Invention Grant
- Patent Title: Gas turbine assembly and corresponding operating method
-
Application No.: US14048878Application Date: 2013-10-08
-
Publication No.: US10774740B2Publication Date: 2020-09-15
- Inventor: Robert Marmilic , Jaan Hellat , Ewald Freitag , Adnan Eroglu
- Applicant: Ansaldo Energia Switzerland AG
- Applicant Address: CH Baden
- Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee: ANSALDO ENERGIA SWITZERLAND AG
- Current Assignee Address: CH Baden
- Agency: Buchanan Ingersoll & Rooney PC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@13868d0e
- Main IPC: F02C3/00
- IPC: F02C3/00 ; F02C7/141 ; F02C7/228 ; F23R3/34

Abstract:
The invention relates to a gas turbine assembly which substantially includes at least one compressor, at least one first burner, at least one second burner that is connected downstream of the first burner, and at least one turbine that is connected downstream of the second burner. At least the first and second burner form a component of a tubular or quasi-tubular combustion chamber element in the flow direction of the combustion path of the burners. The combustion chamber element being closed or quasi-closed and extending between the compressor and the turbine. The combustion chamber elements are arranged around the rotor of the gas turbine assembly in the shape of a ring.
Public/Granted literature
- US20140033728A1 GAS TURBINE ASSEMBLY AND CORRESPONDING OPERATING METHOD Public/Granted day:2014-02-06
Information query