发明名称 NESTED CORE GAS TURBINE ENGINE
摘要 An aircraft, with the ability to cruise at supersonic speeds, designed to increase cruise lift/drag ratio, reduce sonic boom and have greater downward visibility by having an‘inverted’nose profile that has greater inclination of the lower surfaces to the flight direction than the upper surfaces.
申请公布号 US2011309187(A1) 申请公布日期 2011.12.22
申请号 US201113219314 申请日期 2011.08.26
申请人 DEV SUDARSHAN PAUL 发明人 DEV SUDARSHAN PAUL
分类号 B64C30/00;B64C23/00;F02C3/045;F02C3/06;F02C3/067;F02C3/10;F02C3/16;F02C7/10;F02K3/068 主分类号 B64C30/00
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