发明名称 PROPULSION SYSTEM FOR AN AIRCRAFT
摘要 The invention relates to a propulsion system comprising at least two independent internal combustion engines (4, 5) which are positioned directly next to each other and synchronized and which each act on a common drive shaft (9). Means are provided for in each separate propulsion connection (4 to 9 or 5 to 9) which cut said connection when there is a significant drop in power (rated breaking points, automatic decoupling).
申请公布号 CA2324447(A1) 申请公布日期 1999.10.07
申请号 CA19992324447 申请日期 1999.03.09
申请人 FRICK AEROTECH AG 发明人 FRICK, ALEXANDER
分类号 B64D27/00;B60K5/08;B64C1/00;B64D35/08;(IPC1-7):B64C1/00 主分类号 B64D27/00
代理机构 代理人
主权项
地址