Nothing Special   »   [go: up one dir, main page]

BR112014026280A2 - nacela de motor turbojato possuidora de uma seção a jusante compreendendo pelo menos uma estrutura frontal - Google Patents

nacela de motor turbojato possuidora de uma seção a jusante compreendendo pelo menos uma estrutura frontal

Info

Publication number
BR112014026280A2
BR112014026280A2 BR112014026280A BR112014026280A BR112014026280A2 BR 112014026280 A2 BR112014026280 A2 BR 112014026280A2 BR 112014026280 A BR112014026280 A BR 112014026280A BR 112014026280 A BR112014026280 A BR 112014026280A BR 112014026280 A2 BR112014026280 A2 BR 112014026280A2
Authority
BR
Brazil
Prior art keywords
front frame
engine compartment
turbojet engine
downstream section
downstream
Prior art date
Application number
BR112014026280A
Other languages
English (en)
Inventor
Kioua Hazem
Georges Valleroy Laurent
Peyron Vincent
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 BR112014026280A2 publication Critical patent/BR112014026280A2/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
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
BR112014026280A 2012-04-27 2013-04-26 nacela de motor turbojato possuidora de uma seção a jusante compreendendo pelo menos uma estrutura frontal BR112014026280A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1253902A FR2989952B1 (fr) 2012-04-27 2012-04-27 Nacelle de turboreacteur a section aval
PCT/FR2013/050938 WO2013160627A1 (fr) 2012-04-27 2013-04-26 Nacelle de turboréacteur à section aval

Publications (1)

Publication Number Publication Date
BR112014026280A2 true BR112014026280A2 (pt) 2017-06-27

Family

ID=48468650

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014026280A BR112014026280A2 (pt) 2012-04-27 2013-04-26 nacela de motor turbojato possuidora de uma seção a jusante compreendendo pelo menos uma estrutura frontal

Country Status (8)

Country Link
US (1) US9341083B2 (pt)
EP (1) EP2841340B1 (pt)
CN (1) CN104254481B (pt)
BR (1) BR112014026280A2 (pt)
CA (1) CA2869924A1 (pt)
FR (1) FR2989952B1 (pt)
RU (1) RU2626416C9 (pt)
WO (1) WO2013160627A1 (pt)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3031728B1 (fr) * 2015-01-21 2017-04-28 Aircelle Sa Dispositif d’inversion de poussee a grilles mobiles et berceau
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
CN114291275A (zh) * 2021-12-20 2022-04-08 航天神舟飞行器有限公司 一种无人机发动机热管理软连接装置

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2496766A1 (fr) * 1980-12-23 1982-06-25 Snecma Dispositif de guidage de carenage mobile d'un systeme d'inversion de poussee
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
SU1776000A1 (ru) * 1990-01-30 2002-02-20 Авиационный научно-технический комплекс им. А.Н.Туполева Устройство для управления тягой двигателя летательного аппарата
SU1826436A1 (ru) * 1990-12-25 1995-03-27 Авиационный научно-технический комплекс им.А.Н.Туполева Силовая установка самолета
FR2676707B1 (fr) * 1991-05-23 1993-08-13 Snecma Nacelle pour suspendre sous l'aile d'un avion un groupe turboreacteur du type a double flux.
FR2755942B1 (fr) 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
FR2855494B1 (fr) 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2892706B1 (fr) 2005-10-31 2009-04-24 Airbus France Sas Dispositif d'attache avant d'un turboreacteur a un mat de fixation d'un aeronef
FR2900906B1 (fr) * 2006-05-09 2009-01-09 Airbus France Sas Systeme de fixation tolerant aux dommages pour moteur d'aeronef
FR2901244B1 (fr) * 2006-05-16 2009-01-09 Airbus France Sas Dispositif d'articulation de portes d'une nacelle d'aeronef et nacelle equipee dudit dispositif d'articulation
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
FR2916426B1 (fr) 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.
GB0902909D0 (en) 2009-02-23 2009-04-08 Rolls Royce Plc A thrust mount arrangement for an aircraft engine
US8713910B2 (en) * 2009-07-31 2014-05-06 General Electric Company Integrated thrust reverser/pylon assembly
FR2948635B1 (fr) 2009-07-31 2011-08-26 Airbus Operations Sas Assemblage pour aeronef comprenant un mat d'accrochage de turbomachine dont les moyens d'attache sur la voilure sont agences en t
FR2948636B1 (fr) 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
US8511973B2 (en) * 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly

Also Published As

Publication number Publication date
FR2989952B1 (fr) 2014-04-18
RU2626416C2 (ru) 2017-07-27
CA2869924A1 (fr) 2013-10-31
EP2841340B1 (fr) 2016-04-13
US9341083B2 (en) 2016-05-17
EP2841340A1 (fr) 2015-03-04
FR2989952A1 (fr) 2013-11-01
WO2013160627A1 (fr) 2013-10-31
RU2626416C9 (ru) 2017-09-22
RU2014146921A (ru) 2016-06-20
CN104254481A (zh) 2014-12-31
US20150300204A1 (en) 2015-10-22
CN104254481B (zh) 2015-11-25

Similar Documents

Publication Publication Date Title
DE112013003765A5 (de) Aktuierungseinheit für variable Triebwerkskomponenten
BR112014013740A2 (pt) conjunto de troca de motor rápida
EP2880281A4 (en) FRONT COMPARTMENT DEFLECTOR ARRANGEMENT FOR A DOUBLE GEAR FLOW ENGINE
BR112013030915A2 (pt) estrutura traseira de um veículo.
EP3008323A4 (en) Turbofan engine front section
EP2639142A4 (en) FRONT COVER STRUCTURE FOR ONE VEHICLE
EP2738047A4 (en) CONSTRUCTION OF A VEHICLE FRONT
EP2679471A4 (en) CONSTRUCTION OF A BONNET PART
BR302013003578S1 (pt) Configuração aplicada em tampa frontal para motor de combustão.
BR112013023410A2 (pt) dispositivo de travamento e nacela de motor turbojato compreendendo pelo menos uma carenagem movente
BR112013010654A2 (pt) nacela de motor turbojato compreendendo uma estrutura fixa
GB2490706B (en) Engine diagnostic delay provision
BR112014029898A2 (pt) conjunto para um motor turbojato, compreendendo uma estrutura de montagem e uma nacela sustentada por dita estrutura de montagem.
GB2520823B (en) Front module of a motor vehicle
BR112014026280A2 (pt) nacela de motor turbojato possuidora de uma seção a jusante compreendendo pelo menos uma estrutura frontal
BR112015016839A2 (pt) obturador, e, disposição de compartimento de motor de veículo automotivo
BR112014001981A2 (pt) módulo de extremidade frontal de veículo, particularmente veículo motorizado
BR112014014474A2 (pt) veículo automotivo compreendendo um capô dianteiro
BR112015003926A2 (pt) conjunto para suportar uma armação frontal de um reversor de empuxo para uma carcaça de motor turbojato e conjunto de propulsão compreendendo um motor turbojato.
BR112014001982A2 (pt) módulo de face frontal de veículo automotivo
BR112015011725A2 (pt) disposição de uma face exterior dianteira de um veículo automotivo, e, veículo automotivo.
BR112014007202A2 (pt) unidade de compressor de motor
BR112014030131A2 (pt) veículo automotivo compreendendo uma armação de carroceria
CO7061048A2 (es) Estructura frontal para vehículo de montar horcajadas
FR2983278B1 (fr) Eclairage frontal de vehicule

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 4A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]