- 专利标题: Gas turbine engine fan blade, design, and fabrication
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申请号: US15650107申请日: 2017-07-14
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公开(公告)号: US10808545B2公开(公告)日: 2020-10-20
- 发明人: Tahany Ibrahim El-Wardany , Matthew E. Lynch , Om P. Sharma , Catalin G. Fotache
- 申请人: United Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: United Technologies Corporation
- 当前专利权人: United Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 代理机构: Kinney & Lange, P.A.
- 主分类号: F01D5/18
- IPC分类号: F01D5/18 ; F01D5/14 ; F04D29/38 ; B22F3/11 ; F04D29/02 ; F04D29/32
摘要:
An embodiment of a fan blade includes an interior region between a metallic pressure sidewall and a metallic suction sidewall. Each sidewall extends in span from a base to a tip, and extends in chord from a leading edge to a trailing edge. The interior region of the fan blade includes a first fully dense metallic portion and a first porous metallic portion. The first fully dense metallic portion has a volume occupying at least 10% of a total volume of the interior region, and substantially no porosity. The first porous metallic portion is integrally joined to the fully dense metallic portion, and is selected from a structured lattice, an unstructured foam, and combinations thereof.
公开/授权文献
- US20190017388A1 GAS TURBINE ENGINE FAN BLADE, DESIGN, AND FABRICATION 公开/授权日:2019-01-17
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