发明名称 GAS TURBINE HAVING AN IMPROVED COOLING ARCHITECTURE
摘要 <p>A THERMAL MACHINE INCLUDES A HOT GAS CHANNEL (22); A SHELL (21) BOUNDING THE HOT GAS CHANNEL (22); A COOLING SHIRT (19) SURROUNDING THE SHELL (21) ; AND A COOLING CHANNEL DISPOSED BETWEEN THE SHELL (21) AND THE COOLING SHIRT (19) AND CONFIGURED TO CONVECTION COOL THE HOT GAS CHANNEL (22) WITH A COOLING MEDIUM, WHEREIN THE COOLING SHIRT (19) INCLUDES AT LEAST ONE LOCAL DIVERGENCE IN THE GUIDANCE OF THE COOLING MEDIUM SO AS TO COMPENSATE FOR NON-UNIFORMITIES IN AT LEAST ONE OF A THERMAL LOAD ON THE SHELL (21) AND A FLOW OF THE COOLING MEDIUM IN THE COOLING CHANNEL (20).</p>
申请公布号 MY154620(A) 申请公布日期 2015.07.15
申请号 MY2010PI03908 申请日期 2009.02.16
申请人 ALSTOM TECHNOLOGY LTD 发明人 HARTMUT HÄHNLE;RUSSELL BOND JONES;GREGORY VOGEL;REMIGI TSCHUOR
分类号 F02C1/00 主分类号 F02C1/00
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