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| Surge Control | |||||||
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Introduction
Dresser-Rand has been a leading designer and supplier of surge control systems for centrifugal and axial compressors for over thirty-five years. Recent innovations in control technology have made it possible to supply
surge control systems which are capable of coping with rapid flow fluctuations and process
gas variations. Current surge control systems from Dresser-Rand Control Systems provide
protection against surge with more efficient compressor operation, especially in process
applications that involve variations in the gas mixture and temperature. This worst-case setting approach can result in inefficient compressor operation caused by excess recycle or blow-off flow and wasted energy. A more practical surge control method, which uses a Universal Performance Curve, has been developed and patented by Dresser-Rand. The Universal Performance Curve method offers several benefits when compared to traditional surge control methods. It provides extremely accurate surge control by defining the surge point over a wide range of process gas conditions. This method makes it possible to position the control line for optimum surge protection which eliminates unnecessary recycling and increases overall plant operating efficiency. Compressor Surge and Measurement This surge cycle will continue until some change is made in the process or compressor conditions. A surge controller typically measures a function of pressure rise versus flow. The controller operates a surge valve to maintain sufficient forward flow to prevent surge.
The
system utilizes a characterization of compression ratio (Pd/Ps) versus compensated
compressor inlet flow function (hs / Ps)½ as control parameters. This
algorithm allows for use of the Dresser-Rand surge control system on most applications,
resulting in minimized recycle or blow-off flow. This method reduces the initial cost and
simplifies engineering, testing, operation, and maintenance associated with the system
when compared to alternative methods. The input signals required
to facilitate use of the surge control algorithm on centrifugal compressors are the
suction flow differential pressure, suction pressure and discharge pressure as indicated
in Figure 1.
Surge Control Operation
Under normal operating conditions, PI control is used and surge control action is initiated at the control line by opening the surge valve as required to maintain forward flow through the compressor. This prevents a further shift of the operating point to the left towards surge. In the case of rapid reductions in flow, such as process upsets, three additional controls are implemented. First, a backup line, located between the control line and the surge line, is used. If the compressor operating point moves to the left of the control line and reaches the backup line, Dresser-Rand's Closed Loop Step Logic will quickly force the surge valve open as required to increase forward flow through the compressor. Second, if the operating point of the compressor reaches the backup line a set number of times (i.e. 3), within a specified period of time (i.e. 5 minutes), the control set point will be shifted to the right via Dresser-Rand's Set point Shift Logic. Third, a variable proportional gain action has been added to the control loop to assist in stabilizing the process when rapid decreases in compressor flow are encountered. Step Logic The output to the valve is forced to decrease in discrete, timed steps, thus opening the surge valve much quicker than possible with conventional PI control. Valve opening steps are initiated until the flow has moved to a safe level. Compressor surge is avoided by this quick incremental control of the surge valve thus minimizing the effects of process upsets. Set Point Shift The intent of the set point shift is to prevent surge until the cause of the instability can be corrected. The shifted set point remains in effect until reset by the operator.
In general, the controller needs to be slow for normal operating conditions, but fast when needed to protect the compressor from surge. During rapid decreases in flow near the surge control line, Dresser-Rand uses a Floating Proportional control algorithm to open the surge valve before the operating point reaches the control line. Normal PI control is resumed when the process upset has been stabilized. Implementation
The first method uses the
DI-Tronics®
IV control system. This PLC (Programmable Logic Controller) based control system
incorporates surge control as an integral part of the PLC program without the need for
additional external hardware. Compressor inlet flow, suction pressure, and discharge
pressure measurements are input directly into the system using standard PLC analog inputs.
The tuning parameters are displayed and adjusted from an Operator Interface
(OI) screen.
Compressor curves, with the operating point, control line and back-up line are displayed
on the Operator Interface monitor. The system parameters are trended and displayed on the
Operator Interface monitor. Both systems utilize the Universal Performance Curve concept. Field Devices and
Process Designs Flow measuring devices should be located such that gas disturbances will be minimized (less noise), and designed for the full operating range of the compressor. Transmitters should be located as close as possible to the source of measurement to minimize reaction time. Surge valves should provide a full stroke response preferably within 1 second, but no more than 2 seconds. The surge valve should be linear and should be sized in accordance with the compressor maps and expected operating conditions. Since the effects of opening the surge valve are a decrease in compressor discharge pressure and/or an increase in suction pressure, to increase flow through the compressor, process and piping designers should minimize, as much as practical, the piping volume in the recycle path and the volume between the compressor and the discharge check valve.
Controller
Specifications
Nomenclature (S.I. Units in parenthesis) ACFM
Actual Cubic Feet Per Minute (M3/Hr = 1.6999 ACFM) Subscripts Instrument Symbols Gaston, J.R. "Turbocompressor Antisurge Control, New Solution for an Old Problem", The American Society of Mechanical Engineers 92-GT-428, Presented at the International Gas Turbine And Aeroengine Congress and Exposition, Cologne, Germany (June 1-4, 1992). Rigoni, K.B. "Anti-Surge Control Algorithm", Dresser-Rand Control Systems. |
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| Copyright 1999 Dresser-Rand | |||||||