GAS TURBINE ENGINES CONNECTED IN SERIES
A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature compressor (12), a combustor (14), a high pressure turbine (16), a high temperature compressor (20), a reheat combustor (24), and a low pressur...
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| Main Author | |
|---|---|
| Format | Patent |
| Language | English French |
| Published |
15.07.1999
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| Edition | 6 |
| Subjects | |
| Online Access | Get full text |
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| Abstract | A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature compressor (12), a combustor (14), a high pressure turbine (16), a high temperature compressor (20), a reheat combustor (24), and a low pressure turbine (26). High pressure turbine (16) only partially expands the process gas. High pressure compressor (20), compresses the high pressure turbine exit gas stream (6b) before reheat combustor (24) raises the process gas stream enthalpy h1 to a point approximately equal to the enthalpy of the gas stream entering the high pressure turbine (16). |
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| AbstractList | A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature compressor (12), a combustor (14), a high pressure turbine (16), a high temperature compressor (20), a reheat combustor (24), and a low pressure turbine (26). High pressure turbine (16) only partially expands the process gas. High pressure compressor (20), compresses the high pressure turbine exit gas stream (6b) before reheat combustor (24) raises the process gas stream enthalpy h1 to a point approximately equal to the enthalpy of the gas stream entering the high pressure turbine (16). |
| Author | ATTIA, MAGDY S |
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| Discipline | Medicine Chemistry Sciences |
| DocumentTitleAlternate | MOTEURS DE TURBINE A GAZ CONNECTES EN SERIE |
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| Notes | Application Number: CA19982316875 |
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| PublicationYear | 1999 |
| RelatedCompanies | SIEMENS WESTINGHOUSE POWER CORPORATION |
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| Snippet | A high temperature compression and reheat gas turbine system (10), and method for operating the system, is disclosed. The system includes a high temperature... |
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| SubjectTerms | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| Title | GAS TURBINE ENGINES CONNECTED IN SERIES |
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