Patent US3936013A successfully refreshed from Google Patents.
US3936013A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Vortex control
Assignee: Individual
•
Filing: 1973-12-17
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Granted: 1976-02-03
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Expires: 1993-12-17
Abstract
Abstract This invention is for wings of all types, such as fixed wings for aircraft and hydrofoil boats, and rotary blades (or wings) for helicopters and turbines, to be equipped with a slotted tube, or a tube with series of holes extending outwardly in the spanwise direction near the trailing edge of the wing tip for blowing jets of fluid (such as air or water) in the direction opposite to the lift of the wing, thereby achieving flow in the form of a jet sheet to abate, diffuse and break up the undesirable wing-tip or blade-tip vortices.
Inventors
- 👤 Shao Wen Yuan
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 21:53
CPC Classifications
B; B64; B64C; B64C23/00; B64C23/06; B64C23/065; Y; Y02; Y02T; Y02T50/00; Y02T50/10
Claims Analysis
Total Claims: 21
Claim 1
Independent Claim
213 words
Apparatus for abating wing-tip vortices formed at the tips of a wing when it is in a fluid stream flowing relative to said wing, said vortices being formed as a result of a difference in fluid pressure on one side of the wing relative to the fluid pressure on the opposite side of the wing which causes a rush flow of fluid from the side of higher pressure to the side of lower pressure, said apparatus comprising a wing having at least a pair of wing tips, a source of pressurized fluid, a plurality of jetting means, and means connecting said jetting means to said source of pressurized fluid, each of said plurility of jetting means of being located outwardly of a respective one of said tips for simultaneously emmiting pressurized fluid from said jetting means in the direction toward said side of higher pressure and in a plane substantially perpendicular to the direction of flow of said fluid stream, said wing including a leading edge and a trailing edge, said fluid stream which flows relative to said wing passing from the leading edge toward said trailing edge, and said jetting means are located downstream of the position of the mid-chord of said tips which lies halfway between said leading and trailing edges.
Claim 2
Dependent Claim
213 words
Apparatus for abating wing-tip vortices formed at the tips of a wing when it is in a fluid stream flowing relative to said wing, said vortices being formed as a result of a difference in fluid pressure on one side of the wing relative to the fluid pressure on the opposite side of the wing which causes a rush flow of fluid from the side of higher pressure to the side of lower pressure, said apparatus comprising a wing having at least a pair of wing tips, a source of pressurized fluid, a plurality of jetting means, and means connecting said jetting means to said source of pressurized fluid, each of said plurility of jetting means of being located outwardly of a respective one of said tips for simultaneously emmiting pressurized fluid from said jetting means in the direction toward said side of higher pressure and in a plane substantially perpendicular to the direction of flow of said fluid stream, said wing including a leading edge and a trailing edge, said fluid stream which flows relative to said wing passing from the leading edge toward said trailing edge, and said jetting means are located downstream of the position of the mid-chord of said tips which lies halfway between said leading and trailing edges.
Claim 3
Dependent Claim
18 words
Apparatus as defined in claim 1 wherein said jetting means includes means for continuously emitting said pressurized fluid.
Claim 4
Dependent Claim
38 words
Apparatus as defined in claim 1 wherein said jetting means includes a tube having fluid port means formed therein for emitting said pressurized fluid, and said tube extends outwardly from a respective wing tip in the spanwise direction.
Claim 5
Dependent Claim
33 words
Apparatus as defined in claim 3 wherein said fluid port means extends in the spanwise direction and has a length between approximately 3 and 15 percent of the semi-span length of said wing.
Claim 6
Dependent Claim
14 words
Apparatus as defined in claim 3 wherein said fluid port means comprises a slot.
Claim 7
Dependent Claim
23 words
Apparatus as defined in claim 3 wherein said fluid port means comprises a plurality of orifices extending in a line along said tube.
Claim 8
Dependent Claim
15 words
Apparatus as defined in claim 3 wherein said tube is located downstream from said wing.
Claim 9
Dependent Claim
52 words
Apparatus as defined in claim 1 wherein said jetting means includes a tube having fluid port means formed therein for emitting said pressurized fluid, and said tube is located downstream from said trailing edge up to a distance approximately equal to a length measured between said leading edge and said trailing edge.
Claim 10
Dependent Claim
15 words
Apparatus as defined in claim 5 wherein said slot varies in width along said tube.
Claim 11
Dependent Claim
15 words
Apparatus as defined in claim 6 wherein said plurality of orifices are of varying sizes.
Claim 12
Dependent Claim
32 words
Apparatus as defined in claim 1 wherein said jetting means includes means for adjusting the angular direction of the emitted pressurized fluid with respect to a plane parallel to the wing planform.
Claim 13
Dependent Claim
37 words
Apparatus as defined in claim 3 including means for rotating said tube about its longitudinal axis for adjusting the angular direction of the emitted pressurized fluid with respect to the direction of flow of said fluid stream.
Claim 14
Dependent Claim
24 words
Apparatus as defined in claim 1 wherein said jetting means includes means for intermittently emitting said pressurized fluid according to a predetermined time sequence.
Claim 15
Dependent Claim
27 words
Apparatus as defined in claim 1 wherein said wing is a portion of a fixed-wing aircraft, and said wing is attached to a fuselage of said aircraft.
Claim 16
Dependent Claim
31 words
Apparatus as defined in claim 1 wherein said wing is a portion of a rotary-wing aircraft of the type including rotary blade means and said wing is said rotary blade means.
Claim 17
Dependent Claim
29 words
Apparatus as defined in claim 1 wherein said wing is a portion of a boat of the type including a lift foil, and said wing is said lift foil.
Claim 18
Independent Claim
181 words
A method for abating wing-tip vortices formed at the tips of a wing when it is located in a fluid stream flowing relative to said wing, said vortices being formed as the wing which causes a rush flow of fluid from the side of higher pressure to the side of lower pressure, said method comprising the steps of providing a wing having at least a pair of wing tips, providing a supply of pressurized fluid, and simultaneously emitting a jet of said pressurized fluid from a region located adjacent to and outwardly of each of said wing tips in a direction toward said side of higher pressure and in a plane substantially perpendicular to the direction of flow of said fluid stream, said wing including a leading edge and a trailing edge and said fluid stream passes from the leading edge to the trailing edge, and said step of emitting a jet of pressurized fluid comprises emitting said jet at a location downstream of the position of the mid-chord of said tips which lies halfway between said leading and trailing edges.
Claim 19
Independent Claim
181 words
A method for abating wing-tip vortices formed at the tips of a wing when it is located in a fluid stream flowing relative to said wing, said vortices being formed as the wing which causes a rush flow of fluid from the side of higher pressure to the side of lower pressure, said method comprising the steps of providing a wing having at least a pair of wing tips, providing a supply of pressurized fluid, and simultaneously emitting a jet of said pressurized fluid from a region located adjacent to and outwardly of each of said wing tips in a direction toward said side of higher pressure and in a plane substantially perpendicular to the direction of flow of said fluid stream, said wing including a leading edge and a trailing edge and said fluid stream passes from the leading edge to the trailing edge, and said step of emitting a jet of pressurized fluid comprises emitting said jet at a location downstream of the position of the mid-chord of said tips which lies halfway between said leading and trailing edges.
Claim 20
Dependent Claim
20 words
A method as defined in claim 17 wherein said pressurized fluid is emitted in the form of a jet sheet.
Claim 21
Dependent Claim
24 words
A method as defined in claim 17 wherein said pressurized fluid is emitted in the form of a plurality of closely spaced discrete streams.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-02-02 | 1979-08-04 | 1980-02-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-02-02 | 1983-08-04 | 1984-02-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-02-02 | 1987-08-04 | 1988-02-03 | $7700.00 | Window Closed / Lapsed |