AU2005202147A1 - Compressor Diagnostic System - Google Patents

Compressor Diagnostic System Download PDF

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Publication number
AU2005202147A1
AU2005202147A1 AU2005202147A AU2005202147A AU2005202147A1 AU 2005202147 A1 AU2005202147 A1 AU 2005202147A1 AU 2005202147 A AU2005202147 A AU 2005202147A AU 2005202147 A AU2005202147 A AU 2005202147A AU 2005202147 A1 AU2005202147 A1 AU 2005202147A1
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Australia
Prior art keywords
logic circuitry
compressor
condition
sensor
demand signal
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AU2005202147A
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AU2005202147B2 (en
Inventor
Nagaraj Jayanth
Hank E. Millet
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Copeland LP
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Copeland Corp LLC
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Priority claimed from US09/818,271 external-priority patent/US6615594B2/en
Application filed by Copeland Corp LLC filed Critical Copeland Corp LLC
Priority to AU2005202147A priority Critical patent/AU2005202147B2/en
Publication of AU2005202147A1 publication Critical patent/AU2005202147A1/en
Assigned to EMERSON CLIMATE TECHNOLOGIES, INC. reassignment EMERSON CLIMATE TECHNOLOGIES, INC. Request for Assignment Assignors: COPELAND CORPORATION
Application granted granted Critical
Publication of AU2005202147B2 publication Critical patent/AU2005202147B2/en
Priority to AU2008201988A priority patent/AU2008201988B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Description

2 f 00 Regulation 3.2
AUSTRALIA
Patents Act 1990 COMPLETE SPECIFICATION FOR A STANDARD PATENT
(ORIGINAL)
Name of Applicant: Actual Inventors: Address for Service: Invention Title: COPELAND CORPORATION, of 1675 W. Campbell Road, Sidney, Ohio 45365-0669, United States of America JAYANTH, Nagaraj MILLET, Hank, E.
DAVIES COLLISON CAVE, Patent Attorneys, of 1 Nicholson Street, Melbourne 3000, Victoria, Australia Compressor Diagnostic System The following statement is a full description of this invention, including the best method of performing it known to us: Q:\oper\gcp\I 8844c div 3.doc 18/5/05 P:A0opgcp\1844 div3 t -1- 0 COMPRESSOR DIAGNOSTIC
SYSTEM
[0001] The present invention relates to a compressor system and a diagnostic method for a compressor. More particularly, the present invention may Sbe a compressor system for refrigeration or air-conditioning.
[0002] A class of machines exists in the art generally known as scroll machines which are used for the displacement of various types of fluid. These scroll machines can be configured as an expander, a displacement engine, a pump, a compressor, etc. and the features of the present invention are applicable to any of these machines. For purposes of illustration, however, the disclosed: embodiment is in the form of a hermetic refrigerant scroll compressor used within a refrigeration or air conditioning system.
[0003] Scroll compressors are becoming more and more popular for use as compressors in both refrigeration as well as air conditioning applications due primarily to their capability for extremely efficient operation. Generally, these machines incorporate a pair of intermeshed spiral wraps, one of which is caused to orbit relative to the other so as to define one or more moving chambers which progressively decrease in size as they travel from an outer suction port toward a centre discharge port. An electric motor is provided which operates to drive the orbiting scroll member via a suitable drive shaft affixed to the motor rotor. In a 00 hermetic compressor, the bottom of the hermetic shell normally contains an oil sump for lubricating and cooling purposes. While the diagnostic system of the present invention will be described in conjunction with a scroll compressor, it is to be understood that the diagnostic system of the present invention can be used with other types of compressors also.
S[0004] Traditionally, when an air conditioning or refrigeration system is not performing as designed, a technician is called to the site for trouble shooting the problem. The technician performs a series of checks that assists in isolating the problem with the system. One of the causes of the system's problem could be the compressor used in the system. A faulty compressor exhibits some operational patterns that could be used to detect the fact that the compressor is faulty. Unfortunately, many other causes for system problems can be attributed to other components in the system and these other causes can also affect the performance of the compressor and its operational pattern. It is possible to analyze the system's problems and operational patterns and determine that the compressor is faulty when in fact the problem lies elsewhere and the compressor is not the problem. This confusion of causes usually results in the replacement of a good compressor. This error in diagnosis is costly since the compressor is generally the most expensive component in the system. Further aggravating the problem is that the root cause for the system's problem has not solved and the problem recurs in time. Any tool which can help avoid the misdiagnosing of the system's problem as described above would prove both useful and cost effective.
t The present invention discloses a device that increases the accuracy of the 00 problem diagnrosis for an air conditioning or refrigeration system.
