| 发明名称 |
LIGHT WEIGHT THERMOPLASTIC FLEX FOAM AND HYBRID DUCT SYSTEM |
| 摘要 |
An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.
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| 申请公布号 |
US2008308674(A1) |
申请公布日期 |
2008.12.18 |
| 申请号 |
US20070763427 |
申请日期 |
2007.06.14 |
| 申请人 |
FRANTZ WALTER FORREST;PATEL JAYANT D;MABEN DOUGLAS DEAN;WHITMAN BRUCE;FREEMAN DOUGLAS E |
发明人 |
FRANTZ WALTER FORREST;PATEL JAYANT D.;MABEN DOUGLAS DEAN;WHITMAN BRUCE;FREEMAN DOUGLAS E. |
| 分类号 |
B64D11/00;F16L11/08 |
主分类号 |
B64D11/00 |
| 代理机构 |
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