DE69823330D1 - Stromlinienverkleidungen für Flugzeuge - Google Patents

Stromlinienverkleidungen für Flugzeuge

Info

Publication number
DE69823330D1
DE69823330D1 DE69823330T DE69823330T DE69823330D1 DE 69823330 D1 DE69823330 D1 DE 69823330D1 DE 69823330 T DE69823330 T DE 69823330T DE 69823330 T DE69823330 T DE 69823330T DE 69823330 D1 DE69823330 D1 DE 69823330D1
Authority
DE
Germany
Prior art keywords
aircraft
streamlined fairings
fairings
streamlined
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
DE69823330T
Other languages
English (en)
Other versions
DE69823330T2 (de
Inventor
Brian D Johnson
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 Ltd
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of DE69823330D1 publication Critical patent/DE69823330D1/de
Publication of DE69823330T2 publication Critical patent/DE69823330T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
    • B29K2995/0037—Other properties
    • B29K2995/0046—Elastic
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
DE69823330T 1997-03-26 1998-03-30 Stromlinienverkleidungen für Flugzeuge Expired - Lifetime DE69823330T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9706234A GB2323576B (en) 1997-03-26 1997-03-26 Fairing arrangements for aircraft
EP98302159A EP0947421B1 (de) 1997-03-26 1998-03-30 Stromlinienverkleidungen für Flugzeuge

Publications (2)

Publication Number Publication Date
DE69823330D1 true DE69823330D1 (de) 2004-05-27
DE69823330T2 DE69823330T2 (de) 2004-08-26

Family

ID=26151175

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69823330T Expired - Lifetime DE69823330T2 (de) 1997-03-26 1998-03-30 Stromlinienverkleidungen für Flugzeuge

Country Status (4)

Country Link
EP (1) EP0947421B1 (de)
DE (1) DE69823330T2 (de)
ES (1) ES2215274T3 (de)
GB (1) GB2323576B (de)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6293497B1 (en) 1996-10-22 2001-09-25 The Boeing Company Airplane with unswept slotted cruise wing airfoil
GB9920318D0 (en) 1999-08-27 1999-11-03 British Aerospace A fairing arrangement for an aircraft
US7258308B2 (en) * 2002-07-02 2007-08-21 The Boeing Company Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
EP1686056B1 (de) 2004-12-31 2011-07-27 Airbus Operations S.L. Verstärkte Abdeckung für Öffnungen eines aerodynamischen Profils
ES2277715B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para escotaduras en un contorno aerodinamico.
ES2277716B1 (es) * 2004-12-31 2008-05-16 Airbus España, S.L. Tapa reforzada para ranuras en un contorno aerodinamico.
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7611099B2 (en) * 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
DE102005048434A1 (de) * 2005-10-07 2007-04-26 Airbus Deutschland Gmbh Polyurethanlacke als Scheuerschutz-Beschichtungen
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
FR2905748B1 (fr) * 2006-09-08 2011-04-15 Airbus France Assemblage de panneaux et procede de fabrication
GB0722390D0 (en) 2007-11-15 2007-12-27 Airbus Uk Ltd Aileron actuator bracket
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
GB0803692D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Fitting for pivotally connecting aerodynamic control element to aircraft structure
GB0803689D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Trailing edge aircraft structure with overhaning cover
GB0803691D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Hinge rib
GB0803690D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Aircraft structure with hinge rib assembly
GB0807395D0 (en) 2008-04-23 2008-05-28 Airbus Uk Ltd Flight surface seal
IT1390909B1 (it) * 2008-07-16 2011-10-19 Alenia Aeronautica Spa Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
CN103596840A (zh) * 2011-06-16 2014-02-19 萨博公司 用于覆盖在飞行器的两个结构部之间的缝隙的双曲覆盖件
CN102642609B (zh) * 2012-05-11 2014-08-06 中国航空工业集团公司西安飞机设计研究所 一种翼盒整流口盖连接装置
US10730210B2 (en) 2013-10-31 2020-08-04 Apple Inc. Flexibility-controlled composite material and method of manufacture
GB201522486D0 (en) 2015-12-21 2016-02-03 Airbus Operations Ltd Seal assembly
EP3318783A1 (de) * 2016-11-02 2018-05-09 Airbus Operations GmbH Verkleidung für ein flugzeug

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2216710A1 (de) * 1972-04-07 1973-10-18 Dornier Gmbh Abdeckschild zur stroemungsguenstigen verkleidung von oberflaechenoeffnungen in bauteilen, insbesondere von oeffnungen an teilen von fluggeraeten
GB8919057D0 (en) * 1989-08-22 1989-10-04 British Aerospace Fairing arrangements for aircraft
GB8921749D0 (en) * 1989-09-27 1989-11-08 British Aerospace Fairing arrangements for aircraft
GB8924982D0 (en) * 1989-11-06 1989-12-28 British Aerospace Fairing arrangement for aircraft
GB8924981D0 (en) 1989-11-06 1989-12-28 British Aerospace Fairing arrangements for aircraft

Also Published As

Publication number Publication date
GB9706234D0 (en) 1997-05-14
DE69823330T2 (de) 2004-08-26
EP0947421A1 (de) 1999-10-06
GB2323576B (en) 2001-08-22
EP0947421B1 (de) 2004-04-21
ES2215274T3 (es) 2004-10-01
GB2323576A (en) 1998-09-30

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