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发明名称
Two-stage gas turbine propulsion jet unit with thrust diverting means
摘要
申请公布号
US3255585(A)
申请公布日期
1966.06.14
申请号
US19650431146
申请日期
1965.02.08
申请人
DAIMLER-BENZ AKTIENGESELLSCHAFT
发明人
GRIEB HUBERT J.
分类号
B64C29/00;F02K3/02
主分类号
B64C29/00
代理机构
代理人
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