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US4021069A Expired / Lapsed US ⏱️ 0.0 years remaining

Apparatus for reducing aerodynamic drag

Assignee: NOSE CONE Manufacturing CO Inc
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Filing: 1975-09-29
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Granted: 1977-05-03
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Expires: 1995-09-29
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Abstract

Abstract Aerodynamic drag reducing apparatus for mounting on the bluff, forward face of the trailing element of an over the road vehicle. The apparatus comprises a contoured member carried on the forward face and extending outwardly therefrom with its point of maximum extension substantially aligned for impingement by an air stream. The portion of the surface displaced above the point of maximum extension describes a perturbed paraboloid of revolution with the rearward portions of the apparatus describing three sides of rectangle for aerodynamic merging with the top and side edges of the trailing element.

Inventors

  • 👤 Alan S. Hersh

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-26 09:19
CPC Classifications
B; B62; B62D; B62D35/00; B62D35/001

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 234 words
Apparatus for reducing the aerodynamic drag of a cargo carrying vehicle of the type having forward, side and top walls, said forward wall being contained in a substantially vertical plane disposed normal to the direction of travel of said vehicle, said apparatus comprising: an aerodynamic fairing carried on said forward wall for directing air flow about said vehicle, said fairing including: side and top edge portions aerodynamically shaped to merge with said top and side walls of said vehicle adjacent said forward wall thereof; a continuous contoured outer fairing surface extending away from said side and top edges and converging at a point of maximum extension; said fairing surface being substantially symmetrical horizontally about a central vertical plane normal to said forward wall so that air encountered during forward movement of said vehicle is directed toward both of said side walls; said fairing surface being asymmetrical vertically, with said point of maximum extension being disposed substantially vertically below the center of said fairing, so that the upper fairing surface above said point of maximum extension is substantially longer than the lower fairing surface therebeneath; said fairing acting to reduce air drag on said vehicle by directing air encountered by said fairing surface in such a manner that substantially all of said air flows rearwardly toward and along both sides and top of said vehicle, with the major portion normally being directed over the top.
Claim 2
Dependent Claim 234 words
Apparatus for reducing the aerodynamic drag of a cargo carrying vehicle of the type having forward, side and top walls, said forward wall being contained in a substantially vertical plane disposed normal to the direction of travel of said vehicle, said apparatus comprising: an aerodynamic fairing carried on said forward wall for directing air flow about said vehicle, said fairing including: side and top edge portions aerodynamically shaped to merge with said top and side walls of said vehicle adjacent said forward wall thereof; a continuous contoured outer fairing surface extending away from said side and top edges and converging at a point of maximum extension; said fairing surface being substantially symmetrical horizontally about a central vertical plane normal to said forward wall so that air encountered during forward movement of said vehicle is directed toward both of said side walls; said fairing surface being asymmetrical vertically, with said point of maximum extension being disposed substantially vertically below the center of said fairing, so that the upper fairing surface above said point of maximum extension is substantially longer than the lower fairing surface therebeneath; said fairing acting to reduce air drag on said vehicle by directing air encountered by said fairing surface in such a manner that substantially all of said air flows rearwardly toward and along both sides and top of said vehicle, with the major portion normally being directed over the top.
Claim 3
Dependent Claim 187 words
The apparatus of claim 1, wherein said outer surface at said point of maximum extension is defined by the formula: ##EQU2## where; Y is the distance from said forward wall taken perpendicular to the plane thereof; Y max is the maximum distance from said forward wall taken in a direction perpendicular to the plane thereof; z is the vertical distance from said point of maximum extension taken in a direction parallel to the plane of said wall; H is the distance from the bottom edge to the top edge of said vehicle, including said cargo portion, taken in a direction parallel to the plane of said forward wall; h is the distance from the bottom edge of said vehicle to the point of maximum extension taken in a direction parallel to the plane of said forward wall; x is the transverse distance taken from the center line of said forward wall; w is the transverse distance between said side walls of said cargo portion of said vehicle; and said surface from said point of maximum extension to said side and top edges is contoured to planar configuration.
Claim 4
Dependent Claim 29 words
The apparatus of claim 2, wherein said point of maximum extension of said outer surface is located when: Y max = Y; z = H-h; and x = 0.
Claim 5
Dependent Claim 16 words
The apparatus of claim 3, wherein Y max is between about 16 and about 24 inches.
Claim 6
Dependent Claim 36 words
The apparatus of claim 1, wherein said point of maximum extension is located on said outer surface for impingement by the stagnation stream surface when said fairing is mounted on said forward wall of said vehicle.
Claim 7
Dependent Claim 26 words
The apparatus of claim 1, wherein said upper fairing surface above a horizontal plane through said point of maximum extension describes a perterbed paraboloid of revolution.
Claim 8
Dependent Claim 34 words
The apparatus of claim 6, wherein said upper fairing surface is constrained to a substantially planar shape at said top and side edges to merge with the top and side walls of said vehicle.
Claim 9
Dependent Claim 81 words
The apparatus of claim 1, wherein said vehicle is a cargo trailer adapted to be towed by a separate power unit including a cab, said aerodynamic fairing being carried on said forward wall of the cargo trailer, and wherein said point of maximum extension of said outer fairing surface is so located on said forward wall as to be in substantial vertical alignment with the top surface of the cab of a power unit when the cargo trailer is being towed.
Claim 10
Dependent Claim 46 words
The apparatus of claim 8, wherein said lower fairing surface disposed below the horizontal plane of said point of maximum extension includes an effective bottom edge extending across said forward wall between said side edges a substantial distance above the bottom edge of said forward wall.
Claim 11
Dependent Claim 75 words
The apparatus of claim 1, wherein said vehicle has a power unit including a cab and a substantially rectangular cargo portion located behind said cab, said forward wall being the forward wall of said cargo portion, and wherein said point of maximum extension on said outer fairing surface is located in substantial vertical alignment with the top surface of the cab of said power unit when said aerodynamic fairing is mounted on said forward wall.
Claim 12
Dependent Claim 46 words
The apparatus of claim 1, wherein said lower fairing surface disposed below the horizontal plane of said point of maximum extension includes an effective bottom edge extending across said forward wall between said side edges a substantial distance above the bottom edge of said forward wall.
Claim 13
Dependent Claim 56 words
The apparatus of claim 11, wherein said bottom edge of said fairing is substantially linear and is provided with an angularly oriented flange extending between said side edges, said flange having an inner surface which is contiguous with said forward surface of said trailing element in a direction parallel to the plane of said forward wall.

References Cited (Backward Citations)

US1648505A Cited
US2514695A Cited
US3241876A Cited
US3425740A Cited
US3814472A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-05-02 1980-11-01 1981-05-03 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-05-02 1984-11-01 1985-05-03 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-05-02 1988-11-01 1989-05-03 $7700.00 Window Closed / Lapsed

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