发明名称 Gas turbine transition duct apparatus
摘要 A gas turbine transition duct is provided comprising a generally tubular main body having first and second ends, the first end being adapted to be positioned adjacent to a combustor unit and the second end being adapted to be positioned adjacent to a turbine and a collar coupled to the main body second end. The collar may have upper, lower and side portions. At least one of the side portions may be provided with a notched section.
申请公布号 US8118549(B2) 申请公布日期 2012.02.21
申请号 US20080198413 申请日期 2008.08.26
申请人 SCHIAVO ANTHONY L.;SIEMENS ENERGY, INC. 发明人 SCHIAVO ANTHONY L.
分类号 F01D1/00;F01D9/00;F01D25/24;F03B1/00;F03B3/00;F03B11/02;F03D1/00;F03D3/00;F03D5/00;F03D11/00;F04D1/00;F04D17/00;F04D23/00;F04D29/42 主分类号 F01D1/00
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