Set of aircraft canards

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Description

FIG. 1 is a left side plan view of the set of aircraft canards;

FIG. 2 is a right side plan view of the set of aircraft canards;

FIG. 3 is a front plan view of the set of aircraft canards;

FIG. 4 is a right front elevated isometric view of the set of aircraft canards; and,

FIG. 5 is a top plan view of the set of aircraft canards.

The broken line showing of the aircraft is for the purpose of illustrating the environmental structure in which the claimed elements are found and forms no part of the claimed design.

In addition, thick lines are used to outline objects, while thin lines show contours.

Claims

The ornamental design for a set of aircraft canards, as shown and described.

Referenced Cited
U.S. Patent Documents
4848700 July 18, 1989 Lockheed
5454530 October 3, 1995 Rutherford
D814972 April 10, 2018 Ahn
9981734 May 29, 2018 Ivans
D858420 September 3, 2019 Calcedonio Boscarino
20040262450 December 30, 2004 Cordy, Jr.
20140339354 November 20, 2014 Gaillimore
20160200436 July 14, 2016 North
20170137122 May 18, 2017 Kooiman
20180257764 September 13, 2018 Gandhi
20180297695 October 18, 2018 Ramirez-Serrano
20200086971 March 19, 2020 Heeringa
Patent History
Patent number: D926665
Type: Grant
Filed: May 24, 2019
Date of Patent: Aug 3, 2021
Assignee: Alakai Technologies Corporation (Hopkinton, MA)
Inventors: Brian D. Morrison (Hopkinton, MA), Andre H. De Salis (Pasadena, CA), Martti J. Lampela (Los Angeles, CA), Adil M. Ali (Thousand Oaks, CA), Peter F. Falt (Thousand Oaks, CA)
Primary Examiner: John A Voytek
Application Number: 29/692,499
Classifications