BR9509734A - Trem de pouso para aterrissagem forçada para uma aeronave - Google Patents

Trem de pouso para aterrissagem forçada para uma aeronave

Info

Publication number
BR9509734A
BR9509734A BR9509734A BR9509734A BR9509734A BR 9509734 A BR9509734 A BR 9509734A BR 9509734 A BR9509734 A BR 9509734A BR 9509734 A BR9509734 A BR 9509734A BR 9509734 A BR9509734 A BR 9509734A
Authority
BR
Brazil
Prior art keywords
landing
aircraft
forced
gear
landing gear
Prior art date
Application number
BR9509734A
Other languages
English (en)
Inventor
Berardino Delmonte
Ralph P Barone
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of BR9509734A publication Critical patent/BR9509734A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60—Oleo legs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)
  • Fluid-Damping Devices (AREA)
  • Transmission Devices (AREA)
BR9509734A 1994-11-18 1995-11-08 Trem de pouso para aterrissagem forçada para uma aeronave BR9509734A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/341,786 US5547148A (en) 1994-11-18 1994-11-18 Crashworthy landing gear
PCT/US1995/014544 WO1996015940A1 (en) 1994-11-18 1995-11-08 A crashworthy landing gear for an aircraft

Publications (1)

Publication Number Publication Date
BR9509734A true BR9509734A (pt) 1997-10-21

Family

ID=23339033

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9509734A BR9509734A (pt) 1994-11-18 1995-11-08 Trem de pouso para aterrissagem forçada para uma aeronave

Country Status (8)

