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US3653151A Expired / Lapsed US ⏱️ 0.0 years remaining

Airfoil structure

Assignee: Individual
•
Filing: 1970-10-13
•
Granted: 1972-04-04
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Expires: 1990-10-13
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Abstract

Abstract An airfoil is provided by distorting a relatively stiff piece of a solid material. One starts with an elongated thin, stiff material and forms a gore in the trailing surface and then at least partially closes the gore. This distorts the thin material into a stable, airfoil configuration.

Inventors

  • 👤 Andre J M Laurent

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 09:58
CPC Classifications
A; A63; A63H; A63H27/00

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 82 words
An airfoil structure comprising a generally elongate, thin, stiff material having bilateral symmetry and an elongate leading edge and an elongate trailing edge; a V-shaped gore in the center of the trailing edge with the apex of the V extending toward the leading edge but terminating short of the leading edge; and means for readily opening and closing the gore to distort the airfoil into a stable, self-supporting airfoil shape, said means enabling the characteristics of the airfoil to be readily altered.
Claim 2
Dependent Claim 82 words
An airfoil structure comprising a generally elongate, thin, stiff material having bilateral symmetry and an elongate leading edge and an elongate trailing edge; a V-shaped gore in the center of the trailing edge with the apex of the V extending toward the leading edge but terminating short of the leading edge; and means for readily opening and closing the gore to distort the airfoil into a stable, self-supporting airfoil shape, said means enabling the characteristics of the airfoil to be readily altered.
Claim 3
Dependent Claim 35 words
An airfoil structure as in claim 1, wherein said means comprises an adjustable turnbuckle fastened at opposite ends thereof to opposing facing edges of said gore to adjust the spacing between said opposing facing edges.
Claim 4
Dependent Claim 90 words
An airfoil structure comprising a generally elongate, thin, stiff material having bilateral symmetry and a leading edge and a trailing edge; a V-shaped gore cut in the center of the trailing edge with the apex of the V pointing toward and terminating short of the leading edge and having opposing facing spaced edges; and an adjustable turnbuckle connected at its opposite ends to the opposing facing edges of said V-shaped gore to selectively vary the spacing between said spaced edges to distort the wing into different, stable, self-supporting airfoil shapes.
Claim 5
Dependent Claim 90 words
An airfoil structure comprising a generally elongate, thin, stiff material having bilateral symmetry and a leading edge and a trailing edge; a V-shaped gore cut in the center of the trailing edge with the apex of the V pointing toward and terminating short of the leading edge and having opposing facing spaced edges; and an adjustable turnbuckle connected at its opposite ends to the opposing facing edges of said V-shaped gore to selectively vary the spacing between said spaced edges to distort the wing into different, stable, self-supporting airfoil shapes.

References Cited (Backward Citations)

US1227319A Cited
US2005842A Cited
US2472137A Cited
US2708330A Cited
US3010250A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-04-04 1975-10-04 1976-04-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-04-04 1979-10-04 1980-04-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-04-04 1983-10-04 1984-04-04 $7700.00 Window Closed / Lapsed

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