FR3071478B1 - MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED - Google Patents

MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED Download PDF

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Publication number
FR3071478B1
FR3071478B1 FR1758891A FR1758891A FR3071478B1 FR 3071478 B1 FR3071478 B1 FR 3071478B1 FR 1758891 A FR1758891 A FR 1758891A FR 1758891 A FR1758891 A FR 1758891A FR 3071478 B1 FR3071478 B1 FR 3071478B1
Authority
FR
France
Prior art keywords
aircraft
front part
fuselage
fleets
module
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
FR1758891A
Other languages
French (fr)
Other versions
FR3071478A1 (en
Inventor
Pascal Chaumel
Didier Reynes
Jean-Paul Dourel
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 FR1758891A priority Critical patent/FR3071478B1/en
Priority to CN201811123769.7A priority patent/CN109552593A/en
Publication of FR3071478A1 publication Critical patent/FR3071478A1/en
Application granted granted Critical
Publication of FR3071478B1 publication Critical patent/FR3071478B1/en
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
    • B64C1/14—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
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • B64C1/1492—Structure and mounting of the transparent elements in the window or windscreen
    • 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
    • B64C1/1476—Canopies; Windscreens or similar transparent elements
    • 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
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Automatic Assembly (AREA)
  • Wind Motors (AREA)

Abstract

La zone des glaces et de la casquette d'une partie avant d'aéronef est de fabrication complexe compte-tenu des nombreuses contraintes qui s'y appliquent. La présente invention a pour but d'en faciliter la réalisation. La présente invention concerne un procédé de fabrication d'au moins deux flottes d'aéronefs de familles différentes pour laquelle chaque aéronef présente une partie (12) avant comprenant des glaces (30, 32), un encadrement (34) des glaces et une casquette (36), caractérisé en ce qu'il comprend pour chaque aéronef : • une étape de fabrication d'un module (16) constitué de l'encadrement (34) de l'ensemble des glaces permettant la visibilité vers l'extérieur depuis le poste de pilotage et de la casquette (36) dont la forme est identique et constante pour tous les aéronefs des flottes et indépendante de la forme du fuselage de ceux-ci ; • une étape de fabrication d'un tronçon (20) de fuselage dont au moins une partie du bord (28) est de forme identique au bord dudit module (16) de manière que le module (16) puisse être assemblé directement au tronçon (20) contigu quel que soit l'aéronef des flottes.The zone of the windows and of the fairing of an aircraft front part is complex to manufacture given the numerous constraints which apply thereto. The present invention aims to facilitate its implementation. The present invention relates to a method for manufacturing at least two fleets of aircraft of different families for which each aircraft has a front part (12) comprising windows (30, 32), a window frame (34) and a (36), characterized in that it comprises for each aircraft: a step of manufacturing a module (16) consisting of the frame (34) of all the windows allowing outward visibility from the cockpit and the cap (36) whose shape is identical and constant for all the aircraft of the fleets and independent of the shape of the fuselage thereof; a step of manufacturing a fuselage section (20) of which at least part of the edge (28) is of identical shape to the edge of said module (16) so that the module (16) can be assembled directly to the section ( 20) contiguous regardless of fleets aircraft.

FR1758891A 2017-09-26 2017-09-26 MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED Active FR3071478B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1758891A FR3071478B1 (en) 2017-09-26 2017-09-26 MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED
CN201811123769.7A CN109552593A (en) 2017-09-26 2018-09-26 For constructing the construction method and aircraft fleet of at least two fleets

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1758891 2017-09-26
FR1758891A FR3071478B1 (en) 2017-09-26 2017-09-26 MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED

Publications (2)

Publication Number Publication Date
FR3071478A1 FR3071478A1 (en) 2019-03-29
FR3071478B1 true FR3071478B1 (en) 2021-12-03

Family

ID=60302325

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1758891A Active FR3071478B1 (en) 2017-09-26 2017-09-26 MODULAR MANUFACTURING PROCESS OF THE FRONT PART OF AN AIRCRAFT FUSELAGE AND AIRCRAFT FLEET OBTAINED

Country Status (2)

Country Link
CN (1) CN109552593A (en)
FR (1) FR3071478B1 (en)

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE59806899D1 (en) * 1997-02-05 2003-02-20 Anatoli J Vassiliev Airplane for passenger and / or freight transportation
FR2782495B1 (en) * 1998-08-19 2000-11-10 Aerospatiale FRONT OF AIRPLANE STRUCTURE
US6497388B1 (en) * 2001-08-31 2002-12-24 The Boeing Company Common flight deck module for family of commercial aircraft
FR2905669B1 (en) * 2006-09-13 2009-04-10 Airbus France Sa FRAMEWORK FOR WINDSHIELD AND METHOD FOR MANUFACTURING FRAMEWORK FOR WINDSHIELD
FR2933377B1 (en) * 2008-07-01 2011-04-15 Airbus France PLANE WITH FRONT LANDING TRAIN
FR3000024B1 (en) * 2012-12-21 2015-01-02 Airbus Operations Sas AIRCRAFT COCKPIT WITH FLOOR FLOOR
FR3043646B1 (en) * 2015-11-17 2017-12-22 Airbus Operations Sas STRUCTURAL ASSEMBLY FOR DOUBLE-CURVED AIRCRAFT FUSELAGE COMPRISING OPTIMIZED ORIENTATION FRAMES

Also Published As

Publication number Publication date
FR3071478A1 (en) 2019-03-29
CN109552593A (en) 2019-04-02

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