ES2177228T3 - Estructuras de doble funcion. - Google Patents

Estructuras de doble funcion.

Info

Publication number
ES2177228T3
ES2177228T3 ES99903835T ES99903835T ES2177228T3 ES 2177228 T3 ES2177228 T3 ES 2177228T3 ES 99903835 T ES99903835 T ES 99903835T ES 99903835 T ES99903835 T ES 99903835T ES 2177228 T3 ES2177228 T3 ES 2177228T3
Authority
ES
Spain
Prior art keywords
modules
structural
double function
dual
range
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 - Lifetime
Application number
ES99903835T
Other languages
English (en)
Inventor
Geoffrey James Ash
Colin Whaites
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Application granted granted Critical
Publication of ES2177228T3 publication Critical patent/ES2177228T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • 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)
  • Laminated Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

Un método de fabricación y montaje de aviones, que comprende la fabricación de una gama de módulos estructurales de doble función comprendiendo cada uno de dichos módulos estructurales de doble función equipos de sistemas aeronáuticos específicos integrados con elementos estructurales, proporcionando de ese modo una gama de módulos estructurales específicos de sistemas aeronáuticos, los cuales pueden ser integrados con una estructura de avión, caracterizado porque se mecanizan galerías en los elementos estructurales de dichos módulos para conducir fluidos para su uso dentro de dicho sistema.
ES99903835T 1998-02-06 1999-02-04 Estructuras de doble funcion. Expired - Lifetime ES2177228T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9802440.9A GB9802440D0 (en) 1998-02-06 1998-02-06 Dual function structures

Publications (1)

Publication Number Publication Date
ES2177228T3 true ES2177228T3 (es) 2002-12-01

Family

ID=10826496

Family Applications (1)

Application Number Title Priority Date Filing Date
ES99903835T Expired - Lifetime ES2177228T3 (es) 1998-02-06 1999-02-04 Estructuras de doble funcion.

Country Status (6)

Country Link
EP (1) EP1053174B1 (es)
AU (1) AU2435299A (es)
DE (1) DE69901485T2 (es)
ES (1) ES2177228T3 (es)
GB (1) GB9802440D0 (es)
WO (1) WO1999039975A1 (es)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005060369A1 (de) * 2005-12-16 2007-07-05 Airbus Deutschland Gmbh Luftfahrzeug mit modularem Aufbau
CN102233955B (zh) * 2010-05-06 2016-03-09 中国商用飞机有限责任公司 飞机驾驶舱顶部控制板及其安装方法
DE102011083553A1 (de) 2011-09-27 2013-03-28 Airbus Operations Gmbh Rumpfzelle für ein Luftfahrzeug, insbesondere ein Flugzeug

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3640492A (en) 1970-02-19 1972-02-08 Northrop Corp Modular aircraft structures
US4736910A (en) 1984-08-10 1988-04-12 Flight Concepts Limited Partnership Aircraft with interchangeable fuselage
DE4131569A1 (de) * 1991-09-23 1993-03-25 Josef Dr Fleischer Modul-flugzeug
DE4218197C2 (de) * 1992-06-03 1996-07-11 Daimler Benz Aerospace Ag Mehrzweckflugzeug für verschiedene Missionsaufgaben
US5897078A (en) 1995-12-15 1999-04-27 The Boeing Company Multi-service common airframe-based aircraft

Also Published As

Publication number Publication date
AU2435299A (en) 1999-08-23
DE69901485D1 (de) 2002-06-20
EP1053174B1 (en) 2002-05-15
EP1053174A1 (en) 2000-11-22
WO1999039975A1 (en) 1999-08-12
GB9802440D0 (en) 1998-04-01
DE69901485T2 (de) 2002-10-02

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