FR3059302B1 - Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales - Google Patents

Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales Download PDF

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Publication number
FR3059302B1
FR3059302B1 FR1661683A FR1661683A FR3059302B1 FR 3059302 B1 FR3059302 B1 FR 3059302B1 FR 1661683 A FR1661683 A FR 1661683A FR 1661683 A FR1661683 A FR 1661683A FR 3059302 B1 FR3059302 B1 FR 3059302B1
Authority
FR
France
Prior art keywords
terminal
ribs
self
structural element
raidi
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
FR1661683A
Other languages
English (en)
Other versions
FR3059302A1 (fr
Inventor
Damien Guilloteau
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 FR1661683A priority Critical patent/FR3059302B1/fr
Priority to US15/827,047 priority patent/US10611455B2/en
Priority to CN201711231685.0A priority patent/CN108116652B/zh
Publication of FR3059302A1 publication Critical patent/FR3059302A1/fr
Application granted granted Critical
Publication of FR3059302B1 publication Critical patent/FR3059302B1/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
    • B64C1/12—Construction or attachment of skin panels
    • 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
    • B64C1/061—Frames
    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10—Bulkheads
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • 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
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1461—Structures of doors or surrounding frames

Abstract

Pour permettre un assemblage robuste entre un élément structurel (42) et un panneau auto-raidi (44) comprenant une peau (46) et une structure de raidissement (48) formée d'un maillage de nervures (50) s'étendant en saillie à partir d'une première face (46A) de la peau, l'élément structurel (42) comporte au moins une extrémité (52) formée de languettes terminales (54) séparées par des échancrures (56) et appliquées sur la première face de la peau au niveau d'une partie d'extrémité (46B) de la peau. De plus, la structure de raidissement (48) comporte au moins une extrémité formée de plusieurs nervures terminales (58) s'étendant respectivement au travers des échancrures (56). Enfin, chacune des languettes terminales (54) est fixée à la partie d'extrémité (46B) de la peau au moyen d'organes de fixation (60) traversants.
FR1661683A 2016-11-30 2016-11-30 Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales Active FR3059302B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1661683A FR3059302B1 (fr) 2016-11-30 2016-11-30 Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales
US15/827,047 US10611455B2 (en) 2016-11-30 2017-11-30 Aircraft assembly comprising a self-stiffened panel assembled with a structural element by means of an alternation of terminal ribs and terminal tabs
CN201711231685.0A CN108116652B (zh) 2016-11-30 2017-11-30 飞行器组件

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1661683 2016-11-30
FR1661683A FR3059302B1 (fr) 2016-11-30 2016-11-30 Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales

Publications (2)

Publication Number Publication Date
FR3059302A1 FR3059302A1 (fr) 2018-06-01
FR3059302B1 true FR3059302B1 (fr) 2019-05-17

Family

ID=57861119

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1661683A Active FR3059302B1 (fr) 2016-11-30 2016-11-30 Ensemble pour aeronef comprenant un panneau auto-raidi assemble a un element structurel au moyen d'une alternance de nervures terminales et de languettes terminales

Country Status (3)

Country Link
US (1) US10611455B2 (fr)
CN (1) CN108116652B (fr)
FR (1) FR3059302B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10974806B2 (en) * 2017-10-05 2021-04-13 Gulfstream Aerospace Corporation Unified canopies for aircraft
NL2023459B1 (en) * 2019-07-08 2021-02-02 Kok & Van Engelen Composite Structures B V Fuselage structure of an aircraft and method for manufacturing the same

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2230393A (en) * 1937-03-29 1941-02-04 John B Thomson Airplane structural element
FR2821129B1 (fr) * 2001-02-22 2003-05-16 Eads Airbus Sa Dispositif d'assemblage d'un panneau et d'une structure, apte a transmettre des efforts importants
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
US7861970B2 (en) * 2006-11-02 2011-01-04 The Boeing Company Fuselage structure including an integrated fuselage stanchion
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
US8128025B2 (en) * 2008-03-21 2012-03-06 The Boeing Company Providing skins for aircraft fuselages
FR2930521B1 (fr) * 2008-04-29 2010-09-03 Airbus France Module de plancher d'aeronef, structure et procede de fixation d'un tel module, aeronef comprenant ceux-ci
DE102009012428A1 (de) * 2009-03-10 2010-09-16 Telair International Gmbh Befestigungseinrichtung eines Bodenmoduls
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
EP2530010B1 (fr) * 2011-06-02 2013-09-18 Bell Helicopter Textron Inc. Panneau intégralement raidi
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
DE102012202504A1 (de) * 2012-02-17 2013-08-22 Airbus Operations Gmbh Strukturbauteil für ein Luft- oder Raumfahrzeug
FR3009274A1 (fr) * 2013-08-01 2015-02-06 Airbus Operations Sas Element de cadre de fuselage d'aeronef integrant des languettes pour la fixation de raidisseurs
FR3018267B1 (fr) * 2014-03-07 2017-12-22 Airbus Operations Sas Dispositif de positionnement relatif de deux pieces telles qu'une traverse et un cadre de fuselage
GB2528078B (en) * 2014-07-08 2020-07-29 Airbus Operations Ltd Structure
EP3173330B1 (fr) * 2015-11-30 2018-06-06 Airbus Operations GmbH Système de connexion de tige, composant structural d'aéronef et plot de connexion

Also Published As

Publication number Publication date
US10611455B2 (en) 2020-04-07
CN108116652B (zh) 2022-06-14
CN108116652A (zh) 2018-06-05
FR3059302A1 (fr) 2018-06-01
US20180148155A1 (en) 2018-05-31

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