发明名称 PROPULSION SYSTEM FOR AN AIRCRAFT
摘要 <p>The two small internal combustion engines (4, 5) have reduced overall dimensions (e.g. approximately 500 x 250 x 300 mm). The engines directly next to one another have an identical structure and the same power and drive by means of a toothed belt (7,8) and a common drive shaft (9) for the compressor (1). If one of the engine fails, the power of the second engine is sufficient for an emergency landing.</p>
申请公布号 SK13882000(A3) 申请公布日期 2001.06.11
申请号 SK20000001388 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
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