发明名称 タービンダイアフラム構成
摘要 An axial flow turbine diaphragm (10) is constructed without welding or other metal joining techniques as an annular array of static blade units (12). Each blade unit (12) comprises an aerofoil (18) and radially inner and outer platforms integral with the aerofoil. The radially inner platform consists of a segment (14) of the inner diaphragm ring and the radially outer platform consists of a segment (16) of the outer diaphragm ring. At least the outer ring segment (16) has engagement features (161, 162, 165, 166) that mechanically engage with complementary engagement features on neighbouring outer ring segments in the annular array of blade units, the engagement features acting to mechanically interlock neighbouring outer ring segments and produce a self-supporting turbine diaphragm.
申请公布号 JP5627734(B2) 申请公布日期 2014.11.19
申请号 JP20130106803 申请日期 2013.05.21
申请人 アルストム テクノロジー リミテッドALSTOM Technology Ltd 发明人 アンガス ロバート ブラミット−ブラウン;エイドリアン クリフォード ロード;ニオール マクドナルド
分类号 F01D9/02;F01D9/04 主分类号 F01D9/02
代理机构 代理人
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