Method of heating gas turbine inlet

METHOD OF HEATING GAS TURBINE INLET An air inlet system delivers a flow of air. The system included a temperature controlling section configured to alter temperature of the air flow. The temperature controlling section imparts a temperature variation distribution across different portions of the air...

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Bibliographic Details
Main Authors KIPPEL, BRADLEY AARON, CHILLAR, RAHUL JAIKARAN, RAJESH, PRABHAKARAN SARASWATHI, CONRAD, RICKY DARYL
Format Patent
LanguageEnglish
Published 02.05.2013
Subjects
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
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Summary:METHOD OF HEATING GAS TURBINE INLET An air inlet system delivers a flow of air. The system included a temperature controlling section configured to alter temperature of the air flow. The temperature controlling section imparts a temperature variation distribution across different portions of the air flow. The system also includes a transition section, one or more flow diverters, one or more screens and/or a flow splitter to cause mixing of the different, temperature variant portions of the air flow and reduce the temperature variation distribution. Fig. 2
Bibliography:Application Number: AU20120232951