DE69425058D1 - Aktive kurzsteuerknüppel mit mechanischer verbindung - Google Patents
Aktive kurzsteuerknüppel mit mechanischer verbindungInfo
- Publication number
- DE69425058D1 DE69425058D1 DE69425058T DE69425058T DE69425058D1 DE 69425058 D1 DE69425058 D1 DE 69425058D1 DE 69425058 T DE69425058 T DE 69425058T DE 69425058 T DE69425058 T DE 69425058T DE 69425058 D1 DE69425058 D1 DE 69425058D1
- Authority
- DE
- Germany
- Prior art keywords
- mechanical connection
- active short
- short stick
- stick
- active
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
Links
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
- B64C13/12—Dual control apparatus
-
- 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
- B64C13/10—Initiating means actuated personally comprising warning devices
-
- 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
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
- B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
- B64C13/30—Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
-
- 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
- G05G9/047—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 the controlling member being movable by hand about orthogonal axes, e.g. joysticks
- G05G2009/04766—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 the controlling member being movable by hand about orthogonal axes, e.g. joysticks providing feel, e.g. indexing means, means to create counterforce
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/095,870 US5456428A (en) | 1993-07-21 | 1993-07-21 | Mechanically linked active sidesticks |
PCT/US1994/008121 WO1995003212A1 (en) | 1993-07-21 | 1994-07-19 | Mechanically linked active sidesticks |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69425058D1 true DE69425058D1 (de) | 2000-08-03 |
DE69425058T2 DE69425058T2 (de) | 2001-03-08 |
Family
ID=22253962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69425058T Expired - Fee Related DE69425058T2 (de) | 1993-07-21 | 1994-07-19 | Aktive kurzsteuerknüppel mit mechanischer verbindung |
Country Status (5)
Country | Link |
---|---|
US (1) | US5456428A (de) |
EP (1) | EP0708726B1 (de) |
JP (1) | JPH09501371A (de) |
DE (1) | DE69425058T2 (de) |
WO (1) | WO1995003212A1 (de) |
Families Citing this family (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5694014A (en) * | 1995-08-22 | 1997-12-02 | Honeywell Inc. | Active hand controller redundancy and architecture |
US5806806A (en) * | 1996-03-04 | 1998-09-15 | Mcdonnell Douglas Corporation | Flight control mechanical backup system |
FR2754515B1 (fr) * | 1996-10-14 | 1998-12-24 | Aerospatiale | Dispositif d'aide au pilotage sur un aeronef a commande de vol electrique |
FR2756392B1 (fr) | 1996-11-22 | 1999-01-22 | Aerospatiale | Systeme de couplage de manches de commande |
FR2771071B1 (fr) * | 1997-11-14 | 2000-01-07 | Eurocopter France | Dispositif pour actionner un organe commande sur un aeronef a voilure tournante, notamment un helicoptere |
US6572055B1 (en) * | 1999-08-10 | 2003-06-03 | Bombardier Aerospace Corporation | Hydrostatic sidestick coupling |
US6459228B1 (en) | 2001-03-22 | 2002-10-01 | Mpc Products Corporation | Dual input servo coupled control sticks |
CA2347556A1 (en) * | 2001-05-10 | 2002-11-10 | Bombardier Inc. | Unknown |
JP3923774B2 (ja) | 2001-10-16 | 2007-06-06 | アルプス電気株式会社 | 力覚付入力装置 |
WO2003040844A2 (en) * | 2001-11-06 | 2003-05-15 | Bombardier Inc. | Apparatus for controlling a joystick having force-feedback |
US6880855B2 (en) * | 2003-01-06 | 2005-04-19 | General Motors Corporation | Rotary driver control input device |
DE10305261A1 (de) * | 2003-02-07 | 2004-08-26 | Wittenstein Ag | Vorrichtung zum Steuern eines Fahrzeuges |
US6913226B2 (en) * | 2003-10-30 | 2005-07-05 | The Boeing Company | Methods and systems for redundant control and/or failure detection |
