发明名称
摘要 The engine (I) has an outer envelope (3) defining a peripheral annular space (4) along a side wall (5) of a fire tube (2) that allows flow of air from an air inlet of the engine. Parallel fixed flow guides (11-14) define flow channels in the space. Mobile pins (25) arranged in the space are connected to a mobile transversal base (18) of the tube. The pins block the channels to orient a part of air to an air-fuel detonating mixture intake port (20A) and liberate the channels when the base occupies two limit positions corresponding to chamber supply and mixture detonation phases, respectively.
申请公布号 JP5209783(B2) 申请公布日期 2013.06.12
申请号 JP20110505548 申请日期 2009.04.16
申请人 发明人
分类号 F02C5/12 主分类号 F02C5/12
代理机构 代理人
主权项
地址
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