Patent US4674716A successfully refreshed from Google Patents.
US4674716A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Blown crescent airfoil
Assignee: Grumman Corp
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Filing: 1985-03-13
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Granted: 1987-06-23
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Expires: 2005-03-13
Abstract
Abstract A supercritical movable airfoil over which is blown air to obtain a Coanda affect. A sealing strip is provided on a stationary airfoil portion which seals against the movable airfoil portion during blowing to prevent flow of air therebetween.
Inventors
- 👤 William H. Moore
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 14:56
CPC Classifications
B; B64; B64C; B64C9/00; B64C9/38; B64C23/00; B64C3/00; B64C3/38; B64C3/44; B64C3/50; B64C2230/00; B64C2230/04; Y; Y02; Y02T; Y02T50/00; Y02T50/10; Y02T50/30; Y02T50/40
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
235 words
In an airfoil having a stationary portion and a movable portion, said stationary portion of said airfoil comprising a wing having an upper surface, an undersurface and a trailing edge and said movable portion of said airfoil comprising an upper surface of convex curvature in cross-sectional profile and a lower surface of concave curvature in cross-sectional profile, a device for increasing performance and saving weight in said airfoil, said device comprising a bleed air system for supplying pressurized air to the stationary portion of said airfoil; an air chamber in said stationary portion for receiving said pressurized air, said air chamber having an upper panel and a substantially flexible lower panel movable downwardly away from said upper panel upon bleed air pressurization of said chamber and a nozzle for the exhaust of pressurized air in said chamber; a crescent-shaped airfoil constituting the movable portion of said airfoil pivotally connected to said stationary portion in a manner whereby said crescent-shaped airfoil underlies said lower panel of said chamber; and an essentially frictionless seal strip extending outwardly from said lower panel of said chamber and abutting said crescent-shaped airfoil to prevent airflow from the undersurface of said airfoil to between said stationary portion and said crescent-shaped airfoil upon bleed air pressurization of said air chamber, said seal extending from said undersurface of said wing and limiting movement of said undersurface in a predetermined area of said undersurface.
Claim 2
Dependent Claim
235 words
In an airfoil having a stationary portion and a movable portion, said stationary portion of said airfoil comprising a wing having an upper surface, an undersurface and a trailing edge and said movable portion of said airfoil comprising an upper surface of convex curvature in cross-sectional profile and a lower surface of concave curvature in cross-sectional profile, a device for increasing performance and saving weight in said airfoil, said device comprising a bleed air system for supplying pressurized air to the stationary portion of said airfoil; an air chamber in said stationary portion for receiving said pressurized air, said air chamber having an upper panel and a substantially flexible lower panel movable downwardly away from said upper panel upon bleed air pressurization of said chamber and a nozzle for the exhaust of pressurized air in said chamber; a crescent-shaped airfoil constituting the movable portion of said airfoil pivotally connected to said stationary portion in a manner whereby said crescent-shaped airfoil underlies said lower panel of said chamber; and an essentially frictionless seal strip extending outwardly from said lower panel of said chamber and abutting said crescent-shaped airfoil to prevent airflow from the undersurface of said airfoil to between said stationary portion and said crescent-shaped airfoil upon bleed air pressurization of said air chamber, said seal extending from said undersurface of said wing and limiting movement of said undersurface in a predetermined area of said undersurface.
Claim 3
Dependent Claim
53 words
An airfoil as claimed in claim 1, further comprising mounting means mounting said movable portion of said airfoil to nest within the trailing edge of said wing whereby in the nested position said movable portion of said airfoil lies under said trailing edge and is positioned as a chordal extension of said wing.
Claim 4
Dependent Claim
34 words
An airfoil as claimed in claim 1, wherein said nozzle extends along a predetermined span of said trailing edge to exhaust said fluid over the upper surface of said movable portion of said airfoil.
Claim 5
Dependent Claim
39 words
An airfoil as claimed in claim 1, further comprising actuator means connected to said crescent-shaped airfoil for moving said crescent-shaped airfoil from its nested position with said stationary portion to a normal attitude therewith to provide a speed brake.
Claim 6
Dependent Claim
40 words
An airfoil as claimed in claim 1, wherein said stationary portion of said airfoil includes a slotted area from said undersurface to said upper surface and a flaperon for controlling the opening of said slotted area at said upper surface.
Claim 7
Dependent Claim
33 words
An airfoil as claimed in claim 2, wherein said mounting means permits said movable portion of said airfoil to assume any number of positions from generally aligned with said wing to normal thereto.
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) | 1990-06-22 | 1990-12-22 | 1991-06-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-06-22 | 1994-12-22 | 1995-06-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-06-22 | 1998-12-22 | 1999-06-23 | $7700.00 | Window Closed / Lapsed |