发明名称 |
ROTOR ASSEMBLY, CORRESPONDING GAS TURBINE ENGINE AND METHOD OF ASSEMBLING |
摘要 |
<p>A rotor assembly for use in a gas turbine engine having an axis of rotation includes a plurality of rotor blades. Each rotor blade includes a platform extending between opposing side faces, a shank extending radially inward from the platform, and a slot at least partially defined in each of the opposing side faces. A sealing member is configured to be inserted into each slot of a first rotor blade of the plurality of rotor blades such that at least a portion of each sealing member extends beyond one of the opposing side faces. A second rotor blade of the plurality of rotor blades is coupled adjacent the first rotor blade such that at least a portion of one sealing member is inserted into a corresponding second slot on the second rotor blade.</p> |
申请公布号 |
CA2875810(A1) |
申请公布日期 |
2013.12.19 |
申请号 |
CA20132875810 |
申请日期 |
2013.06.14 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
PEARSON, SHAWN MICHAEL;BRASSFIELD, STEVEN ROBERT;STEGEMILLER, MARK EDWARD;FILIPA, JONATHAN ALAN;DURSTOCK, DANIEL LEE |
分类号 |
F01D5/22;F01D5/30;F01D11/00 |
主分类号 |
F01D5/22 |
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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