ES2174725A1 - Super positioner of an aileron back-fed by an even load. - Google Patents

Super positioner of an aileron back-fed by an even load.

Info

Publication number
ES2174725A1
ES2174725A1 ES200002329A ES200002329A ES2174725A1 ES 2174725 A1 ES2174725 A1 ES 2174725A1 ES 200002329 A ES200002329 A ES 200002329A ES 200002329 A ES200002329 A ES 200002329A ES 2174725 A1 ES2174725 A1 ES 2174725A1
Authority
ES
Spain
Prior art keywords
aileron
positioner
super
well
fed
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.)
Granted
Application number
ES200002329A
Other languages
Spanish (es)
Other versions
ES2174725B1 (en
Inventor
Garcia Ramon Ferreiro
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.)
Universidade da Coruna
Original Assignee
Universidade da Coruna
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.)
Filing date
Publication date
Application filed by Universidade da Coruna filed Critical Universidade da Coruna
Priority to ES200002329A priority Critical patent/ES2174725B1/en
Publication of ES2174725A1 publication Critical patent/ES2174725A1/en
Application granted granted Critical
Publication of ES2174725B1 publication Critical patent/ES2174725B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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  • Control Of Position Or Direction (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)

Abstract

Super positioner of an aileron back-fed by an even load.The present invention refers to the feedback of a super-positioner of the aileron or helm of aerospace vehicles by means of the mechanical pair's transduction developed by the aileron on the vehicle. The pair's reception as well as its transduction is carried out by any accessible physical mediums to the technique (Electric, Electronic, Electromagnetic, Hydraulic), as well as by means of combinations of both, including fiber optics as well as wireless mediums. With this method of feedback of the super-positioner of aileron, it is done without the classic feedback based on the measure of the aileron's angular position, thus obtaining improvements of the behavior as for stability and precision under adverse environmental conditions as a consequence of the elimination of the dynamic effect of non lineal stage originated by the aileron's angular position.
ES200002329A 2000-09-20 2000-09-20 SERVO-POSITIONER OF ALERON FEEDBACK BY LOAD PAIR. Expired - Lifetime ES2174725B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES200002329A ES2174725B1 (en) 2000-09-20 2000-09-20 SERVO-POSITIONER OF ALERON FEEDBACK BY LOAD PAIR.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200002329A ES2174725B1 (en) 2000-09-20 2000-09-20 SERVO-POSITIONER OF ALERON FEEDBACK BY LOAD PAIR.

Publications (2)

Publication Number Publication Date
ES2174725A1 true ES2174725A1 (en) 2002-11-01
ES2174725B1 ES2174725B1 (en) 2004-09-16

Family

ID=8495059

Family Applications (1)

Application Number Title Priority Date Filing Date
ES200002329A Expired - Lifetime ES2174725B1 (en) 2000-09-20 2000-09-20 SERVO-POSITIONER OF ALERON FEEDBACK BY LOAD PAIR.

Country Status (1)

Country Link
ES (1) ES2174725B1 (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US4281811A (en) * 1979-06-15 1981-08-04 Edo-Aire Mitchell Pitch trim system for aircraft
US5188511A (en) * 1991-08-27 1993-02-23 United Technologies Corporation Helicopter anti-torque device direct pitch control
EP0867364A2 (en) * 1997-03-26 1998-09-30 Advanced Technology Institute of Commuter-Helicopter, Ltd. Compensation apparatus for main rotor torque
ES2125163A1 (en) * 1996-04-09 1999-02-16 Univ De La Coruna Y En Su Nomb Feedback system for a rudder servo telemotor for ships
ES2137641T3 (en) * 1995-09-15 1999-12-16 Aerospatiale PROCEDURE AND COMMAND DEVICE FOR THE STEERING HELM OF AN AIRCRAFT.

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US4281811A (en) * 1979-06-15 1981-08-04 Edo-Aire Mitchell Pitch trim system for aircraft
US5188511A (en) * 1991-08-27 1993-02-23 United Technologies Corporation Helicopter anti-torque device direct pitch control
ES2137641T3 (en) * 1995-09-15 1999-12-16 Aerospatiale PROCEDURE AND COMMAND DEVICE FOR THE STEERING HELM OF AN AIRCRAFT.
ES2125163A1 (en) * 1996-04-09 1999-02-16 Univ De La Coruna Y En Su Nomb Feedback system for a rudder servo telemotor for ships
EP0867364A2 (en) * 1997-03-26 1998-09-30 Advanced Technology Institute of Commuter-Helicopter, Ltd. Compensation apparatus for main rotor torque

Also Published As

Publication number Publication date
ES2174725B1 (en) 2004-09-16

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