Aircraft control panel

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Description

This application may be deemed related to commonly owned copending U.S. Design patent application Ser. No. 29/324,988 entitled “Aircraft Cockpit Throttle Console” filed even date herewith, which application is 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;

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;

FIG. 3 is a top plan view thereof, the bottom plan view thereof being unornamented; and,

FIG. 4 is right side elevation view thereof, the left side elevation view being a mirror image thereof.

The broken lines in FIGS. 1 and 2 represent structures in the environment of the claimed design, but which do not form part of the claimed design.

Claims

The ornamental design for an “aircraft control panel,” as shown and described.

Referenced Cited
U.S. Patent Documents
D151688 November 1948 Foster
D284751 July 22, 1986 Soederberg
D378585 March 25, 1997 Duguid et al.
D439556 March 27, 2001 Beigel
6702229 March 9, 2004 Anderson et al.
D556107 November 27, 2007 Figueiredo
Patent History
Patent number: D630142
Type: Grant
Filed: Sep 24, 2008
Date of Patent: Jan 4, 2011
Assignee: Embraer - Empresa Brasileira De Aeronautica S.A. (Sao Jose Dos Campos - SP)
Inventors: Eduardo Leandro da Silveira (São José dos Campos), Mozart Marques Louzada Junior (São José dos Campos)
Primary Examiner: Austin Murphy
Attorney: Nixon & Vanderhye P.C.
Application Number: 29/324,987
Classifications
Current U.S. Class: Instrument Panel Or Element Thereof (D12/192)