| 发明名称 |
PIPE STRUCTURE AND AIRCRAFT |
| 摘要 |
The present invention provides a pipe structure including: a pipe through which a gaseous body having a higher temperature than a temperature of a surrounding atmosphere flows; a cover that covers an outer peripheral portion of the pipe, and defines a plurality of vents from which the gaseous body leaking from the pipe flows out; and a guide member that guides the gaseous body flowing out from the vent toward a line-shaped sensor that passes a position corresponding to each of the plurality of vents, and is sensitive to a temperature or a concentration of a gaseous body outside the cover. |
| 申请公布号 |
US2016238179(A1) |
申请公布日期 |
2016.08.18 |
| 申请号 |
US201514979924 |
申请日期 |
2015.12.28 |
| 申请人 |
MITSUBISHI AIRCRAFT CORPORATION |
发明人 |
YAMAMOTO Hiroyuki;SUZUTA Tadahiko;TAKAO Kei;MAEDA Ichiro |
| 分类号 |
F16L55/168 |
主分类号 |
F16L55/168 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A pipe structure comprising:
a pipe through which a gaseous body having a higher temperature than a temperature of a surrounding atmosphere flows; a cover that covers an outer peripheral portion of the pipe, and defines a plurality of vents from which the gaseous body leaking from the pipe flows out; and a guide member that guides the gaseous body flowing out from the vent toward a line-shaped sensor that passes a position corresponding to each of the plurality of vents, and is sensitive to a temperature or a concentration of a gaseous body outside the cover. |
| 地址 |
Aichi JP |
