FR3097839B1 - Partie d’aeronef comprenant un module interieur a fixation amelioree - Google Patents

Partie d’aeronef comprenant un module interieur a fixation amelioree Download PDF

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Publication number
FR3097839B1
FR3097839B1 FR1906980A FR1906980A FR3097839B1 FR 3097839 B1 FR3097839 B1 FR 3097839B1 FR 1906980 A FR1906980 A FR 1906980A FR 1906980 A FR1906980 A FR 1906980A FR 3097839 B1 FR3097839 B1 FR 3097839B1
Authority
FR
France
Prior art keywords
interior module
aircraft including
fixing
improved fixation
chamber
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
FR1906980A
Other languages
English (en)
Other versions
FR3097839A1 (fr
Inventor
Philippe Bernadet
Benoît COUROUBLE
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 FR1906980A priority Critical patent/FR3097839B1/fr
Priority to CN202010585962.3A priority patent/CN112141316A/zh
Priority to US16/912,195 priority patent/US11679858B2/en
Publication of FR3097839A1 publication Critical patent/FR3097839A1/fr
Application granted granted Critical
Publication of FR3097839B1 publication Critical patent/FR3097839B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64C1/061—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
    • B64C1/0683—Nose cones
    • 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
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Connection Of Plates (AREA)

Abstract

Pour faciliter la fixation d’un module intérieur (8) dans un espace intérieur (10) d’une partie d’aéronef (6), il est prévu un dispositif de fixation (40) comportant : - au moins un organe de fixation (46) comprenant une tige de fixation (50) ; - une chambre (70) d’introduction de l’organe de fixation (46), la chambre comprenant un premier orifice (68) traversé par la tige de fixation (50) en configuration montée du module intérieur (8), ainsi qu’un second orifice (72) permettant l’introduction de l’organe de fixation (46) dans la chambre (70) depuis l’extérieur. Figure pour l’abrégé : Figure 7
FR1906980A 2019-06-26 2019-06-26 Partie d’aeronef comprenant un module interieur a fixation amelioree Active FR3097839B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1906980A FR3097839B1 (fr) 2019-06-26 2019-06-26 Partie d’aeronef comprenant un module interieur a fixation amelioree
CN202010585962.3A CN112141316A (zh) 2019-06-26 2020-06-24 包括具有改进附接的内部模块的飞行器部段
US16/912,195 US11679858B2 (en) 2019-06-26 2020-06-25 Aircraft part comprising an internal module with improved attachment

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1906980A FR3097839B1 (fr) 2019-06-26 2019-06-26 Partie d’aeronef comprenant un module interieur a fixation amelioree
FR1906980 2019-06-26

Publications (2)

Publication Number Publication Date
FR3097839A1 FR3097839A1 (fr) 2021-01-01
FR3097839B1 true FR3097839B1 (fr) 2021-07-02

Family

ID=68343049

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1906980A Active FR3097839B1 (fr) 2019-06-26 2019-06-26 Partie d’aeronef comprenant un module interieur a fixation amelioree

Country Status (3)

Country Link
US (1) US11679858B2 (fr)
CN (1) CN112141316A (fr)
FR (1) FR3097839B1 (fr)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5014934A (en) * 1989-06-30 1991-05-14 The Boeing Company Removable seal for discontinuities in aircraft skin
FR2963314B1 (fr) 2010-07-27 2013-06-14 Airbus Operations Sas Procede et dispositif d'amenagement d'une soute avionique en pointe-avant d'un aeronef
US10578146B2 (en) * 2017-11-27 2020-03-03 The Boeing Company Seal system and method

Also Published As

Publication number Publication date
CN112141316A (zh) 2020-12-29
US20200407035A1 (en) 2020-12-31
US11679858B2 (en) 2023-06-20
FR3097839A1 (fr) 2021-01-01

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