Apparatus for detecting a flammable atmosphere within a compressor, in particular a vacuum pump
Apparatus for detecting a flammable atmosphere within a compressor during operation thereof is provided. The apparatus comprising a test chamber which is selectably connected between the compressor and an exhaust duct of the compressor using isolation device; an ignition device which is located within the test chamber for igniting any flammable fluid mixture present therein; and sensor associated with the test chamber for monitoring a parameter indicative of combustion within the test chamber and for outputting a signal indicative of the parameter to a controller.
1. Apparatus for detecting a flammable atmosphere within a compressor during operation thereof, the apparatus comprising:
a test chamber for receiving fluid, wherein the test chamber is connected to a bypass line between the compressor and an exhaust duct of the compressor or connected to a port of the compressor located between an inlet of the compressor and the exhaust duct of the compressor
isolation means for isolating the fluid received by the test chamber
an ignition device located within the test chamber, for igniting the isolated fluid; and
sensing means associated with the test chamber for monitoring a parameter indicative of combustion therein.
2. Apparatus according to claim 1 wherein the isolation means comprise valve means.
3. Apparatus according to claim 2 wherein the valve means comprise a pair of positive action valves, one located at an inlet of the test chamber and the second located at an outlet of the test chamber.
4. Apparatus according to claim 3 wherein the positive action valves are provided by ball valves.
5. Apparatus according to claim 1 wherein at least part of the isolation means is integral with the test chamber and comprises a rotating unit having a first position for enabling fluid communication through the test chamber, and a second position for isolating the test chamber from the exhaust duct and the compressor.
6. Apparatus according to claim 1 wherein the ignition device is provided by a glow plug.
7. Apparatus according to claim 1 wherein the ignition device is provided by a high energy ignition source.
8. Apparatus according to claim 7 wherein the ignition source is configured to deliver a spark having energy in the range of 0.15 Joules to 100 Joules.
9. Apparatus according to claim 8 wherein the ignition source is configured to deliver a spark having energy in the range of 1 Joules to 20 Joules.
10. Apparatus according to claim 9 wherein the ignition source is configured to deliver a spark having about 10 Joules of energy.
11. Apparatus according to claim 7 wherein the ignition source is configured to deliver a spark for a duration in the range of 1 μs to 10 seconds.
12. Apparatus according to claim 11 wherein the ignition source is configured to deliver a spark for a duration in the range of 1 ms to 3 ms.
13. Apparatus according to claim 1 comprising control means for controlling activation of the ignition device.
14. Apparatus according to claim 1 wherein the ignition device is configured to be activated at predetermined time intervals.
15. Apparatus according to claim 1 wherein the ignition device is configured to be repeatedly activated.
16. Apparatus according to claim 1 wherein the sensing means comprises a pressure sensor located within or in fluid communication with the test chamber.
17. Apparatus according to claim 1 wherein the sensing means comprises at least one of an ionisation sensor, a thermal sensor and an oxygen sensor located within or in fluid communication with the test chamber.
18. Apparatus according to claim 16 wherein the sensing means comprises a reference sensor located within or in fluid communication with either the exhaust duct of the compressor or said port of the compressor, for monitoring a reference parameter comparable to said parameter indicative of combustion in the test chamber.
19. Apparatus for inhibiting an escalation of a flammable atmosphere within a compressor during operation thereof, comprising:
a test chamber for receiving fluid, wherein the test chamber is connected to a bypass line between the compressor and an exhaust duct of the compressor
isolation means for isolating the fluid received by the test chamber from the compressor, and the exhaust duct
an ignition device located within the test chamber, for igniting the isolated fluid; and
sensing means associated with the test chamber for monitoring a parameter indicative of combustion therein; and
a controller for receiving one or more signals from the sensing means and for controlling an inhibition means, wherein the inhibition means inhibits escalation of any flammable atmosphere within the compressor.
20. Apparatus according to claim 19 wherein the inhibition means comprises a gas purge system for delivering a purge gas to the compressor upon detection of a flammable atmosphere.
21. Apparatus according to claim 20 wherein a quantity or duration of the purge gas delivery is dependent upon an increase in the monitored parameter, a duration of an increase in the monitored parameter or the number of times a flammable atmosphere is detected.
22. Apparatus according to claim 19 wherein the inhibition means is configured to isolate and/or terminate operation of the compressor.
23. Apparatus according to claim 1 wherein the compressor is a vacuum pump.
24. A pumping arrangement comprising:
a vacuum pump; and
apparatus for inhibiting the escalation of a flammable atmosphere within the vacuum pump comprising:
a test chamber for receiving fluid, wherein the test chamber is connected to a bypass line between the vacuum pump and an exhaust duct of the vacuum pump
a valve for isolating from the vacuum pump and the exhaust duct fluid received by the test chamber;
an ignition device located within the test chamber, for igniting the isolated fluid; and
a sensor associated with the test chamber for monitoring a parameter indicative of combustion therein; and
a controller for receiving one or more signals from the sensing means and for controlling an inhibition means, wherein the inhibition means inhibits escalation of any flammable atmosphere within the compressor.
25. The pumping arrangement according to claim 24 , wherein the exhaust duct and/or the test chamber comprise heating means for inhibiting condensation of a fluid contained therein.
26. A method of detecting a flammable atmosphere within a compressor during operation thereof comprising the following steps:
diverting a sample of fluid from the compressor via a bypass line connecting the compressor and an exhaust duct of the compressor, wherein the bypass line is connected to a test chamber
isolating the sample of fluid received by the test chamber from the compressor and the exhaust duct;
activating an ignition device within the test chamber; and
monitoring a parameter within the test chamber.
27. The method according to claim 26 wherein the diverting step comprises opening isolating means to enable the sample of fluid to pass into the test chamber and the isolating step comprises closing the isolating means to prevent further passage of fluid therethrough.
28. The method according to claim 26 wherein the activating step comprises repeatedly activating the ignition device to inhibit an accumulation of deposits inside the test chamber.
29. The method according to claim 26 wherein the monitored parameter is pressure.
30. The method according to claim 26 comprising the steps of:
outputting a signal indicative of the monitored parameter from a sensor to a controller; and
determining whether combustion occurs within the test chamber in dependence on the monitored parameter.
31. The method of claim 26 comprising:
providing a signal to an inhibition means for inhibiting escalation of the flammable atmosphere.
32. The method according to claim 31 wherein the inhibition means is provided by a purge system, the method comprising the step of delivering purge gas to the compressor to dilute the fluid located therein.
33. The method according to claim 26 wherein the ignition device is activated for a first period of time to ignite fluid within the chamber, and is periodically cleaned by activation for a second period of time longer than the first period of time.
34. The method according to claim 33 wherein the first period of time is in the range of 1 μs to 10 seconds.
35. The method according to claim 34 wherein the first period of time is in the range of 1 ms to 3 ms.
36. The method according to claim 33 wherein the second period of time is in the range of 5 seconds to 10 minutes.
37. The method according to claim 36 wherein the second period of time is in the range of 30 seconds to 2 minutes.