发明名称 Propulsion unit for hypersonic aircraft - has gas generators mounted inside duct of rectangular cross=section
摘要 The propulsion unit for hypersonic aircraft. It consists of a duct of rectangular cross-section with gas generators (3) mounted inside. Each gas generator consists of a gas turbine which drives a tangential fan. A number of such turbines are installed and mounted one above another to form two parallel banks. Each bank is spaced at a distance from the duct side wall and there is a space between the two banks. The hypersonic propulsion unit for this type may have a duct of circular cross-section instead of the rectangular cross-section. USE - Hypersonic flight.
申请公布号 DE4111396(A1) 申请公布日期 1991.10.02
申请号 DE19914111396 申请日期 1991.04.09
申请人 KASTENS, KARL, DIPL.-ING., 2742 GNARRENBURG, DE 发明人 KASTENS, KARL, DIPL.-ING., 2742 GNARRENBURG, DE
分类号 F02K7/16 主分类号 F02K7/16
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