BR112017004954A2 - processo e dispositivo de montagem de um motor em um pilar de aeronave - Google Patents

processo e dispositivo de montagem de um motor em um pilar de aeronave

Info

Publication number
BR112017004954A2
BR112017004954A2 BR112017004954-6A BR112017004954A BR112017004954A2 BR 112017004954 A2 BR112017004954 A2 BR 112017004954A2 BR 112017004954 A BR112017004954 A BR 112017004954A BR 112017004954 A2 BR112017004954 A2 BR 112017004954A2
Authority
BR
Brazil
Prior art keywords
engine
abutment
pillar
mounting
cradle
Prior art date
Application number
BR112017004954-6A
Other languages
English (en)
Other versions
BR112017004954B1 (pt
Inventor
Lambey Mario
Albert Beutin Bruno
Patrick Tesniere Marc
Original Assignee
Safran Aircraft Engines
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 Safran Aircraft Engines filed Critical Safran Aircraft Engines
Publication of BR112017004954A2 publication Critical patent/BR112017004954A2/pt
Publication of BR112017004954B1 publication Critical patent/BR112017004954B1/pt

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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • 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
    • 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
    • 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
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Prevention Devices (AREA)
  • Motor Or Generator Frames (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Testing Of Balance (AREA)
  • Body Structure For Vehicles (AREA)
  • Automatic Assembly (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)

Abstract

a invenção tem como objeto um processo de montagem de um motor (1) em um pilar (3) de aeronave que compreende órgãos (31) de suspensão do motor solidários do pilar, o motor sendo solidário de um berço (6) de suspensão pelo qual ele é suspenso ao pilar, o processo compreendendo uma etapa de içamento do motor de acordo com uma direção vertical até o pilar e depois uma etapa de acostamento do pilar por um deslocamento do motor de acordo com uma outra direção, caracterizado pelo fato de que é fixada previamente ao pilar, prendendo-se a mesma aos ditos órgãos (31) de suspensão, uma peça intermediária (7) que apresenta uma interface destinada a operar junto com uma interface complementar prevista no berço (6) de modo a posicionar o berço em relação à peça intermediária no final do acostamento do pilar. a invenção tem também como objeto o dispositivo de execução do processo.
BR112017004954-6A 2014-09-16 2015-09-16 Processo e dispositivo de montagem de um motor em um pilar de aeronave BR112017004954B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1458756 2014-09-16
FR1458756A FR3025782B1 (fr) 2014-09-16 2014-09-16 Procede et dispositif de montage d'un moteur sur un pylone d'aeronef
PCT/FR2015/052478 WO2016042264A1 (fr) 2014-09-16 2015-09-16 Procede et dispositif de montage d'un moteur sur un pylone d'aeronef

Publications (2)

Publication Number Publication Date
BR112017004954A2 true BR112017004954A2 (pt) 2018-04-10
BR112017004954B1 BR112017004954B1 (pt) 2022-08-30

Family

ID=51842616

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017004954-6A BR112017004954B1 (pt) 2014-09-16 2015-09-16 Processo e dispositivo de montagem de um motor em um pilar de aeronave

Country Status (8)

Country Link
US (1) US10486819B2 (pt)
EP (1) EP3194272B1 (pt)
CN (1) CN107074370B (pt)
BR (1) BR112017004954B1 (pt)
CA (1) CA2960869C (pt)
FR (1) FR3025782B1 (pt)
RU (1) RU2690834C2 (pt)
WO (1) WO2016042264A1 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9868539B2 (en) * 2015-09-24 2018-01-16 Embraer S.A. Aircraft engine pylon to wing mounting assembly
US10144525B2 (en) * 2015-09-24 2018-12-04 Embraer S.A. Aircraft engine pylon to wing mounting assembly
FR3061148B1 (fr) * 2016-12-23 2022-08-12 Airbus Operations Sas Fixation semi-continue d'un mat d'accrochage de moteur a un dispositif de fixation appartenant a la voilure d'un aeronef
DE102017129060A1 (de) * 2017-12-06 2019-06-06 Rolls-Royce Deutschland Ltd & Co Kg Integrierte Tragstruktur für ein Flugzeugtriebwerk und dessen Zubehörkomponenten
FR3090588B1 (fr) * 2018-12-21 2021-01-22 Safran Aircraft Engines Outillage pour placer un ensemble propulsif d’une position horizontale a une position verticale
CN110844090B (zh) * 2019-10-11 2022-11-22 中国直升机设计研究所 一种直升机活塞发动机的托起式安装装置
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU1637186C (ru) * 1989-10-05 1995-01-20 Авиационный комплекс им.С.В.Ильюшина Пилон подвески двигателя на стреловидном крыле летательного аппарата
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
FR2755944B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
RU63320U1 (ru) * 2006-12-28 2007-05-27 Закрытое акционерное общество "Гражданские самолеты Сухого" Пилон подвески двигателя к крылу
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
FR2920408B1 (fr) * 2007-08-30 2010-02-19 Snecma Pylone de suspension d'un moteur sous une aile d'avion
FR2950323B1 (fr) * 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2974065B1 (fr) * 2011-04-14 2013-05-10 Snecma Procede de montage d'un moteur d'aeronef sur un pylone et attache moteur pour la mise en oeuvre d'un tel procede.

Also Published As

Publication number Publication date
US20170259928A1 (en) 2017-09-14
CN107074370B (zh) 2020-02-21
FR3025782B1 (fr) 2016-09-30
RU2017109393A3 (pt) 2019-04-18
EP3194272B1 (fr) 2018-10-31
CA2960869A1 (fr) 2016-03-24
CN107074370A (zh) 2017-08-18
CA2960869C (fr) 2022-10-25
RU2690834C2 (ru) 2019-06-05
EP3194272A1 (fr) 2017-07-26
FR3025782A1 (fr) 2016-03-18
WO2016042264A1 (fr) 2016-03-24
BR112017004954B1 (pt) 2022-08-30
US10486819B2 (en) 2019-11-26
RU2017109393A (ru) 2018-10-17

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Legal Events

Date Code Title Description
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 16/09/2015, OBSERVADAS AS CONDICOES LEGAIS