[0005] A large part of the compressors used in air conditioning and refrigeration systems have built-in protection devices called "internal line break N protectors". These protectors are thermally sensitive devices which are wired in electrical series with the motor. The protectors react thermally to the line current N drawn by the motor and also other temperatures within the compressor including but not limited to discharge gas temperature, suction gas temperature or temperature of a particular component in the compressor. When one of these temperatures exceeds a designed threshold, the protector will open the electrical connection to the motor. This shuts down the motor operating the compressor which in turn shuts down the compressor and prevents it from operating in regions that would lead to its failure. After a period of time, when the temperatures have fallen to safe levels, the protector automatically resets itself and the compressor operates again. The temperatures that the protector is reacting to are a result of the operation of the compressor and the entire system.
Either the operation of the compressor or the operation of the entire system can influence the temperatures sensed by these protectors. The significant aspect of the protection system is that some categories of faults repeatedly trip the protector with very short compressor ON time and other categories of faults trip the protector less frequently thus providing relatively longer compressor ON times. For example, a compressor with seized bearings would trip the protector within about ten seconds of ON time. On the other hand, a system that has a P:opafgcp\18844 div3 spe do-1805dO -4very low refrigerant charge will trip the protector after tens of minutes of ON time.
00 An analysis of the trip frequency, trip reset times and compressor ON times will provide valuable clues in identifying the cause of the system's problems.
[0005A] Accordingly, one aspect of the present invention provides a 5 system comprising: a compressor; Sa motor protector; Slogic circuitry signal operable to analyze a condition of the motor protector; and an intelligent device in communication with said logic circuitry and operable to indicate said condition.
[0005B] The invention also provides a method comprising: analyzing an operating condition of a motor protector associated with a compressor; identifying a compressor fault cause based on said step of analyzing; and communicating said fault cause to an intelligent device.
[0005C] The invention also provides a diagnostic system for a compressor assembly including a compressor and a motor protector, said system comprising logic circuitry associated with the motor protector and operable to analyze a status of the motor protector as a function of time and identify a specific fault cause.
[0006] The present invention provides in one embodiment a system which is based on the above principle. The system of the present embodiment may continuously record the status of the protector (open or closed) as a function of time and then it analyses this status information to determine a faulty situation.
The system goes further and isolates the fault to either the compressor or to the rest of the system. Once the fault has been isolated, the system will activate a visual indicator (light) and it will also send an electrical signal to any intelligent device (controller, computer, etc.) advising about the situation. The technician, on arriving at the scene, then has a clear indication that the problem is most likely in the system components other than the compressor or the problem is most likely in
I
P:\op&rgp\18844 div3 e.do-I8W5D the compressor. He can then focus his further trouble shooting to the identified 00 area. The device thus avoids the previously described situation of a confused diagnosis and the potential of mistakenly replacing a good compressor.
[0007] Further areas of applicability of the present invention will 5 become apparent from the detailed description provided hereinafter. It should be understood that the detailed description and specific examples, while indicating Sthe preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention.
[0008] The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein: [0009] Figure 1 is a vertical cross section of a hermetic scroll compressor incorporating the unique compressor diagnostic system; [0010] Figure 2 is a schematic representation of the diagnostic system for a single phase motor from the compressor; [0011] Figure 3 is a schematic representation of a diagnostic system for a three phase motor for the compressor; [0012] Figure 4 is a flow diagram of the diagnostic system for the single phase motor for the compressor; [0013] Figure 5 is a flow diagram of the diagnostic system for the three phase motor for the compressor; [0014] Figure 6 is a flow diagram which is followed when diagnosing a compressor system; [0015] Figure 7 is a schematic view of a typical refrigeration system utilizing the compressor and diagnostic system; [0016] Figure 8 is a perspective view of a contactor integrated with the diagnostic system's circuitry; [0017] Figure 9 is a schematic view illustrating the circuitry of the contactor illustrated in Figure 8; and [0018] Figure 10 is a schematic view of a compressor plug which illustrates the diagnostic system's circuitry.
P:Aoper"cp\I 8844 div3 spc.do-I18/05/O S-6- [0019] The following description of the preferred embodiment(s) is 00oo merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.
[0020] Referring now to the drawings in which like reference numerals designate like or corresponding parts throughout the several views, (-i o there is shown in Figure 1 a scroll compressor incorporating the unique (-i I compressor diagnostic system in accordance with one preferred embodiment of Sthe present invention and which is designated generally by the reference numeral While compressor 10 is being illustrated as a scroll compressor in conjunction with a refrigeration or air conditioning system, it is within the scope of the present invention to utilise other types of compressors in the refrigeration or air conditioning system if desired as well as having any of the compressor designs being in conjunction with other types of systems.
