发明名称 |
Hydrogen peroxide based propulsion system |
摘要 |
A micro air vehicle is propelled by a bipropellant micro engine supplied with hydrogen peroxide and a hydrocarbon fuel. The hydrogen peroxide is decomposed to produce steam and oxygen at high temperature and the hydrocarbon fuel is burnt within a combustion chamber with oxygen produced from such decomposition. Products of such decomposition and combustion are exited through a nozzle to produce thrust. In a preferred embodiment there is also a ducted turbofan located downstream of the nozzle exit. |
申请公布号 |
AU1401001(A) |
申请公布日期 |
2001.02.13 |
申请号 |
AU20010014010 |
申请日期 |
2000.06.09 |
申请人 |
THE SECRETARY OF STATE FOR DEFENCE |
发明人 |
JOHN RONALD TILSTON;WAI SAN CHEUNG |
分类号 |
B64C39/00;F02K3/04;F02K9/42;F02K9/68;F02K9/74 |
主分类号 |
B64C39/00 |
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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