Control wheel for aircraft

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Description

FIG. 1 is a perspective view from the upper right side of a control wheel for aircraft.

FIG. 2 is a perspective view from the upper left side thereof.

FIG. 3 is a perspective view from the lower left side thereof.

FIG. 4 is a perspective view from the lower right side thereof.

FIG. 5 is a front elevation view thereof.

FIG. 6 is a rear elevation view thereof.

FIG. 7 is a top plan view thereof.

FIG. 8 is a bottom plan view thereof.

FIG. 9 is a left side elevation view thereof.

FIG. 10 is a right side elevation view thereof; and,

FIG. 11 is an enlarged cross sectional view thereof, taken along the line 11-11 in FIG. 5.

The broken lines shown in the drawings illustrate portions of a control wheel for aircraft that form no part of the claimed design. The dot-dash lines show an unclaimed boundary which forms no part of the claimed design.

Claims

The ornamental design for a control wheel for aircraft, as shown and described.

Referenced Cited
U.S. Patent Documents
2747057 May 1956 Obszarny
D578940 October 21, 2008 Tsay
D776023 January 10, 2017 Allison
D787994 May 30, 2017 Carbone
D813123 March 20, 2018 Allison
10080110 September 18, 2018 McElmurry
Patent History
Patent number: D842180
Type: Grant
Filed: Apr 26, 2017
Date of Patent: Mar 5, 2019
Assignee: MITSUBISHI AIRCRAFT CORPORATION (Aichi)
Inventor: Hiroyasu Aruga (Tokyo)
Primary Examiner: Susan Bennett Hattan
Assistant Examiner: Suzanne E Tisdell
Application Number: 29/601,797
Classifications
Current U.S. Class: Steering Wheel (D12/175)