BR102015011736A8 - sistemas de detecção de inclinação e de alta sustentação para uma aeronave - Google Patents

sistemas de detecção de inclinação e de alta sustentação para uma aeronave

Info

Publication number
BR102015011736A8
BR102015011736A8 BR102015011736A BR102015011736A BR102015011736A8 BR 102015011736 A8 BR102015011736 A8 BR 102015011736A8 BR 102015011736 A BR102015011736 A BR 102015011736A BR 102015011736 A BR102015011736 A BR 102015011736A BR 102015011736 A8 BR102015011736 A8 BR 102015011736A8
Authority
BR
Brazil
Prior art keywords
tilt
aircraft
high lift
detection systems
lift detection
Prior art date
Application number
BR102015011736A
Other languages
English (en)
Other versions
BR102015011736A2 (pt
BR102015011736B1 (pt
Inventor
Tony Jones
Original Assignee
Goodrich Actuation Systems 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 Goodrich Actuation Systems Ltd filed Critical Goodrich Actuation Systems Ltd
Publication of BR102015011736A2 publication Critical patent/BR102015011736A2/pt
Publication of BR102015011736A8 publication Critical patent/BR102015011736A8/pt
Publication of BR102015011736B1 publication Critical patent/BR102015011736B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/0005—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear
    • B64D2045/001—Devices specially adapted to indicate the position of a movable element of the aircraft, e.g. landing gear for indicating symmetry of flaps deflection

Abstract

sistemas de detecção de inclinação e de alta sustentação para uma aeronave. um sistema de detecção de inclinação para um sistema de alta sustentação para uma aeronave, em que os pares de sensores 4a, 4b fornecem uma determinação integrada da inclinação relativa entre os sensores de cada par como uma indicação da inclinação de um flape do sistema de alta sustentação.
BR102015011736-1A 2014-07-07 2015-05-21 Sistemas de detecção de inclinação e de alta sustentação para uma aeronave BR102015011736B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP14176001.7 2014-07-07
EP14176001.7A EP2965993B1 (en) 2014-07-07 2014-07-07 Skew sensing arrangement

Publications (3)

Publication Number Publication Date
BR102015011736A2 BR102015011736A2 (pt) 2016-03-08
BR102015011736A8 true BR102015011736A8 (pt) 2016-03-29
BR102015011736B1 BR102015011736B1 (pt) 2021-10-26

Family

ID=51211529

Family Applications (1)

Application Number Title Priority Date Filing Date
BR102015011736-1A BR102015011736B1 (pt) 2014-07-07 2015-05-21 Sistemas de detecção de inclinação e de alta sustentação para uma aeronave

Country Status (4)

Country Link
US (1) US9656764B2 (pt)
EP (1) EP2965993B1 (pt)
BR (1) BR102015011736B1 (pt)
CA (1) CA2891585C (pt)

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DE102013013340B4 (de) * 2013-08-09 2023-08-10 Liebherr-Aerospace Lindenberg Gmbh Klappensystem für ein Flugzeughochauftriebsystem oder eine Triebwerksaktuation und Verfahren zur Überwachung eines Klappensystems
US20170305530A1 (en) * 2016-04-25 2017-10-26 The Boeing Company System and method for controlling aircraft wing flap motion
EP3339165B1 (en) 2016-12-22 2020-09-09 Goodrich Actuation Systems Limited Wing slat actuator disconnection detection
US10690520B2 (en) 2017-02-27 2020-06-23 The Boeing Company Apparatus, system, and method for determining a position of a part
US10137999B2 (en) * 2017-03-30 2018-11-27 The Boeing Company Methods and apparatus for detecting airflow control surface skew conditions
GB2563242B (en) 2017-06-07 2020-01-29 Ge Aviat Systems Ltd A method and system for enabling component monitoring redundancy in a digital network of intelligent sensing devices
CA2972608A1 (en) * 2017-06-29 2018-12-29 Bombardier Inc. Slat skew detection system and method
CN107963227B (zh) * 2017-11-08 2020-10-27 中国航空工业集团公司金城南京机电液压工程研究中心 一种双发直升机燃油系统显示控制面板
EP3505451A1 (en) * 2017-12-29 2019-07-03 Airbus Operations GmbH Flight control surface assembly
US11338904B2 (en) 2018-05-23 2022-05-24 Airbus Operations Gmbh Flight control surface assembly
CN113661121A (zh) 2019-01-09 2021-11-16 穆格伍尔弗汉普顿有限公司 飞行器操纵面元件监测系统
US11023695B2 (en) * 2019-05-28 2021-06-01 Airbus Canada Limited Partnership System and method for determining a skew level
CN113650796A (zh) * 2021-09-10 2021-11-16 庆安集团有限公司 一种缝翼倾斜监控方法及装置
US20230159183A1 (en) * 2021-11-19 2023-05-25 The Boeing Company Systems and methods for detecting a jam of a flap of a wing of an aircraft

