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The ornamental design for an aircraft, as shown and described. |
FIG. 1 is a top perspective view of an aircraft showing my new design;
FIG. 2 is a bottom perspective view thereof;
FIG. 3 is a top plan view thereof;
FIG. 4 is a side elevation view thereof the opposite side being a mirror image of that shown;
FIG. 5 is a front elevation view thereof;
FIG. 6 is a rear elevation view thereof.
The broken lines shown in FIGS. 1 thru 6 of the drawing are for illustrative purposes only and form no part of the claimed design.
Patent | Priority | Assignee | Title |
7731121, | Sep 28 2004 | Textron Innovations Inc | Propulsive anti-torque system for rotorcraft |
D297005, | Mar 13 1986 | United Technologies Corporation | Helicopter |
Patent | Priority | Assignee | Title |
3351304, | |||
3957226, | Jan 27 1975 | The Boeing Company | Helicopter yaw and propulsion mechanism |
DE1406431, |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Nov 05 1984 | BINDEN, JOHN A | NORTHROP CORPORATION A CA CORP | ASSIGNMENT OF ASSIGNORS INTEREST | 004333 | /0342 | |
Nov 13 1984 | Northrop Corporation | (assignment on the face of the patent) | / |
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