发明名称 ROTARY MECHANICALLY RECIPROCATED SLIDING METAL VANE AIR PUMP AND BOUNDARY LAYER GAS TURBINES INTEGRATED WITH A PULSE GAS TURBINE ENGINE SYSTEM
摘要 <p>A rotary mechanically reciprocated sliding vane air pump is integrated with pulse driven boundary layer gas turbines on a single shaft. The shaft is slotted and is aligned with a slotted rotor that mechanically drives a reciprocating sliding metal vane. The cavity in the housing is offset from the center line of the shaft, creating a cavity between the rotor and the cavity wall. Air is positively induced at the inlet of the cavitated housing and is positively displaced at the outlet. Air inlet and outlet ports enter and exit the cavitated housing wall at 90 degrees and 270 degrees respectively. The compressed air is directed via manifolds into combustion chambers mounted on side walls of the turbine housings. Arcing electrodes detonate the fuel-air mixture producing high temperature and pressure pulsed working fluid that is exhausted via nozzles into the vanes of the boundary layer gas turbines.</p>
申请公布号 WO2009073406(A2) 申请公布日期 2009.06.11
申请号 WO2008US84328 申请日期 2008.11.21
申请人 SCRAGG, ROBERT 发明人 SCRAGG, ROBERT
分类号 F02C3/00;F02B71/04;F04B17/00 主分类号 F02C3/00
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