公开(公告)号：US4275932A

公开(公告)日：1981-06-30

申请号：US46891

申请日：1979-06-08

Applicant: Roy W. Baird ,  Robert E. Berger ,  Richard L. Kirk

Inventor： Roy W. Baird ,  Robert E. Berger ,  Richard L. Kirk

IPC: B60B25/02 ,  B60B21/04 ,  B60B25/10 ,  B64C25/34 ,  B60B21/00 ,  B64C25/32

CPC classification number: B60B25/10 ,  B60B21/04

Abstract: An improved aircraft wheel configuration obviates the hazard of wheel failure during take-off and landing situations when tire deflation occurs and the wheel accepts full loading on its flanges. The wheel is configured to provide a differential flange height between the inboard and outboard flanges such that the total load applied to the wheel is distributed equally between the flanges. Alternatively, and/or in addition the flanges are restructured to provide an increased section modulus and the inboard flange is designed to provide a wider contact surface.

Abstract translation: 改进的飞机车轮配置消除了在出现轮胎放气并且轮子在其法兰上承受满载时起飞和着陆情况下车轮故障的危险。 车轮构造成在内侧和外侧法兰之间提供不同的法兰高度，使得施加到车轮的总负载分布在法兰之间。 或者，和/或另外地，凸缘被重组以提供增加的截面模量，并且内侧凸缘设计成提供更宽的接触表面。