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BRPI0818602A2 - Detecção de carga em um trem de pouso de aeronave - Google Patents

Detecção de carga em um trem de pouso de aeronave

Info

Publication number
BRPI0818602A2
BRPI0818602A2 BRPI0818602A BRPI0818602A2 BR PI0818602 A2 BRPI0818602 A2 BR PI0818602A2 BR PI0818602 A BRPI0818602 A BR PI0818602A BR PI0818602 A2 BRPI0818602 A2 BR PI0818602A2
Authority
BR
Brazil
Prior art keywords
landing gear
load detection
aircraft landing
aircraft
load
Prior art date
Application number
Other languages
English (en)
Inventor
Ian Bennett
Original Assignee
Messier Dowty Ltd
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 Messier Dowty Ltd filed Critical Messier Dowty Ltd
Publication of BRPI0818602A2 publication Critical patent/BRPI0818602A2/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 
    • B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface  wheeled type, e.g. multi-wheeled bogies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • 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
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
    • F16F9/32—Details
    • F16F9/3264—Arrangements for indicating, e.g. fluid level; Arrangements for checking dampers
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L23/00—Devices or apparatus for measuring or indicating or recording rapid changes, such as oscillations, in the pressure of steam, gas, or liquid; Indicators for determining work or energy of steam, internal-combustion, or other fluid-pressure engines from the condition of the working fluid
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/008—Devices for detecting or indicating hard landing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Vehicle Body Suspensions (AREA)
  • Fluid-Damping Devices (AREA)
BRPI0818602 2007-10-09 2008-10-13 Detecção de carga em um trem de pouso de aeronave BRPI0818602A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0719732.0A GB2453554B (en) 2007-10-09 2007-10-09 Load detection in an aircraft landing gear
PCT/EP2008/063743 WO2009047367A2 (en) 2007-10-09 2008-10-13 Load detection in an aircraft landing gear

Publications (1)

Publication Number Publication Date
BRPI0818602A2 true BRPI0818602A2 (pt) 2015-04-22

Family

ID=38787879

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0818602 BRPI0818602A2 (pt) 2007-10-09 2008-10-13 Detecção de carga em um trem de pouso de aeronave

Country Status (10)

