| 发明名称 |
PROBE SYSTEM, MIXED PRIMARY REFERENCE PROBE FOR AN AIRCRAFT, ASSOCIATED AIRCRAFT AND MEASURING METHOD |
| 摘要 |
A probe system, mixed primary reference probe for an aircraft, associated aircraft and measuring method are disclosed. In one aspect, the probe system includes a base designed to be fastened on the cockpit of an aircraft, a plurality of regularly spaced static pressure taps, arranged through the base and designed to be connected to a pressure measurement device. The system includes at least one optical window transparent to laser radiation and inserted into the base. |
| 申请公布号 |
US2015168439(A1) |
申请公布日期 |
2015.06.18 |
| 申请号 |
US201514608962 |
申请日期 |
2015.01.29 |
| 申请人 |
THALES |
发明人 |
GENEVRIER Gilles;LEDAIN Bernard;MANDLE Jacques;SCHLOTTERBECK Jean-Pierre |
| 分类号 |
G01P5/14;G01P5/02;G01S17/58;G01P5/26 |
主分类号 |
G01P5/14 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A probe system, comprising:
a base configured to be fastened on the cockpit of an aircraft; a plurality of regularly spaced static pressure taps arranged through the base and configured to be connected to a pressure measurement device; and at least one optical window transparent to laser radiation and inserted into the base. |
| 地址 |
COURBEVOIE FR |
