High temperature rake for suspersonic flow
US6595062B1 · kind B1 · utility
25Cited by
10References
12Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 31, 2001 |
| Grant date | Jul 22, 2003 |
| Priority date | — |
| Expiry date | May 31, 2021 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2270/303
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
An apparatus measuring the temperature and/or pressure of an exhaust gas plume from a supersonic military jet engine. The apparatus includes a rotatable airfoil having one or more sensors that are impinged by the exhaust gas flow path prior to the exhaust gas flowing over the airfoil. At least one base is attached and adapted to be mounted to a supporting surface for locating the airfoil rearward of the exhaust gas plume.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.