JP2009509841A - 二重シャックル式航空機用エンジン後部アタッチメント - Google Patents
二重シャックル式航空機用エンジン後部アタッチメント Download PDFInfo
- Publication number
- JP2009509841A JP2009509841A JP2008532760A JP2008532760A JP2009509841A JP 2009509841 A JP2009509841 A JP 2009509841A JP 2008532760 A JP2008532760 A JP 2008532760A JP 2008532760 A JP2008532760 A JP 2008532760A JP 2009509841 A JP2009509841 A JP 2009509841A
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- JP
- Japan
- Prior art keywords
- engine
- attachment
- shackle
- holes
- shackles
- 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.)
- Granted
Links
- 230000033001 locomotion Effects 0.000 description 6
- 238000005096 rolling process Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Images
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
- B64D27/40—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
- B64D27/402—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
- 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
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
-
- 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
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pivots And Pivotal Connections (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
- Vehicle Body Suspensions (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Automatic Cycles, And Cycles In General (AREA)
Abstract
Description
6 エンジンマウント
10 アタッチメント
12,12' シャックル(ブラケット)
14 ビーム
16 クレビス
16a,16b ブランチ
18 ピン
20 リンクピン
20a,20b 円筒形層
22,24 孔
24' 第2の孔
26,26' 第3の孔
28 ボールジョイント
30 ピン
Claims (11)
- エンジン(3)と、当該エンジン用のマウント(6)との間に配置される航空機用エンジンアタッチメント(10)であって、
前記エンジンマウント(6)に対して取り付けられ、かつそれぞれが四つの対向するアンカー孔を有する二つのブランチ(16a,16b)を備えた第1の取り付けデバイス(14)と、
それぞれ三つの孔を具備してなる二つのシャックル(12,12')であって、各シャックル(12)の前記孔の二つ(22,24)は、そのアンカー孔を介して前記第1の取り付けデバイス(14)に対してリンクピン(18)によって連結されるようになっており、かつ前記第3の孔(26)はエンジンクレビスに取り付けられるようになっている二つのシャックル(12,12')と、を具備し、
各シャックル(12,12')は、前記孔(22,24,26)に対して直交する方向に互いに隣接する、同一形状の二つの部分(12a,12b)からなる二重構造を有するものであることを特徴とする航空機用エンジンアタッチメント(10)。 - 前記第1のデバイス(14)の各ブランチ(16a,16b)は孔を四つだけ有することを特徴とする請求項1に記載のアタッチメント。
- 前記第1のデバイス(14)の各ブランチ(16a,16b)の前記四つの孔は整列状態となっていることを特徴とする請求項1または請求項2に記載のアタッチメント。
- 各シャックルの前記三つの孔(22,24,26)によって形成された前記三角形は二等辺三角形であることを特徴とする請求項1ないし請求項3のいずれか1項に記載のアタッチメント。
- 前記第1のデバイス(14)の前記ブランチ(16a,16b)間に前記二つのシャックル(12,12')を取り付ける四つのリンクピン(18)をさらに具備してなることを特徴とする請求項1ないし請求項4のいずれか1項に記載のアタッチメント。
- 前記第3の孔(26)と協働するリンクピン(20,30)をさらに具備してなることを特徴とする請求項1ないし請求項5のいずれか1項に記載のアタッチメント。
- 前記第3の孔(26)と協働する前記リンクピン(20)は、二つの同軸部(20a,20b)を具備してなる二重構造を有することを特徴とする請求項6に記載のアタッチメント。
- 二重構造の前記リンクピン(30)は、前記二つの部分(30a,30b)間に半径方向のクリアランスを有することを特徴とする請求項7に記載のアタッチメント。
- 前記リンクピン(18,20,30)は球面結合されていることを特徴とする請求項5ないし請求項8のいずれか1項に記載のアタッチメント。
- エンジンマウント(6)を具備してなる航空機用のエンジンアセンブリであって、エンジン(3)は、請求項5ないし請求項9のいずれか1項に記載の後部アタッチメント(10)によって、前記マウント(6)に対して取り付けられていることを特徴とするエンジンアセンブリ。
- 前記後部アタッチメント(10)は、二重クレビスを介して、前記エンジン(3)に対して取り付けられていることを特徴とする請求項10に記載にエンジンアセンブリ。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR05/52935 | 2005-09-28 | ||
FR0552935A FR2891253B1 (fr) | 2005-09-28 | 2005-09-28 | Attache arriere d'un moteur d'aeronef a deux manilles |
PCT/EP2006/066728 WO2007036515A1 (fr) | 2005-09-28 | 2006-09-26 | Attache arrière d'un moteur d'aéronef à deux manilles |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009509841A true JP2009509841A (ja) | 2009-03-12 |
JP5032485B2 JP5032485B2 (ja) | 2012-09-26 |
Family
ID=36463524
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008532760A Expired - Fee Related JP5032485B2 (ja) | 2005-09-28 | 2006-09-26 | 二重シャックル式航空機用エンジン後部アタッチメント |
Country Status (9)
Country | Link |
---|---|
US (1) | US7909302B2 (ja) |
EP (1) | EP1929140B1 (ja) |
JP (1) | JP5032485B2 (ja) |
CN (1) | CN101273191B (ja) |
BR (1) | BRPI0616194A2 (ja) |
CA (1) | CA2623999C (ja) |
FR (1) | FR2891253B1 (ja) |
RU (1) | RU2435968C2 (ja) |
WO (1) | WO2007036515A1 (ja) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
