COMPRESSOR CONTROL SYSTEMS AND AIR COMPRESSOR SYSTEMS AND VEHICLES EQUIPPED THEREWITH

Abstract

Compressor control systems capable of increasing the reliability and uptime of air compressor systems that operate in harsh corrosive outdoor environments by redundantly sensing one or more operating parameters of the air compressor systems. Such a compressor control system includes a controller adapted to monitor at least a first operating parameter of a component of the air compressor system, at least first and second sensors that are physically separate and spaced apart from each other and that redundantly sense the first operating parameter of a component of the air compressor system, and separate and independent wiring harnesses electrically connecting the first and second sensors to the controller.

Claims

1. A compressor control system of an air compressor system, the compressor control system comprising: a controller adapted to monitor at least a first operating parameter of a component of the air compressor system; at least first and second sensors that are physically separate and spaced apart from each other and redundantly sense the first operating parameter of the component; and separate and independent wiring harnesses electrically connecting the first and second sensors to the controller.

2. The compressor control system of claim 1, wherein the first and second sensors are each mounted to the component at separate locations on the component.

3. The compressor control system of claim 1, wherein the first and second sensors are enclosed in a weather-resistant enclosure that isolates the first and second sensors from moisture and is located remotely from the component.

4. The compressor control system of claim 3, wherein the first and second sensors are both fluidically connected to the component by a first conduit, and the first operating parameter is transmitted with a fluid within through the first conduit from the component to each of first and second sensors.

5. The compressor control system of claim 4, wherein the first conduit draws the fluid from a single location of the component.

6. The compressor control system of claim 4, wherein the first and second sensors are mounted in a manifold within the enclosure, the first conduit fluidically connects the manifold to the component, and the fluid flows from the component through the first conduit and then through the manifold to each of first and second sensors.

7. The compressor control system of claim 5, wherein the first operating parameter is temperature or pressure of the fluid.

8. The compressor control system of claim 3, further comprising at least a third sensor enclosed in the enclosure, the third sensor being fluidically connected to the component by a second conduit that is separate from the first conduit, the fluid flows from a location of the component that is different from a location from which the fluid is drawn to the first and second sensors, and the third sensor is adapted to monitor a second operating parameter of the component that is transmitted with the fluid flowing through the second conduit from the component to the third sensor.

9. The compressor control system of claim 8, wherein the first, second, and third sensors are mounted in a manifold within the enclosure, the first and second conduits fluidically connect the manifold to the component, and the fluid transmits the first and second operating parameters from the component through the first and second conduits and then through the manifold to each of first, second, and third sensors.

10. The compressor control system of claim 9, wherein the component is an air/oil separator tank of the air compressor system.

11. The compressor control system of claim 10, further comprising a third conduit through which the fluid flows from the manifold back to a compressor of the air compressor system.

12. The compressor control system of claim 9, further comprising a third conduit through which the fluid flows from the manifold back to the air compressor system.

13. The compressor control system of claim 8, wherein the first and second sensors are temperature sensors and the first operating parameter is oil temperature of the component.

14. The compressor control system of claim 13, wherein the third sensor is a pressure sensor and the second operating parameter is oil pressure of the component.

15. The compressor control system of claim 8, wherein the first and second sensors are pressure sensors and the first operating parameter is oil pressure of the component.

16. The compressor control system of claim 15, wherein the third sensor is a temperature sensor and the second operating parameter is oil temperature of the component.

17. The compressor control system of claim 1, wherein the air compressor system is a portable air compressor system.

18. The compressor control system of claim 1, wherein the air compressor system is a vehicle-mounted air compressor system.

19. A vehicle on which the compressor control system and the vehicle-mounted air compressor system of claim 18 are mounted.

20. The vehicle of claim 19, wherein the vehicle is a utility vehicle, a maintenance vehicle, a construction vehicle, a repair vehicle, a pipeline vehicle, or a military vehicle.

21. The compressor control system of claim 1, wherein the air compressor system comprises an air compressor directly driven by an engine, a transmission, a driveline gearbox, or a power takeoff of a vehicle or an auxiliary engine, or indirectly driven by a vehicle engine or an auxiliary engine through an auxiliary belt drive or hydraulic power system.

22. The compressor control system of claim 1, wherein the air compressor system is driven by an electric motor used in an industrial or commercial application.

23. The air compressor system comprising the compressor control system of claim 1.

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING

[0014] FIG. 1 schematically represents an air compressor system equipped with a compressor control system in accordance with a first nonlimiting embodiment of this invention.

[0015] FIG. 2 is a diagram of an air compressor system equipped with a compressor control system in accordance with a second nonlimiting embodiment of this invention.

