发明名称 |
Coolable segment for a turbomachinery and combustion turbine |
摘要 |
The invention pertains to a coolable segment (1) for a turbo machinery (20), which turbo machinery (20) is operated with a hot fluid (29). The segment (1) comprises a cooling wall (2) extending in an axial direction (37) and in a circumerential direction (36) orthogonal to said axial direction (37); a hot fluid surface (3) to be exposed to the hot fluid (29). Between the wall (2) and the surface (3) a cooling structure (4) is arranged which is permeable to cooling fluid (5) and provides cooling surfaces (6) for cooling by heat transmission through radiation. The cooling structure (4) comprises either a netting, in particular a wire netting or a porous material. The invention further pertains to a combustion turbine (20) comprising a coolable segment (1).
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申请公布号 |
US2004146399(A1) |
申请公布日期 |
2004.07.29 |
申请号 |
US20040756671 |
申请日期 |
2004.01.13 |
申请人 |
BOLMS HANS-THOMAS;HESELHAUS ANDREAS;HOFFSCHMIDT BERNHARD |
发明人 |
BOLMS HANS-THOMAS;HESELHAUS ANDREAS;HOFFSCHMIDT BERNHARD |
分类号 |
F01D5/28;F01D25/12;F01D25/14;F01D25/24;F02C7/00;F02C7/18;F02K1/82;F23R3/00;F23R3/06;(IPC1-7):F01D5/08 |
主分类号 |
F01D5/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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