UA88223C2 - Gas-turbine engine - Google Patents
Gas-turbine engineInfo
- Publication number
- UA88223C2 UA88223C2 UAA200801191A UAA200801191A UA88223C2 UA 88223 C2 UA88223 C2 UA 88223C2 UA A200801191 A UAA200801191 A UA A200801191A UA A200801191 A UAA200801191 A UA A200801191A UA 88223 C2 UA88223 C2 UA 88223C2
- Authority
- UA
- Ukraine
- Prior art keywords
- compressor
- turbine
- rotor
- group
- console section
- Prior art date
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A gas-turbine one-shaft engine with two-support rotor of turbo-group on elastic-damper bearings proposed that realizes Brayton cycle has a compressor, a combustion chamber, a turbine that brings into action the compressor and electric generator, with actuating of electric generator from side of compressor and with axial outlet for gases from turbine, at that power circuit of bodies comprises connected to each other with outlet and inlet flanges power bodies of compressor, combustion chambers, turbines. The compressor is arranged as centrifugal one, with console section, at that rotor of turbo-group is arranged assembled, of cylinder-disc type, and includes connected to each other rotor of centrifugal compressor with console section, cylindrical insert with disc that has gaskets, rotor of turbine. Front pin of rotor of turbo-group with support and rest bearings is placed in console section of compressor, and to its flange for transfer of torque to console section of compressor flexible hub of middle disc of console section of the rotor is connected. The combustion chamber is arranged as group of remote combustion chambers placed in radial positions, there fire pipes are in middle cross section with telescopic connections and at output through shoe-like branch pipe those are hermetically connected to first nozzle apparatus of the turbine. The power circuit of the bodies additionally has outer power body that consists of connected to each other front cone, cylindrical insert, back cone and tightly surrounds the turbine and at least part of compressor, and outside it is connected to power bodies of group of remote combustion chambers.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200801191A UA88223C2 (en) | 2008-01-31 | 2008-01-31 | Gas-turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200801191A UA88223C2 (en) | 2008-01-31 | 2008-01-31 | Gas-turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
UA88223C2 true UA88223C2 (en) | 2009-09-25 |
Family
ID=50635125
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200801191A UA88223C2 (en) | 2008-01-31 | 2008-01-31 | Gas-turbine engine |
Country Status (1)
Country | Link |
---|---|
UA (1) | UA88223C2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2741994C2 (en) * | 2018-05-16 | 2021-02-01 | Публичное акционерное общество "МОТОР СИЧ" (АО "МОТОР СИЧ") | Gas turbine unit |
-
2008
- 2008-01-31 UA UAA200801191A patent/UA88223C2/en unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2741994C2 (en) * | 2018-05-16 | 2021-02-01 | Публичное акционерное общество "МОТОР СИЧ" (АО "МОТОР СИЧ") | Gas turbine unit |
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