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发明名称
Nested core gas turbine engine
摘要
A gas turbine engine comprising a combustion chamber section, a turbine section, and a compressor section. The turbine section surrounds the combustion chamber and the compressor section surrounds the turbine section.
申请公布号
US7219490(B2)
申请公布日期
2007.05.22
申请号
US20050201441
申请日期
2005.08.10
申请人
D-STAR ENGINEERING
发明人
DEV SUDARSHAN PAUL
分类号
F02K3/02;F02C3/045;F02C3/06;F02C3/067;F02C3/10;F02C3/16;F02C7/10;F02K3/068
主分类号
F02K3/02
代理机构
代理人
主权项
地址
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