[0021] Scroll compressor 10 comprises a generally cylindrical hermetic 00oo shell 12 having welded at the upper end thereof a cap 14 and at the lower end thereof a base 16 having a plurality of mounting feet (not shown) integrally formed therewith. Cap 14 is provided with a refrigerant discharge fitting 18 which may have the usual discharge valve therein. A transversely extending partition is affixed to shell 12 by being welded about is periphery at the same point that c cap 14 is welded to shell 12. A compressor mounting frame 22 is press fit within shell 12 and it is supported by the end of base 16. Base 16 is slightly smaller in diameter than shell 12 such that base 16 is received within shell 12 and welded about its periphery as shown in Figure 1.
[0022] Major elements of compressor 10 that are affixed to frame 22 include a two-piece main bearing housing assembly 24, a lower bearing housing 26 and a motor stator 28. A drive shaft or crankshaft 30 having an eccentric crank pin 32 at the upper end thereof is rotatably journaled in a bearing 34 secured within main bearing housing assembly 24 and a second bearing 36 secured within lower bearing housing 26. Crankshaft 30 has at the lower end thereof a relatively large diameter concentric bore 38 which communicates with a radially outwardly positioned smaller diameter bore 40 extending upwardly therefrom to the top of crankshaft 30. The lower portion of the interior of shell 12 defines an oil sump 44 which is filled with lubricating oil to a level slightly above the lower end of a rotor, and bore 38 acts as a pump to pump lubricating fluid up crankshaft 30 and into bore 40 and ultimately to all of the various portions of compressor 10 which require lubrication.
A I t[0023] Crankshaft 30 is rotatably driven by an electric motor which oO includes stator 28, windings 46 passing therethrough and a rotor 48 press fitted into crankshaft 30. An upper counterweight 50 is secured to crankshaft 30 and a lower counterweight 52 is secured to rotor 48. A temperature protector 54, of the usual type, is provided in close proximity to motor windings 46. Thermal protector 54 will de-energize the motor if thermal protector 54 exceeds its normal C temperature range. Thermal protector 54 can be heated by motor windings 46, suction gas within a suction chamber 56 and/or discharge gas within a discharge chamber 58 which is released into suction chamber 56. Both suction chamber 56 and discharge chamber 58 are defined by shell 12, cap 14, base 16 and partition 22 as shown in Figure 1.
[0024] The upper surface of two-piece main bearing housing assembly 24 is provided with a flat thrust bearing surface on which is disposed an orbiting scroll member 60 having the usual spiral vane or wrap 62 extending.upward from an end plate 64. Projecting downwardly from the lower surface of end plate 64 of orbiting scroll member 60 is a cylindrical hub 66 having a journal bearing therein and which is rotatably disposed a drive bushing 68 having an inner bore in which crank pin 32 is drivingly disposed. Crank pin 32 has a flat on one surface which drivingly engages a flat surface formed in a portion of the inner bore of drive bushing 68 to provide a radially compliant driving arrangement, such as shown in Assignee's U.S. Letters Patent 4,877,382, the disclosure of which is hereby incorporated herein by reference. An Oldham coupling 70 is also provided positioned between orbiting scroll member 60 and two-piece bearing housing eassembly 24. Oldham coupling 70 is keyed to orbiting scroll member 60 and to a 0 non-orbiting scroll member 72 to prevent rotational movement of orbiting scroll member [0025] Non-orbiting scroll member 72 is also provided with a wrap 74 extending downwardly from an end plate 76 which is positioned in meshing engagement with wrap 62 of orbiting scroll member 60. Non-orbiting scroll N member 72 has a centrally disposed discharge passage 78 which communicates with an upwardly open recess 80 which is in turn in communication with discharge chamber 58. An annular recess 82 is also formed in non-orbiting scroll member 72 within which is disposed a floating seal assembly 84.
[0026] Recesses 80 and 82 and floating seal assembly 84 cooperate to define axial pressure biasing chambers which receive pressurized fluid being compressed by wraps 62 and 74 so as to exert an axial biasing force on nonorbiting scroll member 72 to thereby urge the tips of respective wraps 62 and 74 into sealing engagement with the opposed end surfaces of end plates 76 and 64, respectively. Floating seal assembly is preferably of the type described in greater detail in Assignee's U.S. Letters Patent 5,156,639, the disclosure of which is hereby incorporated herein by reference. Non-orbiting scroll member 72 is designed to be mounted for limited axial movement with respect to two-piece main bearing housing assembly 24 in a suitable manner such as disclosed in the aforementioned U.S. Letters Patent 4,877,382 or Assignee's U.S. Letters Patent 5,102,316, the disclosure of which is hereby incorporated herein by reference.
t[0027] Compressor 10 is powered by electricity which is provided to the oo electric motor within shell 12 through a molded electric plug [0028] Referring now to Figures 1 through 3, the present cembodiment is directed to a unique compressor diagnostic system 100.
