System and method involving a variable speed cooling fan used with a compressor and an internal combustion engine
11002175 · 2021-05-11
Assignee
Inventors
Cpc classification
F04D29/584
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/5826
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/022
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/166
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02P15/00
ELECTRICITY
F04D25/026
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02B30/70
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01P7/048
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01P5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B35/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01P7/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04B35/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D17/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01P5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A system and method of a variable speed cooling fan for a skid mounted compressor. A magnetic variable speed clutch is mounted to the cooling fan drive shaft. The clutch mechanism is driven via by a drive pulley on the crankshaft of the engine driving the compressor. The speed of the fan is varied dependent upon the temperature of the fluids being cooled.
Claims
1. A system comprising: an internal combustion engine that includes a rotatable drive shaft that rotates during operation of the internal combustion engine and a rotatable crankshaft that rotates during operation of the internal combustion engine; a compressor operatively connected to the drive shaft of the internal combustion engine so that operation of the internal combustion engine rotates the drive shaft and powers the compressor to compress gas; a cooler including a rotatable cooling fan that rotates to cool the gas and/or the internal combustion engine; a magnetic variable speed drive that operatively connects the cooling fan to the crankshaft of the internal combustion engine so that rotation of the crankshaft is transmitted to the cooling fan by way of the magnetic variable speed drive; the magnetic variable speed drive including only a single plate and only a single disk that are spaced apart from one another, the single plate being comprised of magnetic material and producing a magnetic field, the single disk being comprised of non-ferrous material, the single disk being attracted to the magnetic field of the single plate to couple rotation of the crankshaft to rotation of the cooling fan; and a motor operatively connected to the magnetic variable speed drive to adjust a distance between the single disk and the single plate and thereby vary a speed of rotation of the cooling fan.
2. The system according to claim 1, wherein the single disk is fixed to the crankshaft so that rotation of the crankshaft results in rotation of the single disk.
3. The system according to claim 2, wherein the single plate is fixed to a drive pulley so that the single disk and the drive pulley rotate together.
4. The system according to claim 3, wherein the drive pulley is a first drive pulley and the cooling fan includes a driving shaft, and further comprising a second drive pulley and a belt extending around the first drive pulley and the second drive pulley, the second drive pulley being coaxial with the driving shaft of the cooling fan.
5. The system according to claim 1, wherein the magnetic variable speed drive is coaxial with the crankshaft of the internal combustion engine.
6. The system according to claim 1, wherein the internal combustion engine, the compressor and the cooler are mounted on a skid.
7. A system comprising: an internal combustion engine that includes a rotatable drive shaft that rotates during operation of the internal combustion engine and a rotatable crankshaft that rotates during operation of the internal combustion engine; a compressor connected to the drive shaft of the internal combustion engine so that rotation of the drive shaft powers the compressor to compress gas; a cooler including a plurality of cooling stages and a rotatable cooling fan that rotates to blow air across the plurality of cooling stages to cool the gas and/or the internal combustion engine; a magnetic variable speed drive connecting the crankshaft of the internal combustion engine to the cooling fan so that operation of the internal combustion engine results in rotation of the crankshaft that is transmitted to the cooling fan by way of the magnetic variable speed drive to rotate the cooling fan; the magnetic variable speed drive including only a single disk and only a single plate that are rotatable about an axis, positioned side-by-side and spaced apart from one another so that a gap exists between the single plate and the single disk, the single plate being comprised of magnetic material and producing a magnetic field, the single disk being comprised of non-ferrous material and being attracted to the magnetic field of the single plate to couple rotation of the crankshaft to rotation of the cooling fan; and a motor operatively connected to the magnetic variable speed drive change a size of the gap so that an increase in the size of the gap decreases a rotation speed of the cooling fan while a decrease in the size of the gap increases the rotation speed of the cooling fan.
8. The system according to claim 7, wherein the single disk is fixed to the crankshaft so that rotation of the crankshaft results in rotation of the single disk.
9. The system according to claim 7, wherein the single plate is fixed to a drive pulley so that the single plate and the drive pulley rotate together.
10. The system according to claim 9, wherein the drive pulley is a first drive pulley and the cooling fan includes a driving shaft, and further comprising a second drive pulley and a belt extending around the first drive pulley and the second drive pulley, the second drive pulley being coaxial with the driving shaft of the cooling fan.
11. The system according to claim 7, wherein the axis about which the single disk and the single plate rotate is coaxial with the crankshaft.
12. The system according to claim 7, wherein the plurality of cooling stages includes at least three cooling stages.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Preferred embodiments of the system will now be described in further detail. Other features, aspects, and advantages of the system will become better understood with regard to the following detailed description, appended claims, and accompanying drawings (which are not to scale) where:
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION
(6) Set forth below with reference to the accompanying drawings is a detailed description of embodiments of a system and method representing examples of the inventive system and method disclosed here.
