ES8204681A1 - Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples - Google Patents
Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiplesInfo
- Publication number
- ES8204681A1 ES8204681A1 ES500913A ES500913A ES8204681A1 ES 8204681 A1 ES8204681 A1 ES 8204681A1 ES 500913 A ES500913 A ES 500913A ES 500913 A ES500913 A ES 500913A ES 8204681 A1 ES8204681 A1 ES 8204681A1
- Authority
- ES
- Spain
- Prior art keywords
- aircraft
- force
- stick
- control
- axis
- 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
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1
- 230000003750 conditioning effect Effects 0.000 abstract 1
- 125000004122 cyclic group Chemical group 0.000 abstract 1
- 230000035945 sensitivity Effects 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
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/75—Arm-rests
- B60N2/79—Adaptations for additional use of the arm-rests
- B60N2/797—Adaptations for additional use of the arm-rests for use as electrical control means, e.g. switches
-
- 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
- B64C25/50—Steerable undercarriages; Shimmy-damping
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
- G01L5/22—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers
- G01L5/223—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers to joystick 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Mechanical Engineering (AREA)
- General Physics & Mathematics (AREA)
- Physics & Mathematics (AREA)
- Transportation (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Mechanical Control Devices (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
- Feedback Control In General (AREA)
Abstract
SISTEMA DE CONTROL DE AERONAVES. FORMADO POR EL CONTROLADOR DE BRAZO LATERAL (10) QUE COMPRENDE UNA PALANCA DE MANDO (12), MONTADA SOBRE UN CONJUNTO TRANSDUCTOR DE DETECCION ADECUADA (13) DISPUESTO SOBRE UN BRAZO (14) DEL ASIENTO (16). EL BRAZO (14) VA ARTICULADO (18) DE FORMA QUE SE DESPLAZA PARA PERMITIR EL ACCESO AL ASIENTO. EL CONTROLADOR (10) ES UN CONTROLADOR DE FUERZA, DE FORMA QUE NO PRECISA DE DESPLAZAMIENTOS PARA SU ACCIONAMIENTO. SE PRETENDE CON TODO ELLO MEJORAR LA VISIBILIDAD Y DISMINUIR LA FATIGA DEL PILOTO.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13623380A | 1980-04-01 | 1980-04-01 |
Publications (2)
Publication Number | Publication Date |
---|---|
ES8204681A1 true ES8204681A1 (es) | 1982-05-16 |
ES500913A0 ES500913A0 (es) | 1982-05-16 |
Family
ID=22471948
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES500913A Granted ES500913A0 (es) | 1980-04-01 | 1981-03-31 | Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples |
Country Status (11)
Country | Link |
---|---|
JP (2) | JPS56167596A (es) |
AU (1) | AU538972B2 (es) |
BR (1) | BR8101648A (es) |
CA (1) | CA1158219A (es) |
CH (1) | CH652364A5 (es) |
DE (1) | DE3111604A1 (es) |
ES (1) | ES500913A0 (es) |
FR (1) | FR2479133A1 (es) |
GB (1) | GB2073114B (es) |
IL (1) | IL62270A (es) |
IT (1) | IT1137311B (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109592064A (zh) * | 2018-11-02 | 2019-04-09 | 中国航空工业集团公司西安飞机设计研究所 | 飞机与机械操纵***变形差异对机动操纵影响设计方法 |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2576281B1 (fr) * | 1985-01-18 | 1992-04-30 | Aerospatiale | Poste de pilotage pourvu d'un manche a balai lateral actionnable par une seule main et siege pour un tel poste de pilotage |
FR2604001B1 (fr) * | 1986-09-15 | 1988-12-09 | Aerospatiale | Systeme de commande de vol electrique avec protection en incidence pour aeronef |
US4696445A (en) * | 1986-09-18 | 1987-09-29 | United Technologies Corporation | Collective control system for a helicopter |
FI77334C (fi) * | 1987-03-03 | 1989-02-10 | Teopros Oy | Styranordning. |
GB2248947B (en) * | 1988-02-22 | 1992-08-05 | Honda Motor Co Ltd | Synchronous operation control system for numerically controlled machine |
JPH07107643B2 (ja) * | 1988-02-22 | 1995-11-15 | 本田技研工業株式会社 | Nc同期制御システム |
FR2643331B1 (fr) * | 1989-02-17 | 1995-01-13 | Aerospatiale | Dispositif de commande a manche basculant et systeme de commande de vol pour aeronef comportant au moins un tel dispositif de commande |
FR2647922B1 (fr) * | 1989-05-31 | 1993-12-31 | Sextant Avionique | Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule |
US4947697A (en) * | 1989-06-28 | 1990-08-14 | Cae Electronics Ltd. | System for measuring force versus position of a flight controller in an aircraft or flight simulator |
