| 发明名称 |
Cold start fuel system for two- or four-stroke petrol engine used in a drone or model aero-engine |
| 摘要 |
<p>A two- or four-stroke aero engine burns fuel drawn from a tank and supplied in the start-up phase under pressure via a pump and valve.</p> |
| 申请公布号 |
DE202004009316(U1) |
申请公布日期 |
2004.09.02 |
| 申请号 |
DE20042009316U |
申请日期 |
2004.06.12 |
| 申请人 |
ALBINGER, BERND |
发明人 |
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| 分类号 |
F02B75/34;F02D33/00;F02M37/00;F02M69/46;F02N19/00;(IPC1-7):F02N17/00 |
主分类号 |
F02B75/34 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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