US7272473B2 (en) * | 2004-09-17 | 2007-09-18 | The Boeing Company | Methods and systems for analyzing system operator coupling susceptibility |
US7229047B1 (en) | 2005-08-30 | 2007-06-12 | Cessna Aircraft Company | Aircraft roll disconnect mechanism |
FR2899562B1 (fr) * | 2006-04-05 | 2009-01-09 | Eurocopter France | Dispositif de commandes de vol d'un giravion |
FR2903962B1 (fr) * | 2006-07-18 | 2009-07-03 | Eurocopter France | Dispositif pour lier un premier et un deuxieme manches de commande d'un aeronef en roulis et en tangage. |
US8016566B2 (en) * | 2006-08-03 | 2011-09-13 | Bell Helicopter Textron Inc. | High performance low noise rotorcraft blade aerodynamic design |
US7701161B2 (en) * | 2006-10-02 | 2010-04-20 | Honeywell International Inc. | Motor balanced active user interface assembly |
GB0714916D0 (en) * | 2007-07-31 | 2007-09-12 | Wittenstein Aerospace & Simula | Control device |
EP2097315B1 (de) * | 2007-08-08 | 2017-07-26 | Moog Inc. | Zur verwendung in einem fly-by-wire-flugsteuerverfahren ausgeführter steuerknüppel und gelenkmechanismus zur verwendung darin |
US8078340B2 (en) * | 2007-11-12 | 2011-12-13 | Honeywell International Inc. | Active user interface haptic feedback and linking control system using either force or position data |
JP4691121B2 (ja) * | 2008-02-20 | 2011-06-01 | 三菱重工業株式会社 | 操縦システム、操縦桿リンク切り離し方法 |
FR2928621B1 (fr) * | 2008-03-13 | 2010-02-26 | Eurocopter France | Commande de vol d'un aeronef. |
JP5531414B2 (ja) * | 2009-01-28 | 2014-06-25 | トヨタ自動車株式会社 | 操縦支援装置 |
US9051045B2 (en) | 2010-07-28 | 2015-06-09 | Woodward Mpc, Inc. | Indirect drive active control column |
US9405312B2 (en) | 2010-07-28 | 2016-08-02 | Woodward Mpc, Inc. | Active control column with manually activated reversion to passive control column |
US8814103B2 (en) | 2010-07-28 | 2014-08-26 | Woodward Mpc, Inc. | Position control system for cross coupled operation of fly-by-wire control columns |
US8469317B2 (en) | 2010-10-22 | 2013-06-25 | Woodward Mpc, Inc. | Line replaceable, fly-by-wire control columns with push-pull interconnect rods |
US8729848B2 (en) | 2010-12-22 | 2014-05-20 | Woodward Mpc Inc. | Fail-passive variable gradient control stick drive system |
US8494690B2 (en) * | 2011-04-26 | 2013-07-23 | The Boeing Company | Flight controller management system with a backdrive monitor |
US9791886B2 (en) * | 2011-05-12 | 2017-10-17 | Bombardier Inc. | Controller |
USD675555S1 (en) | 2011-05-13 | 2013-02-05 | Bombardier Inc. | Controller |
US9126676B2 (en) | 2011-10-28 | 2015-09-08 | Woodward Mpc, Inc. | Compact two axis gimbal for control stick |
CA2914392C (en) * | 2013-06-14 | 2021-10-26 | Bombardier Inc. | Aircraft sidestick priority and dual input control logic |
RU2527574C1 (ru) * | 2013-07-22 | 2014-09-10 | Открытое Акционерное Общество "Московский Вертолётный Завод Им. М.Л. Миля" | Система управления вертолетом и раздвижная тяга проводки системы управления |
US9284996B2 (en) * | 2013-10-23 | 2016-03-15 | Sikorsky Aircraft Corporation | Selective electrical control of electromechanical clutch assembly |
US9352824B2 (en) * | 2014-01-23 | 2016-05-31 | Woodward Mpc, Inc. | Line replaceable, fly-by-wire control column and control wheel assemblies with a centrally connected line replaceable disconnect and autopilot assembly |
RU2571992C1 (ru) * | 2014-06-10 | 2015-12-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Московский авиационный институт (национальный исследовательский университет) (МАИ) | Боковая ручка управления самолетом |
RU2572011C1 (ru) * | 2014-06-10 | 2015-12-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования Московский авиационный институт (национальный исследовательский университет) (МАИ) | Система управления жизненно важными рулевыми поверхностями самолета |
WO2016105650A1 (en) * | 2014-11-05 | 2016-06-30 | Tzafrir Sheffer | Autopilot system, and related components and methods |
US11104421B2 (en) | 2014-11-05 | 2021-08-31 | Tzafrir Sheffer | Autopilot system, and related components and methods |
