SYSTEM AND METHOD FOR PROTECTING COMPONENTS IN A GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION
A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an exhaust section disposed downstream from the downstream end of the turbine section, and a fluid supply system coupled to the exhaust section. The...
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| Main Authors | , , , , |
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| Format | Patent |
| Language | English French German |
| Published |
18.11.2015
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| Subjects | |
| Online Access | Get full text |
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| Abstract | A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an exhaust section disposed downstream from the downstream end of the turbine section, and a fluid supply system coupled to the exhaust section. The fluid supply system is configured to route an inert gas to the exhaust section. |
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| AbstractList | A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an exhaust section disposed downstream from the downstream end of the turbine section, and a fluid supply system coupled to the exhaust section. The fluid supply system is configured to route an inert gas to the exhaust section. |
| Author | HUNTINGTON, RICHARD A BIYANI, PRAMOD K MITTRICKER, FRANKLIN F SAHA, RAJARSHI DASOJI, ANIL KUMAR |
| Author_xml | – fullname: SAHA, RAJARSHI – fullname: HUNTINGTON, RICHARD A – fullname: DASOJI, ANIL KUMAR – fullname: BIYANI, PRAMOD K – fullname: MITTRICKER, FRANKLIN F |
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| DocumentTitleAlternate | SYSTÈME ET PROCÉDÉ POUR PROTÉGER DES COMPOSANTS DANS UN MOTEUR À TURBINE À GAZ AVEC RECIRCULATION DES GAZ D'ÉCHAPPEMENT VORRICHTUNG UND VERFAHREN ZUM SCHUTZ VON KOMPONENTEN EINER GASTURBINE MITTELS REZIRKULIERTEM ABGAS |
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| Notes | Application Number: EP20140702371 |
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| RelatedCompanies | EXXONMOBIL UPSTREAM RESEARCH COMPANY |
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| Snippet | A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an... |
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| SubjectTerms | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS |
| Title | SYSTEM AND METHOD FOR PROTECTING COMPONENTS IN A GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION |
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