发明名称 |
Tip turbine engine integral fan, combustor, and turbine case |
摘要 |
A tip turbine engine assembly includes an integral engine outer case located radially outward from a fan assembly. The integral outer case includes a rear portion and a forward portion with an arcuate portion that curves radially inwardly to form a compartment. An annular combustor is housed and mounted in the compartment. Fan inlet guide vanes are integrally formed with the arcuate portion to form the integral case portion. The rear portion, forward portion, and fan inlet guide vanes are integrally formed in a casting process.
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申请公布号 |
US8033092(B2) |
申请公布日期 |
2011.10.11 |
申请号 |
US20040720539 |
申请日期 |
2004.12.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SUCIU GABRIEL L.;NORRIS JAMES W.;NORDEEN CRAIG A.;MERRY BRIAN |
分类号 |
F02K3/02 |
主分类号 |
F02K3/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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