Country Link
US (1) US5547148A (pt)
EP (1) EP0790923B1 (pt)
JP (1) JPH10508813A (pt)
CN (1) CN1070442C (pt)
BR (1) BR9509734A (pt)
CA (1) CA2205489C (pt)
DE (1) DE69504699T2 (pt)
WO (1) WO1996015940A1 (pt)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6763635B1 (en) 1999-11-30 2004-07-20 Shook Mobile Technology, Lp Boom with mast assembly
US6328259B1 (en) 2000-06-06 2001-12-11 The Boeing Company Variable-load shear collar for helicopter landing gear shock struts
JP4515600B2 (ja) * 2000-06-06 2010-08-04 住友精密工業株式会社 航空機用降着装置
DE10249517B4 (de) * 2002-10-23 2008-11-20 Eurocopter Deutschland Gmbh Stoßabsorbierende, lastbegrenzende Verbindungsvorrichtung sowie Drehflügelflugzeug mit einer solchen Verbindungsvorrichtung
JP3888630B2 (ja) * 2002-12-04 2007-03-07 川崎重工業株式会社 エネルギー吸収部材及びそれを用いるヘリコプタの耐衝撃構造
ITMI20031106A1 (it) * 2003-06-03 2004-12-04 Milano Politecnico Sistema di innesco del collasso plastico di un elemento strutturale metallico.
WO2008054831A2 (en) * 2006-02-23 2008-05-08 Sikorsky Aircraft Corporation Aircraft payload retention system for interior loads
DE102007019052A1 (de) * 2007-03-19 2008-09-25 Liebherr-Aerospace Lindenberg Gmbh Flugzeugfahrwerk
GB2469804B (en) * 2009-04-27 2013-08-21 Messier Dowty Ltd Bearing assembly
DE102010032546A1 (de) * 2010-07-29 2012-02-02 Liebherr-Aerospace Lindenberg Gmbh Flugzeugstoßdämpfer
JP5579552B2 (ja) * 2010-09-17 2014-08-27 住友精密工業株式会社 航空機用脚装置
CN102020014B (zh) * 2010-12-09 2012-11-21 南京航空航天大学 一种带偏转机轮收放机构的飞机起落架
US8397800B2 (en) 2010-12-17 2013-03-19 Halliburton Energy Services, Inc. Perforating string with longitudinal shock de-coupler
US8393393B2 (en) 2010-12-17 2013-03-12 Halliburton Energy Services, Inc. Coupler compliance tuning for mitigating shock produced by well perforating
US8985200B2 (en) 2010-12-17 2015-03-24 Halliburton Energy Services, Inc. Sensing shock during well perforating
US8397814B2 (en) 2010-12-17 2013-03-19 Halliburton Energy Serivces, Inc. Perforating string with bending shock de-coupler
WO2012148429A1 (en) 2011-04-29 2012-11-01 Halliburton Energy Services, Inc. Shock load mitigation in a downhole perforation tool assembly
US20120241169A1 (en) 2011-03-22 2012-09-27 Halliburton Energy Services, Inc. Well tool assemblies with quick connectors and shock mitigating capabilities
GB2493744B (en) * 2011-08-17 2014-08-27 Messier Dowty Ltd Improved aircraft landing gear assembly and method of manufacture
GB201114437D0 (en) 2011-08-22 2011-10-05 Airbus Operations Ltd Landing gear attachment
US9091152B2 (en) 2011-08-31 2015-07-28 Halliburton Energy Services, Inc. Perforating gun with internal shock mitigation
FR2983829B1 (fr) * 2011-12-07 2014-01-31 Messier Bugatti Dowty Tige d'atterrisseur pour aeronef
US9297228B2 (en) 2012-04-03 2016-03-29 Halliburton Energy Services, Inc. Shock attenuator for gun system
CN103448902A (zh) * 2012-05-29 2013-12-18 中国航空工业集团公司西安飞机设计研究所 一种下单翼飞机的应急断离结构的内襟翼支臂梁及应用
US9598940B2 (en) 2012-09-19 2017-03-21 Halliburton Energy Services, Inc. Perforation gun string energy propagation management system and methods
WO2014046655A1 (en) 2012-09-19 2014-03-27 Halliburton Energy Services, Inc. Perforation gun string energy propagation management with tuned mass damper
US8978817B2 (en) 2012-12-01 2015-03-17 Halliburton Energy Services, Inc. Protection of electronic devices used with perforating guns
US10549848B2 (en) * 2017-04-26 2020-02-04 Safran Landing Systems Canada Inc. Deployable and retractable shock strut
US10591013B2 (en) * 2017-06-14 2020-03-17 Safran Landing Systems Canada Inc. Lubrication mechanism design for aircraft landing gear bearings
US11332238B2 (en) * 2020-03-22 2022-05-17 Aurora Flight Sciences Corporation Energy absorbing landing gear system for a vertical landing apparatus and method of using the same
CN114110081B (zh) * 2021-11-19 2023-09-08 中国直升机设计研究所 一种直升机起落架缓冲器
US20240140597A1 (en) * 2022-10-26 2024-05-02 Safran Landing Systems Canada Inc. Landing gear main fitting with integral shock absorber

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2731218A (en) * 1949-11-10 1956-01-17 Dowty Equipment Ltd Aircraft alighting gear
US3143321A (en) * 1962-07-12 1964-08-04 John R Mcgehee Frangible tube energy dissipation
US3236333A (en) * 1963-06-17 1966-02-22 Lockheed Aircraft Corp Energy absorber
US3997133A (en) * 1975-07-30 1976-12-14 Textron, Inc. Crash attenuation landing gear

Also Published As

Publication number Publication date
WO1996015940A1 (en) 1996-05-30
CA2205489C (en) 2006-11-28
CN1070442C (zh) 2001-09-05
EP0790923A1 (en) 1997-08-27
JPH10508813A (ja) 1998-09-02
EP0790923B1 (en) 1998-09-09
DE69504699T2 (de) 1999-05-06
CA2205489A1 (en) 1996-05-30
DE69504699D1 (de) 1998-10-15
US5547148A (en) 1996-08-20
CN1164213A (zh) 1997-11-05

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Legal Events

Date Code Title Description
FB36 Technical and formal requirements: requirement - article 36 of industrial property law
FF Decision: intention to grant
FG9A Patent or certificate of addition granted
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 18A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2255 DE 25-03-2014 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.