High-pressure rotor control system
A high-pressure (HP) rotor control system includes an HP rotor and a controller. The HP rotor includes a plurality of rotor blades that rotate about a centerline axis, and a plurality of variable stator vanes (VSVs) that are rotatable about a variable stator vane (VSV) pitch axis. The plurality of VSVs are disposed at an incidence angle. The controller controls the plurality of VSVs to rotate the plurality of VSVs about the VSV pitch axis to change the rotor incidence angle of the plurality of VSVs as the HP rotor approaches a thrust crossover condition.
1 . A high-pressure (HP) rotor control system comprising:
an HP rotor including a plurality of rotor blades that rotate about a centerline axis, and a plurality of variable stator vanes (VSVs) that are rotatable about a variable stator vane (VSV) pitch axis, the plurality of VSVs disposed at an incidence angle; and
a controller that:
determines whether the HP rotor is approaching a thrust crossover condition; and
controls the plurality of VSVs to rotate the plurality of VSVs about the VSV pitch axis to change the incidence angle of the plurality of VSVs if the HP rotor is approaching the thrust crossover condition.
2 . The HP rotor control system of claim 1 , wherein the HP rotor further includes one or more bearings, and the controller controls the plurality of VSVs to rotate the plurality of VSVs about the VSV pitch axis as the HP rotor approaches the thrust crossover condition to increase axial forces on the one or more bearings.
3 . The HP rotor control system of claim 1 , wherein the HP rotor includes an HP compressor, an HP turbine, and an HP shaft that couples the HP compressor to the HP turbine.
4 . The HP rotor control system of claim 1 , wherein the controller controls the plurality of VSVs to change the incidence angle based on HP rotor performance if the HP rotor is not approaching the thrust crossover condition.
5 . The HP rotor control system of claim 1 , wherein the controller determines that the HP rotor is approaching the thrust crossover condition based on HP rotor thrust and HP rotor vibration of the HP rotor.
6 . The HP rotor control system of claim 5 , further including one or more vibration sensors, wherein the controller determines the HP rotor vibration based on one or more HP rotor vibration signals received from the one or more vibration sensors.
7 . The HP rotor control system of claim 5 , wherein the controller determines the HP rotor thrust based on engine mission parameters and ambient conditions.
8 . The HP rotor control system of claim 5 , wherein the controller compares the HP rotor thrust to an HP rotor thrust threshold, and compares the HP rotor vibration to an HP rotor vibration threshold.
9 . The HP rotor control system of claim 8 , wherein the controller determines that the HP rotor is approaching the thrust crossover condition if the HP rotor thrust is less than or equal to the HP rotor thrust threshold and the HP rotor vibration is greater than or equal to the HP rotor vibration threshold.
10 . A method of controlling a high-pressure (HP) rotor, the HP rotor including a plurality of rotor blades that rotate about a centerline axis, and a plurality of variable stator vanes (VSVs) that rotate about a variable stator vane (VSV) pitch axis, the method comprising:
determining, by a controller, whether the HP rotor is approaching a thrust crossover condition; and
controlling, by the controller, the plurality of VSVs to rotate the plurality of VSVs about the VSV pitch axis to change an incidence angle of the plurality of VSVs if the HP rotor is approaching the thrust crossover condition.
11 . The method of claim 10 , wherein the HP rotor further includes one or more bearings, and the method further comprises controlling, by the controller, the plurality of VSVs to rotate the plurality of VSVs about the VSV pitch axis as the HP rotor approaches the thrust crossover condition to increase axial forces on the one or more bearings.
12 . The method of claim 10 , wherein the HP rotor includes an HP compressor, an HP turbine, and an HP shaft that couples the HP compressor to the HP turbine.
13 . The method of claim 10 , further comprising controlling, by the controller, the plurality of VSVs to rotate the plurality of VSVs to change the incidence angle based on HP rotor performance if the HP rotor is not approaching the thrust crossover condition.
14 . The method of claim 10 , further comprising determining, by the controller, that the HP rotor is approaching the thrust crossover condition based on HP rotor thrust and HP rotor vibration of the HP rotor.
15 . The method of claim 14 , wherein the HP rotor further includes one or more vibration sensors, and the method further comprises receiving, by the controller, one or more HP rotor vibration signals from the one or more vibration sensors, and determining, by the controller, the HP rotor vibration based on the one or more HP rotor vibration signals.
16 . The method of claim 14 , further comprising determining, by the controller, the HP rotor thrust based on engine mission parameters and ambient conditions.
17 . The method of claim 14 , further comprising comparing, by the controller, the HP rotor thrust to an HP rotor thrust threshold, and comparing, by the controller, the HP rotor vibration to an HP rotor vibration threshold.
18 . The method of claim 17 , further comprising determining, by the controller, that the HP rotor is approaching the thrust crossover condition if the HP rotor thrust is less than or equal to the HP rotor thrust threshold and the HP rotor vibration is greater than or equal to the HP rotor vibration threshold.
19 . The method of claim 10 , further comprising controlling, by the controller, the plurality of VSVs to change the incidence angle by up to ±5°.
20 . The HP rotor control system of claim 1 , wherein the controller controls the plurality of VSVs to change the incidence angle by up to ±5°.