| 发明名称 |
Superconductive hypersonic liquefaction nosecone |
| 摘要 |
An apparatus and method for mitigating the shock front of an aerospace plane flying at hypersonic speeds. The invention employs supercooling driven by the cryogenic power of liquid hydrogen, regenerative evaporation of liquid hydrogen or liquid nitrogen and consequential isothermal compression, to usurp the shock front in totality at Mach 1. |
| 申请公布号 |
US9193457(B2) |
申请公布日期 |
2015.11.24 |
| 申请号 |
US201313969467 |
申请日期 |
2013.08.16 |
| 申请人 |
|
发明人 |
Janeke Charl Emelio |
| 分类号 |
B64C30/00;B64C1/00;B64C1/38 |
主分类号 |
B64C30/00 |
| 代理机构 |
Law Offices of J. Curtis Edmondson |
代理人 |
Edmondson J. Curtis;Law Offices of J. Curtis Edmondson |
| 主权项 |
1. An aerospace plane flying hypersonically through the atmosphere comprising:
a body; a nosecone on a leading end,
said nosecone is a close-coupled, double-decker made of concentric spheres, optically black spherical heat exchanger with a superconductive outer shell and a supercooled inner shell, wherein the superconductive outer shell is etched or coated glass so that it is optically black; and,
including an aperture for the intake of ambient air, a rocket engine on a tail end. |
| 地址 |
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