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
US5686907A (en) * 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
US5680124A (en) 1995-05-15 1997-10-21 The Boeing Company Skew and loss detection system for adjacent high lift devices
US6299108B1 (en) * 1997-12-12 2001-10-09 Jeffrey V. Lindstrom Method and apparatus for detecting skew and asymmetry of an airplane flap
FR2787652B1 (fr) * 1998-12-18 2001-05-18 Sextant Avionique Dispositif d'acquisition d'etats logiques de multiples capteurs
US6382566B1 (en) * 1998-12-29 2002-05-07 The Boeing Company Method and apparatus for detecting skew and asymmetry of an airplane flap
US7921729B2 (en) * 2008-03-10 2011-04-12 Hamilton Sundstrand Corporation Disconnect sensor
US8527240B2 (en) * 2008-03-26 2013-09-03 United Technologies Corporation Wireless sensor assembly for an aircraft component
US7945425B2 (en) 2008-10-17 2011-05-17 The Boeing Company In-flight detection of wing flap free wheeling skew
US8115649B2 (en) * 2009-04-30 2012-02-14 The Boeing Company Slat skew detection system
DE102009020840A1 (de) * 2009-05-12 2010-11-25 Liebherr-Aerospace Lindenberg Gmbh Flugzeughochauftriebssystem sowie Verfahren zur Ermittlung eines Betriebszustandes eines Flugzeughochauftriebssystems
DE102009053126A1 (de) * 2009-11-13 2011-05-19 Airbus Operations Gmbh Stellsystem eines Flugzeugs mit einer Stellklappe
GB0919988D0 (en) 2009-11-16 2009-12-30 Goodrich Actuation Systems Ltd Skew detection
GB201004026D0 (en) * 2010-03-10 2010-04-28 Airbus Operations Ltd Slat monitoring system
BE1019359A3 (fr) * 2010-06-04 2012-06-05 Sonaca Sa Desalignement de surfaces portantes.
US20130009017A1 (en) * 2011-07-06 2013-01-10 Eaton Corporation Electronically synchronized flap system
US9354324B2 (en) * 2011-10-20 2016-05-31 Qualcomm Incorporated Techniques for affecting a wireless signal-based positioning capability of a mobile device based on one or more onboard sensors
US9073643B2 (en) * 2013-03-28 2015-07-07 The Boeing Company Monitoring of high-lift systems for aircraft
EP2803584B1 (en) * 2013-05-17 2015-09-16 Airbus Operations GmbH Actuation system for flight control surface

Also Published As

Publication number Publication date
BR102015011736A2 (pt) 2016-03-08
CA2891585A1 (en) 2016-01-07
BR102015011736B1 (pt) 2021-10-26
EP2965993A1 (en) 2016-01-13
US9656764B2 (en) 2017-05-23
US20160001894A1 (en) 2016-01-07
CA2891585C (en) 2022-12-06
EP2965993B1 (en) 2017-08-30

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
B03H Publication of an application: rectification [chapter 3.8 patent gazette]

Free format text: REFERENTE A RPI 2357 DE 08/03/2016, QUANTO AO ITEM FIGURA.

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 21/05/2015, OBSERVADAS AS CONDICOES LEGAIS.