BR112014029901A2 - dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma. - Google Patents

dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma.

Info

Publication number
BR112014029901A2
BR112014029901A2 BR112014029901A BR112014029901A BR112014029901A2 BR 112014029901 A2 BR112014029901 A2 BR 112014029901A2 BR 112014029901 A BR112014029901 A BR 112014029901A BR 112014029901 A BR112014029901 A BR 112014029901A BR 112014029901 A2 BR112014029901 A2 BR 112014029901A2
Authority
BR
Brazil
Prior art keywords
mounting
thrust reverser
propulsion assembly
aircraft propulsion
fixed thrust
Prior art date
Application number
BR112014029901A
Other languages
English (en)
Inventor
Duquenoy Florine
Holay 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 BR112014029901A2 publication Critical patent/BR112014029901A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • B64F5/45—Repairing leakages in fuel tanks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/50—Handling or transporting aircraft components
    • 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
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285—Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/74—Reversing at least one flow in relation to at least one other flow in a plural- flow engine
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/68—Assembly methods using auxiliary equipment for lifting or holding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49895—Associating parts by use of aligning means [e.g., use of a drift pin or a "fixture"]
    • Y10T29/49901—Sequentially associating parts on stationary aligning means
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49998—Work holding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/53—Means to assemble or disassemble
    • Y10T29/53087—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer
    • Y10T29/53091—Means to assemble or disassemble with signal, scale, illuminator, or optical viewer for work-holder for assembly or disassembly

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Manufacturing & Machinery (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automatic Assembly (AREA)
BR112014029901A 2012-06-25 2013-06-14 dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma. BR112014029901A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1255990A FR2992292B1 (fr) 2012-06-25 2012-06-25 Dispositif et procede d'assemblage d'une structure fixe d'inverseur de poussee d'un ensemble propulsif d'aeronef
PCT/FR2013/051392 WO2014001685A1 (fr) 2012-06-25 2013-06-14 Dispositif et procédé d'assemblage d'une structure fixe d'inverseur de poussée d'un ensemble propulsif d'aéronef

Publications (1)

Publication Number Publication Date
BR112014029901A2 true BR112014029901A2 (pt) 2017-07-25

Family

ID=46889241

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014029901A BR112014029901A2 (pt) 2012-06-25 2013-06-14 dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma.

Country Status (8)

Country Link
US (1) US9518533B2 (pt)
EP (1) EP2864203A1 (pt)
CN (1) CN104411588B (pt)
BR (1) BR112014029901A2 (pt)
CA (1) CA2874024A1 (pt)
FR (1) FR2992292B1 (pt)
RU (1) RU2015101350A (pt)
WO (1) WO2014001685A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014200760A1 (de) * 2014-01-17 2015-07-23 Siemens Aktiengesellschaft Läuferschwenksystem
WO2015168637A1 (en) * 2014-05-02 2015-11-05 Morey Joel T Aircraft engine stand
CN104354874B (zh) * 2014-08-05 2017-01-18 北京卫星制造厂 一种柔性牵引进行分解复装的单元化结构装配方法
FR3031084B1 (fr) * 2014-12-29 2018-04-27 Safran Nacelles Outillage de support d’une nacelle de moteur d’aeronef
CN107352043B (zh) * 2017-06-26 2019-10-29 大连理工大学 一种用于飞机发动机整机安装的六轴调姿平台
FR3078108B1 (fr) 2018-02-20 2020-01-31 Safran Nacelles Ensemble propulsif comportant des points de levage disposes sur des supports de verins d’inverseur de poussee
FR3085156B1 (fr) * 2018-08-24 2020-09-11 Safran Nacelles Ensemble et procede de manutention d’un ensemble propulsif d’aeronef
CN109764989B (zh) * 2018-11-02 2021-09-03 北京航空航天大学 可自锁定与标定的推力架
FR3098746B1 (fr) 2019-07-17 2021-07-30 Safran Aircraft Engines Outillage et procede de demontage et de deplacement d’un carter de turbine du type trv d’une turbomachine d’aeronef
DE102019218993A1 (de) * 2019-12-05 2021-06-10 MTU Aero Engines AG Trägeranordnung zum aufhängen eines flugtriebwerks oder -moduls zu montage- oder revisionsszwecken

