JP2010512268A - 航空機のハイブリッド複合金属ランディングギア及びエンジンサポートビーム - Google Patents

航空機のハイブリッド複合金属ランディングギア及びエンジンサポートビーム Download PDF

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Publication number
JP2010512268A
JP2010512268A JP2009540494A JP2009540494A JP2010512268A JP 2010512268 A JP2010512268 A JP 2010512268A JP 2009540494 A JP2009540494 A JP 2009540494A JP 2009540494 A JP2009540494 A JP 2009540494A JP 2010512268 A JP2010512268 A JP 2010512268A
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JP
Japan
Prior art keywords
metal part
outer metal
hybrid composite
composite material
inner metal
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
JP2009540494A
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English (en)
Japanese (ja)
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JP2010512268A5 (https=
Inventor
ドナルド， シー． ダロー，
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
Publication of JP2010512268A publication Critical patent/JP2010512268A/ja
Publication of JP2010512268A5 publication Critical patent/JP2010512268A5/ja
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2605/00—Vehicles
    • B32B2605/18—Aircraft
    • 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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
JP2009540494A 2006-12-08 2007-12-07 航空機のハイブリッド複合金属ランディングギア及びエンジンサポートビーム Pending JP2010512268A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/608,534 US20080283667A1 (en) 2006-12-08 2006-12-08 Hybrid composite-metal aircraft landing gear and engine support beams
PCT/US2007/086744 WO2008118229A2 (en) 2006-12-08 2007-12-07 Hybrid composite-metal aircraft landing gear and engine support beams

Publications (2)

Publication Number Publication Date
JP2010512268A true JP2010512268A (ja) 2010-04-22
JP2010512268A5 JP2010512268A5 (https=) 2011-02-03

Family

ID=39789166

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009540494A Pending JP2010512268A (ja) 2006-12-08 2007-12-07 航空機のハイブリッド複合金属ランディングギア及びエンジンサポートビーム

Country Status (6)

Country Link
US (1) US20080283667A1 (https=)
EP (1) EP2097255A2 (https=)
JP (1) JP2010512268A (https=)
CN (1) CN101583487A (https=)
CA (1) CA2666595A1 (https=)
WO (1) WO2008118229A2 (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011121489A (ja) * 2009-12-11 2011-06-23 Nabtesco Corp 航空機用リアクションリンク

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2473007B (en) 2009-08-26 2012-11-21 Messier Dowty Ltd Apparatus comprising an end fitting connected to a body
EP2913267B1 (en) * 2014-02-27 2019-10-30 Airbus Operations S.L. Aircraft with a nacelle-housed main landing gear
US12060473B2 (en) 2018-07-03 2024-08-13 University Of Notre Dame Du Lac Polymer/exfoliated nano-composite films with superior mechanical properties
EP3611390B1 (en) 2018-08-16 2020-12-23 Crompton Technology Group Limited Composite structure having a tapered joint and a method for making the same
EP3792173B1 (en) 2019-09-16 2022-04-27 SKF Aerospace France Fail-safe system intended for use in an aircraft

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS556078A (en) * 1978-05-10 1980-01-17 Textron Inc Force damper * energy absorbing seat * landing device for airplane and shock absorber for vehicle
US4581077A (en) * 1984-04-27 1986-04-08 Nippon Mining Co., Ltd. Method of manufacturing rolled titanium alloy sheets
US4923751A (en) * 1986-10-21 1990-05-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Seamless metal-clad fiber-reinforced organic matrix composite structures, and process for their manufacture
JPH0960676A (ja) * 1995-08-25 1997-03-04 Yokohama Rubber Co Ltd:The 衝撃緩和材及びその製造方法
US20030044256A1 (en) * 2001-08-29 2003-03-06 Nickerson Earl S. Isolated mechanical fastening system
US6830223B1 (en) * 2000-11-16 2004-12-14 Tyee Aircraft Force sensor rod

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584832A (en) * 1945-04-07 1952-02-05 Bendix Aviat Corp Method of making a trunnion for aircraft landing gear
US3416975A (en) * 1965-05-04 1968-12-17 Nasa Etching of aluminum for bonding
US3623203A (en) * 1970-03-24 1971-11-30 Avco Corp Reinforced structural members and method of making same
US4185472A (en) * 1978-03-27 1980-01-29 Celanese Corporation Fiber reinforced composite shaft with metallic connector sleeves mounted by radial pin interlock
US4300439A (en) * 1979-09-10 1981-11-17 United Technologies Corporation Ballistic tolerant hydraulic control actuator and method of fabricating same
DE3017336A1 (de) * 1980-05-06 1981-11-12 Paul Dr. 1000 Berlin Mader Auf biegung beanspruchter rohrfoermiger koerper
DE3103646C2 (de) * 1981-02-04 1984-03-29 Aluminium-Walzwerke Singen Gmbh, 7700 Singen Druckbehälter zur Lagerung sowie zum Transport gasförmiger Strömungsmittel
FR2675563B1 (fr) * 1991-04-22 1993-08-27 Aerospatiale Procede d'assemblage mecanique d'un tube en materiau composite et d'une piece metallique et assemblage ainsi realise.
US5332049A (en) * 1992-09-29 1994-07-26 Brunswick Corporation Composite drill pipe
US6893733B2 (en) * 2000-07-07 2005-05-17 Delphi Technologies, Inc. Modified contoured crushable structural members and methods for making the same
DE102004008523B4 (de) * 2004-02-20 2007-02-01 Liebherr-Aerospace Lindenberg Gmbh Verfahren zur Herstellung eines Druckzylinders und Kolbenstange für Aktuatoren oder Stoßdämpfer und Verfahren zu deren Herstellung

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS556078A (en) * 1978-05-10 1980-01-17 Textron Inc Force damper * energy absorbing seat * landing device for airplane and shock absorber for vehicle
US4581077A (en) * 1984-04-27 1986-04-08 Nippon Mining Co., Ltd. Method of manufacturing rolled titanium alloy sheets
US4923751A (en) * 1986-10-21 1990-05-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Seamless metal-clad fiber-reinforced organic matrix composite structures, and process for their manufacture
JPH0960676A (ja) * 1995-08-25 1997-03-04 Yokohama Rubber Co Ltd:The 衝撃緩和材及びその製造方法
US6830223B1 (en) * 2000-11-16 2004-12-14 Tyee Aircraft Force sensor rod
US20030044256A1 (en) * 2001-08-29 2003-03-06 Nickerson Earl S. Isolated mechanical fastening system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011121489A (ja) * 2009-12-11 2011-06-23 Nabtesco Corp 航空機用リアクションリンク
US8678694B2 (en) 2009-12-11 2014-03-25 Nabtesco Corporation Aircraft reaction link

Also Published As

Publication number Publication date
WO2008118229A2 (en) 2008-10-02
WO2008118229A3 (en) 2009-03-19
CA2666595A1 (en) 2008-10-02
EP2097255A2 (en) 2009-09-09
US20080283667A1 (en) 2008-11-20
CN101583487A (zh) 2009-11-18

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