DETAILED DESCRIPTION OF THE INVENTION

[0016] FIGS. 1 and 2 represent air compressor systems equipped with different compressor control systems that are capable of increasing the reliability and uptime of the air compressor systems by increasing the reliability of sensors that sense operating parameters of the air compressor systems, particularly but not limited to portable compressors and vehicle-mounted compressors operated in harsh corrosive outdoor environments. Notable vehicle applications include utility vehicles, maintenance vehicles, construction vehicles, repair vehicles, pipeline vehicles, and military vehicles. Such air compressor systems comprise an air compressor that may be directly driven by an engine, a transmission, a driveline gearbox, or a power takeoff of a vehicle, or directly driven by an auxiliary engine or an electric motor, or indirectly driven by a vehicle engine, an auxiliary engine, or electric motor through an auxiliary belt drive or hydraulic power system.

[0017] For convenience, consistent reference numbers are used throughout the drawings to identify the same or functionally related/equivalent elements.

[0018] FIG. 1 schematically represents a first embodiment of a control system 12 installed on an air compressor system 10 that comprises an air compressor 18 and an air/oil separator tank 20. The control system 12 is shown with redundant sensors, represented but not limited to temperature sensors (senders) 14 and pressure sensors 16 (transducers) 16 in FIG. 1. Whereas conventional air compressor control systems typically use a single sensor of each type, the system of FIG. 1 uses two or more sensors for sensing each operating parameter of interest (e.g., pressure or temperature), resulting in a redundancy for the sensing of a given operating parameter of the air compressor 18.

[0019] The control system 12 of FIG. 1 includes a controller 24 that is programmed to receive and process the outputs of all four sensors 14 and 16. If there is a failure in any individual sensor 14 or 16, the controller 24 provides a warning message, for example, on a display of the controller 24, that a sensor failure has occurred and service will be required soon. The controller 24 allows the compressor 18 to function normally until the faulty sensor 14 or 16 is replaced, for example, during off hours or during planned maintenance time so as not to cause a work crew using the compressor 18 to lose time on the job. If the operator chooses to ignore the warning, the compressor 18 will continue to operate unless the second/redundant sensor 14 or 16 of the same type fails as well. This arrangement greatly increases the uptime of the compressor 18 when combined with maintenance as indicated by the controller 24.

[0020] Redundant sensors exist that are configured as single devices with dual sensing elements within the same housing. However, depending on the type of failure, dual sensing elements may be only marginally better than single element sensors. If a redundant sensor is vulnerable to ingress by corrosive contamination, the internal connections or electronics inside the device can fail, causing both sensing elements to fail. In addition, redundant sensors with dual sensing elements have a single connection plug that creates another shared failure point. If corrosion inside the connection plug is the cause of an electrical failure, the system sees both sensing elements as having failed and, as a result, will indicate an overall system failure. In contrast, the embodiment of FIG. 1 utilizes redundant sensors 14 and 16 that are entirely separate from each other, with their individual sensing elements (which may be a single sensing element in an individual sensor 14 or 16 or dual (multiple) sensing elements in an individual sensor 14 or 16) located within different sensor housings. Furthermore, as represented in FIG. 1, the individual sensors 14 and 16 each have a separate wiring harness (connector) 26 that electrically connects the sensor 14 or 16 to the controller 24. As such, none of the sensors 14 and 16 shares a connector or harnesses that electrically connects the sensor 14 and 16 to the controller 24, so as to further increase redundancy by enabling the sensors 14 and 16 to operate entirely independently of each other. The use of independent redundant sensors 14 and 16 in this manner avoids system failures attributable to internal corrosion of sensor electronics and plug corrosion failures resulting from operation of the compressor 18 and its control system 12 in hostile outdoor environments. As also shown in FIG. 1, the temperature sensors 14 are located at different locations in the air compressor system 10 (at the compressor 18 and at the tank 20), and the pressure sensors 16 are also located at different locations in the air compressor system 10 (both at the tank 20). As such, the environmental hazards to which the sensors 14 and 16 may be exposed may differ from each other.

[0021] FIG. 2 schematically represents a second embodiment of a control system 12 with redundant sensors 14 and 16, represented but not limited to a pair of temperature sensors (senders) 14 and a pair of pressure sensors 16 (transducers) 16 in FIG. 2, that are each have separate and independent wiring harnesses 26 that electrically connect the sensors 14 and 16 to the controller 24. In contrast to the embodiment of FIG. 1, the compressor control system 12 of FIG. 2 remotely locates the sensors 14 and 16 in a sealed and weather-resistant enclosure (junction box) 28. In the case of a vehicle-mounted compressor, the enclosure 28 can be mounted in a location that is directly exposed to the harsh outdoor environment in which the vehicle is operating, or located in a relatively protected area of the vehicle such as in a compartment or in the service body of a truck. Though redundant temperature and pressure sensors 14 and 16 are shown (e.g., two temperature sensors 14 and two pressure sensors 16), it is foreseeable that a similar configuration could use a single sensor of one or both types and/or multiple sensors of one or both types.

