RO116312B1 - Gas turbine installation with graded expansion - Google Patents

Gas turbine installation with graded expansion

Info

Publication number
RO116312B1
RO116312B1 RO98-01431A RO9801431A RO116312B1 RO 116312 B1 RO116312 B1 RO 116312B1 RO 9801431 A RO9801431 A RO 9801431A RO 116312 B1 RO116312 B1 RO 116312B1
Authority
RO
Romania
Prior art keywords
gas turbine
pressure section
turbine installation
graded
expansion
Prior art date
Application number
RO98-01431A
Other languages
Romanian (ro)
Inventor
Mircea Cârdu
Original Assignee
Mircea Cârdu
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mircea Cârdu filed Critical Mircea Cârdu
Priority to RO98-01431A priority Critical patent/RO116312B1/en
Publication of RO116312B1 publication Critical patent/RO116312B1/en

Links

Abstract

The invention relates to a gas turbine installation with graded expansion. According to the invention, the installation comprises an air compressor (1), a combustion chamber (2), a gas turbine comprising a high pressure section (3) and a medium pressure section (5), an economizer (4), a speed reducer (6) and a driven machine (7), the gases being partially expanded in the high pressure section (3), then passed through the economizer (4), wherein the air compressed by the air compressor (1) is preheated, and further expanded in the medium pressure section (5).
RO98-01431A 1998-09-28 1998-09-28 Gas turbine installation with graded expansion RO116312B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RO98-01431A RO116312B1 (en) 1998-09-28 1998-09-28 Gas turbine installation with graded expansion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RO98-01431A RO116312B1 (en) 1998-09-28 1998-09-28 Gas turbine installation with graded expansion

Publications (1)

Publication Number Publication Date
RO116312B1 true RO116312B1 (en) 2000-12-29

Family

ID=64357827

Family Applications (1)

Application Number Title Priority Date Filing Date
RO98-01431A RO116312B1 (en) 1998-09-28 1998-09-28 Gas turbine installation with graded expansion

Country Status (1)

Country Link
RO (1) RO116312B1 (en)

Similar Documents

Publication Publication Date Title
AU5242599A (en) Quasi-isothermal brayton cycle engine
EP1219800A3 (en) Gas turbine cycle
MY133801A (en) Engine with combustion and expansion of the combustion gases within the combustor
TW354354B (en) Operation of integrating gasification combined cycle power generation systems at part load
TW358853B (en) High pressure combustion turbine and air separation system integration
CA2159634A1 (en) Gas-Turbine Engine with Bearing Chambers and Barrier-Air Chambers
EP1186761A3 (en) Energy recovery from compressor discharge bleed air in gas turbine plants
EP1022436A3 (en) Gas turbine engine seals
EP1128039A3 (en) Gas turbine
PL360351A1 (en) Heat engines and associated methods of producing mechanical energy and their application to vehicles
CA2045371A1 (en) Integrated air separation plant - integrated gasification combined cycle power generator
EP0795728A3 (en) Combustion turbine and elevated pressure air separation system with argon recovery
EP1039115A3 (en) Gas turbine system
EP1331366A3 (en) Gas turbine combined plant and method of operating the same
EP0926317A3 (en) Integrated air separation and combustion turbine process
EP1069282A3 (en) Dual-pressure steam injection partial-regeneration-cycle gas turbine system
SE0101266D0 (en) Engine braking system for a gas turbine and method for engine braking of a gas turbine
GB2396572B (en) Method for recovery of voc-gas and an apparatus for recovery of voc-gas
WO2000020739A3 (en) Gas turbine engine
NO984167L (en) Turbine-driven synthesis gas system and method for operating it
AU2860801A (en) Air separation method and plant
CA2338619A1 (en) Modified fuel gas turbo-expander for oxygen blown gasifiers and related method
ATE421632T1 (en) STEAM AND GAS TURBINE SYSTEM
RO116312B1 (en) Gas turbine installation with graded expansion
AP2001002032A0 (en) Method for operating pollution-free engine expansion chamber and expansion chamber therefor.