|Publication number||USD556107 S1|
|Application number||US 29/271,591|
|Publication date||Nov 27, 2007|
|Filing date||Jan 23, 2007|
|Priority date||Jan 23, 2007|
|Publication number||271591, 29271591, US D556107 S1, US D556107S1, US-S1-D556107, USD556107 S1, USD556107S1|
|Original Assignee||Embraer - Empresa Brasileira De Aeronautica S.A.|
|Export Citation||BiBTeX, EndNote, RefMan|
|Referenced by (1), Classifications (1) |
|External Links: USPTO, USPTO Assignment, Espacenet|
Aircraft control panel
US D556107 S1
The ornamental design for an “aircraft control panel,” as shown and described.
This application may be deemed related to commonly owned copending U.S. Design patent application Ser. Nos. 29/271,590 entitled “Aircraft Control Yoke” and 29/271,589 entitled “Aircraft Cockpit Throttle Console” filed even date herewith, which applications are expressly incorporated hereinto by reference.
FIG. 1 is a front perspective view of an aircraft control panel which embodies my new and original design therefore; and,
FIG. 2 is a front elevation view of thereof, the rear elevation view, left and right side elevation views, and top and bottom plan views being unornamented.
The broken lines in FIGS. 1 and 2 represent adjacent aircraft panel support structures and other aircraft panel components in the environment of the claimed design, but which do not form part of the claimed design.
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US8678312||Aug 31, 2011||Mar 25, 2014||Textron Innovations, Inc.||Aircraft side-ledge console|