Process for preventing rotating stall and surge in a turbomachine
The present application provides a process for preventing rotating stall and surge in a turbomachine compressor. The compressor may include air extraction pipes connecting the compressor to a turbomachine exhaust area or to the atmosphere, at least one of the pipes is fitted with a flow regulation valve, and each valve has an adjustable degree of opening. The process includes, for at least one of the valves, a complete opening command when the compressor rotation speed is less than a predetermined threshold value beyond which there is no longer any risk of rotating stall and surge and a command for lowering the degree of opening of the valve when the rotation speed of the compressor exceeds the threshold value.
1. A process for preventing rotating stall and surge in a compressor of a turbomachine, with air extraction pipes connecting the compressor to an exhaust area of the turbomachine or to the atmosphere, at least one of the air extraction pipes including an air regulation valve, and each valve including an adjustable degree of opening, comprising, for at least one of the valves:
a command for completely opening the valve when the compressor rotation speed is less than a predetermined threshold value; and
a command for lowering the degree of opening of the valve when the compressor rotation speed exceeds the predetermined threshold value, wherein the degree of opening of the valve when the compressor rotation speed exceeds the predetermined threshold value is lowered based at least in part on a final percentage of opening, a margin of pitch point, a margin of a percentage of speed to attain, and a corrected rotation speed of the compressor.
2. The process according to claim 1 , wherein when the compressor rotation speed exceeds the predetermined threshold value, the degree of opening of the valve lowers continuously when the compressor rotation speed increases.
3. The process according to claim 1 , wherein when the compressor rotation speed attains a rated rotation speed of the compressor, a final value of the degree of opening is selected such that the air flow in the air extraction pipes does not cause rotating stall and surge.
4. The process according to claim 1 , wherein when the compressor rotation speed exceeds the predetermined threshold value, the degree of opening of the valve according to the compressor rotation speed is a decreasing linear function or a decreasing function of several linear portions of different slopes.
5. The process according to claim 1 , wherein the predetermined threshold value is selected such that an air extraction speed and sound speed ratio does not exceed 0.4.
6. The process according to claim 1 , wherein at least one of the air extraction pipes is connected to a wicket gate of the turbomachine for cooling.
7. The process according to claim 1 , wherein the turbomachine is a gas turbine.
8. The process according to claim 1 , wherein the predetermined threshold value is between about 5 to about 15% of the compressor rotation speed above the compressor critical point.
9. A turbomachine, comprising:
a compressor;
air extraction pipes connecting the compressor to a turbomachine exhaust area or to the atmosphere;
at least one of the pipes comprising a flow regulation valve with an adjustable degree of opening; and
a control device;
the control device providing instructions to:
open completely the valve when the compressor rotation speed is less than a predetermined threshold value, and
reduce the degree of opening of the valve when the compressor rotation speed exceeds the threshold value, wherein the degree of opening of the valve when the compressor rotation speed exceeds the predetermined threshold value is reduced based at least in part on a final percentage of opening, a margin of pitch point, a margin of a percentage of speed to attain, and a corrected rotation speed of the compressor.