Aircraft control panel

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Description

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.

Claims

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

Referenced Cited
U.S. Patent Documents
D151688 November 1948 Foster
3702504 November 1972 Cramer
3885325 May 1975 Sidoti
D284751 July 22, 1986 Soederberg
D339786 September 28, 1993 Allendorph et al.
D378585 March 25, 1997 Duguid et al.
D395030 June 9, 1998 Hellhake et al.
D397977 September 8, 1998 Hellhake et al.
D439556 March 27, 2001 Beigel
6255964 July 3, 2001 Steele, Jr.
6702229 March 9, 2004 Anderson et al.
D534468 January 2, 2007 Colburn et al.
Patent History
Patent number: D556107
Type: Grant
Filed: Jan 23, 2007
Date of Patent: Nov 27, 2007
Assignee: Embraer - Empresa Brasileira de Aeronautica S.A. (Sao Jose dos Campos - SP)
Inventor: Alexandre Figueiredo (Sao José dos Campos)
Primary Examiner: Stacia Cadmus
Attorney: Nixon & Vanderhye P.C.
Application Number: 29/271,591
Classifications