发明名称 |
METHOD FOR REPAIRING A BLADE |
摘要 |
<p>A method for repairing a blade in a gas turbine engine comprises the steps of: isolating the damage on the airfoil of the blade; forming a cut back in the shape of elongated "D" shaped recess with a pair of fillets, a depth and a longitudinal axis of the "D" shaped recess having a length along the leading or trailing edge of the airfoil; and the fillets having a respective radius.</p> |
申请公布号 |
CA2854727(A1) |
申请公布日期 |
2014.12.21 |
申请号 |
CA20142854727 |
申请日期 |
2014.06.18 |
申请人 |
PRATT & WHITNEY CANADA CORP. |
发明人 |
WARIKOO, RAMAN;BALIKE, KRISHNA PRASAD |
分类号 |
B23P6/00;F01D5/12 |
主分类号 |
B23P6/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|