SDiagnostic system 100 comprises one or more current sensing devices 102 and c- the associated logic circuitry 104. Current sensing devices 102 are mounted in a housing 106 mounted externally to shell 12. Logic circuitry 104 can be mounted in housing 106 or it can be located in a convenient position with respect to compressor 10 as shown in phantom in Figure 2. Optionally, the sensing device and circuitry can be integrated into a special contactor, a special wiring harness or into a molded plug utilized for some compressor designs.
[0029] Current sensing devices 102 sense the current in the power supply wires powering compressor 10. Figure 2 illustrates two current sensing devices 102 in conjunction with a single-phase motor. One of the current sensing devices 102 is associated with the main windings for the compressor motor and the other current sensing device 102 is associated with the auxiliary windings for the compressor motor. Figure 3 also illustrates two current sensing devices 102 in conjunction with a three phase motor. Each current sensing device 102 is associated with one of the phases of the three phase power supply.
While Figure 3 illustrates two current sensing devices sensing current in two phases of the three phase power supply, it is within the scope of the present invention to include a third current sensor 102 to sense the current in the third phase of the three phase power supply as shown in phantom in Figure 3 if tdesired. These current signals represent an indication of the status of protector 0 54 (open or closed). While current sensing devices 102 sense the status of protector 54 utilizing the current in the power supply wires, it is also possible to sense the status of protector 54 by sensing the presence or absence of voltage on the motor side of protector 54. The inventors of the present invention consider this to be a less desirable but effective approach in some cases CI because it requires an additional hermetic feed-through pin extending through shell 12. The signals received from current sensing devices 102 are combined in logic circuitry 104 with the demand signal for compressor 10. The demand signal for compressor 10 is acquired by sensing the presence of supply voltage or by having a system controller (not shown) supply a discrete signal representing the demand. The demand signal and the signal received by logic circuitry 104 are processed by logic circuitry 104 to derive the information about the trip frequency of protector 54 and the average ON time and OFF time of compresspr 10. Logic circuitry 104 analyses the combination of current signals, the demand signal and the derived protector trip frequencies to determine if a fault condition exists.
Logic circuitry also has the unique capability of identifying a specific cause based on some faults. This information is provided to the service people using a green LED light 110 and a yellow LED light 112. Green LED light 110 is utilized to indicate that there is currently no fault condition and that the system is functioning normally.
[0030] Yellow LED light 112 is utilized to indicate the presence of a fault. When yellow LED light 112 is turned ON, green LED light 110 is turned tOFF. Thus, yellow LED light 112 is utilized to visually communicate that there is o00 a fault as well as indicating the type of fault that is present. This communication is accomplished by turning yellow LED light 112 ON and then OFF for a specific duration and sequence to indicate both that there is a fault and to identify what the fault is. For example, turning light 112 ON for one second and turning it OFF for nineteen seconds and repeating this sequence every twenty seconds will Screate the effect of a blinking light that blinks ON once every twenty seconds.
This sequence corresponds to a type of fault that is coded as a type 1 fault. If light 112 is blinked ON twice for one second during the twenty second window, it is an indication that a fault that is coded as a type 2 is present. This sequence continues to indicate a type 3, a type 4 and so on with the type of fault being indicated by the number of blinks of light 112. This scheme of the blinking of light 112 for a specific number of times is employed to visually communicate to the technician the various types of faults detected by logic circuitry 104. While the present embodiment utilizes blinking light 112 to convey the fault codes, it is within the scope of the present invention to utilize a plurality of lights to increase the effectiveness of conveying a large number of fault codes if desired. In addition, other methods of providing the default code, including providing a coded voltage output that can be interfaced with a Digital Volt Meter, can also be employed.
[0031] In addition to visually communicating the specific fault code using light 112, logic circuitry 104 also outputs a coded sequence of electrical pulses to other intelligent controllers that may exist in the system. These coded pulses represent the type of fault that has been detected by diagnostic system t100. The types of faults which can be detected by logic circuitry 104 include, but oO are not limited to: 1. Protector has "tripped".
2. The auxiliary winding of a single phase motor has no power or is open or has a faulty run capacitor.
O 3. The main winding of a single phase motor has no power or that the Swinding is open.
4. The main circuit breaker has contacts that have welded shut.
One of the phases in a 3 phase circuit is missing.
6. The phase sequence in a 3 phase system is reversed.
7. The supply voltage is very low.
8. The rotor inside the compressor has seized.
9. The protector is tripping due to system refrigeration circuit problems.
The motor windings are open or the internal line break protector is faulty.
[0032] As a variation to the above, as shown in Figure 3, diagnostic system 100 may only send the status of protector 54 to an intelligent device 116.
