发明名称 |
JOINT BETWEEN AIRFOIL AND SHROUD |
摘要 |
<p>A stator joint for a gas turbine engine has a center axis, and a shroud having a radial wall facing substantially radially with respect to the center axis. A slot wall defines in-part a slot in the shroud. A relief wall defines a relief area of the slot. The relief wall extends between the radial wall and the slot wall. A vane has an airfoil and a lug extending into the slot. A flowable attachment material is disposed in the relief area for engagement of the vane to the shroud. A vane assembly and a gas turbine engine are also disclosed.</p> |
申请公布号 |
EP2872764(A1) |
申请公布日期 |
2015.05.20 |
申请号 |
EP20130820700 |
申请日期 |
2013.07.12 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
HAYFORD, RICHARD K.;POTTER, GLEN E. |
分类号 |
F02C7/00;B23P6/00;F01D5/00;F01D9/04;F01D25/24;F02C7/04;F02C7/32 |
主分类号 |
F02C7/00 |
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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