发明名称 |
ROTOR ASSEMBLY AND REVERSIBLE TURBINE BLADE RETAINER THEREFOR |
摘要 |
A blade retainer for a gas turbine engine includes a plate-like member (82) with an arcuate outer face (90), an opposed inner face (92), and two spaced-apart end faces (94). The member (82) has an outer portion (96) disposed adjacent the outer face (90), and an inner portion (98) disposed adjacent the inner face (92), and a wedge-shaped recess (100) with a concave radiused valley (102) is formed in the inner portion (98) adjacent each end face. The retainer is left-right symmetrical.
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申请公布号 |
CA2781943(A1) |
申请公布日期 |
2012.12.30 |
申请号 |
CA20122781943 |
申请日期 |
2012.06.28 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
LEE, MICHAEL;COBURN, DAVID;FAGAN, JOSEPH |
分类号 |
F01D5/30;F01D5/02;F01D5/08;F01D5/18 |
主分类号 |
F01D5/30 |
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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