JP6758189B2 - エンジンパイロン構造 - Google Patents

エンジンパイロン構造 Download PDF

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Publication number
JP6758189B2
JP6758189B2 JP2016553812A JP2016553812A JP6758189B2 JP 6758189 B2 JP6758189 B2 JP 6758189B2 JP 2016553812 A JP2016553812 A JP 2016553812A JP 2016553812 A JP2016553812 A JP 2016553812A JP 6758189 B2 JP6758189 B2 JP 6758189B2
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JP
Japan
Prior art keywords
engine
torque box
mount
pylon structure
wing
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
JP2016553812A
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English (en)
Japanese (ja)
Other versions
JP2017508658A (ja
JP2017508658A5 (cg-RX-API-DMAC7.html
Inventor
ウォーリー，アレン・マドセン
クレッグ，ブライアン・ケルビー
ジャスト，マイケル・スコット
パテル，ラメシュチャンドラ・ダーヤバイ
Original Assignee
エムアールエイ・システムズ・エルエルシー
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Publication of JP2017508658A publication Critical patent/JP2017508658A/ja
Publication of JP2017508658A5 publication Critical patent/JP2017508658A5/ja
Application granted granted Critical
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Active legal-status Critical Current
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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 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Prevention Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
JP2016553812A 2014-03-04 2015-02-24 エンジンパイロン構造 Active JP6758189B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US14/196,570 US9238511B2 (en) 2014-03-04 2014-03-04 Engine pylon structure
US14/196,570 2014-03-04
PCT/US2015/017267 WO2015134234A1 (en) 2014-03-04 2015-02-24 Engine pylon structure

Publications (3)

Publication Number Publication Date
JP2017508658A JP2017508658A (ja) 2017-03-30
JP2017508658A5 JP2017508658A5 (cg-RX-API-DMAC7.html) 2018-03-29
JP6758189B2 true JP6758189B2 (ja) 2020-09-23

Family

ID=52596645

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016553812A Active JP6758189B2 (ja) 2014-03-04 2015-02-24 エンジンパイロン構造

Country Status (6)