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
DE2719850C3 (de) * 1977-05-04 1981-06-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Vorrichtung zur Wartung von Gasturbinentriebwerken, insbesondere Gasturbinenstrahltriebwerken
US5681033A (en) * 1996-02-01 1997-10-28 Northrop Grumman Corporation Workpiece pick-up jig and positioning tool
FR2936493A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat.
FR2939409B1 (fr) * 2008-12-08 2011-02-11 Airbus France Systeme de fixation entre deux composants tels qu'un moteur d'aeronef et son mat d'accrochage
US9470108B2 (en) * 2010-02-22 2016-10-18 American Airlines, Inc. Thrust reverser cowl rack

Also Published As

Publication number Publication date
US9518533B2 (en) 2016-12-13
FR2992292A1 (fr) 2013-12-27
CA2874024A1 (fr) 2014-01-03
CN104411588B (zh) 2016-03-09
RU2015101350A (ru) 2016-08-10
FR2992292B1 (fr) 2015-02-20
US20150113787A1 (en) 2015-04-30
CN104411588A (zh) 2015-03-11
EP2864203A1 (fr) 2015-04-29
WO2014001685A1 (fr) 2014-01-03

Similar Documents

Publication Publication Date Title
BR112014029901A2 (pt) dispositivo de montagem de uma estrutura fixa de reversor de empuxo de um conjunto de propulsão de aeronave e método para montar a mesma.
BR112013032845A2 (pt) sugestões de texto para imagens
BR112014004264A2 (pt) nacela e montagem traseira da mesma para motor turbojato
BR112013030887A2 (pt) dispositivo de abertura de emergência para uma porta de aeronave.
BR112014008570A2 (pt) reversor de empuxo para uma nacela de um motor turbojato e nacela para uma aeronave turbojato
BR112014009735A2 (pt) aparelho de imagem de raios-x e método para controlar um aparelho de imagem de raios-x
BR112014017430A8 (pt) reversor de empuxo do tipo cascata para um motor turbojato de aeronaves e nacela oara um motor turbojato de aeronaves
BR112014009939A2 (pt) dispositivo de reversão de empuxo para uma nacela de motor turbojato e nacela de um motor turbojato
BR112014028731A2 (pt) reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BR112015012033A2 (pt) dispositivo de centralização, nacela para motor turbojato e conjunto de propulsão para aeronaves
DK2726188T3 (da) Motorsystemer og fremgangsmåder til at drive en motor
BR112014001679A2 (pt) cone de escape para motor turbojato de aeronave
BR112014002212A2 (pt) dispositivo reversor de empuxo de uma nacela e uma nacela de um motor turbo- ventilador
BR112014001529A2 (pt) nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxo
BR112013025586A2 (pt) conjunto obturador para um sistema elétrico e sistema elétrico
BR112015005879A2 (pt) aparelho formador de imagens, e método para realizar uma tarefa de um aparelho formador de imagens.
BR112014000233A2 (pt) sistema de flape para uma aeronave
BR112014013058A2 (pt) método para montar um equipamento de intervenção, e, transportador para levar um aparelho de intervenção entre uma posição inoperativa e uma posição operativa
GB2510635B (en) Method for predicting faults in an aircraft thrust reverser system
BR112014014144A2 (pt) seção termoacústica para uma aeronave para redução do ruído ao longo de um percurso acústico.
BR112014007961A2 (pt) conjunto de propulsão para aeronave e aeronave
BR112015005181A2 (pt) dispositivo reversor de empuxo para uma nacela de motor turbojato e nacela de motor turbojato.
BR112014010136A2 (pt) reversor de empuxo para uma nacela de motor turbojato de aeronave e nacela
BR112014032069A2 (pt) método para extração por solvente e decantador para extração por solvente
BR112013023410A2 (pt) dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]