FR3031082B1 - Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere - Google Patents

Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere

Info

Publication number
FR3031082B1
FR3031082B1 FR1463448A FR1463448A FR3031082B1 FR 3031082 B1 FR3031082 B1 FR 3031082B1 FR 1463448 A FR1463448 A FR 1463448A FR 1463448 A FR1463448 A FR 1463448A FR 3031082 B1 FR3031082 B1 FR 3031082B1
Authority
FR
France
Prior art keywords
aircraft
singer
particular position
fitting
assembly connecting
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
FR1463448A
Other languages
English (en)
Other versions
FR3031082A1 (fr
Inventor
Francois Rouyre
Christian Cros
Jerome Antypas
Sebastien Menard
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 FR1463448A priority Critical patent/FR3031082B1/fr
Priority to US14/980,515 priority patent/US10358204B2/en
Priority to CN201511001002.3A priority patent/CN105730675A/zh
Publication of FR3031082A1 publication Critical patent/FR3031082A1/fr
Application granted granted Critical
Publication of FR3031082B1 publication Critical patent/FR3031082B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/38—Constructions adapted to reduce effects of aerodynamic or other external heating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
FR1463448A 2014-12-30 2014-12-30 Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere Active FR3031082B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1463448A FR3031082B1 (fr) 2014-12-30 2014-12-30 Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere
US14/980,515 US10358204B2 (en) 2014-12-30 2015-12-28 Joint assembly and method connecting an aircraft belly fairing to the fuselage provided with a particularly positioned stringer
CN201511001002.3A CN105730675A (zh) 2014-12-30 2015-12-28 将飞行器腹部整流罩连接至设置有特定定位的桁条的机身的接头组件

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1463448A FR3031082B1 (fr) 2014-12-30 2014-12-30 Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere

Publications (2)

Publication Number Publication Date
FR3031082A1 FR3031082A1 (fr) 2016-07-01
FR3031082B1 true FR3031082B1 (fr) 2017-02-10

Family

ID=52684524

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1463448A Active FR3031082B1 (fr) 2014-12-30 2014-12-30 Ensemble de jonction raccordant un carenage ventral d'aeronef au fuselage pourvu d'un raidisseur en position particuliere

Country Status (3)

Country Link
US (1) US10358204B2 (fr)
CN (1) CN105730675A (fr)
FR (1) FR3031082B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10766598B2 (en) * 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10773787B2 (en) * 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10773788B2 (en) * 2017-08-15 2020-09-15 The Boeing Company Fairing assembly and method therefor
CN109711015A (zh) * 2018-12-14 2019-05-03 中国航空工业集团公司西安飞机设计研究所 一种飞机大开口结构侧向刚度设计方法
CN113602369A (zh) * 2021-02-10 2021-11-05 唐腊辉 一种交通工具用超声波气流切割降阻装置

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1523404A (fr) * 1967-03-22 1968-05-03 Sud Aviation Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne
FR2836963A1 (fr) * 2002-03-08 2003-09-12 Airbus France Dispositif de fixation d'un element sur une structure d'aeronef
AU2003210634A1 (en) * 2003-01-23 2004-08-23 Bell Helicopter Textron Inc. Proprotor blade with leading edge slot
CN2775582Y (zh) * 2004-12-13 2006-04-26 北京普瑞林科贸发展有限公司 激波式增压热交换器
DE102006023209A1 (de) * 2006-05-17 2007-11-22 Airbus Deutschland Gmbh Isolierung einer Flugzeugrumpfstruktur
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
CN201032034Y (zh) * 2007-06-02 2008-03-05 安徽中科智能高技术有限责任公司 用于管道密封的组合密封件
FR2936489B1 (fr) * 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
FR2940785B1 (fr) * 2009-01-08 2012-10-26 Airbus France Jonction longitudinale pour panneaux de fuselage d'aeronef en materiaux composites
CN201858475U (zh) * 2010-11-10 2011-06-08 洛阳双瑞特种装备有限公司 一种旋转补偿器的新型摩擦副结构
CN201953718U (zh) * 2010-12-17 2011-08-31 乐金空调(山东)有限公司 离心压缩机叶片可调式扩压器
FR2977237B1 (fr) * 2011-06-28 2014-11-21 Airbus Operations Sas Carenage aerodynamique arriere d'un mat de liaison d'un moteur d'aeronef
GB201205079D0 (en) * 2012-03-22 2012-05-09 Airbus Operations Ltd Seal assembly for an aircraft wing
FR2993240B1 (fr) * 2012-07-12 2014-08-29 Dassault Aviat Structure d'aeronef, et procede de montage associe
EP2727820B1 (fr) * 2012-10-31 2016-12-14 Airbus Operations S.L. Lisse
GB201220937D0 (en) * 2012-11-21 2013-01-02 Airbus Uk Ltd Modular structural assembly
CN103670787A (zh) * 2013-12-05 2014-03-26 芜湖荣基密封系统有限公司 一种防滑动密封排气垫
CN104787302B (zh) * 2015-04-07 2017-11-03 中国直升机设计研究所 一种倾斜式整流罩和斜梁之间的连接结构

Also Published As

Publication number Publication date
CN105730675A (zh) 2016-07-06
FR3031082A1 (fr) 2016-07-01
US10358204B2 (en) 2019-07-23
US20160185438A1 (en) 2016-06-30

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