| 发明名称 |
DOUBLE-WALLED PIPE WITH INTEGRATED HEATING CAPABILITY FOR AN AIRCRAFT OR SPACECRAFT |
| 摘要 |
A double-walled pipe with integrated heating capability for an aircraft or spacecraft includes a pipe body rigidly formed from plastic in one piece with an inner wall, with an outer wall and with a plurality of wall supports, the wall supports connecting the inner wall to the outer wall, the inner wall and the outer wall defining an intermediate space. The double-walled pipe further includes an electrically conductive coating surrounding the inner wall within the intermediate space and configured to heat up under application of an electric current such that heat is transferred to the inner wall. |
| 申请公布号 |
US2016312924(A1) |
申请公布日期 |
2016.10.27 |
| 申请号 |
US201615132340 |
申请日期 |
2016.04.19 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Kolarski Robertino;Koehler Magnus;Scheidt Alexander |
| 分类号 |
F16L9/18;B29C67/00 |
主分类号 |
F16L9/18 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A double-walled pipe with integrated heating capability for an aircraft or spacecraft, comprising:
a pipe body rigidly formed in one piece from plastic with an inner wall, with an outer wall and with a plurality of wall supports, the wall supports connecting the inner wall to the outer wall, the inner wall and the outer wall defining an intermediate space; and an electrically conductive coating surrounding the inner wall within the intermediate space and configured to heat up under application of an electric current such that heat is transferred to the inner wall. |
| 地址 |
Hamburg DE |
