CN101583487A - 混合式复合金属的飞行器起落架与发动机支撑梁 - Google Patents

混合式复合金属的飞行器起落架与发动机支撑梁 Download PDF

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Publication number
CN101583487A
CN101583487A CNA2007800417978A CN200780041797A CN101583487A CN 101583487 A CN101583487 A CN 101583487A CN A2007800417978 A CNA2007800417978 A CN A2007800417978A CN 200780041797 A CN200780041797 A CN 200780041797A CN 101583487 A CN101583487 A CN 101583487A
Authority
CN
China
Prior art keywords
metalwork
composite
interior
metal
tapered end
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
CNA2007800417978A
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English (en)
Chinese (zh)
Inventor
D·C·达罗
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 CN101583487A publication Critical patent/CN101583487A/zh
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)
CNA2007800417978A 2006-12-08 2007-12-07 混合式复合金属的飞行器起落架与发动机支撑梁 Pending CN101583487A (zh)

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
US11/608,534 2006-12-08

Publications (1)

Publication Number Publication Date
CN101583487A true CN101583487A (zh) 2009-11-18

Family

ID=39789166

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2007800417978A Pending CN101583487A (zh) 2006-12-08 2007-12-07 混合式复合金属的飞行器起落架与发动机支撑梁

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 (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104875878A (zh) * 2014-02-27 2015-09-02 空中客车西班牙运营有限责任公司 带有容置于引擎机舱内的主起落架的飞机
RU2838700C1 (ru) * 2024-09-03 2025-04-22 Федеральное государственное бюджетное учреждение "Национальный исследовательский центр "Институт имени Н.Е.Жуковского" (ФГБУ "НИЦ "Институт имени Н.Е.Жуковского") Магистральный самолет с гибридной силовой установкой

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
JP5514527B2 (ja) * 2009-12-11 2014-06-04 ナブテスコ株式会社 航空機用リアクションリンク
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

Family Cites Families (17)

* 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
CA1107769A (en) * 1978-05-10 1981-08-25 Henry E. Wilson Composite fibrous tube energy absorber
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
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
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
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
US6893733B2 (en) * 2000-07-07 2005-05-17 Delphi Technologies, Inc. Modified contoured crushable structural members and methods for making the same
US6830223B1 (en) * 2000-11-16 2004-12-14 Tyee Aircraft Force sensor rod
US6582172B2 (en) * 2001-08-29 2003-06-24 The United States Of America As Represented By The Secretary Of The Navy Isolated mechanical fastening system
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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104875878A (zh) * 2014-02-27 2015-09-02 空中客车西班牙运营有限责任公司 带有容置于引擎机舱内的主起落架的飞机
CN104875878B (zh) * 2014-02-27 2019-08-13 空中客车西班牙运营有限责任公司 带有容置于引擎机舱内的主起落架的飞机
RU2838700C1 (ru) * 2024-09-03 2025-04-22 Федеральное государственное бюджетное учреждение "Национальный исследовательский центр "Институт имени Н.Е.Жуковского" (ФГБУ "НИЦ "Институт имени Н.Е.Жуковского") Магистральный самолет с гибридной силовой установкой

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
JP2010512268A (ja) 2010-04-22

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20091118