Combined aircraft tire and wheel

Description

FIG. 1 is a view in perspective, looking at a sidewall and a partial circumferential surface of a combined aircraft tire and wheel constituting the present invention;

FIG. 2 is a side elevational thereof with the direction of wheel rotation being in the counterclockwise direction, the opposite side being a mirror image;

FIG. 3 is an enlarged end elevational view thereof, it being understood that the tread pattern is repeated throughout the circumference of the tire;

FIG. 4 is a greatly enlarged sectional view taken along the plane of 4--4 in FIG. 2 thereof with an impeller vane shown in "activated" condition; and,

FIG. 5 is a greatly enlarged sectional view taken similarly along the plane of 4--4, but with the impeller vane shown not in an "activated" condition.

Referenced Cited
U.S. Patent Documents
D146486 March 1947 Peterson
D283885 May 20, 1986 Kim
2305237 December 1942 Carpenter
2934124 April 1960 Mihlsten
3233849 February 1966 Rubin
Foreign Patent Documents
3416416 July 1985 DEX
2080217 February 1982 GBX
Other references
  • Aero Digest, Jan. 15, 1944, p. 22, Airplane Tire, bottom of page.
Patent History
Patent number: D373337
Type: Grant
Filed: Sep 2, 1994
Date of Patent: Sep 3, 1996
Inventor: Colin R. Hunt (Lake Placid, Cairns, Queensland)
Primary Examiner: James M. Gandy
Attorney: James A. Wong
Application Number: 0/28,243
Classifications
Current U.S. Class: D12/135; D12/145; D12/152; Characterized By Circular Motif (D12/210)