发明名称 |
Fan Stagger Angle for Dirt Rejection |
摘要 |
A gas turbine engine (20) includes a spool (30), a turbine (46) coupled to drive the spool (30), a propulsor (42) coupled to be rotated about an axis by the turbine (46) through the spool (30), and a gear assembly (48) coupled between the propulsor (74) and the spool (30) such that rotation of the turbine (46) drives the propulsor (42) at a different speed than the spool (30). The propulsor (42) includes a hub (76) and a row of propulsor blades (74) that extend from the hub (76). Each of the propulsor blades (74) has a span between a root (68) at the hub (76) and a tip (80), and a chord (30) between a leading edge (82) and a trailing edge (84). The chord forms a stagger angle ± with the axis (A), and the stagger angle ± is less than 15° at a position along the propulsor blade (74) that is within an inboard 20% of the span. |
申请公布号 |
EP2543829(A3) |
申请公布日期 |
2017.03.22 |
申请号 |
EP20120174433 |
申请日期 |
2012.06.29 |
申请人 |
United Technologies Corporation |
发明人 |
Gallagher, Edward J.;Rose, Becky E.;Brilliant, Lisa I |
分类号 |
F01D25/34;F01D5/14;F01D15/12;F01D21/04;F02C7/05;F02K3/06 |
主分类号 |
F01D25/34 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|