Country Link
US (1) US20100288878A1 (pt)
EP (1) EP2195237B1 (pt)
JP (1) JP5252514B2 (pt)
CN (1) CN101821162B (pt)
BR (1) BRPI0818602A2 (pt)
ES (1) ES2408006T3 (pt)
GB (1) GB2453554B (pt)
IL (1) IL204797A0 (pt)
RU (1) RU2478525C2 (pt)
WO (1) WO2009047367A2 (pt)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2452938B (en) * 2007-09-19 2011-08-10 Messier Dowty Ltd Load indicator
GB2465397C (en) * 2008-11-17 2013-04-10 Messier Dowty Ltd Load indicator
GB2469804B (en) 2009-04-27 2013-08-21 Messier Dowty Ltd Bearing assembly
US7946165B2 (en) * 2009-05-05 2011-05-24 Goodrich Corporation Over-speed, rough loads and hard landing detection system
US8903572B1 (en) * 2009-08-11 2014-12-02 The Boeing Company Aircraft landing evaluation system
US8616146B2 (en) * 2010-03-05 2013-12-31 Goodrich Corporation System for indicating an airplane hard landing
US8448900B2 (en) * 2010-03-24 2013-05-28 The Boeing Company Semi-levered landing gear and associated method
FR2959207B1 (fr) * 2010-04-26 2012-04-20 Eurocopter France Systeme a absortion d'energie pour un atterisseur, et aeronef muni dudit systeme a absorption d'energie
US8933713B2 (en) * 2010-07-19 2015-01-13 Goodrich Corporation Capacitive sensors for monitoring loads
GB2483472B (en) * 2010-09-08 2012-08-15 Messier Dowty Ltd Aircraft landing gear
US10131419B2 (en) 2010-10-15 2018-11-20 Goodrich Corporation Systems and methods for detecting landing gear ground loads
US9481452B2 (en) 2010-11-22 2016-11-01 The Boeing Company Hydraulic actuator for semi levered landing gear
GB2485803B (en) * 2010-11-24 2013-02-06 Messier Dowty Ltd Mechanical position indicator
US8939400B2 (en) 2011-02-21 2015-01-27 The Boeing Company Air-ground detection system for semi-levered landing gear
US8862377B2 (en) * 2011-03-31 2014-10-14 Sikorsky Aircraft Corporation Method and system for detecting forces on aircraft
US8998133B2 (en) * 2011-04-01 2015-04-07 The Boeing Company Landing gear system
GB2489058B (en) * 2011-08-22 2013-05-08 Messier Dowty Ltd Aircraft landing gear
GB2496426B (en) 2011-11-11 2013-12-25 Messier Dowty Ltd Gauge
FR2983829B1 (fr) * 2011-12-07 2014-01-31 Messier Bugatti Dowty Tige d'atterrisseur pour aeronef
CN103258105A (zh) * 2012-02-17 2013-08-21 中国航空工业集团公司沈阳飞机设计研究所 一种飞机起落架寿命消耗计算方法
CN103523210A (zh) * 2012-07-06 2014-01-22 哈尔滨飞机工业集团有限责任公司 前起落架摩擦减摆装置
CN103818548B (zh) * 2012-11-16 2016-08-10 哈尔滨飞机工业集团有限责任公司 自适应全地形直升机起落架装置
CN103033380B (zh) * 2012-12-11 2015-07-01 中国飞机强度研究所 一种起落架收放试验加载方法
GB2510412C (en) * 2013-02-04 2021-08-25 Messier Dowty Ltd Aircraft landing gear pitch trimmer actuator with variable damping
KR200467824Y1 (ko) 2013-02-21 2013-07-05 (주) 코마코 항공기의 랜딩기어 레버
US9221556B2 (en) * 2013-10-29 2015-12-29 The Boeing Company Airplane off ground advisory system
CN103983438B (zh) * 2014-04-17 2017-02-01 中国航空工业集团公司沈阳飞机设计研究所 一种飞机转弯操纵系统寿命试验方法
US9652902B2 (en) * 2014-07-24 2017-05-16 Goodrich Corporation Pitch trim actuator servicing monitoring system
GB2532270B (en) * 2014-11-14 2017-05-10 Ge Aviat Systems Ltd An aircraft assembly with load and position indicator
CN105438497A (zh) * 2015-11-26 2016-03-30 中国航空工业集团公司沈阳飞机设计研究所 一种电驱动起落架加载装置
CN105607524B (zh) * 2016-03-16 2018-04-13 中国飞机强度研究所 一种主起假轮垂向传感器输出信号切换控制器
EP3248869B1 (en) * 2016-05-25 2018-09-12 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Retraction / extension of a landing gear in an aircraft
US10384769B2 (en) 2017-01-06 2019-08-20 Goodrich Corporation Two stage strut allowing low initial compression load
US10384767B2 (en) * 2017-01-25 2019-08-20 The Boeing Company Single axle, semi-levered landing gear with shortening mechanism
FR3062636B1 (fr) * 2017-02-03 2021-04-16 Safran Landing Systems Atterrisseur d'aeronef
US10625849B2 (en) * 2017-04-11 2020-04-21 The Boeing Company Levered landing gear with inner shock strut
US10549848B2 (en) * 2017-04-26 2020-02-04 Safran Landing Systems Canada Inc. Deployable and retractable shock strut
GB2569768A (en) * 2017-05-15 2019-07-03 Airbus Operations Ltd Shock absorber dimension
GB2562781A (en) * 2017-05-25 2018-11-28 Airbus Operations Ltd Landing gear bogie pitch trimmer
US10800516B2 (en) 2017-06-02 2020-10-13 The Boeing Company Semi-levered shrink landing gear
GB2563948A (en) 2017-06-30 2019-01-02 Airbus Operations Ltd Aircraft landing gear assembly
GB2563949A (en) * 2017-06-30 2019-01-02 Airbus Operations Ltd Aircraft landing gear assembly
GB2563945A (en) * 2017-06-30 2019-01-02 Airbus Operations Ltd Aircraft landing gear assembly
FR3072943B1 (fr) * 2017-10-27 2021-12-10 Safran Landing Systems Atterrisseur d'aeronef a roues freinees et roues motorisees
US11161599B2 (en) 2018-01-26 2021-11-02 The Boeing Company Landing gear strut assembly and method therefor
US10981646B2 (en) 2018-07-30 2021-04-20 The Boeing Company Landing gear shrink link mechanism
US10625876B2 (en) * 2018-08-08 2020-04-21 Aurora Flight Sciences Corporation Aircraft landing systems and methods for monitoring a vertical landing of an aircraft
CA3060756A1 (en) * 2018-11-07 2020-05-07 Bombardier Inc. Hard landing indicator for an aircraft landing gear
CN109606713B (zh) * 2018-12-03 2022-08-02 江西洪都航空工业集团有限责任公司 一种纯机械式重着陆指示结构
CN109684678B (zh) * 2018-12-04 2023-04-18 中国航空工业集团公司西安飞机设计研究所 全机疲劳试验多轮多支柱起落架疲劳载荷优化处理方法
CN109506819B (zh) * 2018-12-13 2020-06-05 贵州贵航飞机设计研究所 一种飞机着陆时起落架冲击载荷的监控方法
CN110274823B (zh) * 2019-06-28 2020-07-24 郑州航空工业管理学院 机场跑道试飞实验装置
CN111097716B (zh) * 2019-12-25 2022-05-10 昆山孚思格机电科技有限公司 一种链式测力分选机基准端伸出驱动和过载保护方法
GB2602150A (en) * 2020-12-21 2022-06-22 Airbus Operations Ltd An aircraft landing gear
CN114510066B (zh) * 2022-01-26 2022-11-08 广东工业大学 一种倾转旋翼重载物流无人机控制系统
US11939045B2 (en) * 2022-04-27 2024-03-26 The Boeing Company Landing gear assembly for an aircraft, a landing gear system, and a method
US11892052B2 (en) * 2022-05-06 2024-02-06 Goodrich Corporation Temperature compensated shock strut visual health indicator systems and methods
CN114705470B (zh) * 2022-06-07 2022-08-26 中国飞机强度研究所 飞机耐冲击强度测试试验的冲击加载系统及其加载方法
US12043408B2 (en) * 2022-12-05 2024-07-23 Goodrich Corporation Aircraft hard landing indicator
CA3218700A1 (en) * 2022-12-05 2024-06-05 Goodrich Corporation Aircraft hard landing indicator

