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
Links
Landscapes
- 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.
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)
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. |
-
2000
- 2000-09-20 ES ES200002329A patent/ES2174725B1/en not_active Expired - Lifetime
Patent Citations (6)
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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