The present invention generally relates to a method and apparatus for increasing the operational reliability and preferably the safety of a steam turbine's electro-hydraulic control system or electro-mechanical control system with respect to the process of turbine shutdown.
Steam turbine control systems often incorporate electro-mechanical pilot-valve actuator assemblies to regulate hydraulically-driven actuator pistons that modulate steam valves, thereby controlling turbine speed. However, it is becoming more popular to use direct electro-mechanical actuation of the steam valves themselves, since they are fully capable of satisfying force and speed requirements.
In case of electro-mechanical pilot-valve actuation, some of the prior art systems can be applied to provide trip response upon complete power interruption. In case of the direct actuation of the steam valve, however, using electro-mechanical actuators, a complete interruption of electrical power to the electromotor makes this solution unusable in some industries, especially in power utility industries where the requirement is that there be a trip response of the steam valves for many circumstances. The application of the prior art systems, though is technically impractical.
For example, it is well known that the drawback of electromagnetic actuation is that on brief interruptions of electrical power, the actuator causes a trip response to the pilot valve, whereas a drawback of electromotor actuation is that on complete interruptions of electrical power the actuator cannot independently cause a trip response of the pilot valve on demand.
Thus, there is a need for a method and apparatus to provide a trip response of electrically actuated steam turbine control valves in the case of primary electrical power source interruption or failure of any primary control system electrical component.
A general feature of the present invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that addresses the problems in the art.
A further feature of the present invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that provides a means to effect a trip response regardless of the electro-mechanical actuator type used.
Another feature of the present invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that overcomes the drawbacks of electromotor actuation.
A still further feature of the present invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that combines the capabilities of effecting a trip response regardless of the electro-mechanical actuator type used and the drawback of electromotor actuation.
Still yet another feature of the invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that provides a trip response of electrically actuated steam turbine control valves in the case of primary electrical power source interruption or failure of any primary control system electrical component.
Another feature of the present invention is a method and apparatus for improving electro-hydraulic and electro-mechanical integrated control systems for a steam turbine that is simpler than prior art systems.
These and other features or objects of the invention will be addressed further in the remaining descriptions contained herein.
The present invention generally drives steam turbine control valves to a closed position in case of primary power supply interruption in a manner which overcomes the problems associated with the prior art. More specifically, the present invention preferably employs an additional electromotor connected to mechanical actuators and supplementary equipment such as one or more additional digital controllers and battery backup. Also some prior art systems suggested using double coil motors (or a second motor) only to increase the force applied during dynamic control action and to improve control system dynamic characteristics. However, the present invention incorporates implementation of double coil (two motors) actuation for protection purposes. The second coil (motor) is used as a backup actuator in case of primary power source interruption or failure of any primary control systems electrical component.
Generally, in the present invention, when an electromotor actuator is coupled to an additional piston and working in conjunction with a pilot valve, or is coupled directly with the steam valve, the combined effect is still capable of providing electrical trip to shut down the turbine on demand during complete electrical service interruptions. All control system components are preferably fully backed up, including electrical motor, position transmitter, controller, power supply, and cables. The present invention generally includes electro-mechanical actuators that can be equipped with multiple coils (usually a primary and a secondary). In a dual-coil configuration, the primary coil is preferably energized according to an output of a PID controller, whereas the secondary coil is preferably regulated by a separate control element.
The entire system is preferably powered by means of Uninterruptable Power Supply (UPS) with AC output which can provide sufficient time for trip response using a primary coil. At the same time, a secondary coil is preferably powered by an independent source (AC or DC) supported by a UPS and/or a separate battery backup. Thus, whenever trip response is required and there is a complete main power interruption, the secondary coil is quickly energized to provide the necessary trip response.
Consequently, the present invention negates the disadvantage of using electromotor actuators particularly in power utility industry, but also provides higher reliability of the integrated turbo machinery speed-control system.
Prior art systems described independent protection system using hydraulic components which overcomplicates the control system setup, and reduce system reliability. The advantage of the present invention over prior art is it does not require complex implementation of independent hydraulic protection system and uses pure electro-mechanical components.
To provide reliable trip response at the event of complete power interruption from the main source an integrated turbo machinery control system should be capable of compensating that by providing power to the secondary motor from the secondary uninterruptable power source, through secondary drive.
Power to Control System is provided from the main source AC Power #1 113 through the uninterruptable power supply (UPS) 114. Power to the Drive 1 107 is provided from the main source AC Power #2 112, which consequently powers primary coil of the actuator 104.
At the normal operating conditions trip response provided by closing of the steam valve 102 through changing set point reference value to 0 for the Drive 1 107, which consequently manipulates primary coil of the actuator 103 and closes the steam valve 102.
Also at the normal operating conditions Drive 2 106 is monitors position of the steam valve by receiving signal from transmitter (XMTR 2) 120.
Drive 2 106 powered by DC power and provided either from the main source AC Power #3 111 through uninterruptable power supply (UPS) 110, and consequently AC/DC converter or alternately from battery backup 108.
Whenever ESD logic Block 116 senses main source power loss it instantaneously changes set point reference value to the Drive #2 106 to 0, which consequently manipulates secondary coil of the actuator 105 and closes the steam valve 102.
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The turbine-controlled variable described herein is not restrictive nor unique to this invention; in which case, other control-system variables may be considered. However, it should be noted that the type of electro-mechanical actuators is immaterial as long as they are equipped with multiple coils or motors, and corresponding drivers. This invention has many applications wherever electro-mechanical actuators are used. Obviously, many modifications and variations of the present invention are possible in light of the above teachings. It is, therefore, to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described.