In this option, the parameters of trip frequencies, ON times and OFF times with the diagnosis information may be generated at intelligent device 116. Intelligent device 116 can be a compressor controller associated with compressor 10, it can be a system controller monitoring a plurality of compressors 10, it can be a remotely located device or it can be any other device which is selected to monitor diagnostic system 100 of one or more compressors.
[0033] Figure 4 represents a flow diagram for diagnostic system 100 in conjunction with a single phase compressor. The demand signal is provided to logic circuitry 104 from a device or a contactor 120 (Figures 2 and 3) along with the current signal from sensing devices 102. When the system is initially 00powered up, an initializing process is performed at 122 and, if successful, the system, as shown by arrow 124, goes to a normal OFF condition as shown at 126. When sitting at the normal OFF condition 126, if a demand signal is provided to the system, the system moves as shown by arrow 128 to a normal A run condition shown at 130. Once the demand has been met, the system returns C to the normal OFF condition 126 as shown by arrow 132.
[0034] While sitting at the normal OFF condition 126, if current in the main winding or current in the auxiliary winding is detected and there has been no demand signal, the system moves as shown by arrow 134 to a shorted contactor condition 136. While indicating the shortened contactor condition 136, if the demand is signaled, the system moves as shown by arrow 138 to the normal run condition 130. The normal run condition 130 continues until the demand has been satisfied where the system moves as shown by arrow 132 back to the normal OFF condition 126 which may again move to the shortened contactor condition 136 depending on whether or not current is sensed in the main or auxiliary windings.
[0035] While operating in the normal run condition 130, one of three paths other than returning to the normal OFF condition 126 can be followed.
First, if the system senses demand and main winding current but does not sense auxiliary winding current, the system moves as shown by arrow 140 to an open auxiliary circuit condition 142. From here, the system moves to a protector tripped condition 144 as shown by arrow 146 when both a main winding current and an auxiliary winding current are not sensed. Second, if the system senses 00 demand and auxiliary winding current but does not sense main winding current, the system moves as shown by arrow 148 to an open main circuit condition 150.
From here, the system moves to the protector tripped condition 144 as shown by arrow 152 when both a main winding current and an auxiliary winding current are not sensed. Third, if the system senses demand and does not sense auxiliary N winding current and main winding current, the system moves as shown by arrow 154 to the protector tripped condition 144.
[0036] While operating in the protector tripped condition 144, one of four paths can be followed. First, if main winding current or auxiliary winding current is sensed and the demand is satisfied, the system moves as shown by arrow 160 to the normal run condition 130. Second, with the protector tripped, and the moving window average of the ON time of the system has been less than twelve seconds, the system moves as shown by arrow 162 to a multiple short run condition 164. From the multiple short run condition, the system moves back to the protector tripped condition 144 as shown by arrow 166. Third, with the protector tripped, and the moving window average of the ON time of the system has been greater than fifteen minutes, the system moves as shown by arrow 168 to a multiple long run condition 170. The system moves back to the protector tripped condition 144 as shown by arrow 172. Fourth, with the protector tripped, if the tripped time exceeds four hours, the system moves as shown by arrow 174 to a power loss or protector defective condition 176. If, while the system is in the power loss or protector defective condition 176 and main winding current or auxiliary winding current is sensed, the system moves back to the protector 00oO tripped condition 144 as shown by arrow 178.
[0037] When the system moves to the various positions shown in Figure 4, the blinking of light 112 is dictated by the fault condition sensed. In the preferred embodiment, if a protector tripped condition is sensed at 154 because I' demand is present but current is missing, light 112 blinks once. If compressor N is seized or there is a low supply voltage problem such as indicated by arrow 162 because the average ON time during the last five trips was less than twelve seconds, light 112 blinks twice. If the motor windings are open, the protector is faulty or the contactor is faulty as indicated by arrow 174 because the OFF time is greater than four hours, light 112 blinks three times. If the auxiliary windings are open or there is a faulty run capacitor as indicated by arrow 140, light 112 blinks four times. If the main winding is open as indicated by arrow 148, light 112 blinks five times. If the contactor is welded as indicated by arrow 134 because current is sensed but there is no demand, light 112 blinks six times. Finally, if there are repeated protector trips due to other system problems as indicated by arrow 168 because the average ON time during the last five trips was less than fifteen minutes, light 112 blinks seven times.
[0038] Figure 5 represents a flow diagram for diagnostic system 100 in conjunction with a three phase compressor. The demand signal is provided to logic circuitry 104 from contactor 120 (Figures 2 and 3) along with the current signal from sensing devices 102. When the system is initially powered up, an initializing process is performed at 122 and, if successful, the system, as shown tby arrow 124, goes to a normal OFF condition as shown at 126. When sitting at 00 the normal OFF condition 126, if a demand signal is provided to the system, the system moves as shown by arrow 128 to a normal run condition shown at 130.
