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US4198219A Expired / Lapsed US ⏱️ 0.0 years remaining

Air inlet grille for engine compartment

Assignee: United States Department of the Army
•
Filing: 1978-11-22
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Granted: 1980-04-15
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Expires: 1998-11-22
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Abstract

Abstract An air inlet grille for an engine compartment of a military ground vehiclesed in dusty atmospheres, e.g. the desert. The grille comprises a number of relatively thick air-guiding louvers of sinuous shape, each louver being relatively thick in the transverse direction so that the grille has ballistic properties, i.e. the ability to deflect or intercept enemy projectiles directed toward the engine disposed behind the grille. Each louver includes or contains a dust removal mechanism immediately downstream from each air-turn surface on the louver, whereby the grille is enabled to clean the dust-laden air, thereby preventing ambient dust from coating the engine and/or the air passages of engine coolers and radiators.

Inventors

  • 👤 William J. Krisko

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 17:05
CPC Classifications
B; B01; B01D; B01D45/00; B01D45/04; B01D45/08

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 359 words
In a military vehicle having an engine compartment: the improvement comprising an air inlet grille positioned on the vehicle to remove dust particles from air flowing into the engine compartment; said grille comprising a series of sinuous vanes arranged in spaced parallel relation to define S-shaped air passages; each vane having a chisel-shaped leading edge (18), a rounded convergent trailing edge (22), and two reversely curved side surfaces extending from the leading edge to the trailing edge; each vane being a solid non-hollow structure that is approximately five eighth inch thick measured across the vane side surfaces, whereby grille integrity is maintained when enemy projectiles are directed thereagainst; the vanes being spaced so that the defined air passages have slightly less transverse thicknesses than the vanes; one side surface of each vane comprising a first curved concave air-turn surface (16) extending from the vane leading edge and a curved convex surface extending from the air-turn surface to the vane trailing edge; the other side surface of each vane comprising a curved convex surface extending from the vane leading edge and a second curved concave air-turn surface (20) extending from the last-mentioned convex surface to the vane trailing edge; each vane having a first internal cavity (34) at the downstream end of the first concave air-turn surface, and a second internal cavity (54) near the downstream end of the second concave air-turn surface; a slot communicating each cavity with the immediately adjacent concave air-turn surface; a skimmer wall projecting from the vane at the downstream edge of each slot to deflect concentrated dust through the slot into the associated cavity; the upstream face of each skimmer wall being at an acute angle to the associated air-turn surface to guide dust particles into the slot; each skimmer wall projecting from the vane surface into the adjacent passage through a distance (29) that is in the range of 40% to 50% of the passage width; each slot having a width that is in the range from one tenth inch to two tenth inch; and scavenger fan means connected to each cavity for applying a suction force on each of the associated slots.
Claim 2
Dependent Claim 359 words
In a military vehicle having an engine compartment: the improvement comprising an air inlet grille positioned on the vehicle to remove dust particles from air flowing into the engine compartment; said grille comprising a series of sinuous vanes arranged in spaced parallel relation to define S-shaped air passages; each vane having a chisel-shaped leading edge (18), a rounded convergent trailing edge (22), and two reversely curved side surfaces extending from the leading edge to the trailing edge; each vane being a solid non-hollow structure that is approximately five eighth inch thick measured across the vane side surfaces, whereby grille integrity is maintained when enemy projectiles are directed thereagainst; the vanes being spaced so that the defined air passages have slightly less transverse thicknesses than the vanes; one side surface of each vane comprising a first curved concave air-turn surface (16) extending from the vane leading edge and a curved convex surface extending from the air-turn surface to the vane trailing edge; the other side surface of each vane comprising a curved convex surface extending from the vane leading edge and a second curved concave air-turn surface (20) extending from the last-mentioned convex surface to the vane trailing edge; each vane having a first internal cavity (34) at the downstream end of the first concave air-turn surface, and a second internal cavity (54) near the downstream end of the second concave air-turn surface; a slot communicating each cavity with the immediately adjacent concave air-turn surface; a skimmer wall projecting from the vane at the downstream edge of each slot to deflect concentrated dust through the slot into the associated cavity; the upstream face of each skimmer wall being at an acute angle to the associated air-turn surface to guide dust particles into the slot; each skimmer wall projecting from the vane surface into the adjacent passage through a distance (29) that is in the range of 40% to 50% of the passage width; each slot having a width that is in the range from one tenth inch to two tenth inch; and scavenger fan means connected to each cavity for applying a suction force on each of the associated slots.
Claim 3
Dependent Claim 16 words
The improvement of claim 1 wherein each slot has a width that is approximately 0.14 inch.
Claim 4
Dependent Claim 23 words
The improvement of claim 1 wherein the projection of each skimmer wall into the adjacent passage is approximately 40% of the passage width.
Claim 5
Dependent Claim 36 words
The improvement of claim 1 wherein each vane is metal, except that the second air-turn surface on each vane is defined by a relatively soft plastic insert of sufficient thickness to imbed ricocheting ballistic fragments therein.
Claim 6
Dependent Claim 33 words
The improvement of claim 1 wherein each cavity has an approximately circular cross-sectional configuration devoid of shape internal corners that would otherwise impede swirling motion of concentrated dust toward the scavenger fan means.

References Cited (Backward Citations)

US2816658A Cited
US3237777A Cited
US3368332A Cited
US3673771A Cited
US3977977A Cited
US3970439A Cited
US4061478A Cited
US4141706A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-04-15 1983-10-15 1984-04-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-04-15 1987-10-15 1988-04-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-04-15 1991-10-15 1992-04-15 $7700.00 Window Closed / Lapsed

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