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Publication numberUSD624865 S1
Publication typeGrant
Application numberUS 29/271,590
Publication dateOct 5, 2010
Filing dateJan 23, 2007
Priority dateJan 23, 2007
Publication number271590, 29271590, US D624865 S1, US D624865S1, US-S1-D624865, USD624865 S1, USD624865S1
InventorsAlexandre Figueiredo
Original AssigneeEmbraer - Empresa Brasileira De Aeronautica S.A.
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Aircraft control yoke
US D624865 S1
Abstract  available in
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  1. The ornamental design for an aircraft control yoke, as shown and described.

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.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
USD737184 *Dec 13, 2013Aug 25, 2015Nissan Motor Co., Ltd.Steering wheel unit for an automobile
U.S. ClassificationD12/345