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公开(公告)号:US10309434B2
公开(公告)日:2019-06-04
申请号:US15087531
申请日:2016-03-31
申请人: The Boeing Company
IPC分类号: F16B5/01 , F01D25/24 , F02K1/54 , F16B5/02 , F02C7/20 , B64D27/12 , B64D29/06 , F02K1/60 , F02K1/76
摘要: Provided is an aircraft propulsor thrust reverser with a fastening system. The fastening system may include a male spool and a female spool configured to be threaded into the male spool. The male spool and the female spool may be coupled to a honeycomb structure and may evenly distribute force to the honeycomb structure to prevent plastic deformation of a honeycomb core of the honeycomb structure.
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公开(公告)号:US20170284338A1
公开(公告)日:2017-10-05
申请号:US15087531
申请日:2016-03-31
申请人: The Boeing Company
CPC分类号: F02K1/766 , B64D27/12 , B64D29/06 , F01D25/243 , F02C7/20 , F02K1/54 , F02K1/605 , F05D2220/323 , F05D2230/60 , F05D2250/283 , F05D2260/30 , F05D2260/31 , F16B5/01 , F16B5/02 , Y02T50/672
摘要: Systems and methods are provided for an aircraft propulsor thrust reverser with a fastening system. The fastening system may include a male spool and a female spool configured to be threaded into the male spool. The male spool and the female spool may be coupled to a honeycomb structure and may evenly distribute force to the honeycomb structure to prevent plastic deformation of a honeycomb core of the honeycomb structure.
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