US5037044A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aerodynamic or hydrodynamic surfaces
Assignee: BAE Systems PLC
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Filing: 1987-11-04
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Granted: 1991-08-06
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Expires: 2007-11-04
Abstract
Abstract An aerodynamic or hydrodynamic surface having a swept-back leading edge includes at least one flow separation device located on an attachment line of the leading edge, such as a step-up, step-down, fence or gap. The flow separation devices are preferably arranged normal to the leading edge and are dimensioned so that span-wise turbulent air flow is re-laminarized downstream of the devices thus reducing skin-friction and greatly improving the aerodynamic or hydrodynamic efficiency of the surface.
Inventors
- 👤 George R. Seyfang
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 10:42
CPC Classifications
B; B64; B64C; B64C23/00; B64C23/06; B64C2230/00; B64C2230/20; B64C2230/28; Y; Y02; Y02T; Y02T50/00; Y02T50/10
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
106 words
An aerodynamic or hydrodynamic surface having a leading edge inclined at an angle to the normal to the general flow of air or water respectively over said surface when in use, including at least one leading edge boundary layer laminar flow control means, defined on said leading edge substantially at an attachment line thereof, for re-laminarising turbulent flow along the span-wise direction of the surface, said at least one boundary layer laminar flow control means including at least one of a rearward facing step and a forward facing step having a height in the range 2%r to 40%r where r is radius of the leading edge.
Claim 2
Dependent Claim
106 words
An aerodynamic or hydrodynamic surface having a leading edge inclined at an angle to the normal to the general flow of air or water respectively over said surface when in use, including at least one leading edge boundary layer laminar flow control means, defined on said leading edge substantially at an attachment line thereof, for re-laminarising turbulent flow along the span-wise direction of the surface, said at least one boundary layer laminar flow control means including at least one of a rearward facing step and a forward facing step having a height in the range 2%r to 40%r where r is radius of the leading edge.
Claim 3
Dependent Claim
48 words
An aerodynamic or hydrodynamic surface as claimed in claim 1 wherein the at least one boundary layer laminar flow control means comprises a combination of a forward facing step and a rearward facing step spaced a relatively short distance apart and defining a fence on said leading edge.
Claim 4
Dependent Claim
30 words
An aerodynamic or hydrodynamic surface as claimed in claim 1 and where the boundary layer laminar flow control means is defined so as to be normal to said leading edge.
Claim 5
Dependent Claim
162 words
An aerodynamic or hydrodynamic surface having a leading edge inclined at an angle to the normal to the general flow of air or water respectively over said surface when in use, including at least on boundary layer laminar flow control means, defined on said leading edge substantially at an attachment line thereof, for re-laminarising turbulent flow along the span-wise direction of the surface, said at least one boundary layer laminar flow control means including at least one of a rearward facing step and a forward facing step having a height in the range 2%r to 40%r where r is radius of the leading edge, the at least one boundary layer laminar flow control means comprising a combination of a rearward facing step and a forward facing step spaced a relatively short distance apart and defining a gap in said leading edge, the gap depth and the gap width being substantially equal to 10%r where r is the radius of the leading edge.
Claim 6
Dependent Claim
162 words
An aerodynamic or hydrodynamic surface having a leading edge inclined at an angle to the normal to the general flow of air or water respectively over said surface when in use, including at least on boundary layer laminar flow control means, defined on said leading edge substantially at an attachment line thereof, for re-laminarising turbulent flow along the span-wise direction of the surface, said at least one boundary layer laminar flow control means including at least one of a rearward facing step and a forward facing step having a height in the range 2%r to 40%r where r is radius of the leading edge, the at least one boundary layer laminar flow control means comprising a combination of a rearward facing step and a forward facing step spaced a relatively short distance apart and defining a gap in said leading edge, the gap depth and the gap width being substantially equal to 10%r where r is the radius of the leading edge.
References Cited (Backward Citations)
DE434778C
Cited
US2358985A
Cited
US2885161A
Cited
US2743888A
Cited
US2769602A
Cited
US3130944A
Cited
US3288399A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-08-05 | 1995-02-04 | 1995-08-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-08-05 | 1999-02-04 | 1999-08-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-08-05 | 2003-02-04 | 2003-08-06 | $7700.00 | Window Closed / Lapsed |