Temperature sensor arrangement in combination with a gas turbine combustion chamber
US6142665A · kind A · utility
38Cited by
4References
6Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 29, 1997 |
| Grant date | Nov 7, 2000 |
| Priority date | — |
| Expiry date | May 29, 2017 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23N2900/05005
- WIPO fieldThermal processes and apparatus
- WIPO sectorMechanical engineering
Abstract
In a temperature-measuring device, in particular for measuring the flame temperature in a gas turbine combustion chamber, a number of optical measuring sensors (7) are arranged directly upstream of a flame front (8) in a premixing zone (3) of a burner (1). Each optical measuring sensor (7) is aligned essentially parallel to and/or coaxial with a fuel flow (5) directed into the gas turbine combustion chamber.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.