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发明名称
Turbine engine nozzle
摘要
A convergent/divergent nozzle for a gas turbine engine has a throat portion of non-constant radius of curvature varying from an upstream high value to an intermediate low value and then to a downstream high value.
申请公布号
US2005217271(A1)
申请公布日期
2005.10.06
申请号
US20040013224
申请日期
2004.12.14
申请人
PETERS DONALD W
发明人
PETERS DONALD W.
分类号
B64D33/04;F02K1/00;F02K1/06;F02K1/12;F02K1/44;(IPC1-7):F02K1/12
主分类号
B64D33/04
代理机构
代理人
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地址
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