Combined aircraft angle of attack and dynamic/static pressure sensor assembly
US5544526A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Jun 30, 1994 |
| Grant date | Aug 13, 1996 |
| Priority date | — |
| Expiry date | Jun 30, 2014 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG01P5/165
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A rotatable airstream direction probe is additionally provided with a dynamic pressure sensing port positioned substantially midway between a pair of pneumatic sensing ports with respect to the probe's stagnation line. Pneumatic output ports may thus be provided, each of which communicates with a respective one of the pneumatic sensing and dynamic sensing ports in the probe. The pressure outputs from such output ports may thus be indicative of static and dynamic pressure of an airstream so as to be capable of determining flight information of an aircraft such as airspeed, altitude and vertical speed.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.