发明授权
EP1370428B1 OPTIMIZED DEMOUNTABLE FLANGE AND RETAINING RING GEOMETRY FOR AIRCRAFT WHEELS 有权
优化,可拆卸法兰和HALTERING-几何的飞机

  • 专利标题: OPTIMIZED DEMOUNTABLE FLANGE AND RETAINING RING GEOMETRY FOR AIRCRAFT WHEELS
  • 专利标题(中): 优化,可拆卸法兰和HALTERING-几何的飞机
  • 申请号: EP02719245.9
    申请日: 2002-03-14
  • 公开(公告)号: EP1370428B1
    公开(公告)日: 2006-09-06
  • 发明人: CHAMPION, Jon, H.
  • 申请人: Honeywell International Inc.
  • 申请人地址: 101 Columbia Road, P.O. Box 2245 Morristown, New Jersey 07960 US
  • 专利权人: Honeywell International Inc.
  • 当前专利权人: Honeywell International Inc.
  • 当前专利权人地址: 101 Columbia Road, P.O. Box 2245 Morristown, New Jersey 07960 US
  • 代理机构: Hucker, Charlotte Jane
  • 优先权: US276740P 20010316; US887837 20010622
  • 国际公布: WO2002074556 20020926
  • 主分类号: B60B25/14
  • IPC分类号: B60B25/14
OPTIMIZED DEMOUNTABLE FLANGE AND RETAINING RING GEOMETRY FOR AIRCRAFT WHEELS
摘要:
A technique for reducing the likelihood of fatigue damage to a wheel rim assembly (11) of the type having an annular wheel rim (13) with a first bead flange (19), a second separable bead flange (15, 21), and a retaining ring (17) disposable within a groove (35) in the wheel rim to secure the separable bead flange to the wheel rim includes forming the retaining ring to have an annular bead (41), a portion of which has an arcuate cross-sectional configuration by shaping the annular bead, in cross-section, as at least two tangentially joined circular segments (43, 45) of unequal radii (27, 29). The separable bead flange is formed to have a concave retaining ring engaging annular surface (25) which, in cross section has a finite radius of curvature (5) and the retaining ring is formed to have a separable bead flange engaging convex annular surface (23) which, in cross-section, has a finite radius of curvature (61).
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