Country Link
US (1) US9238511B2 (cg-RX-API-DMAC7.html)
EP (1) EP3114030B1 (cg-RX-API-DMAC7.html)
JP (1) JP6758189B2 (cg-RX-API-DMAC7.html)
CN (1) CN106061841B (cg-RX-API-DMAC7.html)
CA (1) CA2940748A1 (cg-RX-API-DMAC7.html)
WO (1) WO2015134234A1 (cg-RX-API-DMAC7.html)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201204231D0 (en) * 2012-03-09 2012-04-25 Airbus Uk Ltd Space frame structure
FR3013678B1 (fr) * 2013-11-25 2015-11-20 Airbus Operations Sas Carenage aerodynamique
FR3016344B1 (fr) * 2014-01-10 2017-09-01 Snecma Structure de suspension d'un turbopropulseur a double helices non carenees sur un element structurel d'un aeronef a fixation rigide de la structure d'entree d'air
FR3020798B1 (fr) * 2014-05-09 2017-12-22 Airbus Operations Sas Ensemble propulsif pour aeronef comprenant un conduit formant barriere thermique integre au caisson de la structure rigide du mat d'accrochage
FR3042475B1 (fr) * 2015-10-16 2018-07-13 Airbus Operations (S.A.S.) Mat porteur de moteur d'aeronef
US9896217B2 (en) * 2016-01-07 2018-02-20 The Boeing Company Enhanced performance jet engine mounting struts
FR3054202B1 (fr) 2016-07-25 2018-07-13 Safran Aircraft Engines Berceau pour turbopropulseur a manche d'entree d'air integree
FR3058704B1 (fr) * 2016-11-14 2018-11-16 Safran Aircraft Engines Berceau bipartite a coulissement pour turbopropulseur
US10604265B2 (en) * 2016-11-15 2020-03-31 The Boeing Company Integrated strut support fittings with underwing longerons
FR3061147B1 (fr) * 2016-12-26 2019-05-31 Safran Aircraft Engines Turbopropulseur d'aeronef de type a arbre deporte comportant des moyens de suspension a un pylone d'aeronef
FR3061149B1 (fr) * 2016-12-27 2023-11-03 Airbus Operations Sas Structure primaire d'un mat pour groupe propulseur d'aeronef comportant une partie pyramidale a montants convergents
US10414509B2 (en) * 2017-02-23 2019-09-17 United Technologies Corporation Propulsor mounting for advanced body aircraft
US10899463B2 (en) * 2017-05-16 2021-01-26 Rohr, Inc. Segmented pylon for an aircraft propulsion system
US10583930B2 (en) * 2017-06-02 2020-03-10 Spirit Aerosystems, Inc. Aircraft engine attachment assembly
FR3072364A1 (fr) * 2017-10-18 2019-04-19 Airbus Operations Procede d'assemblage d'une structure primaire d'un mat d'aeronef et structure primaire d'un mat d'aeronef ainsi obtenue
EP3473548B1 (fr) 2017-10-18 2019-12-04 Airbus Operations S.A.S. Procede d'assemblage d'une structure primaire d'un mât d'aeronef
FR3072945B1 (fr) * 2017-10-27 2020-11-20 Airbus Operations Sas Structure primaire de mat de support d'un groupe propulseur d'aeronef comportant une partie inferieure en u obtenue de maniere monobloc ou par soudage
FR3078950B1 (fr) * 2018-03-15 2020-12-18 Airbus Operations Sas Structure primaire d'un mat de support d'un groupe propulseur d'aeronef dont la partie arriere est formee par un ensemble de bielles
FR3079215B1 (fr) * 2018-03-22 2020-11-20 Airbus Operations Sas Carenage avant d'un mat d'aeronef comprenant une coiffe mobile et aeronef equipe dudit carenage avant
FR3085351B1 (fr) * 2018-09-04 2021-12-31 Airbus Operations Sas Carenage central d'un mat d'aeronef comprenant au moins un panneau articule et aeronef equipe dudit carenage central
EP3647538A1 (en) 2018-10-30 2020-05-06 Siemens Aktiengesellschaft Safety apparatus for containing an energy release from a rotor assembly
CN109455304B (zh) * 2018-11-30 2024-02-23 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞机静不定吊挂结构
US11635024B2 (en) 2019-08-16 2023-04-25 Pratt & Whitney Canada Corp. Pusher turboprop powerplant installation
FR3102151B1 (fr) * 2019-10-21 2021-10-29 Airbus Operations Sas Aéronef comprenant une attache voilure arrière présentant au moins deux bielles latérales et un pion de cisaillement
US11674414B2 (en) * 2021-03-19 2023-06-13 Pratt & Whitney Canada Corp. Gas turbine engine and mount assembly therefor
FR3122644B1 (fr) * 2021-05-04 2023-06-16 Airbus Operations Sas Assemblage d’une structure primaire d’un mât d’aéronef et d’une attache-moteur arrière comprenant au moins un élément de fixation latéral et aéronef comprenant au moins un tel assemblage
US12377993B2 (en) 2022-04-15 2025-08-05 The Boeing Company Engine attachment system for aircraft and method for attaching an engine
FR3135450A1 (fr) * 2022-05-12 2023-11-17 Airbus Operations (S.A.S.) Assemblage d’un mât réacteur avec une aile d’un aeronef.
US12415610B2 (en) * 2022-05-13 2025-09-16 The Boeing Company Strut assembly and method for coupling an engine to a wing of an aircraft
US12337976B2 (en) 2022-11-02 2025-06-24 The Boeing Company Systems and methods for coupling a strut to a wing of an aircraft
FR3141676A1 (fr) * 2022-11-08 2024-05-10 Airbus Operations Ensemble pour un aéronef comportant une aile et un mât réacteur pour coupler un système de propulsion à ladite aile
FR3148995A1 (fr) * 2023-05-23 2024-11-29 Airbus Operations Ensemble pour un aéronef comportant une aile et un mât réacteur pour coupler un système de propulsion à ladite aile

