Integral aft frame mount for a gas turbine combustor transition piece
US5414999A · kind A · utility
51Cited by
13References
6Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Nov 5, 1993 |
| Grant date | May 16, 1995 |
| Priority date | — |
| Expiry date | Nov 5, 2013 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/30
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A transition piece (110) for a gas turbine comprising a tubular body having an upstream end (112) and a downstream end (114), the downstream end (114) formed with an integral frame (116) surrounding an opening at the downstream end; and an aft mount connector 126) adapted to connect the transition piece (110) to a first stage nozzle of the gas turbine, the aft mount connector (126) formed integrally with the frame (116).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.