公开(公告)号：US10350940B2

公开(公告)日：2019-07-16

申请号：US15153270

申请日：2016-05-12

Applicant: Parker-Hannifin Corporation

Inventor： Joseph Zeisler

IPC: B64C25/34 ,  B60B23/10 ,  B60B25/04 ,  B64C25/36 ,  B60B3/08 ,  B60B25/00

Abstract: An aircraft wheel assembly that includes first and second hub components having an axis and respective first and second sets of circumferentially spaced apart interface elements. The first and second hub components may be rotatable relative to one another about the axis between a first position and a second position. In the first position, the first set of interface elements is axially movable relative to the second set of interface elements. In the second position the first set of interface elements axially overlaps the second set of interface elements to prevent axial movement of the first hub component relative to the second hub component.

公开(公告)号：US20170274989A1

公开(公告)日：2017-09-28

申请号：US15153270

申请日：2016-05-12

Applicant: Parker-Hannifin Corporation

Inventor： Joseph Zeisler

IPC: B64C25/34 ,  B60B25/00 ,  B60B3/08

CPC classification number: B60B23/10 ,  B60B3/085 ,  B60B25/002 ,  B60B25/04 ,  B60B2320/14 ,  B64C25/36

Abstract: An aircraft wheel assembly that includes first and second hub components having an axis and respective first and second sets of circumferentially spaced apart interface elements. The first and second hub components may be rotatable relative to one another about the axis between a first position and a second position. In the first position, the first set of interface elements is axially movable relative to the second set of interface elements. In the second position the first set of interface elements axially overlaps the second set of interface elements to prevent axial movement of the first hub component relative to the second hub component.