- 专利标题： Attritable engine additively manufactured inlet cap
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申请号： US17746206申请日： 2022-05-17
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公开(公告)号： US11739690B2公开(公告)日： 2023-08-29
- 发明人: Lawrence A. Binek , Jesse R. Boyer , Evan J. Butcher , Michael Winter , Jesus A. Garcia , Sean R. Jackson
- 申请人： Raytheon Technologies Corporation
- 申请人地址： US CT Farmington
- 专利权人： Raytheon Technologies Corporation
- 当前专利权人： Raytheon Technologies Corporation
- 当前专利权人地址： US CT Farmington
- 代理机构： Bachman & LaPointe, P.C.
- 主分类号： F02C7/055
- IPC分类号： F02C7/055 ; B22F10/28
摘要：
A turbine engine has: a compressor; a combustor; a turbine, a gas flowpath passing consecutively through the compressor, combustor, and turbine; and inlet member along the gas flowpath upstream of the compressor. The inlet member includes the unitarily-formed single piece combination of: a three dimensional (3D) lattice portion; and a nose cap body surrounding the lattice portion.
公开/授权文献
- US20230077719A1 Attritable Engine Additively Manufactured Inlet Cap 公开/授权日：2023-03-16
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