Airplane turbine engine shield

Skip to: Description  ·  Claims  ·  References Cited  · Patent History  ·  Patent History
Description

FIG. 1 is a front elevation view of an airplane turbine engine shield showing my new design;

FIG. 2 is a rear elevation view thereof;

FIG. 3 is a right elevation view thereof, the opposite side being a mirror image of the shown; and,

FIG. 4 is an in-use isometric view thereof.

The broken lines in the drawings depict environmental subject matter only and form no part of the claimed design.

Claims

The ornamental design for an airplane turbine engine shield, as shown and described.

Referenced Cited
U.S. Patent Documents
3426981 February 1969 Allcock
3871844 March 1975 Calvin, Sr.
4077739 March 7, 1978 Heilenbach
4833879 May 30, 1989 Verduyn et al.
D303784 October 3, 1989 Micallef
5114098 May 19, 1992 Campbell
5411224 May 2, 1995 Dearman et al.
D433029 October 31, 2000 Eidson
7051509 May 30, 2006 Grimlund
7160345 January 9, 2007 Pavlatos
7625415 December 1, 2009 Durocher et al.
D614560 April 27, 2010 Alexander
D621852 August 17, 2010 Zunik
Patent History
Patent number: D631420
Type: Grant
Filed: Aug 12, 2009
Date of Patent: Jan 25, 2011
Inventor: Joseph Locklear (Shannon, NC)
Primary Examiner: Cathron C. Brooks
Assistant Examiner: Maurice Stevens
Attorney: Crossley Patent Law
Application Number: 29/341,742
Classifications
Current U.S. Class: Element Or Attachment (9) (D12/345)