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WO2008150202A1 (en) * | 2007-06-08 | 2008-12-11 | Volvo Aero Corporation | A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure |
US8905368B2 (en) * | 2010-06-14 | 2014-12-09 | Lord Corporation | Helicopter engine mounting system and methods |
US20130074517A1 (en) * | 2011-09-23 | 2013-03-28 | United Technologies Corporation | Gas turbine engine mount assembly |
US9016623B2 (en) * | 2011-11-30 | 2015-04-28 | The Boeing Company | Jam protection and alleviation for control surface linkage mechanisms |
US9217337B2 (en) | 2012-05-10 | 2015-12-22 | United Technologies Corporation | Adjustable engine mount |
FR3000529B1 (fr) * | 2012-12-28 | 2015-03-06 | Airbus Operations Sas | Dispositif de liaison souple pour ensemble propulsif d'aeronef |
FR3000467A1 (fr) * | 2012-12-28 | 2014-07-04 | Airbus Operations Sas | Manille a trois points a capacite de filtrage de vibrations et attache moteur d'aeronef equipee d'une telle manille |
JP6137846B2 (ja) * | 2013-01-25 | 2017-05-31 | 三菱航空機株式会社 | パイロンと翼を連結するリンク部材、航空機のパイロンおよび航空機 |
CN103101628B (zh) * | 2013-02-06 | 2015-05-27 | 中国商用飞机有限责任公司 | 一种与飞机吊挂一体化的前安装节 |
US10220950B2 (en) * | 2013-03-15 | 2019-03-05 | United Technologies Corporation | Engine mount waiting fail safe lug joint with reduced dynamic amplification factor |
FR3003896B1 (fr) * | 2013-03-29 | 2015-03-20 | Snecma | Dispositif d'articulation a rotule pour la suspension d'une turbomachine a un pylone ou la suspension d'un equipement au corps de la turbomachine |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
GB201315968D0 (en) * | 2013-09-09 | 2013-10-23 | Rolls Royce Plc | Aircraft engine mount |
CN110182373B (zh) * | 2015-01-07 | 2023-01-10 | 洛德公司 | 用于飞行器发动机安装架的轴承组件 |
US10144525B2 (en) * | 2015-09-24 | 2018-12-04 | Embraer S.A. | Aircraft engine pylon to wing mounting assembly |
FR3049582B1 (fr) * | 2016-03-31 | 2023-01-13 | Snecma | Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur |
FR3058388B1 (fr) * | 2016-11-04 | 2019-05-10 | Airbus Operations | Attache arriere d'un moteur d'aeronef |
FR3058986B1 (fr) * | 2016-11-21 | 2021-04-16 | Airbus Operations Sas | Attache arriere d'un moteur d'aeronef comportant des temoins de rupture |
US10577976B2 (en) * | 2017-10-30 | 2020-03-03 | United Technologies Corporation | Mounting assembly with rotatable and/or translatable retainer pins |
EP3663206B1 (en) | 2018-12-06 | 2023-09-06 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An attachment for suspending an aircraft engine |
FR3103465A1 (fr) | 2019-11-27 | 2021-05-28 | Airbus Operations | Systeme d’attache moteur avant pour un moteur d’aeronef qui comporte une structure allegee |
US11760498B2 (en) | 2020-12-19 | 2023-09-19 | Rohr, Inc. | Engine mount waiting fail safe detection |
FR3126695A1 (fr) * | 2021-09-03 | 2023-03-10 | Airbus Operations | Système d’attache moteur avant pour un moteur d’aéronef qui comporte une structure compacte |
US11884410B2 (en) | 2022-02-04 | 2024-01-30 | General Electric Company | Dual function links for gas turbine engine mounts |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US4786202A (en) * | 1985-02-12 | 1988-11-22 | The United States Of America As Represented By The Secretary Of The Air Force | Dual load path pin clevis joint |
US20030002533A1 (en) * | 2000-02-03 | 2003-01-02 | Doron Rajwan | Coding method |
US20030025033A1 (en) * | 2001-07-31 | 2003-02-06 | Stephane Levert | Device for the attachment of an engine to an aircraft |
JP2004352233A (ja) * | 2003-05-27 | 2004-12-16 | Snecma Moteurs | 航空機エンジン用前部締結装置 |
EP1535838A1 (fr) * | 2003-11-25 | 2005-06-01 | AIRBUS France | Disporstif d'accrochage d'un moteur sous une voilure d'aéronef |
Family Cites Families (17)
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FR2635751B1 (fr) * | 1988-09-01 | 1991-01-04 | Snecma | Dispositif de fixation d'une biellette de suspension d'un turboreacteur |