Once the demand has been met, the system returns to the normal OFF condition 126 as shown by arrow 132.
[0039] While sitting at the normal OFF condition 126, if current in one (N of the three phases or current in a second of the three phases is detected and there has been no demand signal the system moves as shown by arrow 234 to a shorted contactor condition 136. While indicating the shortened contactor condition 136, if the demand is signaled, the system moves as shown by arrow 238 to the normal run condition 130. The normal run condition 130 continues until the demand has been satisfied where the system moves as shown by arrow 132 back to the normal OFF condition 126 which may again move to the shortened contactor condition 136 depending on whether or not current is sensed in the main or auxiliary windings.
[0040] While operating in the normal run condition 130, one of three paths other than returning to the normal OFF condition 126 can be followed.
First, if the system senses demand and eleven milliseconds is less than the zero crossing time difference between the first and second phases of the three phase power supply or this time difference is less than fourteen milliseconds, the system moves as shown by arrow 240 to a phase sequence reversed condition 242. From here, the system moves to a protector tripped condition 144 as shown by arrow 246 when both a first phase current or a second phase current is not sensed. Second, if the system senses demand and sixteen milliseconds is less 00 than the zero crossing time difference between the first and second phases or this time difference is less than twenty-one milliseconds, the system moves as shown by arrow 248 to a phase missing condition 250. From here, the system 0 moves to the protector tripped condition 144 as shown by arrow 252 when both a C first phase current and a second phase current are not sensed. Third, if the system senses demand and does not sense first phase current and second phase current, the system moves as shown by arrow 254 to the protector tripped condition 144.
[0041] While operating in the protector tripped condition 144, one of four paths can be followed. First, if first phase current or second phase current is sensed and the demand is satisfied, the system moves as shown by arrow 260 to the normal run condition 130. Second, with the protector tripped, and the moving window average of the ON time of the system has been less,.than twelve seconds, the system moves as shown by arrow 162 to a multiple short run condition 164. From the multiple short run condition, the system moves back to the protector tripped condition 144 as shown by arrow 166. Third, with the protector tripped, and the moving window average of the ON time of the system has been greater than fifteen minutes, the system moves as shown by arrow 168 to a multiple long run condition 170. The system moves back to the protector tripped condition 144 as shown by arrow 172. Fourth, with the protector tripped, if the tripped time exceeds four hours, the system moves as shown by arrow 174 to a power loss or protector defective condition 176. If, while the system is in the power loss or protector defective condition 176 and first phase current or second 00 phase current is sensed, the system moves back to the protector tripped condition 144 as shown by arrow 278.
[0042] When the system moves to the various positions shown in C Figure 5, the blinking of light 112 is dictated by the fault condition sensed. In the preferred embodiment, if a protector tripped condition is sensed at 254 because Sdemand is present but current is missing, light 112 blinks once. If compressor is seized or there is a low supply voltage problem such as indicated by arrow 162 because the average ON time during the last five trips was less than twelve seconds, light 112 blinks twice. If the motor windings are open, the protector is faulty or the contactor is faulty as indicated by arrow 174 because the OFF time is greater than four hours, light 112 blinks three times. If the contactor is welded as indicated by arrow 234 because current is sensed but there is no demand, light 112 blinks four times. If there are repeated protector trips due to other system problems as indicated by arrow 168 because the average ON time during the last five trips was less than fifteen minutes, light 112 blinks five times. If the power supply phases are reversed as indicated by arrow 240 because the zero crossing time difference is between eleven and fourteen milliseconds, light 112 blinks six times. Finally, if there is a phase missing in the three phase power supply as indicated by arrow 248 because the zero crossing time difference is between sixteen and twenty-one milliseconds, light 112 blinks seven times.
[0043] While the above technique has been described as monitoring the moving window averages for compressor 10, it is within the scope of the 1 L it present invention to have logic circuitry 104 utilize a real time or the o00 instantaneous conditions for compressor 10. For instance, in looking at arrows 162 or 168, rather than looking at the moving window average, logic circuitry 104 could look at the previous run time for compressor [0044] Figure 6 represents a flow diagram which is followed when diagnosing a system problem. At step 300, the technician determines if there is Sa problem by checking the LEDs at step 302. If green LED 110 is lit, the indication at 304 is that compressor 10 is functioning normally and the problem is with other components. If yellow LED light 112 is blinking, the technician counts the number of blinks at 306. Based upon the number of blinks of light 112 the determination of the failure type is made at 308. The fault is corrected and the system is recycled and started at 310. The system returns to step 300 which again will indicate any faults with compressor [0045] Thus, diagnostic system 100 provides the technician who arrives at the scene with a clear indication of most likely where the problem with the system is present. The technician can then direct his attention to the most likely cause of the problem and possibly avoid the replacement of a good compressor.
