DE60329077D1 - Flugzeugflügel - Google Patents

Flugzeugflügel

Info

Publication number
DE60329077D1
DE60329077D1 DE60329077T DE60329077T DE60329077D1 DE 60329077 D1 DE60329077 D1 DE 60329077D1 DE 60329077 T DE60329077 T DE 60329077T DE 60329077 T DE60329077 T DE 60329077T DE 60329077 D1 DE60329077 D1 DE 60329077D1
Authority
DE
Germany
Prior art keywords
wing
aircraft wing
leading edge
constitutes
structural part
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
DE60329077T
Other languages
English (en)
Inventor
Patrice R Verdan
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.)
Pilatus Flugzeugwerke AG
Original Assignee
Pilatus Flugzeugwerke AG
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 Pilatus Flugzeugwerke AG filed Critical Pilatus Flugzeugwerke AG
Application granted granted Critical
Publication of DE60329077D1 publication Critical patent/DE60329077D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Vibration Dampers (AREA)
  • Slide Fasteners, Snap Fasteners, And Hook Fasteners (AREA)
  • Radio Relay Systems (AREA)
  • Feedback Control In General (AREA)
  • Joining Of Building Structures In Genera (AREA)
DE60329077T 2003-05-09 2003-05-09 Flugzeugflügel Expired - Lifetime DE60329077D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03010467A EP1475304B1 (de) 2003-05-09 2003-05-09 Flugzeugflügel

Publications (1)

Publication Number Publication Date
DE60329077D1 true DE60329077D1 (de) 2009-10-15

Family

ID=32981854

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60329077T Expired - Lifetime DE60329077D1 (de) 2003-05-09 2003-05-09 Flugzeugflügel

Country Status (5)

Country Link
US (1) US20070272799A1 (de)
EP (1) EP1475304B1 (de)
AT (1) ATE441573T1 (de)
DE (1) DE60329077D1 (de)
WO (1) WO2004098993A1 (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0611802D0 (en) 2006-06-14 2006-07-26 Airbus Uk Ltd Improved composite aircraft component
GB0611804D0 (en) 2006-06-14 2006-07-26 Airbus Uk Ltd Improved aircraft component
US7866605B2 (en) * 2007-04-24 2011-01-11 The Boeing Company Energy absorbing impact band and method
GB0720387D0 (en) 2007-10-18 2007-11-28 Airbus Uk Ltd Panel with impact protection membrane
CN102390520B (zh) * 2011-09-29 2014-06-18 西北工业大学 一种能够提高飞机抗鸟撞性能的尾翼
FR2993857B1 (fr) * 2012-07-26 2015-03-27 Airbus Operations Sas Dispositif de protection d'une structure de longeron avant d'un caisson central d'aile d'aeronef et d'au moins un equipement situe dans ladite aile
BR112015011344A2 (pt) 2012-11-20 2017-07-11 Saab Ab borda de ataque de uma fuselagem
FR3000464B1 (fr) * 2012-12-27 2016-01-15 Eads Europ Aeronautic Defence Dispositif d'absorption d'energie pour element de structure d'aeronef
FR3000463B1 (fr) * 2012-12-27 2016-02-05 Eads Europ Aeronautic Defence Dispositif d'absorption d'energie pour element de structure d'aeronef
US20170130585A1 (en) * 2015-11-09 2017-05-11 General Electric Company Airfoil with energy absorbing edge guard
EP3216693A1 (de) * 2016-03-10 2017-09-13 Airbus Operations, S.L. Aerodynamische fläche eines flugzeugs mit abnehmbarer vorderkante
ES2744569T3 (es) * 2016-05-24 2020-02-25 Airbus Operations Sl Borde de ataque blindado y procedimiento de fabricación del mismo
ES2822933T3 (es) * 2016-11-04 2021-05-05 Airbus Operations Sl Estructura de panel para una aeronave y procedimiento de fabricación de la misma
US10556701B2 (en) * 2017-04-14 2020-02-11 Rohr, Inc. Bird-strike energy absorbing net
FR3100796B1 (fr) * 2019-09-12 2021-12-03 Safran Nacelles Entrée d’air de nacelle pour turboréacteur, contenant dans son volume un tissu d’armure multicouches

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2693922A (en) 1952-01-19 1954-11-09 Northrop Aircraft Inc Leading edge structure for airfoil
US3028128A (en) * 1960-08-02 1962-04-03 Eugene W Friedrich Reentry vehicle leading edge
US3640492A (en) * 1970-02-19 1972-02-08 Northrop Corp Modular aircraft structures
FR2125111B1 (de) * 1971-02-11 1974-02-15 Aerospatiale
US3962506A (en) * 1974-04-29 1976-06-08 Fiber Science, Inc. Multi-chambered cellular structure and method for manufacture
US3974313A (en) * 1974-08-22 1976-08-10 The Boeing Company Projectile energy absorbing protective barrier
US4083656A (en) * 1975-03-21 1978-04-11 Textron, Inc. Composite rotor blade
US4204358A (en) * 1978-03-13 1980-05-27 Briggs Donald L Aluminum model airplane kit
US4284443A (en) * 1979-02-05 1981-08-18 The Boeing Company Single stage hot bonding method for producing composite honeycomb core structures
US4667906A (en) * 1985-04-02 1987-05-26 Grumman Aerospace Corporation Replaceable tip for aircraft leading edge
DE3936194A1 (de) * 1989-10-31 1991-05-02 Basf Ag Wiederaufarbeitbares stossfaengersystem
DE4313592C2 (de) * 1993-04-26 2000-02-17 Daimler Chrysler Aerospace Großraumflugzeug
GB9504372D0 (en) * 1995-03-04 1995-04-26 British Aerospace A composite laminate
US6027078A (en) * 1998-02-27 2000-02-22 The Boeing Company Method and apparatus using localized heating for laminar flow
JP2000006893A (ja) * 1998-06-23 2000-01-11 Fuji Heavy Ind Ltd 複合材翼構造
ES2197727B1 (es) * 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
US6758507B2 (en) * 2001-03-01 2004-07-06 Venture Industries Energy absorbing external component for vehicle
DE10129576B4 (de) * 2001-06-20 2005-06-02 Fairchild Dornier Gmbh Strukturelement für ein Luftfahrzeug
US6779757B2 (en) * 2002-06-28 2004-08-24 Lockheed Martin Corporation Preforms for acute structural edges
DE102004018579A1 (de) * 2004-04-16 2005-11-03 Airbus Deutschland Gmbh Verkleidung für eine Struktur eines Flugzeugs

Also Published As

Publication number Publication date
ATE441573T1 (de) 2009-09-15
EP1475304A1 (de) 2004-11-10
EP1475304B1 (de) 2009-09-02
WO2004098993A1 (en) 2004-11-18
US20070272799A1 (en) 2007-11-29

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition