发明名称 |
Reduced height ligaments to minimize non-integral vibrations in rotor blades |
摘要 |
A system for minimizing non-integral vibrations in rotor blades located in a compressor section of a gas turbine engine includes a casing having a plurality of bleed slots, at least one of the bleed slots being located in close proximity to a row of rotor blades, a plurality of structural ligaments, at least one of the structural ligaments extending between two adjacent ones of the bleed slots; and a channel for reducing the height of at least one of the structural ligaments so as to minimize the non-integral vibrations in the rotor blades in the row. |
申请公布号 |
US9394792(B2) |
申请公布日期 |
2016.07.19 |
申请号 |
US201213632352 |
申请日期 |
2012.10.01 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
LeBlanc Ryan Edward;Cummings Kevin J.;Ali Amr |
分类号 |
F01D5/10;F01D25/06;F02C6/08 |
主分类号 |
F01D5/10 |
代理机构 |
Bachman & LaPointe, P.C. |
代理人 |
Bachman & LaPointe, P.C. |
主权项 |
1. A system for minimizing non-integral vibrations in rotor blades, comprising:
a casing having a plurality of bleed slots; at least one of said bleed slots being located in close proximity to a row of rotor blades; a plurality of structural ligaments; at least one of said structural ligaments extending between two adjacent ones of said bleed slots; a plurality of valves for sealing said bleed slots and for preventing a flow of air through said bleed slots; and a channel in said at least one structural ligament, wherein said rotor blades rotate about an axis and two opposed ends of said structural ligament are inclined at a non-perpendicular angle with respect to said axis. |
地址 |
Farmington CT US |