[0022] When mounted in the weather-resistant enclosure 28, the sensors 14 and 16 are isolated from moisture and corrosion, which are typically the primary cause of failure in harsh outdoor environments. The sensors 14 and 16 are shown as mounted to a manifold 38 located within the enclosure 28 and to which conduits 30, 32, and 34 are connected. As evident from FIG. 2, the manifold 38 provides oil from the same single location and source to both of temperature sensors 14, and supplies oil from the same single location and source to both of the pressure sensors 16, so that the temperature sensors 14 are redundant to each other and the pressure sensors 16 are redundant to each other.

[0023] For pressure sensing a suitable compressor operating pressure, the pressure sensors 16 are represented as connected with the conduit 30 to the separator tank 20 of the compressor system 10 as shown, so that oil within the conduit 30 equally transmits pressure to each of the pressure sensors 16. Though flowing oil is unnecessary for the pressure sensors 16, it is within the scope of the invention for oil to flow through the conduit 30 to the sensors 16. Porting within the manifold 38 is arranged so that the oil contacts the sensing elements of the pressure sensors 16 within the manifold 38.

[0024] As a result of the temperature sensors 14 being remote from the components of the air compressor system 10 and enclosed within the enclosure 28, accurate temperature sensing of the air compressor 18 requires that the temperature sensors 14 are subjected to flowing oil so that the sensors 14 are able to sense the true operating temperature of the compressor 18. For this reason, accurate temperature sensing is shown in FIG. 2 as being accomplished by routing flowing oil through the conduit 32 (preferably insulated) from a hot oil connection of the tank 20, so that oil flowing within the conduit 32 equally transmits temperature to each of the temperature sensors 14. The oil flows and contacts the sensing elements of the temperature sensors 16 within the manifold 38 before exiting the manifold 38 and being returned by the conduit 34 to the low pressure side of the compressor 18, for example, in the same location that the separator scavenge oil is returned. The conduit 34 can be equipped with an orifice 36 to regulate the oil flow to prevent excessive hot oil from being returned to the compressor 18. The orifice 36 may be equipped with a filter to ensure that contaminants are not entrained in the oil being returned to the compressor 18.

[0025] In view of the above, the nonlimiting embodiment of FIG. 2 represents oil from the same location within the air compressor system 10 being supplied to both of the temperature sensors 14 through a single insulated conduit 32, and oil from the same location within the air compressor system 10 being suppled to both of the pressure sensors 16 through a single insulated conduit 30. It is foreseeable that the oil for the sensors 14 and 16 could be drawn from other locations in the oil system of the air compressor system 10.

[0026] In view of the above, the embodiment of FIG. 2 combines redundant sensing with physically locating the sensors 14 and 16 in one location that is protected and remote from the harsh corrosive environment where the compressor 18 and its air/oil receiver tank 20 are typically mounted.

[0027] Though described and shown as utilizing two temperature sensors 14 and two pressure sensors 16, other embodiments of the invention may utilize only one or more temperature sensors 14, and/or one or more pressure sensors 16, and/or one or more sensors adapted to sense an operating parameter other than temperature or pressure. As a nonlimiting example, the control system 12 could make use of only two sensors 14 and/or 16, including one of each type of sensor 14 or 16, mounted to the manifold 38 within the enclosure 28. Furthermore, though described and shown in reference to portable compressors 18 and vehicle-mounted compressors 18, the redundant and remote-mounted sensor arrangements represented in FIGS. 1 and 2 may be useful in other types of compressor systems, such as electric-driven industrial duty-type compressors, where sensor failures can also occur and reductions in downtime achievable with the control systems 12 described above would be desirable.

[0028] In view of the above, while the invention has been described in terms of particular embodiments, it should be apparent that alternatives could be adopted by one skilled in the art. Additionally, the air compressor systems 10, the control systems 12, and their components could differ in appearance and construction from the embodiments described herein and shown in the drawings, functions of certain components of the systems 10 and 12 could be performed by components of different construction but capable of a similar (though not necessarily equivalent) function, and various materials could be used in the fabrication of the systems 10 and 12 and/or their components. As such, it should be understood that the above detailed description is intended to describe the particular embodiments represented in the drawings and certain but not necessarily all features and aspects thereof, and to identify certain but not necessarily all alternatives to the represented embodiments and described features and aspects. As a nonlimiting example, the invention encompasses additional or alternative embodiments in which one or more features or aspects of a particular embodiment could be eliminated or two or more features or aspects of different embodiments could be combined. Accordingly, it should be understood that the invention is not necessarily limited to any embodiment described herein or illustrated in the drawings. It should also be understood that the purpose of the above detailed description and the phraseology and terminology employed therein is to describe the illustrated embodiments, and not necessarily to serve as limitations to the scope of the invention. Therefore, the scope of the invention is to be limited only by the following claims.