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公开(公告)号：US10144245B2
公开(公告)日：2018-12-04
申请号：US14939340
申请日：2015-11-12
Applicant: Goodrich Corporation
Inventor： John Stevenson
Abstract: Systems and apparatus for an oval O-ring groove for aircraft wheels may generally comprise an inboard wheel portion and an inboard O-ring groove. The inboard wheel portion may include an inboard rim located opposite of an inboard tubewell. The inboard tubewell may have an inboard mating surface located on an axially outward edge of the inboard tubewell. The inboard O-ring groove may be formed as a partial oval-shaped recess located on an outer edge of the inboard mating surface.
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公开(公告)号：US20170136812A1
公开(公告)日：2017-05-18
申请号：US14939340
申请日：2015-11-12
Applicant: Goodrich Corporation
Inventor： John Stevenson
CPC classification number: B60B3/08 , B60B25/002 , B60B25/006 , B60B25/22 , B60B2900/325 , B60B2900/511 , B60Y2200/51 , B64C25/36
Abstract: Systems and apparatus for an oval O-ring groove for aircraft wheels may generally comprise an inboard wheel portion and an inboard O-ring groove. The inboard wheel portion may include an inboard rim located opposite of an inboard tubewell. The inboard tubewell may have an inboard mating surface located on an axially outward edge of the inboard tubewell. The inboard O-ring groove may be formed as a partial oval-shaped recess located on an outer edge of the inboard mating surface.
