发明名称 Methods and apparatus for fabricating a turbine nozzle assembly
摘要 An apparatus enables a turbine nozzle, including at least two turbine nozzle singlets to be fabricated. Each singlet includes inner and outer bands and a vane extending therebetween. The vane also includes first and second sidewalls coupled together at a leading edge and a trailing edge. The apparatus comprises a fixture, and at least two support members extending from the fixture. Each support member has first and second abutment surfaces, wherein a first of the at least two support members contacts at least one of the leading and trailing edges of a first of the vanes. At least two locating features extend from the fixture, wherein a first of the locating features contacts one of the first and second sidewalls of the first vane. At least two biasing members are coupled to the fixture, wherein a first of the biasing members biases the first vane against the first locating feature.
申请公布号 US8020269(B2) 申请公布日期 2011.09.20
申请号 US20080968501 申请日期 2008.01.02
申请人 GENERAL ELECTRIC COMPANY 发明人 BEVERLEY MICHAEL;LEEKE, JR. LESLIE EUGENE
分类号 B23P6/00;F01D9/02;B23K37/04;B23P15/04;B23Q3/06;B24B41/06;B25B5/14;F01D9/04;F01D25/00;F02C7/00 主分类号 B23P6/00
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