Aircraft control yoke

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Description

This application may be deemed related to commonly owned copending U.S. Design Patent Application Ser. Nos. 29/271,591, now U.S. Patent D556,107, entitled “Aircraft Control Panel” and 29/271,589, now U.S. Patent D553,554, 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 yoke which embodies my new and original design therefore;

FIG. 2 is a front elevation view thereof;

FIG. 3 is a rear elevation view thereof,

FIG. 4 is a top plan view thereof;

FIG. 5 is a bottom plan view thereof;

FIG. 6 is a left side elevation view thereof; and,

FIG. 7 is a right side elevation view thereof.

The broken lines shown in the drawings represent unclaimed portions of the design and form no part thereof.

Claims

The ornamental design for an aircraft control yoke, as shown and described.

Referenced Cited
U.S. Patent Documents
D297028 August 2, 1988 McCann
D316879 May 14, 1991 Shulman et al.
D328315 July 28, 1992 Shulman
D433077 October 31, 2000 Yamazaki
6371829 April 16, 2002 Kato et al.
D556107 November 27, 2007 Figueiredo
D578940 October 21, 2008 Tsay et al.
Patent History
Patent number: D624865
Type: Grant
Filed: Jan 23, 2007
Date of Patent: Oct 5, 2010
Assignee: Embraer - Empresa Brasileira De Aeronautica S.A. (Sao Jose Dos Campos - SP)
Inventor: Alexandre Figueiredo (Sao José dos Campos - SP)
Primary Examiner: Cathron C Brooks
Assistant Examiner: Kevin K Rudzinski
Attorney: Nixon & Vanderhye P.C.
Application Number: 29/271,590
Classifications