发明名称 |
CABIN AIR COMPRESSOR CROSS-SUPPORT BRACKET |
摘要 |
A cross-support bracket for a cabin air compressor assembly includes a mating portion having a first group of apertures at a first end and a second group of apertures at a second end. A reference line is defined between a lowermost primary aperture of the first group of apertures and a lowermost primary aperture of the second group of apertures. A stiffener portion is formed along a lower edge of the mating portion. A curved region is formed in the mating portion between a first and second upper edge of the mating portion. The curved region includes a first curved portion, a substantially straight portion, and a second curved portion. A ratio of a radius of the first and second curved portions of the curved region to a length from the substantially straight portion to the reference line is between 9.06 and 10.19. |
申请公布号 |
US2014346302(A1) |
申请公布日期 |
2014.11.27 |
申请号 |
US201313901831 |
申请日期 |
2013.05.24 |
申请人 |
Hamilton Sundstrand Corporation |
发明人 |
Vignali Mark;Mayo Luke J. |
分类号 |
F16M13/02;B64D13/02 |
主分类号 |
F16M13/02 |
代理机构 |
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代理人 |
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主权项 |
1. A cross-support bracket for a cabin air compressor assembly, the cross-support bracket comprising:
a mating portion comprising a first group of apertures at a first end and a second group of apertures at a second end, wherein a reference line is defined between a lowermost primary aperture of the first group of apertures and a lowermost primary aperture of the second group of apertures; a stiffener portion formed along a lower edge of the mating portion; and a curved region formed in the mating portion between a first and second upper edge of the mating portion, the curved region comprising a first curved portion, a substantially straight portion, and a second curved portion, wherein a ratio of a radius of the first and second curved portions of the curved region to a length from the substantially straight portion to the reference line is between 9.06 and 10.19. |
地址 |
Windsor Locks CT US |