发明名称 ONE STROKE/AEROTORBINE ENGINE
摘要 In any vehicle or power plant run by either reciprocal or rotary type of engine, said engine converted such that it will use only compressed natural air of 2,500 - 3,000 PSI pressure to push its piston/s beginning at 30o DOCR before BDC. Then said piston/s will be pulled-up by vacuumized natural air "in equivalent BARS" at 30o DOCR after BDC until 30o DOCR before TDC in a reciprocal engine. In a rotary engine converted, a timed pressurized-air through its Pressure Valve (PV) is opened to work/push on the "just-arrived-edge" of the pressure chamber, after RFNZ, until after 70 pcnt of it have passed by the pressure port, then a timed vacuumized-air pulling off its open exhaust valve neutralizes "residue pressure within" the said pressure chamber or remaining 13 pcnt of said pressure chamber "travel" to relieve stress on the entire Aerotorbine Engine's drive train before pulling on the rest of the oncoming/passing vacuum chamber. In this "One-stroke Engine" and/or "Aerotorbine Engine", all cylinders/chambers of both engine types converted will deliver "Simultaneous Power Stroke Overlaps" to the crankshaft/outputshaft, respectively.
申请公布号 PH12014000083(A1) 申请公布日期 2015.09.14
申请号 PH12014000083 申请日期 2014.03.07
申请人 ALBERTO N. MACALISANG;JONATHAN C. SADDI 发明人 JONATHAN C. SADDI;ALBERTO N. MACALISANG
分类号 F02B53/00;F02B73/00;F02B75/02 主分类号 F02B53/00
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