IT8120794A0 - Sistema di controllo del volo di un aeromobile autoequilibrato con barra di forza a molti assi. - Google Patents

Sistema di controllo del volo di un aeromobile autoequilibrato con barra di forza a molti assi.

Info

Publication number: IT8120794A0
Authority: IT; Italy
Prior art keywords: self; control system; flight control; aircraft flight; axis force
Prior art date: 1980-04-01

Application number

IT8120794A

Other languages

English (en)

Other versions

IT1137311B (it

Inventor

Edmond Daniel Diamond

Joseph Richard Maciolek

Leo Kingston

Original Assignee

United Technologies Corp

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.)

1980-04-01

Filing date

1981-03-30

Publication date

1981-03-30

1981-03-30 Application filed by United Technologies Corp filed Critical United Technologies Corp

1981-03-30 Publication of IT8120794A0 publication Critical patent/IT8120794A0/it

1986-09-10 Application granted granted Critical

1986-09-10 Publication of IT1137311B publication Critical patent/IT1137311B/it

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

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)
Feedback Control In General (AREA)
Toys (AREA)

IT20794/81A 1980-04-01 1981-03-30 Sistema di controllo del volo di un aeromobile autoequilibrato con barra di forza a molti assi IT1137311B (it)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US13623380A	1980-04-01	1980-04-01

Publications (2)

Publication Number	Publication Date
IT8120794A0 true IT8120794A0 (it)	1981-03-30
IT1137311B IT1137311B (it)	1986-09-10

Family

ID=22471948

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
IT20794/81A IT1137311B (it)	1980-04-01	1981-03-30	Sistema di controllo del volo di un aeromobile autoequilibrato con barra di forza a molti assi

Country Status (11)

Country	Link
JP (2)	JPS56167596A (it)
AU (1)	AU538972B2 (it)
BR (1)	BR8101648A (it)
CA (1)	CA1158219A (it)
CH (1)	CH652364A5 (it)
DE (1)	DE3111604A1 (it)
ES (1)	ES500913A0 (it)
FR (1)	FR2479133A1 (it)
GB (1)	GB2073114B (it)
IL (1)	IL62270A (it)
IT (1)	IT1137311B (it)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
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.
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
GB2248947B (en) *	1988-02-22	1992-08-05	Honda Motor Co Ltd	Synchronous operation control system for numerically controlled machine
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
US10676185B2 (en)	2014-08-28	2020-06-09	Sikorsky Aircraft Corporation	Rotary wing aircraft 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
ES2949956T3 (es) *	2017-12-21	2023-10-04	Bae Systems Plc	Sistemas de control de aeronaves
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
CN109592064B (zh) *	2018-11-02	2022-04-19	中国航空工业集团公司西安飞机设计研究所	飞机与机械操纵系统变形差异对机动操纵影响设计方法
WO2021248116A1 (en) *	2020-06-05	2021-12-09	Joby Aero, Inc.	Aircraft control system and method
GB2602953B (en) *	2020-08-21	2024-08-14	Hill Group Tech Limited	Helicopter collective control apparatus
FR3119601B1 (fr)	2021-02-10	2025-05-02	Airbus Helicopters	Système de commande d’un aéronef et aéronef associé

Family Cites Families (5)

* Cited by examiner, † Cited by third party
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 (it) *	1976-11-05	1978-06-05

1981
- 1981-01-06 CA CA000367937A patent/CA1158219A/en not_active Expired
- 1981-03-03 GB GB8106575A patent/GB2073114B/en not_active Expired
- 1981-03-03 IL IL62270A patent/IL62270A/xx not_active IP Right Cessation
- 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 JP JP4835981A patent/JPS56167596A/ja active Granted
- 1981-03-30 IT IT20794/81A patent/IT1137311B/it active
- 1981-03-31 ES ES500913A patent/ES500913A0/es active Granted
1989
- 1989-02-02 JP JP1024733A patent/JPH0725355B2/ja not_active Expired - Lifetime

