DE3379945D1 - High strength to weight horizontal and vertical aircraft stabilizer - Google Patents

High strength to weight horizontal and vertical aircraft stabilizer

Info

Publication number
DE3379945D1
DE3379945D1 DE8484900153T DE3379945T DE3379945D1 DE 3379945 D1 DE3379945 D1 DE 3379945D1 DE 8484900153 T DE8484900153 T DE 8484900153T DE 3379945 T DE3379945 T DE 3379945T DE 3379945 D1 DE3379945 D1 DE 3379945D1
Authority
DE
Germany
Prior art keywords
high strength
weight horizontal
vertical aircraft
aircraft stabilizer
stabilizer
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
Application number
DE8484900153T
Other languages
English (en)
Inventor
Robert Hamm
Uri Soudak
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE3379945D1 publication Critical patent/DE3379945D1/de
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/20—Integral or sandwich constructions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)
  • Laminated Bodies (AREA)
DE8484900153T 1983-09-29 1983-09-29 High strength to weight horizontal and vertical aircraft stabilizer Expired DE3379945D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1983/001551 WO1985001489A1 (en) 1983-09-29 1983-09-29 High strength to weight horizontal and vertical aircraft stabilizer

Publications (1)

Publication Number Publication Date
DE3379945D1 true DE3379945D1 (en) 1989-07-06

Family

ID=22175476

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8484900153T Expired DE3379945D1 (en) 1983-09-29 1983-09-29 High strength to weight horizontal and vertical aircraft stabilizer

Country Status (4)

Country Link
US (1) US4667905A (de)
EP (1) EP0157778B1 (de)
DE (1) DE3379945D1 (de)
WO (1) WO1985001489A1 (de)

