BR112015012033A2 - dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves - Google Patents

dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves

Info

Publication number
BR112015012033A2
BR112015012033A2 BR112015012033A BR112015012033A BR112015012033A2 BR 112015012033 A2 BR112015012033 A2 BR 112015012033A2 BR 112015012033 A BR112015012033 A BR 112015012033A BR 112015012033 A BR112015012033 A BR 112015012033A BR 112015012033 A2 BR112015012033 A2 BR 112015012033A2
Authority
BR
Brazil
Prior art keywords
centering device
propulsion assembly
aircraft propulsion
turbojet nacelle
turbojet
Prior art date
Application number
BR112015012033A
Other languages
English (en)
Inventor
Kioua Hazem
Conet Olivier
Holay Xavier
Raymond Yves Lore Xavier
Original Assignee
Aircelle Sa
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 Aircelle Sa filed Critical Aircelle Sa
Publication of BR112015012033A2 publication Critical patent/BR112015012033A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • B64D29/06—Attaching of nacelles, fairings or cowlings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BR112015012033A 2012-12-12 2013-11-27 dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves BR112015012033A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1261955A FR2999154B1 (fr) 2012-12-12 2012-12-12 Centreur d'assemblage pour nacelle de turboreacteur
PCT/FR2013/052870 WO2014091110A1 (fr) 2012-12-12 2013-11-27 Centreur d'assemblage pour nacelle de turboréacteur

Publications (1)

Publication Number Publication Date
BR112015012033A2 true BR112015012033A2 (pt) 2017-07-11

Family

ID=47741137

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015012033A BR112015012033A2 (pt) 2012-12-12 2013-11-27 dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves

Country Status (8)

Country Link
US (1) US10087781B2 (pt)
EP (1) EP2931606A1 (pt)
CN (1) CN104918855A (pt)
BR (1) BR112015012033A2 (pt)
CA (1) CA2893617A1 (pt)
FR (1) FR2999154B1 (pt)
RU (1) RU2015128021A (pt)
WO (1) WO2014091110A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9915225B2 (en) 2015-02-06 2018-03-13 United Technologies Corporation Propulsion system arrangement for turbofan gas turbine engine
CN107263042B (zh) * 2016-04-08 2023-11-21 中国航发贵州黎阳航空动力有限公司 航空发动机高压压气机装配定心旋转装置
FR3051840B1 (fr) * 2016-05-31 2020-01-10 Safran Aircraft Engines Carter intermediaire de turbomachine, equipee d'une piece d'etancheite a interface bras/virole
FR3085156B1 (fr) * 2018-08-24 2020-09-11 Safran Nacelles Ensemble et procede de manutention d’un ensemble propulsif d’aeronef
FR3085358B1 (fr) * 2018-08-31 2020-09-25 Safran Nacelles Ensemble et procede de manutention d’un ensemble propulsif d’aeronef
FR3090041B1 (fr) * 2018-12-14 2020-11-27 Safran Aircraft Engines Dispositif de resistance au feu ameliore destine a etre interpose entre une extremite de mat d’accrochage de turbomachine d’aeronef, et un capotage de la turbomachine delimitant un compartiment inter-veine
US11414200B2 (en) 2019-04-29 2022-08-16 Rohr, Inc. Fan cowl securement retainers
FR3101616B1 (fr) * 2019-10-03 2021-09-17 Airbus Operations Sas Procédé et dispositif pour l'installation d'une ferrure de positionnement d'un capot de soufflante.
FR3108097B1 (fr) * 2020-03-10 2022-07-29 Safran Aircraft Engines Dispositif de positionnement pour un capot de nacelle d’un ensemble propulsif d’aeronef
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
CN114212276B (zh) * 2021-11-30 2023-08-11 北京卫星制造厂有限公司 一种空间站舱门和一种舱门密封结构的装调方法
EP4257481A1 (en) * 2022-04-05 2023-10-11 Rohr, Inc. Nacelle inlet structure fitting with locator clip and hoist bracket

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE487116A (pt) * 1946-07-16
US5251917A (en) * 1987-06-22 1993-10-12 The Boeing Company Fire-resistant seal
FR2767560B1 (fr) * 1997-08-19 1999-11-12 Aerospatiale Ensemble reducteur de bruit pour turboreacteur d'aeronef
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
FR2891243B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2938237B1 (fr) * 2008-11-13 2011-05-20 Aircelle Sa Nacelle pour turboreacteur a capot amont translatable
US8172176B2 (en) * 2009-02-04 2012-05-08 Spirit Aerosystems, Inc. Integral composite slider for aircrafts

Also Published As

Publication number Publication date
US20150267560A1 (en) 2015-09-24
FR2999154A1 (fr) 2014-06-13
US10087781B2 (en) 2018-10-02
RU2015128021A (ru) 2017-01-18
EP2931606A1 (fr) 2015-10-21
WO2014091110A1 (fr) 2014-06-19
CN104918855A (zh) 2015-09-16
FR2999154B1 (fr) 2014-11-28
CA2893617A1 (fr) 2014-06-19

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law
B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)