(7)
(8) Natural gas from a well or other source may enter the system 18 through the inlet 54 of the first compression stage 42 where it is compressed. The compressed gas leaves through the first compression stage outlet 56 which may be in fluid communication with the first stage cooling inlet 58. Heat is removed from the compressed gas as it passes through the first cooling stage 46. The cooled compressed gas leaves the first cooling stage 46 through the outlet 60 which may be in fluid communication with the inlet 62 of the second compression stage 44. The gas is compressed and leaves the second compression stage 44 via the outlet 64 which may be in fluid communication with the inlet 66 of the second cooling stage 48. The gas is cooled as it passes through the second cooling stage 48. The gas leaves the second cooling stage 48 via the outlet 68 and passes on to a pipeline or further processing which varies based on the specific installation. Condensate knockout drums and other liquid removal may also be incorporated in the process between the cooling stages and compression stages as necessary.
(9) The third cooling stage 50 of the fin fan cooler 26 may be in fluid communication with the cooling system of the internal combustion engine 24. The third cooling stage 50 may thus cool the cooling fluid of the internal combustion engine 24.
(10) The fourth cooling stage 52 in this example, provides cooling fluid for the intercooler 112 of the turbo (turbocharger) 70 on the internal combustion engine 24. The turbo 70 may be powered by the exhaust 72 leaving the internal combustion engine 24. This may be used to pressurize combustion air. The combustion air enters the turbo 70 through the inlet 74. It is pressurized in the turbo 70 and exits through the outlet 76 where it may be cooled in the intercooler prior to entering the intake 82 of the internal combustion engine 24. The compressed and cooled combustion air may be mixed with fuel and used in the operation of the internal combustion engine 24.
(11) Cooling fluid leaves the intercooler 112 via the outlet 114 which may be in fluid communication with the inlet 78 of the fourth cooling stage 52 of the fin fan cooler 26. The cooling fluid is cooled and then leaves the fourth cooling stage 52 through the outlet 80 which may be in fluid communication with the inlet 116 of the intercooler 112. Many applications of the system disclosed by way of example here use a turbo charged engine thus the example includes a turbo 70 and fourth cooling stage 52, used to cool an intercooler 112. However the present invention may also be used with a normally aspirated engine in which case the intercooler would not be needed.
(12) During operation of the system disclosed by way of example, the fan 30 may blow air across the first, second, third and fourth cooling stages 46, 48, 50 and 52. This helps remove heat from the compressed gas, compressed combustion air and cooling fluids flowing through the fin fan heat exchanger 26. Temperature sensors 84, 86, 88 and 90 may be located at the outlets 60, 68, 80 and 82 of the various stages to provide temperature information about the fluid at the outlets 60, 68, 80 and 82 of the various stages. The temperature detected at these points may be sent to a controller 92. The connection between the temperature sensors 84, 86, 88, and 90 and the controller 92 can be hardwired or wireless.
(13) If the temperature at any one of these locations exceeds a preset upper limit, the speed of the fan 30 may be increased through operation of the magnetic variable speed drive 38. This increase in fan speed and air flow in turn increases the amount of the heat removed from the fluids flowing through the other side of the heat exchanger 26. The fan speed can be stepped up (increased) or down (decreased) incrementally based upon hitting predetermined temperature levels.
(14)
(15) There is a natural slippage between the plates 104 and the disk 102. This slippage can be increased by increasing the gap 106 thus decreasing the fan speed. Conversely the fan speed can be increased by reducing the gap 106 and thus reducing the slip. The gap 106 can be adjusted through operation of the one or more solenoids 108. The solenoids 108 are operable by the controller 92. The linkage 110 ensures the gaps 106 on either side of the disk 102 remain equal.
(16) The embodiment of the skid mounted compressor assembly (system) described above is configured so that rotation of the drive pulley 94 is transferred to the fan drive shaft 100 by way of the magnetic variable speed drive 38. Thus, the rotational drive of the magnetic variable speed drive 38 is directly delivered to the fan drive shaft 100. The magnetic variable speed drive 38 is thus positioned at an intermediate position, with reference to the rotation transmission path, relative to the drive pulley 94 and the fan drive shaft 100. In this embodiment, the magnetic variable speed drive 38 is coaxial with the fan drive shaft 100 and the drive pulley 94 as depicted in
(17) The positioning of the magnetic variable speed drive is not limited to the positioning described above. For example,
(18)
(19) There is a natural slippage between the plate 104 and the disk 102. This slippage can be increased by increasing the gap 106 between the plate 102 and the disk 102. Increasing the size of the gap (i.e., increasing the distance between the disk 102 and the plate 104) decreases the fan speed. Conversely the fan speed can be increased by reducing the size of the gap 106 (i.e., moving the disk 102 and the plate 104 relatively closer), thus reducing the slip. The size of the gap 106 (i.e., the distance between the disk 102 and the plate 104) may be adjusted through operation of the motor 108. The motor 108 may be operable by the controller 92.
(20) The detailed description above describes embodiments of a system and method representing examples of the inventive system and method disclosed here. The invention is not limited, however, to the precise embodiments described. Various changes, modifications and equivalents can be effected by one skilled in the art without departing from the spirit and scope of the invention as defined in the accompanying claims. It is expressly intended that all such changes, modifications and equivalents which fall within the scope of the claims are embraced by the claims.