FR3014414B1 - Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation - Google Patents

Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation

Info

Publication number
FR3014414B1
FR3014414B1 FR1362424A FR1362424A FR3014414B1 FR 3014414 B1 FR3014414 B1 FR 3014414B1 FR 1362424 A FR1362424 A FR 1362424A FR 1362424 A FR1362424 A FR 1362424A FR 3014414 B1 FR3014414 B1 FR 3014414B1
Authority
FR
France
Prior art keywords
translation
connection device
fixing bracket
device mounted
vessel part
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.)
Expired - Fee Related
Application number
FR1362424A
Other languages
English (en)
Other versions
FR3014414A1 (fr
Inventor
Frederic Rossi
Laurent Alcala
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1362424A priority Critical patent/FR3014414B1/fr
Priority to US14/565,173 priority patent/US9381994B2/en
Priority to CN201410766494.4A priority patent/CN104709468B/zh
Publication of FR3014414A1 publication Critical patent/FR3014414A1/fr
Application granted granted Critical
Publication of FR3014414B1 publication Critical patent/FR3014414B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/32Wings specially adapted for mounting power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/005Accessories not provided for in the groups B64D37/02 - B64D37/28
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/40Sound or heat insulation, e.g. using insulation blankets
    • B64C1/403Arrangement of fasteners specially adapted therefor, e.g. of clips
    • B64C1/406Arrangement of fasteners specially adapted therefor, e.g. of clips in combination with supports for lines, e.g. for pipes or cables

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Clamps And Clips (AREA)
  • Connection Of Plates (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
FR1362424A 2013-12-11 2013-12-11 Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation Expired - Fee Related FR3014414B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1362424A FR3014414B1 (fr) 2013-12-11 2013-12-11 Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation
US14/565,173 US9381994B2 (en) 2013-12-11 2014-12-09 Aerofoil portion of an aircraft comprising an attachment support of a connecting device mounted in translation
CN201410766494.4A CN104709468B (zh) 2013-12-11 2014-12-11 包括平移安装连接装置的附接支承件的飞行器的机翼部分

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1362424A FR3014414B1 (fr) 2013-12-11 2013-12-11 Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation

Publications (2)

Publication Number Publication Date
FR3014414A1 FR3014414A1 (fr) 2015-06-12
FR3014414B1 true FR3014414B1 (fr) 2017-08-11

Family

ID=50231355

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1362424A Expired - Fee Related FR3014414B1 (fr) 2013-12-11 2013-12-11 Partie de voilure d'aeronef comportant un support de fixation d'un dispositif de raccordement monte en translation

Country Status (3)

Country Link
US (1) US9381994B2 (fr)
CN (1) CN104709468B (fr)
FR (1) FR3014414B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2577540A (en) * 2018-09-28 2020-04-01 Airbus Operations Ltd Joint for connecting aircraft structures

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9423726D0 (en) * 1994-11-24 1995-01-11 Horobin Ltd Connector
CN1108479C (zh) * 1999-11-01 2003-05-14 陆秀成 一种管道补偿接头
US6607165B1 (en) * 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
US7261256B2 (en) * 2004-03-29 2007-08-28 The Boeing Company Variable-duct support assembly
US7485808B2 (en) * 2005-04-28 2009-02-03 Airbus Deutschland Gmbh Holder for attaching electrical line bundles and pipes etc. to carriers and boards
FR2898867B1 (fr) * 2006-03-27 2008-12-19 Airbus France Sas Systeme pour le degivrage d'un capot d'entree d'air pour turbomoteur.
US7837144B2 (en) * 2006-08-11 2010-11-23 Techno-Sciences, Inc. Fluid-driven artificial muscles as mechanisms for controlled actuation
FR2916018B1 (fr) * 2007-05-10 2009-08-21 Snecma Propulsion Solide Sa Systeme d'echappement pour turbine a gaz
FR2918724B1 (fr) * 2007-07-10 2011-08-05 Peugeot Citroen Automobiles Sa Dispositif de fixation et ensemble correspondant.
FR2969578B1 (fr) * 2010-12-27 2013-02-08 Snecma Dispositif de suspension d'un turboreacteur
CN102826440B (zh) * 2011-06-15 2014-07-09 华锐风电科技(集团)股份有限公司 齿轮箱安装调整装置
FR2987401B1 (fr) * 2012-02-28 2017-05-12 Snecma Procede pour maintenir une piece d'adaptation sur un carter tubulaire d'un turbomoteur, piece d'adaptation et systeme de maintien correspondants.
CN102705203A (zh) * 2012-06-27 2012-10-03 苏州欧康泰压缩机科技有限责任公司 一种可游动的柔性管接头
US8851417B2 (en) * 2012-08-07 2014-10-07 United Technologies Corporation Self-retaining shear pin for blind mount location
CN103352902B (zh) * 2013-06-14 2015-09-16 严松法 微流量液压系统压力控制装置

Also Published As

Publication number Publication date
US9381994B2 (en) 2016-07-05
FR3014414A1 (fr) 2015-06-12
CN104709468B (zh) 2018-07-13
CN104709468A (zh) 2015-06-17
US20150183507A1 (en) 2015-07-02

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