeronave con carena movil y estructura de soporte de unidad auxiliar de energia y de sus elementos anexos.
FR2912378B1 (fr) * 2007-02-14 2009-03-20 Aircelle Sa Nacelle de moteur a reaction pour un avion
FR2916426B1 (fr) * 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
FR2920136B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Systeme de liaison entre une structure interne et un structure externe d'une nacelle
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8262050B2 (en) 2008-12-24 2012-09-11 General Electric Company Method and apparatus for mounting and dismounting an aircraft engine
US8469309B2 (en) * 2008-12-24 2013-06-25 General Electric Company Monolithic structure for mounting aircraft engine
ES2398861B1 (es) * 2010-10-08 2014-04-29 Airbus Operations, S.L. Concepto de unión intercambiable para un cono de un fuselaje trasero de un avión.
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
CN105765204B (zh) 2013-10-07 2019-07-30 罗尔公司 具有金属和复合构造的混合式内部固定结构
US10371047B2 (en) 2013-10-16 2019-08-06 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
US10161356B2 (en) * 2014-06-02 2018-12-25 Ge Aviation Systems Llc Integrated thrust reverser actuation system
US10759541B2 (en) 2016-10-14 2020-09-01 Rohr, Inc. Nacelle bifurcation with leading edge structure
US10611490B2 (en) * 2016-11-02 2020-04-07 Rohr, Inc. Fan cowl fairing restraining system
US10543927B2 (en) 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
US10899463B2 (en) 2017-05-16 2021-01-26 Rohr, Inc. Segmented pylon for an aircraft propulsion system
CN109502034B (zh) * 2018-12-11 2021-10-19 湖北航天飞行器研究所 一种小口径飞行器燃气舵挡火结构

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB758205A (en) * 1953-12-30 1956-10-03 Armstrong Siddeley Motors Ltd Improvements relating to by-pass, turbo-jet engines
GB966522A (en) * 1960-02-02 1964-08-12 Bristol Siddeley Engines Ltd Improvements relating to aerial vehicles having jet propulsion engines
US3542152A (en) * 1968-04-08 1970-11-24 Gen Electric Sound suppression panel
US3508838A (en) * 1968-09-16 1970-04-28 Gen Electric Sound suppression of compressors used in gas turbine engines
US3541794A (en) * 1969-04-23 1970-11-24 Gen Electric Bifurcated fan duct thrust reverser
US3670964A (en) * 1971-01-18 1972-06-20 Gen Motors Corp Jet nozzle
GB1375868A (xx) * 1972-09-22 1974-11-27
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
GB1522558A (en) * 1976-04-05 1978-08-23 Rolls Royce Duct linings
GB1543312A (en) * 1976-07-21 1979-04-04 Rolls Royce Honeycomb linings
CA1324999C (en) * 1986-04-30 1993-12-07 Walter M. Presz, Jr. Bodies with reduced surface drag
US4696159A (en) * 1986-08-04 1987-09-29 United Technologies Corporation Gas turbine outlet arrangement
US4790137A (en) * 1987-07-17 1988-12-13 The United States Of America As Represented By The Secretary Of The Air Force Aircraft engine outer duct mounting device
GB2212859B (en) * 1987-12-02 1991-03-06 Rolls Royce Plc Ducted fan gas turbine engine with surge controller

Also Published As

Publication number Publication date
DE68908321D1 (de) 1993-09-16
EP0361901A1 (en) 1990-04-04
WO1990003309A1 (en) 1990-04-05
GB2225060B (en) 1993-03-24
JPH03501835A (ja) 1991-04-25
GB8822798D0 (en) 1988-11-02
BR8907100A (pt) 1991-02-05
US5136839A (en) 1992-08-11
AU633518B2 (en) 1993-02-04
AU4327789A (en) 1990-04-18
EP0361901B1 (en) 1993-08-11
ES2043032T3 (es) 1993-12-16
DE68908321T2 (de) 1994-02-24
GB2225060A (en) 1990-05-23
GB8921744D0 (en) 1989-11-08
CA1334723C (en) 1995-03-14

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Legal Events

Date Code Title Description
KB Patent renewed
RH1 Patent not in force