Turbine acceleration governing system

• US 4,204,258 A
• Filed: 10/03/1978
• Issued: 05/20/1980
• Est. Priority Date: 10/03/1978
• Status: Expired due to Term

• Current Assignee: Siemens Westinghouse Power Corporation
• Original Assignee: Westinghouse Electric Corporation (Paramount Global (f/k/a ViacomCBS Inc.))
• Inventors: Heltsley, Alan T., Zitelli, William E.
• Primary Examiner(s): Ruggiero, Joseph F.
• Application Number:
  US05/948,263
• Time in Patent Office: 595 Days
• Field of Search: 364/494, 364/101, 364/107, 364/110, 364/300, 364/565, 60/645, 60/660, 60/646, 290/40 R, 290/40 A, 290/40 B, 290/40 C, 415/15, 415/16, 415/17
• US Class Current: 700/290
• CPC Class Codes: F01D 17/24 electrical
• CPC Class Codes: F01D 19/00 Starting of machines or engines; Regulating, controlling, or safety means in connection therewith warming-up before starting F01D25/10; turning or inching gear F01D25/34

Abstract

A turbine speed control system comprising a pair of concurrently operable electronic microprocessor-based controllers which are coupled together by a data link to functionally cooperate in controlling turbine acceleration primarily during start-up operations in accordance with a set of predetermined measured and calculated turbine conditions. One controller is operative to control the speed of the turbine at selected accelerations from turning gear to a predetermined speed value. This same controller monitors a plurality of temperature differences from preselected regions of the turbine and inhibits turbine acceleration in accordance with an out-of-limit temperature condition associated therewith. In addition, the one controller is further operative to selectively override the turbine speed hold initiated by an out-of-limit temperature condition, the override permitting the one controller to proceed with controlling the speed of the turbine at a desired acceleration. The other controller is selectively operative to govern the turbine acceleration as controlled by the one controller based on calculated present and anticipated rotor stresses which are derived concurrently with the speed control operations of the one controller. A turbine speed hold may be initiated by either a detected differential temperature out-of-limit condition or a detected calculated rotor stress limit condition. In either case, the one controller is further operative to detect if the speed hold occurs in one of a number of predetermined critical speed zones and to adjust the turbine speed outside of the zone in which the speed hold occurs.

Claims

1. In a turbine speed control system which is operative to control the speed of a steam turbine through a turbine start-up operation by regulating the position of at least one steam admission valve of said turbine in accordance with a speed control function based on a computed speed error between an adjustable speed reference signal and a signal representative of the actual speed of said turbine, said speed reference signal being adjusted, at times, to converge to a desired speed demand signal at a selected acceleration, an improvement comprising:

a first controller operative to control the speed of said turbine at selected accelerations from turning gear to a predetermined turbine speed value;

a second controller selectively operative to govern said turbine accelerations as controlled by said first controller in accordance with calculated present and anticipated rotor stresses of said steam turbine, said second controller performing said rotor stress calculations concurrently with the speed control operations of said first controller;

means for generating a plurality of signals representative of actual temperature differences of predetermined portions of said steam turbine and for providing said differential temperature representative signals to said first controller;

and wherein said first controller is further operative to reduce said turbine acceleration to substantially zero upon the detection of at least one of said representative temperature difference signals exceeding a preset limit value respectively associated therewith, said first controller being still further operative to detect when said turbine speed is controllably held substantially fixed in one of a number of predetermined critical speed zones as a result of said acceleration governing by said second controller or as a result of a temperature difference signal exceeding its preset limit value and to adjust said turbine speed outside of said one critical speed zone during either one of said detected turbine speed states.

2. A turbine speed control system in accordance with claim 1 wherein the second controller is additionally operative to govern the first controller to reduce the acceleration of the turbine to substantially zero for a predetermined time interval during the turbine start-up operation initiated by the occurrence of at least one of a plurality of conditions including a selective heat soak actuation and an event in which the turbine speed is controlled substantially to a predetermined heat soak speed value, said selective heat soak actuation being conditionally permitted when the speed reference signal is adjusted substantially equal to the desired speed demand signal by said first controller.

3. A turbine speed control system in accordance with claim 1 wherein the first controller is additionally operative to selectively override the reduction of the turbine acceleration to substnatially zero as caused by at least one representative temperature difference signal exceeding its preset limit value, said override when selected renders control of the turbine speed to proceed at the desired accelerations.

