A kind of computational methods of Thermal generation unit speed diversity factor
Technical field
The invention belongs to technical field of power generation, more particularly, to a kind of calculating side of Thermal generation unit speed diversity factor
Method.
Background technology
With the development of economy, industry manufacture and requirement of the resident living to power quality are higher and higher.Mains frequency is made
It is deep to be paid attention to by power department to weigh one of the major criterion of power quality.The primary frequency function of Thermal generation unit is made
For the direct approach of power grid frequency modulation function, the quality that function is realized directly affects the quality of mains frequency.Therefore reinforce to combustion
The primary frequency modulation management of coal power generation unit, to safeguarding that power grid security is of great significance.And it weighs Thermal generation unit and once adjusts
One of the important indicator of frequency function is exactly speed diversity factor, and traditional speed diversity factor calculates and uses load variations amount and frequency difference
The ratio between variable quantity obtains, due to power transducer reaction, stand between the delay issues such as communication so that calculated speed diversity factor is not
It can actual response actual load pace of change and amplitude.Therefore according to Thermal generation unit load responding the characteristics of establishes a kind of
The computational methods of Thermal generation unit speed diversity factor, the authenticity and accuracy for improving speed diversity factor result of calculation very must
It wants.
Invention content
It is an object of the invention to overcome the deficiencies of the prior art and provide a kind of meters of Thermal generation unit speed diversity factor
Calculation method.
The present invention solves its technical problem and following technical scheme is taken to realize:
A kind of computational methods of Thermal generation unit speed diversity factor, including steps are as follows:
The first step, generating set operation conditions confirm
(1) 90% rated load of band is at least stablized 24 hours after generating set overhaul;
(2) determine that primary frequency function design meets relevant regulatory requirements;
(3) generating set is exited into AGC control modes;
(4) coordinated control system or DEH power control systems are normally put into, and unit allocation is stablized;
(5) determine that basic control system is normally put into;
(6) it is without exception to determine that the major parameter of generating set operation is stablized;
(7) confirm that rotary speed of generator group and mains frequency signal checking are qualified, and have relevant verification certificate;
(8) confirm that the storage of generating set major parameter data is normal, the sampling period is no less than 1s;
Second step, data obtain
(1) after confirming that the main measuring point of generating set is shown normally, rated speed n before acquisition disturbance0, first stage pressure p0And
Load N0Measuring point data;
(2) simulation tach signal n1, the record first stage pressure p after disturbance is stablized1, load N1;
Third walks, and handles data
(1) rotating speed deviation is calculated:Δ n=n0-n1……(1)
(2) rotating speed change of error perunit is calculated:
(3) first stage pressure perunit benchmark is calculated:
(4) first stage pressure changing value is calculated:Δ P=| P1-P0|……(4)
(5) according to formula (3), the result of calculation of (4), show that first stage pressure changes perunit:
(6) according to the result of calculation of formula (5), the speed diversity factor calculated with first stage pressure is obtained:
Wherein, each meaning of parameters is:n0--- rated speed before disturbance, p0--- first stage pressure before disturbance, N0--- it disturbs
Dynamic preload, n1--- simulation rotating speed, p1--- first stage pressure after disturbance, N1--- disturbance afterload, Δ n --- rotating speed is inclined
Difference, Δ n' --- rotating speed change of error perunit, P1e--- first stage pressure perunit benchmark being calculated, Δ P --- first stage pressure becomes
Change value, Δ P' --- first stage pressure change perunit, δ --- speed diversity factor.
Moreover, it includes Stream temperature, main vapour pressure, steam water-level that major parameter, which is stablized without exception, in (6) step of the first step
Centrum's temperature, combustion chamber draft are stable, alarm free or exception.
Moreover, major parameter data include rotating speed, power, main vapour pressure, governing stage pressure in (8) step of the first step
Power, pitch aperture and instruction.
The advantages and positive effects of the present invention are:
The present invention proposes a kind of computational methods of Thermal generation unit speed diversity factor, is reacted by first stage pressure negative
The variation of lotus reaches fast and accurately purpose, while saving cumbersome Conversion of measurement unit and parameter conversion ring using perunit value calculating
Section provides scientific algorithm method to improve speed diversity factor calculating speed and authenticity.
Description of the drawings
Fig. 1 is the logic step schematic diagram of the method for the present invention.
Specific implementation mode
The embodiment of the present invention is further described below in conjunction with attached drawing:It is emphasized that implementation of the present invention
Example is illustrative, every without being restrictive, therefore the present invention is not limited to the embodiment described in specific implementation mode
The other embodiment obtained according to the technique and scheme of the present invention by those skilled in the art also belongs to the model that the present invention protects
It encloses.
A kind of computational methods of Thermal generation unit speed diversity factor, as shown in Figure 1,
The first step, generating set operation conditions confirm
(1) 90% rated load of band is at least stablized 24 hours after generating set overhaul;
(2) determine that primary frequency function design meets relevant regulatory requirements;
(3) generating set is exited into AGC control modes;
(4) coordinated control system or DEH power control systems are normally put into, and unit allocation is stablized;
(5) determine that basic control system is normally put into;
(6) it is without exception to determine that the major parameter of generating set operation is stablized;
Wherein, major parameter includes that Stream temperature, main vapour pressure, steam water-level centrum's temperature, combustion chamber draft are stable, nothing
Alarm is abnormal;
(7) confirm that rotary speed of generator group and mains frequency signal checking are qualified, and have relevant verification certificate;
(8) confirm that the storage of generating set major parameter data is normal, the sampling period is no less than 1s.
Wherein, major parameter data include rotating speed, power, main vapour pressure, first stage pressure, pitch aperture and instruction.
Second step, data obtain
(1) after confirming that the main measuring point of generating set is shown normally, rated speed n before acquisition disturbance0, first stage pressure p0And
Load N0Measuring point data;
(2) simulation tach signal n1, the record first stage pressure p after disturbance is stablized1, load N1;
Third walks, and handles data
(1) rotating speed deviation is calculated:Δ n=n0-n1……(1)
(2) rotating speed change of error perunit is calculated:
(3) first stage pressure perunit benchmark is calculated:
(4) first stage pressure changing value is calculated:Δ P=| P1-P0|……(4)
(5) according to formula (3), the result of calculation of (4), show that first stage pressure changes perunit:
(6) according to the result of calculation of formula (5), the speed diversity factor calculated with first stage pressure is obtained:
Wherein, each meaning of parameters is:n0--- rated speed before disturbance, p0--- first stage pressure before disturbance, N0--- it disturbs
Dynamic preload, n1--- simulation rotating speed, p1--- first stage pressure after disturbance, N1--- disturbance afterload, Δ n --- rotating speed is inclined
Difference, Δ n' --- rotating speed change of error perunit, P1e--- first stage pressure perunit benchmark being calculated, Δ P --- first stage pressure becomes
Change value, Δ P' --- first stage pressure change perunit, δ --- speed diversity factor.