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2579180A (en) * 1949-03-15 1951-12-18 Cons Vultee Aircraft Corp Tandem-wheel shock absorbing aircraft landing gear
US2826381A (en) * 1954-03-26 1958-03-11 Lockheed Aircraft Corp Landing gear for aircraft
GB1006522A (en) * 1963-10-08 1965-10-06 Electro Hydraulics Ltd Retractable undercarriages for aircraft
GB1510554A (en) 1976-03-31 1978-05-10 British Aircraft Corp Ltd Aircraft undercarriage unit
CA1127191A (en) * 1978-10-13 1982-07-06 L. Dale Coad Viscous spring damper
US4296897A (en) * 1979-01-22 1981-10-27 The Boeing Company Brake torque limiter
FR2616410B1 (fr) * 1987-06-09 1992-08-21 Messier Hispano Sa Dispositif d'atterrissage a poutre basculante
CA2129521C (en) * 1992-02-07 2003-04-15 C. Kirk Nance Aircraft weight and center of gravity indicator
FR2699886B1 (fr) * 1992-12-28 1995-03-24 Messier Bugatti Atterrisseur relevable, notamment pour avion gros porteur.
CN2309284Y (zh) * 1997-07-08 1999-03-03 马金山 一种飞机起落架的减震支柱
IL138399A (en) * 1998-03-19 2004-01-04 Goodrich Co B F Dual-mode operator for the main beam of an airplane pedestrian
US6182925B1 (en) * 1999-03-30 2001-02-06 The Boeing Company Semi-levered landing gear and auxiliary strut therefor
US6575405B2 (en) * 1999-03-30 2003-06-10 The Boeing Company Control system and method for a semi-levered landing gear for an aircraft
JP2003054496A (ja) * 2001-08-09 2003-02-26 Mitsubishi Heavy Ind Ltd 航空機の脚部構造
US6676075B2 (en) * 2001-08-30 2004-01-13 The Boeing Company Airplane hard landing indication system
US7274310B1 (en) * 2005-03-29 2007-09-25 Nance C Kirk Aircraft landing gear kinetic energy monitor
US7193530B2 (en) * 2005-03-29 2007-03-20 Nance C Kirk Aircraft landing gear automated inspection and life limitation escalation system and method
CA2509742A1 (en) * 2005-06-10 2006-12-10 Messier-Dowty Inc. System and method for determining aircraft hard landing events from inertial and aircraft reference frame data
GB0515359D0 (en) * 2005-07-26 2005-08-31 Airbus Uk Ltd Landing gear
GB2428650B (en) * 2005-08-04 2011-01-12 Messier Dowty Ltd Landing gear
GB0517351D0 (en) * 2005-08-24 2005-10-05 Airbus Uk Ltd Landing load monitor for aircraft landing gear
US7815143B2 (en) * 2006-08-11 2010-10-19 The Boeing Company Aircraft landing gear truck orientation for noise reduction