US10239633B2 (en) * | 2014-11-26 | 2019-03-26 | Embraer S.A. | System and method to interchange flight control inceptors in an aircraft flight control system and cockpit |
US9969484B2 (en) * | 2015-02-26 | 2018-05-15 | Grant Norwitz | Adjustable height cyclic control assembly and method |
US9823686B1 (en) * | 2016-08-15 | 2017-11-21 | Clause Technology | Three-axis motion joystick |
US9889874B1 (en) * | 2016-08-15 | 2018-02-13 | Clause Technology | Three-axis motion joystick |
CN107031822B (zh) * | 2016-11-30 | 2019-05-14 | 江西洪都航空工业集团有限责任公司 | 一种舵面铰链力矩辅助装置 |
US11014648B2 (en) | 2017-04-17 | 2021-05-25 | Textron Innovations, Inc. | Interconnected sidesticks for fly-by-wire flight control |
US10894595B1 (en) * | 2017-07-25 | 2021-01-19 | Rockwell Collins, Inc. | Spring detent for over-ridable interconnect |
RU2681462C1 (ru) * | 2017-10-31 | 2019-03-06 | Акционерное общество Московский научно-производственный комплекс "Авионика" имени О.В. Успенского (АО МНПК "Авионика") | Боковая ручка управления (варианты) |
AT520763B1 (de) * | 2017-12-21 | 2022-09-15 | Hans Kuenz Gmbh | Kransteuerung |
US11124309B2 (en) | 2018-01-09 | 2021-09-21 | General Electric Company | Single lever control system for engines with multiple control modes |
EP3650336A1 (de) | 2018-11-12 | 2020-05-13 | Goodrich Actuation Systems SAS | Trimsteuerungssystem |
CN110525665B (zh) * | 2019-07-16 | 2022-09-20 | 中国特种飞行器研究所 | 一种主副驾驶联动的侧杆装置 |
CN114162309A (zh) * | 2021-11-30 | 2022-03-11 | 中国商用飞机有限责任公司 | 主动侧杆系统 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2958484A (en) * | 1957-07-29 | 1960-11-01 | Frederick W Ross | Electrical aerodynamic aircraft control system |
US3140843A (en) * | 1962-09-06 | 1964-07-14 | Sperry Rand Corp | Servo system |
US3528633A (en) * | 1967-11-14 | 1970-09-15 | Siegfried Knemeyer | System for controlling and stabilizing an aircraft in yaw |
US3576302A (en) * | 1968-07-10 | 1971-04-27 | Bendix Corp | Solid-state position sensor for sensing an adjusted position of a control element |
US4122927A (en) * | 1977-05-13 | 1978-10-31 | The United States Of America As Represented By The Secretary Of The Navy | Disconnect linkage for force transmission system |
DE3151623A1 (de) * | 1981-12-28 | 1983-07-07 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Steuereinrichtung zum einstellen von steuerflaechen fuer luftfahrzeuge |
US4603388A (en) * | 1983-02-16 | 1986-07-29 | Sperry Corporation | VTOL altitude hold system with automatic ground effect compensation |
FR2603866A1 (fr) * | 1986-09-12 | 1988-03-18 | Messerschmitt Boelkow Blohm | Systeme de commande de gouvernes de profondeur |
FR2643502B1 (fr) * | 1989-02-20 | 1996-01-19 | Aerospatiale | Dispositif de commande a manche basculant, notamment pour aeronef, et systeme comportant un tel dispositif |
US5156363A (en) * | 1991-02-28 | 1992-10-20 | United Technologies Corporation | Helicopter collective stick of the displacement type occupying a minimum space envelope yet whose grip generates an arc of large radius |
US5149023A (en) * | 1991-07-12 | 1992-09-22 | The Boeing Company | Mechanically-linked side stick controllers with isolated pitch and roll control movement |
-
1993
- 1993-07-21 US US08/095,870 patent/US5456428A/en not_active Expired - Fee Related
-
1994
- 1994-07-19 DE DE69425058T patent/DE69425058T2/de not_active Expired - Fee Related
- 1994-07-19 WO PCT/US1994/008121 patent/WO1995003212A1/en active IP Right Grant
- 1994-07-19 EP EP94923545A patent/EP0708726B1/de not_active Expired - Lifetime
- 1994-07-19 JP JP7505264A patent/JPH09501371A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0708726A1 (de) | 1996-05-01 |
DE69425058T2 (de) | 2001-03-08 |
EP0708726B1 (de) | 2000-06-28 |
WO1995003212A1 (en) | 1995-02-02 |
JPH09501371A (ja) | 1997-02-10 |
US5456428A (en) | 1995-10-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |