BR112018071564A2 - pivô da alavanca de controle - Google Patents
pivô da alavanca de controleInfo
- Publication number
- BR112018071564A2 BR112018071564A2 BR112018071564-6A BR112018071564A BR112018071564A2 BR 112018071564 A2 BR112018071564 A2 BR 112018071564A2 BR 112018071564 A BR112018071564 A BR 112018071564A BR 112018071564 A2 BR112018071564 A2 BR 112018071564A2
- Authority
- BR
- Brazil
- Prior art keywords
- pivot bearing
- redundant
- primary
- control lever
- bearing
- Prior art date
Links
- 230000007257 malfunction Effects 0.000 abstract 2
- 238000001514 detection method Methods 0.000 abstract 1
- 238000012423 maintenance Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C19/00—Bearings with rolling contact, for exclusively rotary movement
- F16C19/02—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
- F16C19/14—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load
- F16C19/16—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with a single row of balls
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C21/00—Combinations of sliding-contact bearings with ball or roller bearings, for exclusively rotary movement
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
- G05G9/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously
- G05G9/02—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only
- G05G9/04—Manually-actuated control mechanisms provided with one single controlling member co-operating with two or more controlled members, e.g. selectively, simultaneously the controlling member being movable in different independent ways, movement in each individual way actuating one controlled member only in which movement in two or more ways can occur simultaneously
-
- 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
- B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Mechanical Engineering (AREA)
- Mounting Of Bearings Or Others (AREA)
- Pivots And Pivotal Connections (AREA)
- Mechanical Control Devices (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Abstract
a presente invenção refere-se a um pivô da alavanca de controle (200) que compreende um rolamento de pivô primário (210), um rolamento de pivô redundante (220) e um componente de detecção para detectar o mau funcionamento do rolamento de pivô primário. o rolamento de pivô redundante é fornecido em um lado do rolamento de pivô primário. o rolamento de pivô redundante torna-se operativo como um rolamento no caso do mau funcionamento do rolamento de pivô primário. o componente de detecção pode compreender um ou mais recursos (230) fornecidos no rolamento de pivô redundante para aplicação de um torque ao rolamento de pivô redundante durante a manutenção ou teste e/ou um sensor (300; 310; 320) configurado para detectar movimento relativo em uma interface entre o rolamento de pivô primário e o rolamento de pivô redundante.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2016/000670 WO2017182836A1 (en) | 2016-04-22 | 2016-04-22 | Control stick pivot |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112018071564A2 true BR112018071564A2 (pt) | 2019-02-12 |
BR112018071564B1 BR112018071564B1 (pt) | 2023-04-11 |
Family
ID=56116470
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112018071564-6A BR112018071564B1 (pt) | 2016-04-22 | 2016-04-22 | Pivô da alavanca de controle, conjunto de pivô e método para detecção do mau funcionamento de um pivô de alavanca de controle |
Country Status (7)
Country | Link |
---|---|
US (1) | US11084570B2 (pt) |
EP (1) | EP3445647B1 (pt) |
CN (1) | CN109415117A (pt) |
BR (1) | BR112018071564B1 (pt) |
CA (1) | CA3021904A1 (pt) |
RU (1) | RU2708470C1 (pt) |
WO (1) | WO2017182836A1 (pt) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4151523B1 (en) * | 2021-09-17 | 2024-04-17 | Ratier-Figeac SAS | Redundant pivot bearing with mechanical detection |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2475393A (en) * | 1944-02-19 | 1949-07-05 | Kirsch Co | Coupling bearing |
US3429198A (en) | 1967-03-28 | 1969-02-25 | Enstrom Corp | Pivoting spring capsule trim apparatus for helicopter rotor collective pitch control |
BR8707802A (pt) * | 1987-06-15 | 1989-10-17 | Bell Helicopter Textron Inc | Manche desengatavel para controle de aeronave e manche de copiloto com controle ciclico de rapida conexao |
US4865277A (en) * | 1987-06-15 | 1989-09-12 | Bell Helicopter Textron Inc. | Copilot quick connect cyclic stick |
US4811921A (en) | 1987-06-22 | 1989-03-14 | Whitaker Charles N | Cyclic control stick |
US5261291A (en) * | 1992-08-17 | 1993-11-16 | Schoch Paul T | Ergonomic apparatus for controlling a vehicle |
FR2777326B1 (fr) * | 1998-04-09 | 2000-05-12 | Snecma | Procede de liaison a deux degres de liberte en rotation et palier pour mettre en oeuvre le procede |
US6712515B2 (en) * | 2002-01-02 | 2004-03-30 | Intel Corporation | Redundant ball bearing |
DE102006037526A1 (de) * | 2006-08-10 | 2008-02-14 | Linde Material Handling Gmbh | Steuerorgan mit einem Bedienhebel und einer Lagerkugel mit integriertem Permanentmagnet |
US8033197B2 (en) * | 2006-11-20 | 2011-10-11 | Honeywell International Inc. | Fully floating, self-aligning, self-adjusting gimbal assembly for an active human machine interface |
US7740207B2 (en) * | 2007-08-22 | 2010-06-22 | Embraer - Empresa Brasileira De Aeronautica S.A. | Aircraft flight control systems and methods |
CN101910965A (zh) * | 2008-01-14 | 2010-12-08 | 雷马·利普兰特有限及两合公司 | 操纵杆 |
FR2952448B1 (fr) * | 2009-11-06 | 2012-08-03 | Ratier Figeac Soc | Dispositif de controle electronique d'un organe de pilotage a microcontroleurs multifonctionnels, dispositif de pilotage et aeronef |
AT511205B1 (de) * | 2011-06-24 | 2012-10-15 | Iat 21 Innovative Aeronautics Technologies Gmbh | Schwenklager |
EP2597034B1 (en) * | 2011-11-28 | 2015-11-04 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Counterbalanced control stick system |
US9199722B2 (en) * | 2012-10-09 | 2015-12-01 | Robert Dennis Kennedy | Electronic flight controls with parallel processed torque and positioning for pilot or astronaut touch feedback |
FR3001706B1 (fr) * | 2013-02-05 | 2015-03-06 | Midi Ingenierie | Mini-manche de commande electromecanique a retour d'effort |
FR3001707A1 (fr) * | 2013-02-05 | 2014-08-08 | Midi Ingenierie | Mini-manche de commande a retour d'effort |
CN103292995B (zh) * | 2013-05-28 | 2015-07-01 | 常州大学 | 滚动轴承检测及故障诊断的装置与方法 |
CN104565054A (zh) * | 2013-10-24 | 2015-04-29 | 武汉理工大学 | 一种轴向磁力轴承冗余结构 |
US20160122001A1 (en) * | 2014-11-01 | 2016-05-05 | Robert Dennis Kennedy | Electronic flight controls with parallel processed torque & positioning for pilot or astronaut touch feedback |
CN109311531B (zh) * | 2016-04-22 | 2022-08-09 | 拉蒂尔菲雅克股份有限公司 | 三轴控制杆 |
-
2016
- 2016-04-22 CN CN201680084848.4A patent/CN109415117A/zh active Pending
- 2016-04-22 US US16/095,503 patent/US11084570B2/en active Active
- 2016-04-22 EP EP16728091.6A patent/EP3445647B1/en active Active
- 2016-04-22 RU RU2018139016A patent/RU2708470C1/ru active
- 2016-04-22 BR BR112018071564-6A patent/BR112018071564B1/pt active IP Right Grant
- 2016-04-22 WO PCT/IB2016/000670 patent/WO2017182836A1/en active Application Filing
- 2016-04-22 CA CA3021904A patent/CA3021904A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
US20190127081A1 (en) | 2019-05-02 |
EP3445647A1 (en) | 2019-02-27 |
BR112018071564B1 (pt) | 2023-04-11 |
US11084570B2 (en) | 2021-08-10 |
WO2017182836A1 (en) | 2017-10-26 |
EP3445647B1 (en) | 2021-06-02 |
CA3021904A1 (en) | 2017-10-26 |
CN109415117A (zh) | 2019-03-01 |
RU2708470C1 (ru) | 2019-12-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112015019996A2 (pt) | dispositivo e método para controlar um veículo autônomo com uma falha | |
BR112018076865A2 (pt) | protetor auditivo com sensores de monitoramento de posição e som para evitar riscos sonoros proativos | |
BR112015001058A2 (pt) | método e sistema de perfuração de poço | |
BR112017015786A2 (pt) | método de análise do estado operacional de uma máquina, produto de programa de computador e sistema para a análise do estado operacional de uma máquina | |
BR112018076962A2 (pt) | equipamento de proteção individual (epi) com processamento de fluxo analítico para detecção de eventos de segurança | |
BR112015025405A2 (pt) | aparelho de controle numérico | |
BR112015017395A2 (pt) | dispositivos de calibração para um sistema de treinamento de soldagem | |
BR112017019353A2 (pt) | mitigação de desligamento (do) de posicionamento dinâmico (dp) com sistema de navegação inercial | |
BR112017002876A2 (pt) | método de detecção de vírus do computador e sistema deste | |
BR112013009710A2 (pt) | sistema de diagnóstico e método para monitoramento de condições de operação dos componentes de um máquina de turbina | |
BR112012020284A2 (pt) | dispositivo de avaliação de coeficiente aerodinâmico e dispositivo de deteção de falha/danificação de superfície de controle | |
BR112015019746A2 (pt) | sistema de detecção de defeitos na via férrea, sistema para detecção e relatório dos defeitos na via férrea enquanto um trem se desloca sobre as vias da ferrovia, método de detecção de defeitos na via da ferrovia enquanto um veículo ferroviário está em movimento, e, produto de programa de computador | |
BR112018008270A2 (pt) | dispositivo e método de detecção de linha de vaga de estacionamento | |
BR112017025156A2 (pt) | método e aparelho de configuração de posição de parada de veículo | |
BR102014008333B8 (pt) | método e sistema para detectar falhas | |
BR112014011957A2 (pt) | sistema de determinação de estado de sensor | |
BR112017017490A2 (pt) | ?sistemas de controle de bop e métodos relacionados? | |
BR112015032444A2 (pt) | método para diagnosticar uma falha do sistema estabilizador horizontal em uma aeronave | |
BR112018001848A2 (pt) | processo e dispositivo para monitorar o estado de um freio de serviço, bem como freio de serviço e sistema de freio | |
BR112017005761A2 (pt) | dispositivo de controle de movimento e método de controle de movimento | |
BR112012027852A2 (pt) | dispositivo de detecção da ruptura de uma via primária em um acionador de comando de voo | |
BR112013022910A2 (pt) | processo e dispositivo para testar a capacidade de funcionar corretamente de um elevador | |
BR112017009025A2 (pt) | métodos para calibrar dispositivos de computação óptica ou sensores ópticos. | |
BR112012020389A2 (pt) | método para determinar desvios entre sistemas de coordenadas de diferentes sistemas técnicos, objeto de teste, e, dispositivo para cirurgia a lazer oftalmológica | |
BR112016002517A2 (pt) | método de monitorização de uma válvula de um motor de aeronave |
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 4A ANUIDADE. |
|
B08G | Application fees: restoration [chapter 8.7 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B350 | Update of information on the portal [chapter 15.35 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 22/04/2016, OBSERVADAS AS CONDICOES LEGAIS |