Also Published As

Publication number Publication date
GB2453554A (en) 2009-04-15
JP5252514B2 (ja) 2013-07-31
WO2009047367A2 (en) 2009-04-16
GB0719732D0 (en) 2007-11-21
CN101821162A (zh) 2010-09-01
CN101821162B (zh) 2013-06-05
US20100288878A1 (en) 2010-11-18
IL204797A0 (en) 2010-11-30
EP2195237B1 (en) 2013-02-27
WO2009047367A3 (en) 2009-11-12
RU2478525C2 (ru) 2013-04-10
ES2408006T3 (es) 2013-06-17
GB2453554B (en) 2012-03-14
EP2195237A2 (en) 2010-06-16
RU2010113906A (ru) 2011-11-20
JP2011504829A (ja) 2011-02-17

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Legal Events

Date Code Title Description
B15I Others concerning applications: loss of priority

Free format text: PERDA DA PRIORIDADE GB0719732.0 DE 09/10/2007 REIVINDICADA NO PCT/EP2008/063743, CONFORME AS DISPOSICOES PREVISTAS NA LEI 9.279 DE 14/05/1996 (LPI) ART. 16 7O, DECRETO NO. 635 DE 21/08/1992 E CONVENCAO DA UNIAO DE PARIS (REVISTA EM ESTOCOLMO 14/07/1967), ART. 4O, ALINEA C, ITEM 1. ESTA PERDA SE DEU PELO FATO DO BRASIL NAO ACEITAR RESTAURACAO DE PRIORIDADE (RESERVA DO BRASIL DE ACORDO COM A REGRA 49TER.1 ALINEA (G) E 49TER.2 ALINEA (H) DO REGULAMENTO DE EXECUCAO DO PCT), RESTAURACAO ESTA QUE FOI CONCEDIDA PELA OMPI, JA QUE O PRAZO PARA O DEPOSITO INTERNACIONAL COM REIVINDICACAO DE PRIORIDADE ULTRAPASSOU OS 12 MESES.

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 6A E 7A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.