Patent US4684085A successfully refreshed from Google Patents.
US4684085A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft automatic trim system
Assignee: Boeing Co
•
Filing: 1985-10-31
•
Granted: 1987-08-04
•
Expires: 2005-10-31
Abstract
Abstract An aircraft automatic trim system is operable during autopilot control to transfer trim from the elevators to the stabilizers. The thresholds for trim transfer are based on the ratio of elevator demand to available elevator control. Trim commands are produced responsive to this ratio exceeding an amplitude and time dependent limit.
Inventors
- 👤 James W. Berwick, Jr.
- 👤 Gary C. Thomason
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 07:50
CPC Classifications
G; G05; G05D; G05D1/00; G05D1/04; G05D1/06; G05D1/0607
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
99 words
An aircraft automatic trim system for producing control signals to transfer trim from the aircraft's elevators to the stabilizers during an automatic aircraft flight control mode, the system comprising: available elevator control means for producing a signal representative of the available elevator control in said automatic flight control mode; elevator demand means for producing a signal representative of actual elevator demand; ratio means for producing a ratio signal representative of the ratio of said elevator demand signal to said available elevator control signal; and detector means for producing predetermined stabilizer trim command signals in response to said ratio signal.
Claim 2
Dependent Claim
99 words
An aircraft automatic trim system for producing control signals to transfer trim from the aircraft's elevators to the stabilizers during an automatic aircraft flight control mode, the system comprising: available elevator control means for producing a signal representative of the available elevator control in said automatic flight control mode; elevator demand means for producing a signal representative of actual elevator demand; ratio means for producing a ratio signal representative of the ratio of said elevator demand signal to said available elevator control signal; and detector means for producing predetermined stabilizer trim command signals in response to said ratio signal.
Claim 3
Dependent Claim
42 words
The system of claim 1 wherein said available elevator control means comprises: feel pressure means for producing a signal representative of feel pressure on the aircraft's control column; and means for converting said feel pressure signal to said available elevator control signal.
Claim 4
Dependent Claim
112 words
The system of claim 2 wherein said feel pressure means comprises: means for producing a signal representative of aircraft total pressure; means for producing a signal representative of aircraft static pressure; means for combining said total pressure signal with said static pressure signal to produce a signal representative of aircraft dynamic pressure; means for converting said aircraft dynamic pressure signal to an intermediate feel pressure signal; means for producing a signal representative of stabilizer position; means for producing a feel pressure zero intercept signal responsive to said stabilizer position signal; and means for combining said intermediate feel pressure signal with said feel pessure zero intercept signal to produce said feel pressure signal.
Claim 5
Independent Claim
81 words
The system of any one of claims 1 through 3 wherein said detector means comprises: a level detector for producing a trim signal in response to said ratio signal exceeding a predetermined first threshold and an end trim signal in response to said ratio signal falling below a predetermined second threshold; and a time amplitude detector for producing said predetermined trim command signals responsive to said level detector producing a trim signal for a predetermined portion of a predetermined time interval.
Claim 6
Dependent Claim
91 words
The system of claim 4 wherein said level detector comprises: means for producing a trim+ signal responsive to said ratio signal exceeding said first threshold in a positive sense; means for producing a trim- signal responsive to said ratio signal exceeding said first threshold in a negative sense; means for producing an end trim+ signal responsive to said ratio signal falling below said second threshold in a positive sense; and means for producing an end trim+ signal responsive to said ratio signal falling below said second threshold in a negative sense.
Claim 7
Independent Claim
83 words
A method for transferring trim control from an aircraft's elevators to the stabilizers during an automatic aircraft flight control mode, the method comprising the steps of: (a) producing a signal representative of the available elevator control in said automatic flight control mode; (b) producing a signal representative of actual elevator demand; (c) producing a signal representative of the ratio of said elevator demand signal to said available elevator control signal; and (d) producing predetermined stabilizer trim command signals responsive to said ratio signal.
Claim 8
Independent Claim
83 words
A method for transferring trim control from an aircraft's elevators to the stabilizers during an automatic aircraft flight control mode, the method comprising the steps of: (a) producing a signal representative of the available elevator control in said automatic flight control mode; (b) producing a signal representative of actual elevator demand; (c) producing a signal representative of the ratio of said elevator demand signal to said available elevator control signal; and (d) producing predetermined stabilizer trim command signals responsive to said ratio signal.
Claim 9
Dependent Claim
38 words
The method of claim 6 wherein step (a) comprises the steps of: (i) producing a signal representative of feel pressure on the aircraft's control column; and (ii) converting said feel pressure signal to said available elevator control signal.
Claim 10
Dependent Claim
98 words
The method of claim 7 wherein step (i) comprises the steps of: producing a signal representative of aircraft total pressure; producing a signal representative of aircraft static pressure; combining said total pressure signal with said static pressure signal to produce a signal representative of aircraft dynamic pressure; converting said aircraft dynamic pressure signal to an intermediate feel pressure signal; producing a signal representative of stabilizer position; producing a feel pressure zero intercept signal responsive to said stabilizer position signal; and combining said intermediate feel pressure signal with said feel pressure intercept signal to produce said feel pressure signal.
Claim 11
Independent Claim
75 words
The method of any one of claims 6 through 8 wherein step (d) comprises the steps of: (i) producing a trim signal in response to said ratio signal exceeding a predetermined first threshold; (ii) producing an end trim signal in response to said ratio signal falling below a predetermined second threshold; and (iii) producing said predetermined trim command signals responsive to said trim signal being produced for a predetermined portion of a predetermined time interval.
Claim 12
Dependent Claim
93 words
The method of claim 9 wherein: step (i) comprises the steps of: producing a trim+ signal responsive to said ratio signal exceeding said first threshold in a positive sense; and producing a trim- signal responsive to said ratio signal exceeding said first threshold in a negative sense; and step (ii) comprises the steps of: producing an end trim+ signal responsive to said ratio signal falling below said second threshold in a positive sense; and producing an end trim- signal responsive to said ratio signal falling below said second threshold in a negative sense.
References Cited (Backward Citations)
US24273A
Cited
USRE24273E
Cited
US3079109A
Cited
US3378217A
Cited
US3409251A
Cited
US3578268A
Cited
US4032093A
Cited
US4127248A
Cited
US4382282A
Cited
US4442490A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-08-03 | 1991-02-02 | 1991-08-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-08-03 | 1995-02-02 | 1995-08-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-08-03 | 1999-02-02 | 1999-08-04 | $7700.00 | Window Closed / Lapsed |