Compressor control method and system

Patent metadata

Field	Value
Publication number	US-9574572-B2
Application number	US-201113575075-A
Country	US
Kind code	B2
Filing date	Jan 25, 2011
Priority date	Jan 27, 2010
Publication date	Feb 21, 2017
Grant date	Feb 21, 2017

Abstract

A compressor control method includes providing variable aerodynamic sizing of fluid flow through a compressor at multiple operating points of the compressor. A head is determined for an operating point, based on a process input at that operating point. Further, for that operating point, a control pressure number is determined as a function aerodynamic flow sizing at that operating point. The control pressure number is determined a function of the head divided by the square of a tip speed of the impeller of the compressor. An operating speed setpoint is determined based on the determined head and control pressure number.

First claim

The invention claimed is:

1. A control method for a compressor, comprising:
providing variable aerodynamic sizing of fluid flow through the compressor at a plurality of operating points of the compressor,
for an operating point of the plurality of operating points, determining a head of the compressor based on a process input at the operating point,
for the operating point of the plurality of operating points, determining a pressure number as a function of aerodynamic flow sizing at the operating point, and
determining, by a control device of the compressor, an operating speed setpoint of the compressor based on the determined head and pressure number, wherein the compressor comprises a rotating impeller having a tip rotating at a tip speed, wherein the pressure number is a function of the head divided by the square of the tip speed,
controlling shaft rotational speed of the compressor using the determined operating speed setpoint, based on a closed loop feedback control mechanism,
wherein the process input includes a measured compressor inlet temperature, and
wherein the process input includes a compressor discharge pressure, further wherein the head is determined based on a pressure surge margin added to the compressor discharge pressure.

2. The method according to claim 1 , wherein the aerodynamic flow sizing is defined by a variable diffuser position.

3. The method according to claim 1 , wherein the determining of the pressure number is based on a relationship between pressure number and aerodynamic flow sizing, the relationship being defined by a control curve configured for operating the compressor with a minimum margin to surge at the operating point.

4. The method according to claim 3 , wherein the control curve is obtained by:
determining maximum and minimum aerodynamic flow sizing limits for which flow is achievable,
determining a maximum pressure number that would produce flow for the maximum aerodynamic flow sizing limit, and a maximum speed possible for the maximum pressure number, based on performance data of the compressor,
obtaining a test data graph of pressure number at surge versus aerodynamic flow sizing, for various compressor speeds,
plotting a first point on the graph defined by the maximum aerodynamic flow sizing limit and the maximum pressure number obtained from the performance data,
plotting a second point on the graph defined by a minimum pressure number at surge at the maximum speed and a corresponding aerodynamic flow sizing value, the corresponding aerodynamic flow sizing value being intermediate to the maximum and minimum aerodynamic flow sizing limits,
plotting a third point on the graph defined by the minimum aerodynamic flow sizing limit and the corresponding pressure number at surge for the minimum aerodynamic flow sizing limit, at the maximum speed, and
obtaining a first line defined by the first point and the second point, and a second line defined the second point and the third point, wherein the control curve is formed by the first line and the second line.

5. The method according to claim 4 , further comprising obtaining a test data graph of head versus flow for various aerodynamic flow sizing values, and therefrom determining maximum and minimum aerodynamic flow sizing limits for which flow is achievable.

6. The method according to claim 1 , further comprising:
determining a positive and a negative dead band window around the operating speed setpoint,
obtaining a measured speed feedback, and
providing the operating speed setpoint to a variable frequency drive if the measured speed lies outside the positive and negative dead band windows.

7. The method according to claim 1 , wherein the control device comprises a non-transitory computer readable media having computer readable program code embodied therein, the program code being executable by the control device,
wherein the computer readable media is selected from the group consisting of a programmable logic controller, a microcontroller, a desktop computer and a general purpose microprocessor.

8. A compressor system, comprising:
a rotating impeller comprising a tip rotating at a tip speed,
an arrangement for providing variable aerodynamic sizing of fluid flow through the compressor at multiple operating points of the compressor,
a variable frequency drive for controlling compressor speed based on the operating speed setpoint, and
a control device, comprising:
a head determination module configured to determine a head of the compressor based on a process input at an operating point,
a pressure number determination module configured to determine a control pressure number as a function of aerodynamic flow sizing at the operating point, wherein the control pressure number is determined as a function of the head divided by the square of the tip speed, and
an operating speed setpoint determination module configured to determine an operating speed setpoint of the compressor based on the determined head and control pressure number,

wherein the process input includes a measured compressor inlet temperature, and
wherein the process input includes a compressor discharge pressure, further wherein the head is determined based on a pressure surge margin added to the compressor discharge pressure.

9. The system according to claim 8 , wherein the arrangement for providing a variable aerodynamic sizing of fluid flow through the compressor comprises a variable diffuser.

10. The system according to claim 8 , wherein the control device includes a programmable logic controller.

11. The system according to claim 8 , further comprising a sensor module for measuring the process input, the sensor module including at least a temperature sensor for measuring compressor inlet temperature.

Assignees

• Andersen Soeren Boegh
• Ploeger Frans
• Vinton Richard H
• Siemens Ag

Inventors

• Andersen Soeren Boegh
• Ploeger Frans
• Vinton Richard H

Classifications

• F04D27/0284

  Conjoint control of two or more different functions · CPC title

• F04D27/0246

  by varying geometry within the pumps, e.g. by adjusting vanes · CPC title

• F04D27/0261 Primary

  by varying driving speed · CPC title

• Y02B30/70

  Efficient control or regulation technologies, e.g. for control of refrigerant flow, motor or heating · CPC title