US4648569A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Airplane automatic control force trimming device for asymmetric engine failures
Assignee: National Aeronautics and Space Administration
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Filing: 1985-10-23
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Granted: 1987-03-10
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Expires: 2005-10-23
Abstract
Abstract The difference in dynamic pressure in the propeller slipstreams as measured by sensors 20 and 20a is divided by the freestream dynamic pressure generating a quantity proportional to the differential thrust coefficient. This quantity is used to command an electric trim motor 26 to change the position of trim tab 14 thereby retrimming the airplane to the new asymmetric power condition. The change in position of the trim tab produced by the electric trim motor is summed with the pilot's input to produce the actual trim tab position.
Inventors
- 👤 Eric C. Stewart
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 00:46
CPC Classifications
B; B64; B64C; B64C13/00; B64C13/02; B64C13/16
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
100 words
A method of improving the controllability of twin-engine propeller-driven airplanes operating in an asymmetric power mode comprising: measuring the freestream dynamic pressure and the propeller slipstream dynamic pressures; generating a quantity proportional to the differential thrust coefficient including dividing the difference between said propeller slipstream dynamic pressures by said freestream dynamic pressure; and adjusting the secondary control surfaces on the airplane in response to the quantity proportional to the differential thrust coefficient to help reduce the large control force felt in the cockpit due to the asymmetric power condition wherein the reduced control forces improve the controllability of the airplane.
Claim 2
Independent Claim
100 words
A method of improving the controllability of twin-engine propeller-driven airplanes operating in an asymmetric power mode comprising: measuring the freestream dynamic pressure and the propeller slipstream dynamic pressures; generating a quantity proportional to the differential thrust coefficient including dividing the difference between said propeller slipstream dynamic pressures by said freestream dynamic pressure; and adjusting the secondary control surfaces on the airplane in response to the quantity proportional to the differential thrust coefficient to help reduce the large control force felt in the cockpit due to the asymmetric power condition wherein the reduced control forces improve the controllability of the airplane.
Claim 3
Dependent Claim
22 words
The method of claim 1 wherein adjusting the secondary control surfaces includes a summer for adding pilot adjustment to the system adjustment.
Claim 4
Dependent Claim
97 words
An automatic trimming device to help reduce the large asymmetric control forces felt in the cockpit of a twin-engine propeller-driven airplane operating in an asymmetric power mode comprising: a means for measuring the freestream dynamic pressure and the propeller slipstream dynamic pressures; a means for generating a quantity proportional to the differential thrust coefficient including dividing the difference between said propeller slipstream dynamic pressures by said freestream dynamic pressure; and a means for adjusting the trim tab position on each of the primary control surfaces in response to said quantities to help reduce said large control forces.
Claim 5
Dependent Claim
97 words
An automatic trimming device to help reduce the large asymmetric control forces felt in the cockpit of a twin-engine propeller-driven airplane operating in an asymmetric power mode comprising: a means for measuring the freestream dynamic pressure and the propeller slipstream dynamic pressures; a means for generating a quantity proportional to the differential thrust coefficient including dividing the difference between said propeller slipstream dynamic pressures by said freestream dynamic pressure; and a means for adjusting the trim tab position on each of the primary control surfaces in response to said quantities to help reduce said large control forces.
Claim 6
Dependent Claim
23 words
An automatic trimming device as in claim 3 wherein said means for producing quantities proportional to the dynamic pressure comprises dynamic pressure sensors.
Claim 7
Dependent Claim
28 words
An automatic trimming device as in claim 3 wherein said means for adjusting the trim tab position includes a summer for adding pilot adjustment to the system adjustment.
Claim 8
Dependent Claim
25 words
An automatic trimming device as in claim 5 wherein said means for generating said quantity proportional to the differential coefficient comprises an amplifier or micro-computer.
Claim 9
Dependent Claim
24 words
An automatic trimming device as in claim 5 wherein said means for automatically adjusting comprises an electric trim motor connected to said trim tabs.
Claim 10
Dependent Claim
17 words
An automatic trimming device as in claim 5 wherein said means for summing is a mechanical summer.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-03-09 | 1990-09-08 | 1991-03-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-03-09 | 1994-09-08 | 1995-03-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-03-09 | 1998-09-08 | 1999-03-10 | $7700.00 | Window Closed / Lapsed |