[0046] Figure 7 illustrates a typical refrigeration system 320.
Refrigeration system 320 includes compressor 10 in communication with a condensor 322 which is in communication with an expansion device 324 which is in communication with an evaporator 326 which is in communication with I tcompressor 10. Refrigerant tubing 328 connects the various components as 00 shown in Figure 7.
[0047] Referring now to Figure 8, a contactor 120 is illustrated which incorporates diagnostic system 100 in the form of current sensors 102, logic 0 circuitry 104, green LED light 110 and yellow light 112. Contactor 120 is (i~r designed to receive information from various system controls such as a system c thermostat 350 (Figures 2 and a group of system safeties 352 (Figures 2 and 3) and/or other sensors incorporated into the system and based upon three inputs provide power to compressor [0048] Contactor 120 includes a set of power-in connectors 354, a set of power-out connectors 356, a set of contactor coil connectors 358, light 110 and light 112. The internal schematic for contactor 120 is shown in Figure 9. A power supply 360 receives power from connectors 354, converts the input power as needed and then supplies the required power to input circuitry 362, processing circuitry 364 and output circuitry 366, which collectively form logic circuitry 104.
[0049] Input circuitry 362 receives the input from current sensors 102 and the demand signal in order to diagnose the health of compressor 10. The information received by input circuitry 362 is directed to processing circuitry 364 which analyses the information provided and then provides information to output circuitry 366 to operate compressor 10 and/or activate LED lights 110 and 112.
The incorporation of logic circuitry 104 into contactor 120 simplifies the system due to the fact that both the line power and the demand signal are already P:\opaocp\18844 div3 sp.doc-8I/05) -22c-I provided to contactor 120. The function and operation of diagnostic system 100 0_ incorporated into contactor 120 is the same as described above for housing 106.
[0050] Referring now to Figure 10, molded plug 90 is illustrated incorporating diagnostic system 100 in the form of current sensors 102, logic circuitry 104, light 110 and light 112. In some applications, incorporation of Sdiagnostic system 100 into molded plug 90 offers some distinct advantages.
SWhen diagnostic system 100 is incorporated into molded plug 90, power is (-i provided through connectors 354 and must also be provided to diagnostic system from the input power or it can be provided separately through connector 370. In addition, the demand signal must also be provided to plug 90 and this can be done through connectors 372. The function and operation of diagnostic system 100 incorporated into molded plug 90 is the same as described above for housing 106..
Communication from plug 90 is accomplished through connection 374.
[0051] The description of the invention is merely exemplary in nature and thus variations that do not depart from the gist of the invention are intended to be within the scope of the invention. Such variations are not to be regarded as a departure from the spirit and scope of the invention.
[0052] Throughout this specification and the claims which follow, unless the context requires otherwise, the word "comprise", and variations such as "comprises" and "comprising", will be understood to imply the inclusion of a stated integer or step or group of integers or steps but not the exclusion of any other integer or step or group of integers or steps.
[0053] The reference to any prior art in this specification is not, and should not be taken as, an acknowledgment or any form of suggestion that that prior art forms part of the common general knowledge in Australia.

Claims (34)

1. A system comprising: a compressor; a motor protector; logic circuitry signal operable to analyze a condition of the motor protector; (-i Sand San intelligent device in communication with said logic circuitry and operable (-i to indicate said condition.
2. The system according to claim 1, wherein said logic circuitry analyzes said condition and said intelligent device indicates a specific fault cause.
3. The system according to claim 1, wherein said logic circuitry determines the trip frequency of the motor protector.
4. The system according to claim 1, wherein the logic circuitry determines the average ON time of the compressor.
5. The system according to claim 1, wherein said intelligent device is operable to visually communicate said specific fault cause.
6. The system according to claim 1, wherein said logic circuitry is operable to output to said intelligent device a coded sequence of electrical pulses to identify said specific fault cause.
7. The system according to claim 1, further comprising a demand signal sensor associated with said logic circuitry.
8. The system according to claim 7, wherein said demand signal sensor monitors a supply voltage. P:oprffcp\18844 div3 spe.doe-18/05 O-24
9. The system according to claim 7, wherein said demand signal sensor is in oo communication with a system controller supplying a signal indicating demand.
The system according to claim 7, further comprising a current sensor associated with said logic circuitry.
11. The system according to claim 10, wherein said logic circuitry receives an 0output of said current sensor, an output of said demand sensor and derives a motor protector trip frequency from said received current and demand signal.
12. The diagnostic system according to claim 10, wherein said current sensor includes a main winding current sensor and an auxiliary winding current sensor, said logic circuitry communicating said condition based on input received from said demand signal sensor, main winding current sensor and auxiliary winding current sensor.
