DE1268272T1 - Gestaltung eines holmes in k-form für eine geklebte flügelstruktur - Google Patents

Gestaltung eines holmes in k-form für eine geklebte flügelstruktur

Info

Publication number
DE1268272T1
DE1268272T1 DE1268272T DE01923140T DE1268272T1 DE 1268272 T1 DE1268272 T1 DE 1268272T1 DE 1268272 T DE1268272 T DE 1268272T DE 01923140 T DE01923140 T DE 01923140T DE 1268272 T1 DE1268272 T1 DE 1268272T1
Authority
DE
Germany
Prior art keywords
glued
designing
hole
shape
wing structure
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.)
Pending
Application number
DE1268272T
Other languages
English (en)
Inventor
Earl Nunn
Antonin Fila
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of DE1268272T1 publication Critical patent/DE1268272T1/de
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
DE1268272T 2000-04-05 2001-04-05 Gestaltung eines holmes in k-form für eine geklebte flügelstruktur Pending DE1268272T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US19461000P 2000-04-05 2000-04-05
PCT/US2001/010991 WO2001076939A2 (en) 2000-04-05 2001-04-05 K-spar configuration for bonded wing construction

Publications (1)

Publication Number Publication Date
DE1268272T1 true DE1268272T1 (de) 2003-06-26

Family

ID=22718241

Family Applications (2)

Application Number Title Priority Date Filing Date
DE60128664T Expired - Lifetime DE60128664T2 (de) 2000-04-05 2001-04-05 Gestaltung eines holmes in k-form für eine geklebte flügelstruktur
DE1268272T Pending DE1268272T1 (de) 2000-04-05 2001-04-05 Gestaltung eines holmes in k-form für eine geklebte flügelstruktur

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE60128664T Expired - Lifetime DE60128664T2 (de) 2000-04-05 2001-04-05 Gestaltung eines holmes in k-form für eine geklebte flügelstruktur

Country Status (6)

Country Link
US (1) US6739553B2 (de)
EP (1) EP1268272B1 (de)
AU (1) AU2001249862A1 (de)
CA (1) CA2402848C (de)
DE (2) DE60128664T2 (de)
WO (1) WO2001076939A2 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT410656B (de) * 2001-10-24 2003-06-25 Fischer Adv Components Gmbh Trag- bzw. führungsvorrichtung für flugzeugkomponenten
GB0611875D0 (en) * 2006-06-15 2006-07-26 Airbus Uk Ltd A stringer for an aircraft wing and a method of forming thereof
US7686251B2 (en) * 2006-12-13 2010-03-30 The Boeing Company Rib support for wing panels
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
ES2346834B1 (es) 2007-04-30 2011-08-17 Airbus Operations, S.L. Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave.
CN103434638A (zh) * 2013-09-16 2013-12-11 哈尔滨工业大学 复合材料机翼中梁与加强肋的混合连接方法
US9517833B2 (en) * 2015-04-28 2016-12-13 The Boeing Company Apparatuses and methods for manufacturing a structure
GB2575102A (en) * 2018-06-29 2020-01-01 Airbus Operations Ltd Duct stringer with bulkhead
GB2617556A (en) * 2022-04-08 2023-10-18 Airbus Operations Ltd Wing-box structure

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE361286C (de) * 1922-01-21 1922-10-16 Hugh Lwan Gramatzki Mikrometer
US1822940A (en) * 1928-08-20 1931-09-15 American Avigation Corp Wing structure for airplanes
US1900067A (en) * 1928-09-25 1933-03-07 Messerschmitt Willy Spar for airplanes
US1880478A (en) * 1929-05-03 1932-10-04 Budd Edward G Mfg Co Airplane structure
US1956823A (en) * 1929-06-13 1934-05-01 Cairns Dev Company Wing structure
US1908757A (en) * 1929-08-06 1933-05-16 Curtiss Aeroplane & Motor Co Aeronautical truss and method of forming the same
US1919088A (en) * 1931-03-25 1933-07-18 Aviation Louis Breguet Sa Wing structure for flying machines
US1866961A (en) * 1931-07-02 1932-07-12 Giuseppe M Bellanca Wing structure
US1976480A (en) * 1931-10-29 1934-10-09 Curtiss Aeroplane & Motor Co Aerofoil
US1988079A (en) * 1932-05-27 1935-01-15 Curtiss Wright Airplane Compan Airplane wing
US2233969A (en) * 1938-12-30 1941-03-04 Bell Aircraft Corp Pressed wing rib
US2693922A (en) 1952-01-19 1954-11-09 Northrop Aircraft Inc Leading edge structure for airfoil
FR2292623A1 (fr) * 1974-11-26 1976-06-25 Aerospatiale Procede pour la realisation de structures composites resistantes, notamment pour aerodynes et structures ainsi obtenues
US4095322A (en) * 1976-08-30 1978-06-20 The Boeing Company Method of fabricating a composite aerodynamic rotorblade assembly
US4356616A (en) * 1980-02-25 1982-11-02 Rockwell International Corporation Method of making rib structures for an airfoil
US4565595A (en) 1981-09-30 1986-01-21 The Boeing Company Method of making composite aircraft wing
WO1987001431A1 (en) * 1984-02-28 1987-03-12 Offshore Marine Pty. Ltd. Structural member
US4892435A (en) * 1989-02-06 1990-01-09 Grumman Aerospace Corporation Interlocking structural members employing transverse locking double interfitting wedge
US5330092A (en) 1991-12-17 1994-07-19 The Boeing Company Multiple density sandwich structures and method of fabrication
DE19529476C2 (de) 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
US5848765A (en) 1996-06-20 1998-12-15 The Boeing Company Reduced amplitude corrugated web spar
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
FR2803821B1 (fr) * 2000-01-17 2002-04-05 Dassault Aviat Bec de voilure d'aeronef equipe d'un dispositif d'antigivrage, voilure equipee d'un tel bec, et aeronef equipe d'une telle voilure

Also Published As

Publication number Publication date
US6739553B2 (en) 2004-05-25
US20040035981A1 (en) 2004-02-26
CA2402848C (en) 2009-06-16
AU2001249862A1 (en) 2001-10-23
DE60128664D1 (de) 2007-07-12
WO2001076939A2 (en) 2001-10-18
EP1268272A4 (de) 2006-05-31
EP1268272A2 (de) 2003-01-02
DE60128664T2 (de) 2008-01-31
EP1268272B1 (de) 2007-05-30
CA2402848A1 (en) 2001-10-18
WO2001076939A3 (en) 2002-05-23

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