Patent US4121483A successfully refreshed from Google Patents.
US4121483A
Expired / Lapsed
US
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Aircraft flight control system
Assignee: RTX Corp
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Filing: 1977-02-10
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Granted: 1978-10-24
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Expires: 1997-02-10
Abstract
Abstract An aircraft flight control including a linkage system having a walking beam to which control inputs are imparted and from which a control output is taken and having anti-jamming and over-control abatement provisions.
Inventors
- 👤 Albert Raymond Sedlock
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 20:20
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/54; B64C27/58; B64C27/64; Y; Y10; Y10T; Y10T137/00; Y10T137/1624; Y10T137/1632; Y10T137/1789; Y10T74/00; Y10T74/20; Y10T74/20207; Y10T74/20372; Y10T74/20384; Y10T74/2039
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
240 words
An aircraft flight control system having a linkage system including: (A) a pivotally supported walking beam, (B) control output means operatively connected to said walking beam so as to be actuated by pivot motion of said walking beam, (C) first control input means operatively connected to impart motion input to said walking beam to cause said walking beam to pivot and thereby actuate said output means, (D) second control input means operatively connected to impart motion input to said walking beam to cause said walking beam to pivot and thereby actuate said output means, (E) said walking beam being of two-piece construction with each piece pivotally supported about the walking beam pivot axis and including: (1) a shear pin operative to join the two pieces of the walking beam so as to operate as a unitary walking beam during normal operation and so that when one of said input means is jammed to thereby prevent pivot motion of the unitary walking beam, increased input force from the other input means will cause said shear pin to shear and free said walking beam pieces so that the other input means can impart pivot motion to one of said walking beam pieces and thereby actuate said output means, and (2) over-control abatement means operative to resist motion input to said walking beam from said other input means after said shear pin shears so as to prevent excessive actuation of said output means.
Claim 2
Dependent Claim
240 words
An aircraft flight control system having a linkage system including: (A) a pivotally supported walking beam, (B) control output means operatively connected to said walking beam so as to be actuated by pivot motion of said walking beam, (C) first control input means operatively connected to impart motion input to said walking beam to cause said walking beam to pivot and thereby actuate said output means, (D) second control input means operatively connected to impart motion input to said walking beam to cause said walking beam to pivot and thereby actuate said output means, (E) said walking beam being of two-piece construction with each piece pivotally supported about the walking beam pivot axis and including: (1) a shear pin operative to join the two pieces of the walking beam so as to operate as a unitary walking beam during normal operation and so that when one of said input means is jammed to thereby prevent pivot motion of the unitary walking beam, increased input force from the other input means will cause said shear pin to shear and free said walking beam pieces so that the other input means can impart pivot motion to one of said walking beam pieces and thereby actuate said output means, and (2) over-control abatement means operative to resist motion input to said walking beam from said other input means after said shear pin shears so as to prevent excessive actuation of said output means.
Claim 3
Dependent Claim
19 words
A flight control system accordng to claim 1 wherein said over-control abatement means is fabricated for selectively limited operation.
Claim 4
Dependent Claim
42 words
A control system according to claim 2 wherein said over-control abatement means is a one-stroke hydraulic or pneumatic cylinder-piston arrangement fabricated to offer resistance to relative motion between said piston and cylinder for a single stroke therebetween and to be inoperative thereafter.
Claim 5
Dependent Claim
123 words
A control system according to claim 3 wherein said over-control abatement means includes a cam mechanism located on one of said walking beam pieces and a hydraulic or pneumatic cylinder-piston assembly located on the other of said walking beam pieces and operatively connected so that when the shear pin shears the relative motion between the walking beam pieces will cause the cam to drive the piston in one-stroke reciprocating motion within the cylinder so as to displace the fluid in the cylinder-piston assembly to perform a motion damping function for a single stroke of the piston within the cylinder in one direction and so that the cylinder remains retracted following that single stroke so as to be out of contact with the cam.
Claim 6
Dependent Claim
31 words
A control system according to claim 1 wherein said other input means is a manually imposed pilot input control and so that said jammed input means is a pilot "feel" control.
Claim 7
Dependent Claim
55 words
A control system according to claim 3 wherein one of said control input means is connected to one of said walking beam pieces so as to cause it to pivot while the other of said control input means is connected to the other of said walking beam pieces so as to cause it to pivot.
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) | 1981-10-23 | 1982-04-24 | 1982-10-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-10-23 | 1986-04-24 | 1986-10-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-10-23 | 1990-04-24 | 1990-10-24 | $7700.00 | Window Closed / Lapsed |