Family Cites Families (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
US3948469A (en) * 1974-11-25 1976-04-06 The Boeing Company Engine mounting and boundary layer control fluid supply apparatus
US4531694A (en) 1982-10-18 1985-07-30 Soloy Conversions, Ltd. Turbine engine drive and mounting assembly for fixed wing aircraft
US5064144A (en) 1987-05-19 1991-11-12 The Boeing Company Engine mounting assembly
US5467941A (en) 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
FR2738034B1 (fr) 1995-08-23 1997-09-19 Snecma Dispositif de suspension d'un turbopropulseur
US5918833A (en) 1997-01-16 1999-07-06 Applied Power Inc. Hydraulic torque restraint system
US6126110A (en) 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
GB2375513B (en) 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US6517027B1 (en) * 2001-12-03 2003-02-11 Pratt & Whitney Canada Corp. Flexible/fixed support for engine cowl
US6607165B1 (en) 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
FR2851226B1 (fr) 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
FR2862612B1 (fr) 2003-11-25 2006-02-17 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2862610B1 (fr) 2003-11-25 2007-03-23 Airbus France Dispositif d'accrochage reliant un moteur et une voilure d'aeronef
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2862945B1 (fr) * 2003-12-01 2006-04-28 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef.
FR2867157B1 (fr) 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867158B1 (fr) 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867156B1 (fr) 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method
FR2873987B1 (fr) 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
FR2878229B1 (fr) * 2004-11-23 2008-04-18 Airbus France Sas Systeme de fixation d'un mat de moteur a l'aile d'un aeronef
FR2883256B1 (fr) 2005-03-18 2008-10-24 Airbus France Sas Attache moteur d'un systeme de montage interpose entre un mat d'accrochage et un moteur d'aeronef
FR2885877B1 (fr) 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef
FR2891250B1 (fr) 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891252B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Mat a ossature monolithique
FR2891803B1 (fr) * 2005-10-07 2007-11-30 Airbus France Sas Structure rigide pour mat d'accrochage de moteur d'aeronef, et mat comportant une telle structure
DE102006027707A1 (de) * 2006-06-14 2007-12-20 Airbus Deutschland Gmbh Heckstruktur für ein Luft- oder Raumfahrzeug
FR2905932B1 (fr) 2006-09-20 2008-12-05 Airbus France Sa Agencement pour attache de dispositif d'accrochage d'un moteur d'aeronef
FR2909973B1 (fr) 2006-12-13 2009-03-20 Airbus France Sa Mat d'accrochage de turboreacteur pour aeronef a structure arriere de largeur transversale reduite
FR2915177B1 (fr) 2007-04-20 2009-07-10 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
FR2915175B1 (fr) 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
FR2915176B1 (fr) 2007-04-20 2009-07-10 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet
FR2915178B1 (fr) 2007-04-23 2009-07-10 Airbus France Sa Attache d'un caisson de mat sur une voilure, pincant un panneau lateral du caisson
FR2916736B1 (fr) 2007-06-04 2009-09-04 Airbus France Sa Dispositif d'accrochage d'un turbopropulseur d'aeronef comprenant des moyens de fixation hydrauliques.
FR2917712B1 (fr) 2007-06-20 2009-09-25 Airbus France Sas Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere formant palonnier.
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
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
FR2939101B1 (fr) * 2008-12-01 2010-12-31 Airbus France Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation
US8353476B2 (en) * 2009-11-23 2013-01-15 Spirit Aerosystems, Inc. Truss-shaped engine pylon and method of making same
JP5642379B2 (ja) * 2009-12-01 2014-12-17 三菱航空機株式会社 航空機のエンジンマウント、航空機
US8672260B2 (en) * 2009-12-02 2014-03-18 United Technologies Corporation Single plane mount system for gas turbine engine
FR2955311B1 (fr) 2010-01-15 2012-03-23 Airbus Operations Sas Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef
US9027875B2 (en) * 2010-10-28 2015-05-12 Spirit Aerosystems, Inc. Pylon arrangement for open structure
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.
EP2631180B1 (en) * 2012-02-27 2014-04-02 Airbus Operations (S.A.S.) An engine attachment pylon
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft

Also Published As

Publication number Publication date
JP2017508658A (ja) 2017-03-30
US9238511B2 (en) 2016-01-19
EP3114030A1 (en) 2017-01-11
WO2015134234A1 (en) 2015-09-11
EP3114030B1 (en) 2023-09-13
CN106061841A (zh) 2016-10-26
US20150251768A1 (en) 2015-09-10
CN106061841B (zh) 2018-05-15
CA2940748A1 (en) 2015-09-11

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