发明名称 Variable mode jet engine - compact
摘要 This Jet engine comprises of a complete low bypass turbofan unit 1 including secondary fan unit 2 and engine core, some five to eight feet ahead of which sits a larger diameter main fan unit 3 driven from the secondary fan via drive shaft 4. Between the main and secondary fans sits a reversed variable area nozzle 5 connected to the forward end of the secondary fan by a short inlet tube 6 (fitted with intercooler 12). At the back of the core sits another variable area nozzle 7 facing rearwards. This arrangement (front nozzle, inlet tube, secondary fan, core, rear nozzle) is enclosed by a variable diameter cylinder 8, providing a variable area bypass duct 9 between cylinder and engine outer casing 10 that extends backwards from the outer diameter of the main fan. A third variable area nozzle 11 is positioned aft of the outer casing facing rearwards.
申请公布号 US2002017096(A1) 申请公布日期 2002.02.14
申请号 US20010765706 申请日期 2001.01.22
申请人 HUBBARD ADRIAN ALEXANDER 发明人 HUBBARD ADRIAN ALEXANDER
分类号 F02K3/075;F02K7/16;(IPC1-7):F02K3/02 主分类号 F02K3/075
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