The present invention relates to compressors. More specifically, the present invention relates to a subsea located compressor that can operate in order to compress gas provided a liquid contents in the gas inlet flow is below a maximum limit.
Compressors are well known technology having numerous applications. It is also known that compressors will be damaged if the compressor blades, rotating at high speed, are hit by heavy objects. Such heavy objects include excessive quantities of oil drops and water drops. Accordingly, a compressor can only operate reliably if the liquid contents of the gas to be compressed is within a maximum acceptable limit.
For compressors operating on dry sites, such as industrial sites, the liquid contents can be separated out from the inlet gas. The separated liquid can be used for any convenient purpose or be discharged after being cleaned if required.
For a compressor located subsea, neither of separation, use and discharge of the liquid is straightforward. The actual location of the compressor can be tens or hundreds of kilometers away from land or surface installations and the depth can be hundreds of meters. Use of the separated liquid, typically oil and possibly water, requires huge investments in equipment and pipes. Discharge of the oil will violate regulations. The equipment for subsea separation and cleaning is very expensive. Currently, collection of sample bottles with an ROV (remotely operated vehicle) and nuclear density gauges are the techniques for determination of liquid in gas volume fraction. The above mentioned high cost and limited availability of technology are disadvantages of the prior art subsea compression technology.
There is a demand for both a system and a method for control of a subsea located compressor, providing improvements with respect to the disadvantages mentioned above.
The demand is met with the present invention.
More specifically, the invention provides a system for control of a subsea located compressor fluidly connected to receive an inlet flow of gas through an inlet line, said flow may include liquid in an amount that may vary. The control system comprises
In a preferable embodiment the system comprises:
The sensor means is preferably an optical sensor using dark-field illumination with objective and camera arranged between a multitude of light sources, arranged outside of or including a window to be arranged in the pipe wall. The sensor is the subject matter of parallel patent application NO 2009 3598 to which it is referred for further information. Alternatively, the sensor is according to the teaching of EP 1159599.
The control means preferably comprises at least one of an atomiser or injection mixer or ejector; a gas scrubber or separator further upstream separating and retaining liquid contents from the inlet flow, and a line arranged for injecting and mixing retained liquid back into the inlet flow, via the atomiser or injection mixer or ejector, as small droplets of size distribution and liquid volume fraction within a maximum acceptable limit, a switch or speed control operatively connected to the subsea compressor. Accordingly, the control means can stop or reduce the speed of the compressor, or the control means can affect the droplet size distribution and liquid volume fraction of the inlet line to the compressor. Preferably, the atomiser or injection mixer uses the venturi effect in order to draw in liquid. The injection mixer can be a ProPure injection mixer. Preferably a line with high pressure gas from the outlet side of the compressor is fed back to the injection mixer or atomiser in order to draw in liquid and achieve a good mixing or atomisation. An injection pump and a control valve are preferably arranged in the line for liquid from the scrubber or separator.
Preferably a scrubber is arranged in the inlet line, a liquid level sensor is arranged in the scrubber, a gas outlet from the scrubber includes an atomiser or injection mixer upstream of a sensor means in the inlet line to the compressor, the atomiser or injection mixer is operatively connected to a control device and the atomiser or injection mixer is fluidly connected to the outlet side of the compressor and to a liquid outlet from the scrubber.
Preferably, the atomiser or injection mixer is arranged immediately upstream of the compressor, for example within a distance of two inlet pipe diameters, with only the sensor in between the compressor and atomiser or injection mixer. This is preferable in order to avoid coalescence or similar effect by the droplets and avoid precipitation of droplets on surfaces before reaching the compressor.
Preferably, the gas inlet line includes a flow rate and/or flow velocity meter, which makes it easier to relate the droplet size distribution and the liquid volume fraction to the impact effect of the liquid contents on the compressor, and improves the quality of the calculations. Preferably, the flow meter is integrated as a venturi flow meter as a part of the injection mixer or atomiser. A separate measurement of flow rate, combined with the measurements of the optical darkfield sensor of droplet size and thereby droplet size distribution and liquid volume fraction or droplet density, facilitates the processing of the measured data in order to calculate the impact effect of the liquid contents, in order to ensure that the liquid contents is below the acceptable limit. Alternatively, the parameters are calculated only based on data from the darkfield sensor, for example by taking many representative droplet pictures, thereby finding liquid volume fraction, and determining droplet movement as a function of time, thereby finding flow rate and velocity.
The invention also provides a method for control of a subsea located compressor fluidly connected to receive an inlet flow of gas through an inlet line, said flow may include liquid in an amount that may vary. The method comprises
The method preferably comprises the step:
The amount of liquid that a compressor can operate with depends on the droplet size. As large droplets have higher momentum than small droplets, they cause more damage. Field tests have shown that a compressor can operate with several percent of liquid content indefinitely as long as the droplet size is very small. This is indicated principally in
Normally there will be a range of droplet sizes present. From the sensor signals, droplet size statistics are collected for a number of droplets. The statistics are divided into size groups. The statistics are then further converted into momentum using the gas velocity, and for each group it is verified that the concentration does not exceed the allowed maximum limit from
Preferably, liquid is retained in a scrubber upstream of the sensor means, at excessive liquid level in the scrubber liquid is injected into the inlet line via an atomiser or injection mixer between the scrubber and sensor means, the liquid is drawn into the atomiser or injection mixer by the venturi effect. Preferably high pressure gas from the outlet side of the compressor, as delivered through a line from the compressor outlet line to the atomiser or injection mixer, preferably with a control valve in the line, is used to facilitate drawing in liquid. Pumping is preferably an additional, supplementary or replacing way of injecting liquid into the inlet flow to the compressor.
The invention also provides use of an optical dark field sensor for measuring and determining the liquid droplet size distribution and liquid volume fraction upstream of a subsea compressor. Preferably, the measurement results are used for control of the subsea compressor or control means or equipment upstream of the compressor.
The invention is illustrated by two figures, of which
Reference is made to
Further reference is made to
The system of the invention can be combined with features as described or illustrated in this document in any operative combination, which combinations are embodiments of the present invention. The method of the invention can be combined with features as described or illustrated in this document in any operative combination, which combinations are embodiments of the present invention. The use of the invention can be combined with features as described or illustrated in this document in any operative combination, which combinations are embodiments of the present invention.
Number | Date | Country | Kind |
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20093599 | Dec 2009 | NO | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/NO10/00477 | 12/20/2010 | WO | 00 | 6/21/2012 |