发明名称 Compact tuned exhaust system for aircraft with reciprocating engines
摘要 A tuned exhaust system for a multi-cylinder, reciprocating, internal combustion engine is disclosed. Each exhaust tube has approximately the same overall length resulting in a predetermined resonant frequency. The overall length includes the sum of the header tube length and the internal length of the collector assembly portions of the exhaust channels in the heat exchanger box. Calculating the correct length and bending the pipes to fit in the space available resulted in increased horsepower, reduced fuel consumption, cooler cylinder head temperatures, reduced noise and vibration for four-cylinder and six-cylinder aircraft engines.
申请公布号 US6581376(B1) 申请公布日期 2003.06.24
申请号 US20020123921 申请日期 2002.04.17
申请人 THOMAS ROBIN G. 发明人 THOMAS ROBIN G.
分类号 F01N1/06;F02B27/04;F02B61/04;F02B75/18;(IPC1-7):F02B27/02 主分类号 F01N1/06
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