US5320307A (en) * | 1992-03-25 | 1994-06-14 | General Electric Company | Aircraft engine thrust mount |
US5351930A (en) * | 1992-08-11 | 1994-10-04 | Lord Corporation | Mounting for engines and the like |
US5620154A (en) * | 1995-05-03 | 1997-04-15 | The Boeing Company | Three link failsafe engine mount |
FR2770486B1 (fr) * | 1997-11-06 | 2000-01-28 | Aerospatiale | Dispositif d'accrochage d'un moteur sur un aeronef |
FR2774358B1 (fr) * | 1998-02-04 | 2000-04-21 | Aerospatiale | Dispositif d'accrochage d'un moteur d'aeronef |
US6309131B1 (en) * | 1998-10-29 | 2001-10-30 | General Electric Company | Redundant clevis pin pair |
US6189830B1 (en) * | 1999-02-26 | 2001-02-20 | The Boeing Company | Tuned engine mounting system for jet aircraft |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
FR2820402B1 (fr) * | 2001-02-08 | 2003-05-02 | Eads Airbus Sa | Dispositif d'accrochage d'un moteur sur un aeronef |
FR2855496B1 (fr) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | Suspension arriere de moteur d'avion avec reprise de poussee |
FR2855494B1 (fr) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | Dispositif d'accrocharge arriere de moteur d'avion |
FR2856656B1 (fr) * | 2003-06-30 | 2006-12-01 | Snecma Moteurs | Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang |
FR2862612B1 (fr) * | 2003-11-25 | 2006-02-17 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
US6843449B1 (en) * | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
FR2867155B1 (fr) * | 2004-03-08 | 2007-06-29 | Snecma Moteurs | Suspension d'un moteur a la structure d'un avion |
FR2894934B1 (fr) | 2005-12-15 | 2009-11-13 | Airbus France | Attache arriere d'un moteur d'aeronef avec manille en attente et ressort pour un tel axe en attente |
-
2005
- 2005-09-28 FR FR0552935A patent/FR2891253B1/fr not_active Expired - Fee Related
-
2006
- 2006-09-26 BR BRPI0616194-4A patent/BRPI0616194A2/pt active Search and Examination
- 2006-09-26 CN CN2006800357775A patent/CN101273191B/zh not_active Expired - Fee Related
- 2006-09-26 RU RU2008116733/06A patent/RU2435968C2/ru not_active IP Right Cessation
- 2006-09-26 EP EP06793823A patent/EP1929140B1/fr active Active
- 2006-09-26 WO PCT/EP2006/066728 patent/WO2007036515A1/fr active Application Filing
- 2006-09-26 JP JP2008532760A patent/JP5032485B2/ja not_active Expired - Fee Related
- 2006-09-26 US US12/067,298 patent/US7909302B2/en not_active Expired - Fee Related
- 2006-09-26 CA CA2623999A patent/CA2623999C/fr not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4786202A (en) * | 1985-02-12 | 1988-11-22 | The United States Of America As Represented By The Secretary Of The Air Force | Dual load path pin clevis joint |
US20030002533A1 (en) * | 2000-02-03 | 2003-01-02 | Doron Rajwan | Coding method |
US20030025033A1 (en) * | 2001-07-31 | 2003-02-06 | Stephane Levert | Device for the attachment of an engine to an aircraft |
JP2004352233A (ja) * | 2003-05-27 | 2004-12-16 | Snecma Moteurs | 航空機エンジン用前部締結装置 |
EP1535838A1 (fr) * | 2003-11-25 | 2005-06-01 | AIRBUS France | Disporstif d'accrochage d'un moteur sous une voilure d'aéronef |
Also Published As
Publication number | Publication date |
---|---|
CA2623999A1 (fr) | 2007-04-05 |
BRPI0616194A2 (pt) | 2011-06-14 |
JP5032485B2 (ja) | 2012-09-26 |
CN101273191B (zh) | 2011-07-20 |
US20080230675A1 (en) | 2008-09-25 |
WO2007036515A1 (fr) | 2007-04-05 |
US7909302B2 (en) | 2011-03-22 |
FR2891253A1 (fr) | 2007-03-30 |
EP1929140A1 (fr) | 2008-06-11 |
CA2623999C (fr) | 2014-09-16 |
RU2008116733A (ru) | 2009-11-10 |
RU2435968C2 (ru) | 2011-12-10 |
EP1929140B1 (fr) | 2012-10-31 |
CN101273191A (zh) | 2008-09-24 |
FR2891253B1 (fr) | 2007-10-26 |
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Free format text: JAPANESE INTERMEDIATE CODE: R250 |
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R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
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