13. The system according to claim 12, wherein said logic circuitry is operable in a normal run condition, said logic circuitry moving the protector to a tripped condition in the absence of a signal from both said main winding current sensor and said auxiliary winding current sensor.
14. The system according to claim 12, wherein said logic circuitry is operable in a protector trip condition, said logic outputting a normal run condition signal when receiving output from at least one of said main winding current sensor and said auxiliary winding current sensor and output from said demand sensor is acceptable. The system according to claim 12, wherein said logic circuitry derives a motor protector trip frequency from said input received from said demand signal sensor and at least one of said main and auxiliary winding current sensors.
P:korgp\18844 div3 pc.do-I8d505
16. The system according to claim 12, wherein said intelligent device is 00 operable to indicate a fault based on input received by said logic circuitry from at least one of said demand signal sensor, main winding current sensor, and auxiliary winding current sensor. C
17. The system according to claim 16, wherein said intelligent device is I operable to indicate a specific fault cause.
18. A method comprising: analyzing an operating condition of a motor protector associated with a compressor; identifying a compressor fault cause based on said step of analyzing; and communicating said fault cause to an intelligent device.
19. The method according to claim 18, wherein said operating condition includes a trip frequency of the motor protector.
The method according to claim 18, further comprising determining an average ON time of the compressor.
21. The method according to claim 18, further comprising sensing a demand signal and a current and deriving a motor protector trip frequency from said sensed current and demand signal.
22. The method according to claim 21, wherein said identifying a compressor fault cause includes indicating a specific fault cause based on said sensed current and demand signal.
23. The system according to claim 18, wherein said communicating includes outputting a coded sequence of electrical pulses to identify a specific fault cause. P:Apergcp\18844 div3 .d€-18/05 O -26
24. A diagnostic system for a compressor assembly including a compressor 00 and a motor protector, said system comprising logic circuitry associated with the motor protector and operable to analyze a status of the motor protector as a t function of time and identify a specific fault cause.
The diagnostic system of claim 24, further comprising a demand signal Ssensor, wherein said logic circuitry is associated with said demand signal sensor.
26. The diagnostic system of claim 25, further comprising a current sensor, wherein said logic circuitry is associated with said current sensor.
27. The diagnostic system according to claim 25, wherein said demand signal sensor monitors a supply voltage.
28. The diagnostic system according to claim 25, wherein said demand signal sensor is in communication with a system controller supplying a signal indicating demand.
29. The diagnostic system according to claim 24, further comprising an indicator associated with said logic circuitry, said indicator receiving a signal from said logic circuitry to indicate a fault based on said current and demand signal.
The diagnostic system according to claim 29, wherein said indicator is a plurality of lights indicating the presence or absence of a fault condition.
31. The diagnostic system according to claim 24, wherein said logic circuitry is operable to output a coded sequence of electrical pulses to identify said specific fault cause. I P:oper\gcp\8844 div3 spe.doc-I 8l5/5 O -27-
32. The diagnostic system according to claim 24, wherein said logic circuitry is 00 operable to analyze said operating condition and identify a specific fault cause while the compressor is operating.
33. A system substantially as hereinbefore described with reference to the 0accompanying drawings. (N
34. A method substantially as hereinbefore described with reference to the accompanying drawings. A diagnostic system for a compressor assembly substantially as hereinbefore described with reference to the accompanying drawings. DATED this 18th day of May, 2005 COPELAND CORPORATION By its Patent Attorneys DAVIES COLLISON CAVE
AU2005202147A 2001-03-27 2005-05-18 Compressor Diagnostic System Ceased AU2005202147B2 (en)

Priority Applications (2)

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AU2005202147A AU2005202147B2 (en) 2001-03-27 2005-05-18 Compressor Diagnostic System
AU2008201988A AU2008201988B2 (en) 2001-03-27 2008-05-06 Compressor Diagnostic Method

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US09/818,271 US6615594B2 (en) 2001-03-27 2001-03-27 Compressor diagnostic system
US09/818271 2001-03-27
AU18844/02A AU783666B2 (en) 2001-03-27 2002-03-01 Compressor diagnostic system
AU2005202147A AU2005202147B2 (en) 2001-03-27 2005-05-18 Compressor Diagnostic System

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Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4387368A (en) * 1980-12-03 1983-06-07 Borg-Warner Corporation Telemetry system for centrifugal water chilling systems
US5454229A (en) * 1994-05-18 1995-10-03 Thermo King Corporation Refrigeration unit control with shutdown evaluation and automatic restart
US6453687B2 (en) * 2000-01-07 2002-09-24 Robertshaw Controls Company Refrigeration monitor unit

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