BRPI0418976A - sensor de peso sobre o trem de pouso - Google Patents

sensor de peso sobre o trem de pouso

Info

Publication number
BRPI0418976A
BRPI0418976A BRPI0418976-0A BRPI0418976A BRPI0418976A BR PI0418976 A BRPI0418976 A BR PI0418976A BR PI0418976 A BRPI0418976 A BR PI0418976A BR PI0418976 A BRPI0418976 A BR PI0418976A
Authority
BR
Brazil
Prior art keywords
centerline
center member
displacement sensor
weight sensor
landing gear
Prior art date
Application number
BRPI0418976-0A
Other languages
English (en)
Inventor
James Grant Mast
Charles Eric Covington
Paul Eugene Darden
William L Mckeown
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0418976A publication Critical patent/BRPI0418976A/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 
    • B64C25/52—Skis or runners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/001—Devices not provided for in the groups B64C25/02 - B64C25/68
    • 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 
    • B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

SENSOR DE PESO SOBRE O TREM DE POUSO. Revela-se um sensor de peso sobre o trem de pouso para uso em uma aeronave com esquis de pouso possuindo um suporte e um sensor de deslocamento ligado ao suporte. O suporte possui um membro central que conecta um primeiro membro de extremidade a um segundo membro de extremidade. O membro central possui uma linha central e os membros de extremidade se estendem a partir da linha central do membro central. Membros de montagem se estendem ao longo da linha central do membro central para facilitar a ligação do suporte a um tubo transversal. O sensor de deslocamento conecta o primeiro membro de extremidade ao segundo membro de extremidade. O sensor de deslocamento é paralelo à, e afastado da linha central do membro central de modo que, quando um momento de curvatura for aplicado ao membro central, o primeiro sensor de deslocamento seja alongado ou encurtado.
BRPI0418976-0A 2004-08-10 2004-08-10 sensor de peso sobre o trem de pouso BRPI0418976A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2004/025821 WO2006022700A1 (en) 2004-08-10 2004-08-10 Weight-on-gear sensor

Publications (1)

Publication Number Publication Date
BRPI0418976A true BRPI0418976A (pt) 2007-12-11

Family

ID=35967781

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0418976-0A BRPI0418976A (pt) 2004-08-10 2004-08-10 sensor de peso sobre o trem de pouso

Country Status (7)

Country Link
US (2) US7637459B2 (pt)
EP (1) EP1776270B1 (pt)
CN (1) CN100441479C (pt)
BR (1) BRPI0418976A (pt)
CA (1) CA2574191C (pt)
DE (1) DE04786485T1 (pt)
WO (1) WO2006022700A1 (pt)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2891240B1 (fr) * 2005-09-28 2007-12-07 Eurocopter France Atterisseur a patins anti-resonnance pour aeronef a voilure tournante, et aeronef
US8366037B2 (en) * 2009-05-22 2013-02-05 Heliplane, Llc Towable aerovehicle system with automated tow line release
US8540183B2 (en) * 2009-12-12 2013-09-24 Heliplane, Llc Aerovehicle system including plurality of autogyro assemblies
DE102010020445B4 (de) * 2010-05-12 2019-04-04 Deutsches Zentrum für Luft- und Raumfahrt e.V. Bodenkontakterkennung
EP2397406B1 (en) * 2010-06-14 2019-08-07 Airbus Defence and Space SA Pin bearing arrangement for aircraft landing gear
US8646719B2 (en) * 2010-08-23 2014-02-11 Heliplane, Llc Marine vessel-towable aerovehicle system with automated tow line release
EP2450677B1 (en) 2010-11-09 2014-01-22 Eurocopter Deutschland GmbH Helicopter weighing system and method of operating such a weighing system
CA2842596C (en) * 2011-08-02 2017-01-03 Bell Helicopter Textron Inc. Skid landing gear system
US8662442B2 (en) * 2011-11-01 2014-03-04 Textron Innovations Inc. Active prop rotor stability system
US9354635B2 (en) 2012-06-05 2016-05-31 Textron Innovations Inc. Takeoff/landing touchdown protection management system
US20130341461A1 (en) * 2012-06-26 2013-12-26 Bell Helicopter Textron Inc. Lightweight Helicopter Skid Shoes
FR3035978A1 (fr) * 2015-05-04 2016-11-11 Airbus Helicopters Systeme de commande de giravion, giravion associe et methode de commande correspondante
EP3375708A1 (en) 2017-03-17 2018-09-19 Safran Landing Systems UK Limited Aircraft landing gear assembly
WO2019007528A1 (en) * 2017-07-07 2019-01-10 Volvo Truck Corporation CHARGE SENSOR ASSEMBLY FOR VEHICLE AXLE
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
DE102020109854A1 (de) 2020-04-08 2021-10-14 Audi Aktiengesellschaft Verfahren zur Transportsteuerung und gemäß dem Verfahren steuerbares Transportsystem mit zumindest einem Luftfahrzeug
EP3961177B1 (en) * 2020-08-25 2022-06-15 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A measurement apparatus for determining a bending moment
DE102020134583B4 (de) 2020-12-22 2024-04-25 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schutz von Hubschraubern gegen Dynamic Rollover
US20230373650A1 (en) * 2022-05-23 2023-11-23 Safran Landing Systems Canada Inc. Landing gear load measurement system

