发明名称 3-STROKE/6-STROKE ROCKET JET ENGINE
摘要 The present invention provides an engine pump that has: a housing (1) having a cylinder space; an output shaft unit (2) formed with one or more pistons (4) capable of constant velocity true-circle rotation within the cylinder space, a ring disk (5), and an output disk (3); a rotor (7) capable of constant velocity true-circle rotation at a fixed relative rotational velocity with respect to the rotation of the pistons (4); a rotor guide (8), which is concentric with the output shaft unit (2), governs the inside of the aforementioned cylinder, has a retaining part that makes concave contact with the rotor (7) and has an outer circumferential surface that makes surface contact with the pistons (4), and supports the rotor (7) and the center of the output shaft unit (2) which rotates at constant velocity in a true circle; and a drive means that actuates the pistons (4). A portion of the inner circumferential wall surface of the cylinder of the housing (1) has a notch part (14) that is used for sealing and makes surface contact with a portion of the outer circumferential surface of the rotor (7).
申请公布号 WO2012128267(A1) 申请公布日期 2012.09.27
申请号 WO2012JP57107 申请日期 2012.03.21
申请人 ISHII TAKESHI;ISHII RYUJI 发明人 ISHII TAKESHI
分类号 F01C1/22;F01C1/24;F01C1/36;F02B53/00;F04C18/344;F04C27/00;F04C29/00 主分类号 F01C1/22
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