FR2668750B1 (fr) * | 1990-11-06 | 1993-01-22 | Aerospatiale | Systeme pour la commande integree en profondeur et en poussee d'un aeronef. |
JP2681428B2 (ja) * | 1992-01-29 | 1997-11-26 | 日本航空電子工業株式会社 | 無人ヘリコプタ用飛行制御装置 |
JP2607205B2 (ja) * | 1992-06-30 | 1997-05-07 | 川崎重工業株式会社 | 航空機用多軸サイドスティックコントローラ |
FR2769283B1 (fr) * | 1997-10-06 | 1999-12-03 | Eurocopter France | Procede et dispositif pour realiser le decouplage du comportement d'un aeronef, notamment un helicoptere |
JP3091743B1 (ja) | 1999-03-30 | 2000-09-25 | 株式会社コミュータヘリコプタ先進技術研究所 | 操縦装置 |
US6671588B2 (en) | 2001-12-27 | 2003-12-30 | Toyota Jidosha Kabushiki Kaisha | System and method for controlling traveling direction of aircraft |
DE10310717A1 (de) * | 2003-03-10 | 2004-09-23 | Wittenstein Ag | Vorrichtung zum Steuern eines Fahrzeuges |
FR2899562B1 (fr) * | 2006-04-05 | 2009-01-09 | Eurocopter France | Dispositif de commandes de vol d'un giravion |
FR2903660B1 (fr) * | 2006-07-12 | 2009-06-12 | Airbus France Sas | Systeme de commandes de vol electriques pour aeronef et siege l'incorporant |
FR2991295B1 (fr) * | 2012-06-04 | 2015-02-27 | Eurocopter France | Aeronef a grande visibilite |
US9033284B2 (en) | 2012-11-20 | 2015-05-19 | Sikorsky Aircraft Corporation | Integrated seat mounted inceptor |
FR3001439B1 (fr) | 2013-01-29 | 2015-02-27 | Eurocopter France | Organe de commande muni d'un levier de pas collectif de pales et d'un moyen de commande en lacet, et aeronef |
JP5698802B2 (ja) | 2013-06-28 | 2015-04-08 | ヤマハ発動機株式会社 | 遠隔操縦装置 |
EP3186146B1 (en) * | 2014-08-28 | 2019-10-09 | Sikorsky Aircraft Corporation | Pitch control system |
CN104502009B (zh) * | 2014-11-28 | 2018-10-26 | 湖南三一智能控制设备有限公司 | 一种臂架防碰撞装置、方法及工程机械 |
FR3060528B1 (fr) * | 2016-12-16 | 2018-12-07 | Safran Electronics & Defense | Dispositif de commande des surfaces mobiles et d'une roue directrice d'un aeronef |
CN108407879B (zh) * | 2018-05-15 | 2023-12-12 | 北京美佳靓丽日用品有限公司 | 一种三维方向控制装置 |
WO2021248116A1 (en) * | 2020-06-05 | 2021-12-09 | Joby Aero, Inc. | Aircraft control system and method |
GB2602953A (en) * | 2020-08-21 | 2022-07-27 | Hill Group Tech Limited | Helicopter collective control apparatus |
FR3119601A1 (fr) | 2021-02-10 | 2022-08-12 | Airbus Helicopters | Système de commande d’un aéronef et aéronef associé |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3447766A (en) * | 1967-02-14 | 1969-06-03 | Bendix Corp | Control stick with solid state sensors |
US3584814A (en) * | 1967-07-18 | 1971-06-15 | Bell Aerospace Corp | Stability and control augmentation system |
GB1240866A (en) * | 1968-08-22 | 1971-07-28 | Amf Inc | Control device |
US3771037A (en) * | 1973-03-15 | 1973-11-06 | Nasa | Solid state controller three-axes controller |
JPS5366600U (es) * | 1976-11-05 | 1978-06-05 |
-
1981
- 1981-01-06 CA CA000367937A patent/CA1158219A/en not_active Expired
- 1981-03-03 IL IL62270A patent/IL62270A/xx not_active IP Right Cessation
- 1981-03-03 GB GB8106575A patent/GB2073114B/en not_active Expired
- 1981-03-19 BR BR8101648A patent/BR8101648A/pt unknown
- 1981-03-24 DE DE19813111604 patent/DE3111604A1/de active Granted
- 1981-03-25 FR FR8105943A patent/FR2479133A1/fr active Granted
- 1981-03-26 CH CH2046/81A patent/CH652364A5/de not_active IP Right Cessation
- 1981-03-27 AU AU68864/81A patent/AU538972B2/en not_active Ceased
- 1981-03-30 IT IT20794/81A patent/IT1137311B/it active
- 1981-03-30 JP JP4835981A patent/JPS56167596A/ja active Granted
- 1981-03-31 ES ES500913A patent/ES500913A0/es active Granted
-
1989
- 1989-02-02 JP JP1024733A patent/JPH0725355B2/ja not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109592064A (zh) * | 2018-11-02 | 2019-04-09 | 中国航空工业集团公司西安飞机设计研究所 | 飞机与机械操纵***变形差异对机动操纵影响设计方法 |
Also Published As
Publication number | Publication date |
---|---|
FR2479133B1 (es) | 1984-03-30 |
IL62270A (en) | 1985-03-31 |
BR8101648A (pt) | 1981-10-06 |
GB2073114B (en) | 1983-10-12 |
CA1158219A (en) | 1983-12-06 |
FR2479133A1 (fr) | 1981-10-02 |
JPH0358959B2 (es) | 1991-09-09 |
GB2073114A (en) | 1981-10-14 |
AU6886481A (en) | 1981-10-08 |
AU538972B2 (en) | 1984-09-06 |
CH652364A5 (de) | 1985-11-15 |
DE3111604C2 (es) | 1993-07-29 |
JPH01289798A (ja) | 1989-11-21 |
ES500913A0 (es) | 1982-05-16 |
IT8120794A0 (it) | 1981-03-30 |
JPS56167596A (en) | 1981-12-23 |
JPH0725355B2 (ja) | 1995-03-22 |
DE3111604A1 (de) | 1982-04-22 |
IT1137311B (it) | 1986-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 20010402 |