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BR112012011535A2 - montagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato - Google Patents

montagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato

Info

Publication number
BR112012011535A2
BR112012011535A2 BR112012011535A BR112012011535A BR112012011535A2 BR 112012011535 A2 BR112012011535 A2 BR 112012011535A2 BR 112012011535 A BR112012011535 A BR 112012011535A BR 112012011535 A BR112012011535 A BR 112012011535A BR 112012011535 A2 BR112012011535 A2 BR 112012011535A2
Authority
BR
Brazil
Prior art keywords
agb
longitudinal axis
turbine engine
intermediate housing
mounting
Prior art date
Application number
BR112012011535A
Other languages
English (en)
Other versions
BR112012011535B1 (pt
Inventor
Jérémy Edmond Fert
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BR112012011535A2 publication Critical patent/BR112012011535A2/pt
Publication of BR112012011535B1 publication Critical patent/BR112012011535B1/pt

Links

Classifications

    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

"mo0ntagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato". a invenção refere-se a uma carcaça intermediária (20) para um compartimento de ventilador (cs) de turbojato, compreendendo: - uma cobertura (22) centralizada ao longo de um eixo longitudinal (x-x) do motor de turbina; - uma aleta lateral anular (24) centralizada ao longo do eixo longitudinal do motor de turbina e montada contra uma face à jusante da cobertura; - uma vigia de suspensão (28) fixada na aleta lateral e se estendendo à jusante paralela ao eixo longitudinal do motor de turbina; e - uma agb (30) suspensa a partir da viga e compreendendo uma face lateral a montante (30b) separada axialmente da aleta lateral, uma face lateral à jusante (30a) oposta à face lateral a montante, e uma pluralidade de acessórios (32,34) montados contra sua face lateral à jusante e distribuídos em torno do eixo longitudinal do motor de turbina.
BR112012011535A 2009-11-17 2010-11-16 montagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato BR112012011535B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0958105A FR2952672B1 (fr) 2009-11-17 2009-11-17 Montage d'un boitier d'accessoires sur un carter intermediaire pour compartiment de soufflante de turboreacteur
PCT/FR2010/052431 WO2011061437A1 (fr) 2009-11-17 2010-11-16 Montage d'un boitier d'accessoires sur un carter intermediaire pour compartiment de soufflante de turboreacteur

Publications (2)

Publication Number Publication Date
BR112012011535A2 true BR112012011535A2 (pt) 2016-06-28
BR112012011535B1 BR112012011535B1 (pt) 2020-05-05

Family

ID=42289688

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012011535A BR112012011535B1 (pt) 2009-11-17 2010-11-16 montagem de uma agb em uma carcaça intermediária para um compartimento de ventilador de turbojato

Country Status (9)

Country Link
US (1) US8607578B2 (pt)
EP (1) EP2501613B1 (pt)
JP (1) JP5591944B2 (pt)
CN (1) CN102666279B (pt)
BR (1) BR112012011535B1 (pt)
CA (1) CA2780659C (pt)
FR (1) FR2952672B1 (pt)
RU (1) RU2542730C2 (pt)
WO (1) WO2011061437A1 (pt)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201121971D0 (en) * 2011-12-21 2012-02-01 Rolls Royce Deutschland & Co Kg Accessory mounting for a gas turbine
FR3004701B1 (fr) * 2013-04-22 2015-04-03 Snecma Dispositif de delestage des alternateurs d'un turboreacteur pendant ses accelerations
FR3010700B1 (fr) * 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
US10634061B2 (en) * 2014-03-06 2020-04-28 United Technologies Corporation Gas turbine engine accessory architecture
CN105173093B (zh) * 2015-09-24 2018-01-30 江西洪都航空工业集团有限责任公司 一种悬挂快卸式安装节
US10526915B2 (en) * 2016-03-07 2020-01-07 United Technologies Corporation Firewall mount hub
CN109625294B (zh) * 2018-12-16 2022-07-15 中国航发沈阳发动机研究所 航空发动机与外部附件机匣之间的吊挂结构
FR3117530B1 (fr) 2020-12-15 2024-01-05 Safran Aircraft Engines Ensemble pour turbomachine d’aéronef comprenant un support d’équipements
FR3123377B1 (fr) 2021-05-27 2023-05-19 Safran Aircraft Engines Ensemble de supportage d’une boite d’accessoires d’une turbomachine d'aéronef
FR3123948B1 (fr) 2021-06-09 2023-06-09 Safran Aircraft Engines Ensemble pour turbomachine d’aéronef comprenant un support d’équipements
FR3124551B1 (fr) 2021-06-25 2024-04-12 Safran Trans Systems Ensemble pour turbomachine d’aéronef comprenant un support d’équipements
FR3124545B1 (fr) 2021-06-28 2023-06-23 Safran Aircraft Engines Ensemble pour turbomachine d’aéronef comprenant un support d’équipements
US12104539B2 (en) 2022-10-25 2024-10-01 General Electric Company Gas turbine engine
US12098649B2 (en) 2022-10-25 2024-09-24 General Electric Company Gas turbine engine accessory packaging

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3543588A (en) * 1968-11-12 1970-12-01 Gen Motors Corp Accessory installation
SU1394636A1 (ru) * 1986-10-03 2004-07-27 В.С. Вигант Узел крепления двигателя
US6260351B1 (en) * 1998-12-10 2001-07-17 United Technologies Corporation Controlled spring rate gearbox mount
US6357220B1 (en) * 1998-12-22 2002-03-19 United Technologies Corporation Gearbox accessory mount
US7500365B2 (en) * 2005-05-05 2009-03-10 United Technologies Corporation Accessory gearbox
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891248B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef

Also Published As

Publication number Publication date
FR2952672A1 (fr) 2011-05-20
FR2952672B1 (fr) 2011-12-09
CA2780659C (fr) 2017-01-17
CN102666279A (zh) 2012-09-12
BR112012011535B1 (pt) 2020-05-05
CN102666279B (zh) 2015-01-14
RU2542730C2 (ru) 2015-02-27
RU2012125021A (ru) 2013-12-27
WO2011061437A1 (fr) 2011-05-26
US8607578B2 (en) 2013-12-17
CA2780659A1 (fr) 2011-05-26
JP2013510996A (ja) 2013-03-28
US20120224950A1 (en) 2012-09-06
JP5591944B2 (ja) 2014-09-17
EP2501613A1 (fr) 2012-09-26
EP2501613B1 (fr) 2013-10-16

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 16/11/2010, OBSERVADAS AS CONDICOES LEGAIS.