4. A turbine speed control system in accordance with claim 1 wherein the turbine comprises at least a high pressure turbine section and a lower pressure turbine section;

and wherein the temperature differences are rendered between the following predetermined portions of the turbine;

(1) the first stage steam and first stage metal regions of the high pressure turbine section,

(2) the horizontal flange and horizontal bolt regions of the high pressure turbine section, and

(3) the horizontal flange and horizontal bolt regions of the lower pressure turbine section.

5. A turbine speed control system in accordance with claim 1 wherein the turbine comprises at least a high pressure turbine section;

and wherein the temperature differences are rendered between the following predetermined portions of the high pressure tubrine section;

(1) the first stage steam and first stage metal regions,

(2) the horizontal flange bolt and horizontal flange inner regions, and

(3) the horizontal bolt and horizontal flange center regions.

6. A turbine speed control system in accordance with claim 1 wherein the first controller comprises:

a plurality of permanently programmable memory devices for storage of addressable ordered sets of selected instructions and data words;

a microprocessor bus;

means for coupling said plurality of permanently programmable memory devices to said microprocessor bus in accordance with an addressable pattern;

a system clock for generating a first periodic timing signal;

a real time clock for generating a second periodic timing signal;

a microprocessor coupled to said microprocessor bus and governed by said first periodic timing signal to process the instructions and data words of said plurality of permanently programmable memory devices, said processing enabling the first controller to control the speed of the turbine at desired turbine accelerations;

a speed monitoring means coupled to said microprocessor bus and operative in accordance with the processing of a first set of instructions by said microprocessor to periodically generate a speed signal representative of the actual speed of the turbine;

a temporary memory means, coupled to said microprocessor bus, for storage of temporary data words resulting from the instruction processing operations of the microprocessor; and

an analog input means coupled to said microprocessor bus and operative in accordance with the processing of a second set of instructions by said microprocessor to digitize the temperature difference signals and to update the contents of corresponding registers in said temporary memory means with said digitized signals periodically as governed by said real time clock;

wherein the second controller comprises;

a plurality of permanently programmable memory devices for storage of addressably ordered sets of selected instructions and data words;

a microprocessor bus;

means for coupling said plurality of permanently programmable memory devices to said microprocessor bus in accordance with an addressable pattern;

a system clock for generating a first periodic timing signal;

a real time clock for generating a second periodic timing signal;

a microprocessor coupled to said microprocessor bus and governed by said first periodic timing signal to process the instructions and data words of said plurality of permanently programmable memory devices, said processing including the computation of the present and anticipated rotor stress values and the generation of the governing accelerations therefrom;

a speed monitoring means coupled to said microprocessor bus and operative in accordance with the processing of a first set of instructions by said microprocessor to periodically generate a speed signal representative of the actual speed of the turbine;

a temporary memory means, coupled to said microprocessor bus, for storage of temporary data words resulting from the instruction processing operations of the microprocessor; and

an analog input means coupled to said microprocessor bus and operative in accordance with the processing of a second set of instructions by said microprocessor to digitize a preselected number of turbine analog variables associted with said rotor stress calculations and to update corresponding registers in said temporary memory means with said digitized signals periodically as governed by said real time clock; and

wherein each microprocessor-based first and second controller contains an interface to provide a data link for signal communication between the two controllers.

7. A turbine speed control system in accordance with claim 6 wherein the data link interface of each of the first and second microprocessor-based controllers comprises a didigal input/output means coupled to its corresponding microprocessor bus and operative in accordance with another set of instructions by its corresponding microprocessor to conduct digital information between the first and second microprocessor-based controllers.

8. A turbine speed control system in accordance with claim 6 wherein the second controller, upon being selectively actuated to govern the acceleration of the turbine as controlled by the first controller, generates a plurality of acceleration governing signals which are conducted between the second and first controllers over the data link interface.

9. A turbine speed control system in accordance with claim 8 wherein the plurality of acceleration governing signals includes a control signal indicating that the second controller has been selectively actuated to govern the turbine acceleration as controlled by the first controller, and a plurality of signals which when combined form a digital coded word that is representative of the desired accelertion value for turbine speed control.