ES530062A0 - IMPROVEMENTS IN AUTOMATIC FLIGHT CONTROL SYSTEMS IN AIRCRAFT - Google Patents

IMPROVEMENTS IN AUTOMATIC FLIGHT CONTROL SYSTEMS IN AIRCRAFT

Info

Publication number: ES530062A0
Authority: ES; Spain
Prior art keywords: aircraft; control systems; flight control; automatic flight; automatic
Prior art date: 1983-02-28
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.): Granted

Application number

ES530062A

Other languages

Spanish (es)

Other versions

ES8502931A1 (en

Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)

RTX Corp

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.)

1983-02-28

Filing date

1984-02-27

Publication date

1985-02-01

1984-02-27 Application filed by United Technologies Corp filed Critical United Technologies Corp

1985-02-01 Publication of ES8502931A1 publication Critical patent/ES8502931A1/en

1985-02-01 Publication of ES530062A0 publication Critical patent/ES530062A0/en

Status Granted legal-status Critical Current

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
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
- B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
- 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

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Automation & Control Theory (AREA)
Remote Sensing (AREA)
Physics & Mathematics (AREA)
General Physics & Mathematics (AREA)
Radar, Positioning & Navigation (AREA)
Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Numerical Control (AREA)
Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Communication Control (AREA)
Catching Or Destruction (AREA)
Mechanical Control Devices (AREA)
Position Input By Displaying (AREA)
Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)

ES530062A 1983-02-28 1984-02-27 IMPROVEMENTS IN AUTOMATIC FLIGHT CONTROL SYSTEMS IN AIRCRAFT Granted ES530062A0 (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US47040183A	1983-02-28	1983-02-28

Publications (2)

Publication Number	Publication Date
ES8502931A1 ES8502931A1 (en)	1985-02-01
ES530062A0 true ES530062A0 (en)	1985-02-01

Family

ID=23867487

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
ES530062A Granted ES530062A0 (en)	1983-02-28	1984-02-27	IMPROVEMENTS IN AUTOMATIC FLIGHT CONTROL SYSTEMS IN AIRCRAFT

Country Status (8)

Country	Link
JP (1)	JPS59171794A (en)
AU (1)	AU558086B2 (en)
DE (1)	DE3407223C2 (en)
DK (1)	DK104284A (en)
ES (1)	ES530062A0 (en)
GB (1)	GB2135796B (en)
NO (1)	NO158455C (en)
SE (1)	SE451827B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3431583A1 (en) *	1984-08-28	1986-03-13	Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn	DEVICE FOR THE AUTOMATIC ELIMINATION OF TAX FORCE ERRORS IN AIRCRAFT, IN PARTICULAR HELICOPTERS
GB2339614B (en) *	1998-07-14	2000-06-21	Infrared Integrated Syst Ltd	Detector-array sensor with mask warning
US6325331B1 (en) *	1998-12-11	2001-12-04	Bell Helicopter Textron Inc.	Trim actuator
JP3091743B1 (en)	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	Pilot device
US6311930B1 (en) *	1999-07-16	2001-11-06	Swales Aerospace	Anti-friction release device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4387432A (en) *	1981-03-30	1983-06-07	United Technologies Corporation	Pulsed aircraft actuator

1984
- 1984-02-03 GB GB08402941A patent/GB2135796B/en not_active Expired
- 1984-02-14 AU AU24585/84A patent/AU558086B2/en not_active Ceased
- 1984-02-23 SE SE8400998A patent/SE451827B/en not_active IP Right Cessation
- 1984-02-23 NO NO840682A patent/NO158455C/en unknown
- 1984-02-27 ES ES530062A patent/ES530062A0/en active Granted
- 1984-02-27 DK DK104284A patent/DK104284A/en not_active Application Discontinuation
- 1984-02-28 JP JP59037200A patent/JPS59171794A/en active Granted
- 1984-02-28 DE DE3407223A patent/DE3407223C2/en not_active Expired - Fee Related

Also Published As

Publication number	Publication date
JPS59171794A (en)	1984-09-28
NO158455C (en)	1988-09-14
GB2135796A (en)	1984-09-05
GB8402941D0 (en)	1984-03-07
NO840682L (en)	1984-08-29
SE8400998D0 (en)	1984-02-23
JPH046600B2 (en)	1992-02-06
SE8400998L (en)	1984-08-29
SE451827B (en)	1987-11-02
ES8502931A1 (en)	1985-02-01
DK104284A (en)	1984-08-29
AU2458584A (en)	1984-09-06
AU558086B2 (en)	1987-01-15
DK104284D0 (en)	1984-02-27
GB2135796B (en)	1986-07-09
DE3407223C2 (en)	1994-06-30
NO158455B (en)	1988-06-06
DE3407223A1 (en)	1984-08-30

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ES530062A0 (en)	1985-02-01	IMPROVEMENTS IN AUTOMATIC FLIGHT CONTROL SYSTEMS IN AIRCRAFT
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Legal Events

Date	Code	Title	Description
1997-05-01	FD1A	Patent lapsed	Effective date: 19970401