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US3827658A Expired / Lapsed US ⏱️ 0.0 years remaining

Actuating means for a vane

Assignee: Lockheed Martin Corp
•
Filing: 1973-04-05
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Granted: 1974-08-06
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Expires: 1993-04-05
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Abstract

Abstract A mechanism, two of which position a vane in proper working and aerodynamic relationship with a flap throughout the latter''s travel in a Fowler flap assembly for an aircraft. The forward end of a folding linkage is operatively connected, via a vane support fitting, to a vane, and is operatively connected at its rear end to a flap. Each vane support fitting is secured to one or more carriages having banks of rollers mounted on tracks fixed to wing structure. A cam is mounted on the forward end of the linkage to co-act with a follower stationarily disposed upon wing structure. In flap extension, the latching of cam upon follower prevents the folded linkage, its vane support fitting and vane from further opening and extending. Continued rotation of the unfolding linkage and cam provides disengagement from the follower. The linkage unfolds to a biased stiff or unyielding position as the flap pulls the linkage. In flap retraction, engagement of cam with follower breaks the biased unyielding position of the linkage. The linkage folds as the flap retracts. The vane does not further retract until the linkage is folded to a degree where the cam can pass by its follower. The folding linkage includes a spring-piston-cable arrangement which assures biasing thereof in its unyielding and extended position, until the cam engages the follower in the retracting mode for the flap.

Inventors

  • 👤 R Hallworth

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 19:54
CPC Classifications
B; B64; B64C; B64C9/00; B64C9/14; B64C9/16; B64C9/20; Y; Y10; Y10T; Y10T74/00; Y10T74/20; Y10T74/20012

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 361 words
In an aircraft wing lift increasing device including a vane and flap positioned and functioning in accordance with a Fowler flap action or principle and which includes means for mounting the vane and flap independently of each other but in sliding relation to their wing structure for the purposes of extending and retracting them in an efficient aerodynamic relationship, an improvement for actuating the vane in proper and efficient relationship to the flap in such extension and retraction modes, and comprising in combination, foldable linkage means comprising a pair of rigid members hingedly attached together at their adjacent ends, the respective free ends of said members constituting a forward end and a rear end for said linkage means, respectively, means for biasing said members towards an unyielding, unfolded position for said linkage means, a cam member in fixed and non-rotatable relation to and mounted on said forward end for rotation with its rigid member as said members unfold and fold, said forward end and cam member being adapted for rotation about the mounting means for the vane, and means mounted on the wing structure and upon which said cam member engages as said linkage means movingly folds and unfolds during the extending and retracting modes for the vane and flap, said cam member being disposed forwardly of said mounted means and with folded position for its linkage means, said cam member engaging said mounted means to prevent extension of the vane as the flap extends until the flap extends to a point at which said linkage means becomes unfolded to cause said cam member to become disengaged from said mounted means to provide for extension of the vane as the flap continues to extend, said cam member with its unyielding, unfolded linkage means being disposed rearwardly of said mounted means, the vane remaining extended until said cam member engages said mounted means as the flap is retracting, such engagement overcoming said biasing means to break the unfolded linkage means, said linkage means continuing to fold to a point where said cam member disengages from said mounted means to thereby provide for retraction of the vane as the flap continues to retract.
Claim 2
Dependent Claim 361 words
In an aircraft wing lift increasing device including a vane and flap positioned and functioning in accordance with a Fowler flap action or principle and which includes means for mounting the vane and flap independently of each other but in sliding relation to their wing structure for the purposes of extending and retracting them in an efficient aerodynamic relationship, an improvement for actuating the vane in proper and efficient relationship to the flap in such extension and retraction modes, and comprising in combination, foldable linkage means comprising a pair of rigid members hingedly attached together at their adjacent ends, the respective free ends of said members constituting a forward end and a rear end for said linkage means, respectively, means for biasing said members towards an unyielding, unfolded position for said linkage means, a cam member in fixed and non-rotatable relation to and mounted on said forward end for rotation with its rigid member as said members unfold and fold, said forward end and cam member being adapted for rotation about the mounting means for the vane, and means mounted on the wing structure and upon which said cam member engages as said linkage means movingly folds and unfolds during the extending and retracting modes for the vane and flap, said cam member being disposed forwardly of said mounted means and with folded position for its linkage means, said cam member engaging said mounted means to prevent extension of the vane as the flap extends until the flap extends to a point at which said linkage means becomes unfolded to cause said cam member to become disengaged from said mounted means to provide for extension of the vane as the flap continues to extend, said cam member with its unyielding, unfolded linkage means being disposed rearwardly of said mounted means, the vane remaining extended until said cam member engages said mounted means as the flap is retracting, such engagement overcoming said biasing means to break the unfolded linkage means, said linkage means continuing to fold to a point where said cam member disengages from said mounted means to thereby provide for retraction of the vane as the flap continues to retract.

References Cited (Backward Citations)

US2169416A Cited
US2404956A Cited
US2826379A Cited
US3528632A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-08-05 1978-02-04 1978-08-06 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-08-05 1982-02-04 1982-08-06 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-08-05 1986-02-04 1986-08-06 $7700.00 Window Closed / Lapsed

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