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4020911A (en) * 1973-08-10 1977-05-03 Structural Instrumentation, Inc. Load cell scale
BR7905238A (pt) * 1978-08-16 1980-05-06 Toft Bros Ind Ltd Metodo e aparelho para colheita de cana de acucar
US4215754A (en) * 1978-11-20 1980-08-05 Structural Instrumentation, Inc. Load measuring system for leaf spring suspensions
US4270711A (en) * 1979-01-29 1981-06-02 Textron, Inc. Helicopter landing gear with crosstube pivot
US4269070A (en) 1979-09-28 1981-05-26 Weico Corporation Strain/deflection sensitive variable reluctance transducer assembly
FR2520870A1 (fr) * 1982-01-29 1983-08-05 Sfena Dispositif permettant de mesurer la charge repartie sur les moyens de roulement d'un train d'atterrissage d'un aeronef
US4574360A (en) 1983-04-01 1986-03-04 Sundstrand Data Control, Inc. Helicopter weight measuring system
FR2586806B1 (fr) 1985-08-27 1988-07-29 Sfena Dispositif de montage de capteur de deplacement relatif sur une poutre munie d'oreilles radiales
JPH01503530A (ja) * 1987-04-29 1989-11-30 ベル、ヘリカプタ、テクストロン、インコーパレイテイド 着陸装置荷重変換器
WO1991004908A1 (en) 1989-10-03 1991-04-18 Bell Helicopter Textron Inc. Self-adjusting slide assembly for weight on gear switch
DE4112674A1 (de) 1990-09-13 1992-03-19 Vdo Schindling Anordnung von sensoren an dem fahrwerk eines flugkoerpers zur messung von gewicht und schwerpunktlage des flugkoerpers
DE4112675A1 (de) 1990-10-20 1992-04-23 Vdo Schindling Anordnung mindestens eines sensors an dem fahrwerk eines flugzeugs zur messung dessen gewichts und schwerpunktlage
GB9828475D0 (en) * 1998-12-24 1999-02-17 British Aerospace Load measurement
JP2001296175A (ja) * 2000-02-13 2001-10-26 Yazaki Corp 車両用荷重測定装置

Also Published As

Publication number Publication date
US8226030B2 (en) 2012-07-24
US20100095788A1 (en) 2010-04-22
DE04786485T1 (de) 2007-10-11
EP1776270B1 (en) 2013-05-29
CN100441479C (zh) 2008-12-10
CA2574191A1 (en) 2006-03-02
EP1776270A1 (en) 2007-04-25
US7637459B2 (en) 2009-12-29
EP1776270A4 (en) 2012-07-18
CN1997550A (zh) 2007-07-11
US20070228210A1 (en) 2007-10-04
CA2574191C (en) 2010-07-13
WO2006022700A1 (en) 2006-03-02

Similar Documents

Publication Publication Date Title
BRPI0418976A (pt) sensor de peso sobre o trem de pouso
UA97475C2 (uk) Пілон підвіски двигуна під крилом літака
BR9709056A (pt) Sistema de suspensão para emprego com um veìculo que tem um chassi.
BR112016023808A8 (pt) veículo
BRPI0516357A (pt) sistema para fixar montante de motor de avião
BRPI0401809A (pt) Dispositivo de fixação dianteiro de motor de avião
FR2915173B1 (fr) Dispositif de fixation d'un organe de sustentation au fuselage d'un avion.
BRPI1008978A2 (pt) avião com empenagem em cauda de bacalhau e motor traseiro
ATE519674T1 (de) Motorbefestigung eines zwischen einer befestigungsstrebe und einem flugzeugtriebwerk angebrachten montagesystems
EP2977316B1 (en) Aircraft landing gear
BR112014016660A2 (pt) conjunto absorvedor de energia para absorção de energia de impacto; veículo; e sistema para absorção de energia de impacto
US9555877B2 (en) Landing gear
BRPI0709570B8 (pt) Método para aumentar a altura de passeio de uma aeronave
EP2208670A3 (en) A nose landing gear arrangement for an aircraft and an aircraft having such an arrangement
BR112015014717A2 (pt) veículo de trabalho e sistema de suspensão de cabine para acoplar uma armação de cabine a uma armação de chassi de um veículo de trabalho
WO2009106871A3 (en) Aerodynamic structure with non-uniformly spaced shock bumps
DE602005000155D1 (de) Aufhängevorrichtung eines Flugzeugtriebwerks an einem Flügelpylon
BR112013032919A2 (pt) "junta telescópica de riser, unidade de conduto pescoço de ganso para uma junta telescópica e sistema"
BR0110910A (pt) Asa em veìculo de efeito terrestre com chapas de extremidade
BR112012031627A2 (pt) turbomotor fixado a um pilar de fuselagem de uma aeronave por uma suspensão com segurança integrada
FR2805799B1 (fr) Atterisseur d'aeronef a axe de pivotement de jambe fortement deporte
BR112016001865A2 (pt) dispositivo de suspensão telescópica encaixado em um sistema de rastreamento de pré-tensão
BR112015013283A2 (pt) unidade de acionamento de roda para afixação a um trem de rolamento de aeronave
BR0212337A (pt) Mecanismo de suporte de roda de aeronave
FR2960214B1 (fr) Train d'atterrissage monte sous une aile d'aeronef.

Legal Events

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

Free format text: REFERENTE A 11A ANUIDADE.

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 2318 DE 09-06-2015 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.