US4078749A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Helicopter stick force augmentation null offset compensation
Assignee: RTX Corp
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Filing: 1977-05-24
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Granted: 1978-03-14
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Expires: 1997-05-24
Abstract
Abstract In the cyclic pitch stick controls of a helicopter of the type in which feel is provided to the pilot by inducing a force which is proportional but opposite to the motion of the cyclic stick from an adjustable trim position, null offset errors which may be due, inter alia, to temperature variation of the hydraulic fluid in the system, are periodically overcome by means of sensing the pressure differential across the force augmentation hydraulic servo actuator at times when the differential pressure thereacross should be nearly zero, during trim release with small stick motion, and providing a countermanding bias in response thereto; the pressure differential is measured by a differential pressure transducer having a full scale which is only sufficient to measure the expected null errors, which may be about an order of magnitude lower than the full scale, operative pressure differentials which may occur.
Inventors
- 👤 Raymond G. Johnson, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 05:58
CPC Classifications
B; B64; B64C; B64C13/00; B64C13/24; B64C13/26; B64C13/36
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
239 words
In a helicopter force augmentation system in which differential hydraulic pressure is provided to a force augmenting hydraulic servo actuator to provide force to a cyclic control stick in the helicopter, said cyclic control stick being associated with a trim release switch, said differential hydraulic pressure being provided by an electro/hydraulic servo valve in response to electric signals indicative of positioning of the cyclic control stick, the improvement comprising: pressure means for sensing the magnitude and polarity of differential pressure input provided by said servo valve to said force augmentation hydraulic servo actuator and providing a pressure signal indicative thereof; means for sensing the rate of motion of the cyclic stick and providing a low motion signal indicative of the rate of motion being less than a threshold rate; means responsive to said trim release switch to provide a trim release signal indicating that stick trim control has been released; means responsive to concurrent presence of said low motion signal and said trim release signal to provide a track signal; and bias means responsive to said pressure signal and to said track signal to provide a null offset compensation bias signal input to said servo valve in response to the value of said pressure signal during the presence of said track signal and, in the absence of said track signal, in response to the last value of said pressure signal at the time of disappearance of said track signal.
Claim 2
Dependent Claim
239 words
In a helicopter force augmentation system in which differential hydraulic pressure is provided to a force augmenting hydraulic servo actuator to provide force to a cyclic control stick in the helicopter, said cyclic control stick being associated with a trim release switch, said differential hydraulic pressure being provided by an electro/hydraulic servo valve in response to electric signals indicative of positioning of the cyclic control stick, the improvement comprising: pressure means for sensing the magnitude and polarity of differential pressure input provided by said servo valve to said force augmentation hydraulic servo actuator and providing a pressure signal indicative thereof; means for sensing the rate of motion of the cyclic stick and providing a low motion signal indicative of the rate of motion being less than a threshold rate; means responsive to said trim release switch to provide a trim release signal indicating that stick trim control has been released; means responsive to concurrent presence of said low motion signal and said trim release signal to provide a track signal; and bias means responsive to said pressure signal and to said track signal to provide a null offset compensation bias signal input to said servo valve in response to the value of said pressure signal during the presence of said track signal and, in the absence of said track signal, in response to the last value of said pressure signal at the time of disappearance of said track signal.
Claim 3
Dependent Claim
38 words
The improvement according to claim 1 wherein said pressure means has a full scale pressure range which is significantly lower than the range of operative differential hydraulic pressure provided by said servo valve to said hydraulic servo actuator.
Claim 4
Dependent Claim
28 words
The improvement according to claim 1 wherein said bias means includes means to provide said bias signal in response to proportional and integral functions of said pressure signal.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-03-13 | 1981-09-12 | 1982-03-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-03-13 | 1985-09-12 | 1986-03-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-03-13 | 1989-09-12 | 1990-03-14 | $7700.00 | Window Closed / Lapsed |