发明名称 |
Dual Compressor Turbocharger |
摘要 |
A dual compressor turbocharger includes two compressors. One compressor supplies fuel pressure, and one compressor supplies air pressure. The dual compressor turbocharger includes a turbine driven by exhaust of an engine and a shaft coupled to the turbine. The first compressor is mounted on the shaft and includes a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine. The second compressor is mounted on the shaft and includes a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine. |
申请公布号 |
US2016108810(A1) |
申请公布日期 |
2016.04.21 |
申请号 |
US201414517300 |
申请日期 |
2014.10.17 |
申请人 |
Kohler Co. |
发明人 |
Frampton Isaac S.;Danforth, III Robert J.;Honkanen Paul |
分类号 |
F02C6/12;F02M37/14;F02M55/02;F02B37/18;F02B37/24;F02M35/10;F02M37/04;F02M37/06 |
主分类号 |
F02C6/12 |
代理机构 |
|
代理人 |
|
主权项 |
1. A turbocharger comprising:
a turbine driven by exhaust of an engine; a shaft coupled to the turbine; a first compressor mounted on the shaft and having a first inlet coupled to an air supply and a first outlet coupled to an air intake of the engine; and a second compressor mounted on the shaft having a second inlet coupled to a fuel supply and a second outlet coupled to a fuel supply rail of the engine. |
地址 |
Kohler WI US |