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Patent
D307259
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Priority
Nov 23 1987
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Filed
Nov 23 1987
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Issued
Apr 17 1990
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Expiry
Apr 17 2004
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Assg.orig
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Entity
unknown
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9
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6
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n/a
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The ornamental design for an aircraft hot air release shroud, as shown and described.
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FIG. 1 is a side perspective view of an aircraft hot air release shroud
showing my new design;
FIG. 2 is an enlarged top and right side perspective view thereof;
FIG. 3 is an enlarged top and left side perspective view thereof; and
FIG. 4 is a front elevational view thereof.
The broken lines shown in FIGS. 1 through 4 are for illustrative purposes
only and form no part of the claimed design.
Holt, Hiram B.
Patent |
Priority |
Assignee |
Title |
3129910, |
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3717163, |
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3838425, |
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4372505, |
Dec 17 1979 |
The Boeing Company |
Supersonic inlet having variable area sideplate openings |
4378097, |
Nov 24 1980 |
The Boeing Company |
High performance submerged air inlet |
4418708, |
Mar 12 1980 |
MESSERSCHMITT-BOLKOW-BLOHM GESELLSCHAFT MIT BESCHRANKTER HAFTUNG, POSTFACH 801109, 8000 MUNICH 80, GERMANY |
Two-dimensional, unilateral oblique shock diffuser as the air inlet for a gas turbine jet engine for the propulsion of heavy-duty aircraft |
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