Also Published As

Publication number	Publication date
CH652364A5 (de)	1985-11-15
IT1137311B (it)	1986-09-10
DE3111604C2 (it)	1993-07-29
AU6886481A (en)	1981-10-08
BR8101648A (pt)	1981-10-06
DE3111604A1 (de)	1982-04-22
JPH01289798A (ja)	1989-11-21
AU538972B2 (en)	1984-09-06
CA1158219A (en)	1983-12-06
GB2073114B (en)	1983-10-12
JPH0725355B2 (ja)	1995-03-22
ES8204681A1 (es)	1982-05-16
IL62270A (en)	1985-03-31
JPS56167596A (en)	1981-12-23
FR2479133A1 (fr)	1981-10-02
JPH0358959B2 (it)	1991-09-09
FR2479133B1 (it)	1984-03-30
ES500913A0 (es)	1982-05-16
GB2073114A (en)	1981-10-14

Legal Events

Date	Code	Title	Description
1999-10-27	TA	Fee payment date (situation as of event date), data collected since 19931001	Effective date: 19970228

Publication	Publication Date	Title
IT8120794A0 (it)	1981-03-30	Sistema di controllo del volo di un aeromobile autoequilibrato con barra di forza a molti assi.
IT7920458A0 (it)	1979-02-23	Controreazione meccanica attiva per dispositivo di comando con il sistema di governo di un aereo.
MX6588E (es)	1985-07-26	Mejoras en sistema de control para elevadores o estabilizadores de un helicoptero
ES490715A0 (es)	1981-02-16	Sistema control de direccion de helicoptero coaxial, paso colectivo a la vez que tambien variable simultaneamente con signo contrario
DE3166395D1 (en)	1984-11-08	Aircraft landing control system
IT8123608A0 (it)	1981-08-24	Sistema di controllo per turbine a vapore con derivazione o bypass.
DE3677315D1 (de)	1991-03-07	Flugzeugsteuersystem.
IT8119271A0 (it)	1981-01-22	Sistema di comando di bloccaggio per differenziale.
MX151348A (es)	1984-11-12	Mejoras a sistema de control para un procesamiento industrial con unidades de control distantes
IT7829132A0 (it)	1978-10-26	Sistema di controllo di volo duplice.
IT8168488A0 (it)	1981-11-16	Aeromobile con propulsione a razzo e relativo sistema di governo
NO161525C (no)	1989-08-23	Styringsanordning for kabler med seismisk utstyr, saerlig for kanonkabler med en eller flere kanongrupper.
IT1139381B (it)	1986-09-24	Impianto di controllo per dirigere un velivolo lungo un percorso di discesa curvilineo predeterminato
ES2017738B3 (es)	1991-03-01	Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.
DE3789097D1 (de)	1994-03-24	Flugsteuersysteme für Hubschrauber.
FI791570A7 (fi)	1981-01-01	Hissiryhmän säätöjärjestelmä.
IT8320403A0 (it)	1983-03-31	Comando di volo,specialmente per un elicottero.
IT7829131A0 (it)	1978-10-26	Sistema di controllo di volo duplice.
ES509674A0 (es)	1983-01-16	Perfeccionamientos en un sistema de control de bucles multiples para aviones.
IT8222269A0 (it)	1982-07-06	Sistema di controllo del combustibile per un essiccatore.
IT963657B (it)	1974-01-21	Sistema di controllo del volo di aerei accoppiati per il solleva mento multiplo di un carico
NO155233C (no)	1987-03-04	Anordning for avfoeling av manglende driftsevne av et antiskrensesystem paa et luftfartoey.
IT8024212A0 (it)	1980-08-19	Sistema di controllo idromeccanico del combustibile con interfaccia elettromeccanica indipendente.
BE594741A (fr)	1961-01-02	Système directeur de la pente de la trajectoire d'atterrissage à bord de l'avion.
ES525395A0 (es)	1984-12-16	Un controlador de sistema informatico.