DE69221389D1 - Vorrichtung zur abnehmbaren Verbindung eines Kerngehäuses mit einem Leitschaufelgehäuse mittels festem Mittelring - Google Patents

Vorrichtung zur abnehmbaren Verbindung eines Kerngehäuses mit einem Leitschaufelgehäuse mittels festem Mittelring

Info

Publication number
DE69221389D1
DE69221389D1 DE69221389T DE69221389T DE69221389D1 DE 69221389 D1 DE69221389 D1 DE 69221389D1 DE 69221389 T DE69221389 T DE 69221389T DE 69221389 T DE69221389 T DE 69221389T DE 69221389 D1 DE69221389 D1 DE 69221389D1
Authority
DE
Germany
Prior art keywords
housing
guide vane
detachable connection
center ring
fixed center
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.)
Expired - Lifetime
Application number
DE69221389T
Other languages
English (en)
Inventor
Eugene Jesus Antuna
Donald Frederick Keck
James William Brantley
Robert Howard Roth
Thomas George Wakeman
Alan Blake Corbeil
Michael Leon Barron
Jeffrey Brian Fravel
William James Strock
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.)
General Electric Co
Original Assignee
General Electric Co
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
Priority claimed from US07/785,365 external-priority patent/US5222360A/en
Application filed by General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE69221389D1 publication Critical patent/DE69221389D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE69221389T 1991-05-28 1992-05-27 Vorrichtung zur abnehmbaren Verbindung eines Kerngehäuses mit einem Leitschaufelgehäuse mittels festem Mittelring Expired - Lifetime DE69221389D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US70826391A 1991-05-28 1991-05-28
US07/785,365 US5222360A (en) 1991-10-30 1991-10-30 Apparatus for removably attaching a core frame to a vane frame with a stable mid ring

Publications (1)

Publication Number Publication Date
DE69221389D1 true DE69221389D1 (de) 1997-09-11

Family

ID=27108045

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69221389T Expired - Lifetime DE69221389D1 (de) 1991-05-28 1992-05-27 Vorrichtung zur abnehmbaren Verbindung eines Kerngehäuses mit einem Leitschaufelgehäuse mittels festem Mittelring

Country Status (3)

Country Link
EP (1) EP0516389B1 (de)
JP (1) JPH06105048B2 (de)
DE (1) DE69221389D1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08319865A (ja) * 1995-05-26 1996-12-03 Mitsubishi Motors Corp 筒内噴射式内燃機関における燃料噴射制御装置
WO2005025274A1 (en) 2003-09-04 2005-03-17 Koninklijke Philips Electronics, N.V. Led temperature-dependent power supply system and method
FR2872485B1 (fr) * 2004-07-05 2006-09-15 Snecma Moteurs Sa Raidisseur pour compresseur basse pression d'un moteur d'aeronef
FR2887850B1 (fr) * 2005-06-29 2008-11-07 Airbus France Sas Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur
RU2554381C2 (ru) 2011-03-09 2015-06-27 АйЭйчАй КОРПОРЕЙШН Крепежная конструкция направляющих лопастей и вентилятор
JP5962887B2 (ja) 2012-02-02 2016-08-03 株式会社Ihi 翼の連結部構造及びこれを用いたジェットエンジン
JP6082193B2 (ja) 2012-06-20 2017-02-15 株式会社Ihi 翼の連結部構造及びこれを用いたジェットエンジン
US10443447B2 (en) 2016-03-14 2019-10-15 General Electric Company Doubler attachment system
GB201907545D0 (en) 2019-05-29 2019-07-10 Siemens Ag Heatshield for a gas turbine engine
CN115387906B (zh) * 2022-05-12 2024-04-16 中国航发四川燃气涡轮研究院 低进口轮毂比发动机的进气承力框架连接结构及装配方法
CN115716536B (zh) * 2022-10-25 2023-07-21 中国航发沈阳发动机研究所 一种薄壁高强斜支板承力框架结构

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1149513A (en) * 1966-10-06 1969-04-23 Rolls Royce Bearing assembly
US3830058A (en) * 1973-02-26 1974-08-20 Avco Corp Fan engine mounting
GB2192233B (en) * 1986-07-02 1990-11-28 Rolls Royce Plc A gas turbine engine load transfer structure
US4785625A (en) * 1987-04-03 1988-11-22 United Technologies Corporation Ducted fan gas turbine power plant mounting
US4934140A (en) * 1988-05-13 1990-06-19 United Technologies Corporation Modular gas turbine engine

Also Published As

Publication number Publication date
JPH06105048B2 (ja) 1994-12-21
JPH05149148A (ja) 1993-06-15
EP0516389A3 (en) 1993-08-25
EP0516389A2 (de) 1992-12-02
EP0516389B1 (de) 1997-08-06

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Legal Events

Date Code Title Description
8332 No legal effect for de