Families Citing this family (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4315600C2 (de) * 1993-05-11 1996-07-25 Daimler Benz Aerospace Airbus Tragstruktur für eine aerodynamische Fläche
DE4329744C1 (de) * 1993-09-03 1994-09-08 Deutsche Forsch Luft Raumfahrt Flügel mit Flügelschalen aus Faserverbundwerkstoffen, insbesondere CFK, für Luftfahrzeuge
DE19529476C2 (de) * 1995-08-11 2000-08-10 Deutsch Zentr Luft & Raumfahrt Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge
GB9802597D0 (en) * 1998-02-07 1998-04-01 Hurel Dubois Uk Ltd Panels and structures
US6173925B1 (en) * 1998-04-16 2001-01-16 Daimlerchrysler Ag Skin-rib structure
US6513757B1 (en) * 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
ES2197727B1 (es) * 2000-07-27 2005-04-01 Construcciones Aeronauticas, S.A. Borde de ataque de superficies sustentadoras de aeronaves.
US6386481B1 (en) 2001-01-08 2002-05-14 Patria Finavicomp Oy Arrangement for fastening stringers to aircraft wing ribs
US7197852B2 (en) * 2002-09-20 2007-04-03 The Boeing Company Internally stiffened composite panels and methods for their manufacture
US20060060696A1 (en) * 2004-08-26 2006-03-23 Cordy Clifford B Jr Link between the wing and canard for flutter reduction
DE102005038851A1 (de) * 2005-08-17 2007-03-01 Airbus Deutschland Gmbh Fachwerk-Mittelkasten für einen Flügel
US7628358B2 (en) * 2006-10-26 2009-12-08 The Boeing Company Wing panel structure
WO2008092451A2 (en) * 2007-01-29 2008-08-07 Danmarks Tekniske Universitet Wind turbine blade
US20080277531A1 (en) * 2007-05-11 2008-11-13 The Boeing Company Hybrid Composite Panel Systems and Methods
ES2330180B1 (es) * 2007-06-28 2010-09-14 Airbus España S.L. Cajon de torsion multilarguero rigidizado.
US8268107B2 (en) * 2007-09-21 2012-09-18 The Boeing Company Fly away caul plate
FR2921899B1 (fr) * 2007-10-04 2011-04-15 Airbus France Procede de renforcement local d'un element en materiau composite, et caisson central de voilure pour aeronef renforce
US20090140527A1 (en) * 2007-11-30 2009-06-04 General Electric Company Wind turbine blade stiffeners
GB0803689D0 (en) 2008-02-29 2008-04-09 Airbus Uk Ltd Trailing edge aircraft structure with overhaning cover
FI20080208L (fi) * 2008-03-13 2008-03-27 Patria Aerostructures Oy Ilma-aluksen johtoreunaelementti, menetelmä sen valmistamiseksi sekä siipi ja vakain
ES2364109B1 (es) * 2008-11-27 2012-07-04 Airbus Operations, S.L. Un herraje delantero de trimado y su ensamblaje a la unión a tracción de los dos cajones laterales del estabilizador horizontal de un avión
IT1392320B1 (it) * 2008-12-09 2012-02-24 Alenia Aeronautica Spa Bordo d'attacco per ali ed impennaggi di aeromobili
US8424805B2 (en) * 2009-10-07 2013-04-23 Donald Smith Airfoil structure
US8844873B2 (en) 2011-09-23 2014-09-30 The Boeing Company Stabilizer torque box assembly and method
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
ES2606591T3 (es) * 2012-11-21 2017-03-24 Airbus Operations S.L. Un cajón de torsión optimizado para una aeronave
AU2014200142B2 (en) * 2013-01-26 2017-02-23 The Boeing Company Box structures for carrying loads and methods of making the same
US9681527B2 (en) * 2013-03-29 2017-06-13 The Boeing Company Method and apparatus for providing a current return network in an aircraft structure
ES2755765T3 (es) * 2013-12-23 2020-04-23 Airbus Operations Sl Superficie de control de aeronave
EP2889215A1 (de) * 2013-12-27 2015-07-01 Airbus Operations S.L. Horizontales Höhenleitwerk eines Flugzeugs
US9656738B2 (en) * 2015-07-06 2017-05-23 Embraer S.A. Airframe wing spar structures with contiguous unitary and integrally fastened upper and lower chord sections
US10513325B2 (en) * 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Joint member for a composite wing structure
US10639854B2 (en) 2016-02-08 2020-05-05 Bell Helicopter Textron Inc. Composite wing structure and methods of manufacture
US10016955B2 (en) * 2016-04-19 2018-07-10 The Boeing Company Panel apparatus including multiple panels and mechanical fasteners and methods of assembling the panel apparatus
CN106114819A (zh) * 2016-07-22 2016-11-16 中国航空工业集团公司西安飞机设计研究所 一种复合材料翼面结构
US10207789B2 (en) * 2016-08-16 2019-02-19 The Boeing Company Aircraft composite wingbox integration
US10647407B2 (en) * 2018-03-30 2020-05-12 The Boeing Company Wing flap with torque member and method for forming thereof
US10597141B2 (en) * 2018-03-30 2020-03-24 The Boeing Company Wing flap with torque member and method for forming thereof
US11597489B2 (en) * 2020-06-11 2023-03-07 Amazon Technologies, Inc. Aerial vehicle airframe design and manufacturing
US11623734B2 (en) 2020-12-02 2023-04-11 The Boeing Company Apparatus, system and method for supporting a wing flap of an aircraft

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB699070A (de) *
FR962428A (de) * 1950-06-10
DE337928C (de) * 1921-06-10 Georg Kruck Fa Tragflaeche fuer Flugzeuge
FR497275A (fr) * 1918-04-04 1919-12-02 Pierre Henri Groves Perfectionnements aux aéroplanes
US1809913A (en) * 1929-11-19 1931-06-16 Bendix Aviat Corp Airfoil
US1835532A (en) * 1929-11-19 1931-12-08 Bendix Aviat Corp Airfoil
US2031662A (en) * 1935-04-17 1936-02-25 Mercier Pierre Ernest Wing structure
US2593714A (en) * 1943-06-30 1952-04-22 Roy H Robinson Method of making cellular structures
US2410056A (en) * 1945-01-11 1946-10-29 Fresco Jacque Variable camber wing
US2998947A (en) * 1957-09-06 1961-09-05 Rolls Royce Supersonic narrow delta aircraft construction
US2997262A (en) * 1960-01-21 1961-08-22 Gen Dynamics Corp Aircraft wing structure
US3109614A (en) * 1961-10-23 1963-11-05 Boeing Co Fin-tip mounted horizontal control surface for airplanes
US3436038A (en) * 1967-04-11 1969-04-01 Aerojet General Co Structures
US3910531A (en) * 1972-10-17 1975-10-07 Aerospatiale Shell-type structure for light aircraft

Also Published As

Publication number Publication date
WO1985001489A1 (en) 1985-04-11
EP0157778A1 (de) 1985-10-16
EP0157778B1 (de) 1989-05-31
US4667905A (en) 1987-05-26

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee