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US4736912A Expired / Lapsed US ⏱️ 0.0 years remaining

Apparatus for reducing turbulent drag

Assignee: Airbus Defence and Space GmbH
•
Filing: 1987-08-12
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Granted: 1988-04-12
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Expires: 2007-08-12
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Abstract

Abstract The turbulent drag is reduced on the surface of a body moving through a fluid by providing longitudinal channels in the surface, for example of an aircraft wing, which channels extend in parallel to the flow direction and which channels are interconnected with the boundary layer by a longitudinal gap communicating the channel with the boundary layer.

Inventors

  • 👤 Gerhard Loebert

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 01:09
CPC Classifications
B; B64; B64C; B64C23/00; B63; B63B; B63B1/00; B63B1/32; B63B1/34; B64C21/00; B64C21/10; B64C2230/00; B64C2230/20; Y; Y02; Y02T; Y02T50/00; Y02T50/10; Y02T70/00; Y02T70/10

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 162 words
An apparatus for reducing turbulent drag caused on a surface of a body by relative movement between said body and a fluid, said movement defining a given movement direction, comprising a surface zone in said body adjacent to said body surface in direct contact with said fluid, a plurality of longitudinal channels inside said surface zone, said channels extending in parallel to each other and in parallel to said given movement direction, each channel comprising a longitudinal gap in said body surface communicating the respective channel with a boundary layer of said fluid on said body surface, said channels having an internal width (b, b') which is within the range of about 0.5 to 10 mm to be sufficiently small for assuring a laminar pipe flow inside said longitudinal channels, said longitudinal gaps having a width (s) which has a determined ratio to said sufficiently small internal channel width (b, b'), such that said ratio is smaller than or equal to 1.
Claim 2
Independent Claim 162 words
An apparatus for reducing turbulent drag caused on a surface of a body by relative movement between said body and a fluid, said movement defining a given movement direction, comprising a surface zone in said body adjacent to said body surface in direct contact with said fluid, a plurality of longitudinal channels inside said surface zone, said channels extending in parallel to each other and in parallel to said given movement direction, each channel comprising a longitudinal gap in said body surface communicating the respective channel with a boundary layer of said fluid on said body surface, said channels having an internal width (b, b') which is within the range of about 0.5 to 10 mm to be sufficiently small for assuring a laminar pipe flow inside said longitudinal channels, said longitudinal gaps having a width (s) which has a determined ratio to said sufficiently small internal channel width (b, b'), such that said ratio is smaller than or equal to 1.
Claim 3
Dependent Claim 13 words
The apparatus of claim 1, wherein said longitudinal channels have a circular cross-section.
Claim 4
Dependent Claim 14 words
The apparatus of claim 1, wherein said longitudinal channels have a substantially square cross-section.
Claim 5
Dependent Claim 37 words
The apparatus of claim 1, wherein said channels have a given width and are closely spaced from each other so that a partition wall between neighboring channels has a thickness substantially smaller than said given channel width.
Claim 6
Dependent Claim 51 words
The apparatus of claim 1, wherein said channel has a given channel width (b), and wherein said longitudinal gap has a gap width (s), said channel width and said gap width being so dimensioned that the ratio of s to b is within a determined range of about 0.1 to 1.0.
Claim 7
Dependent Claim 67 words
The apparatus of claim 1, wherein said longitudinal channels have ends which merge gradually into said body surface in said movement direction so that a transition is formed between a body surface portion without said longitudinal channels and said surface zone having said longitudinal channels, said longitudinal channels having a narrow channel width where said transition begins, said narrow channel width widening toward a constant channel width.

References Cited (Backward Citations)

US1303544A Cited
US2899150A Cited
FR656859A Cited
DE845900C Cited
US2800291A Cited
US3137261A Cited
US4650138A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-04-12 1991-10-12 1992-04-12 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-04-12 1995-10-12 1996-04-12 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-04-12 1999-10-12 2000-04-12 $7700.00 Window Closed / Lapsed

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