RADIAL LOCK FOR FAN BLADE SHEATH

更新时间:2023-06-12 00:03:54 阅读: 评论:0

专利名称:RADIAL LOCK FOR FAN BLADE SHEATH
发明人:McKAVENEY, Christopher S.,ELLIOTT, Jason英语作文常用短语
申请号:EP15202175.4
申请日:20151222
公开号:EP3040517A1镜子的英文
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公开日:
20160706
专利内容由知识产权出版社提供
专利附图:
狮子座的爱情摘要:A turbojet fan blade (132) adapted for curement to an engine rotor (130)includes a titanium sheath (150) that extends continuously over its leading edge (142)from blade tip (148) to blade root (146). The sheath (150) provides impact protection over the leading edge (142) of the blade (132), and also incorporates enhanced radial
curement of the sheath (150) to the rotor (130). As such, a radial lock system for the sheath (150) is disclod that includes a fully integrated sheath portion that extends completely over the frontal face (170) of a fan blade dovetail, providing a radial lock of the sheath (150) to the rotor (130) in the event of failure of any adhesive (158) ud to attach the sheath (150) to the leading edge (142). Becau the sheath (150) extends continuously from blade tip (148) to the blade root (146), lightning strike protection is enhanced by avoidance of any discontinuities otherwi associated with related art sheaths that typically extend over only a flow path portion of the leading edge.
申请人:United Technologies Corporation
面罩共鸣地址:10 Farm Springs Rd. Farmington, CT 06032 US
国籍:US
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越南巨人蜈蚣代理机构:Hague, Alison Jane
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