发明名称 INTERNALLY COOLED SPOKE
摘要 A turbine engine includes a compressor section, a combustor section in fluid communication with the compressor section, a high pressure turbine in fluid communication with the combustor, a low pressure turbine in fluid communication with the high pressure turbine, and a mid turbine frame located axially between the high pressure turbine and the low pressure turbine. The mid turbine frame includes an outer frame case, an inner frame case, and a plurality of hollow spokes that distribute loads from the inner frame case to the outer frame case. The spokes are hollow to allow cooling airflow to be supplied through the spokes to the inner frame case.
申请公布号 US2013192267(A1) 申请公布日期 2013.08.01
申请号 US201213361480 申请日期 2012.01.30
申请人 SANCHEZ PAUL K.;PAREKH KALPENDU J.;DANIELS WILLIAM A.;TU JOHN S.;UNITED TECHNOLOGIES CORPORATION 发明人 SANCHEZ PAUL K.;PAREKH KALPENDU J.;DANIELS WILLIAM A.;TU JOHN S.
分类号 F01D25/24;F02C7/12 主分类号 F01D25/24
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