BE693994A - - Google Patents

Info

Publication number
BE693994A
BE693994A BE693994DA BE693994A BE 693994 A BE693994 A BE 693994A BE 693994D A BE693994D A BE 693994DA BE 693994 A BE693994 A BE 693994A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE693994A publication Critical patent/BE693994A/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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/60—Mounting; Assembling; Disassembling
    • F04D29/64—Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE693994D 1966-05-25 1967-02-13 BE693994A (uk)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US552755A US3398535A (en) 1966-05-25 1966-05-25 Engine supporting structure

Publications (1)

Publication Number Publication Date
BE693994A true BE693994A (uk) 1967-07-17

Family

ID=24206666

Family Applications (1)

Application Number Title Priority Date Filing Date
BE693994D BE693994A (uk) 1966-05-25 1967-02-13

Country Status (5)

Country Link
US (1) US3398535A (uk)
BE (1) BE693994A (uk)
DE (1) DE1626084A1 (uk)
FR (1) FR1516333A (uk)
GB (1) GB1151613A (uk)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3494129A (en) * 1968-03-06 1970-02-10 Gen Electric Fluid compressors and turbofan engines employing same
GB1294324A (en) * 1969-05-03 1972-10-25 Dowty Rotol Ltd Engine installations
US3830058A (en) * 1973-02-26 1974-08-20 Avco Corp Fan engine mounting
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
US4571936A (en) * 1985-07-10 1986-02-25 The United States Of America As Represented By The Secretary Of The Air Force Length adjustable strut link with low aerodynamic drag
US4722184A (en) * 1985-10-03 1988-02-02 United Technologies Corporation Annular stator structure for a rotary machine
US4820117A (en) * 1987-07-09 1989-04-11 United Technologies Corporation Crossed I-beam structural strut
CA2021087A1 (en) * 1989-09-07 1991-03-08 Eugene J. Antuna Ultra high bypass engine integrated fan/cowl and transportation/removal
US5161947A (en) * 1991-05-08 1992-11-10 United Technologies Corporation Fan case strut for turbomachine
US5224341A (en) * 1992-01-06 1993-07-06 United Technologies Corporation Separable fan strut for a gas turbofan powerplant
WO1992019854A1 (en) * 1991-05-08 1992-11-12 United Technologies Corporation Separable fan strut for a gas turbofan powerplant
US5609467A (en) * 1995-09-28 1997-03-11 Cooper Cameron Corporation Floating interturbine duct assembly for high temperature power turbine
JPH11247605A (ja) 1997-12-26 1999-09-14 United Technol Corp <Utc> タ―ボマシ―ンコンポ―ネントの振動緩衝方法及び装置
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
US7124572B2 (en) * 2004-09-14 2006-10-24 Honeywell International, Inc. Recuperator and turbine support adapter for recuperated gas turbine engines
GB0520850D0 (en) * 2005-10-14 2005-11-23 Rolls Royce Plc Fan static structure
BRPI0708547B1 (pt) * 2006-03-03 2018-02-06 Dresser-Rand Company Dispositivo de processamento de fluido multifásico
FR2925121B1 (fr) * 2007-12-18 2014-07-04 Snecma Carter intermediaire pour turboreacteur d'aeronef a conception amelioree
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2933130B1 (fr) * 2008-06-25 2012-02-24 Snecma Carter structural pour turbomachine
GB2468485A (en) * 2009-03-09 2010-09-15 Aircelle Ltd Turbine engine support arm
US8316523B2 (en) 2009-10-01 2012-11-27 Pratt & Whitney Canada Corp. Method for centering engine structures
US8784050B2 (en) * 2010-06-15 2014-07-22 Rolls-Royce Corporation Aggregate vane assembly
US20130084174A1 (en) * 2011-10-03 2013-04-04 United Technologies Corporation Strut rods for structural guide vanes
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
US9163525B2 (en) * 2012-06-27 2015-10-20 United Technologies Corporation Turbine wheel catcher
US10227895B2 (en) * 2013-12-20 2019-03-12 Pratt & Whitney Canada Corp. Gas turbine case and reinforcement strut for same
US20160201516A1 (en) * 2015-01-09 2016-07-14 United Technologies Corporation Gas turbine engine mid-turbine frame tie rod arrangement
GB201803571D0 (en) * 2018-03-06 2018-04-18 Rolls Royce Plc Component
CN113443124B (zh) * 2021-07-20 2022-08-19 北京理工大学 采用两级大小叶片的边界层吸入式推进器
US11555420B1 (en) 2021-08-20 2023-01-17 Raytheon Technologies Corporation Frame connection between fan case and core housing in a gas turbine engine
US11674415B2 (en) 2021-08-20 2023-06-13 Raytheon Technologies Corporation Front section stiffness ratio
US11708772B2 (en) 2021-11-12 2023-07-25 Raytheon Technologies Corporation Triangular-frame connection between fan case and core housing in a gas turbine engine
US11608796B1 (en) 2021-11-12 2023-03-21 Raytheon Technologies Corporation Radial strut frame connection between fan case and core housing in a gas turbine engine
US11686220B2 (en) 2021-11-12 2023-06-27 Raytheon Technologies Corporation H-frame connection between fan case and core housing in a gas turbine engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070285A (en) * 1959-11-26 1962-12-25 Rolls Royce Gas turbine engine
US3262270A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser

Also Published As

Publication number Publication date
FR1516333A (fr) 1968-03-08
DE1626084A1 (de) 1971-05-13
GB1151613A (en) 1969-05-14
US3398535A (en) 1968-08-27

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