The present disclosure relates to a fluid pump. More particularly, an integrated motor, pump and controller assembly includes an internal coolant flow path to transfer heat from motor and the controller to the fluid being pumped.
This section provides background information related to the present disclosure which is not necessarily prior art.
A variety of motor driven fluid pumps have been controlled with switches or electronics positioned remotely from the motor and pump combination. Relatively unwieldy packaging and wire routing concerns may exist regarding the installation and use of these devices.
Other electric motor and pump combinations have been configured to include a controller positioned within the same or an adjacent housing. Robust operation becomes a concern due to possible overheating of the electronic components within the controller. Known designs are relatively large, costly and complex. Accordingly, a need in the art may exist to define a simplified, low cost, low weight electric motor, pump and controller combination.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
An electric pump comprises an outer housing including a motor cavity and a controller cavity separated by a partition wall. An inner housing is positioned within the motor cavity of the outer housing. One of the inner and outer housings includes radially extending ribs positioned adjacent to the other of the inner and outer housings to define a coolant flow path between the inner housing and the outer housing. The flow path is partially defined by the partition wall. An electric motor is positioned within the inner housing and includes a hollow rotor shaft driving a pump member. The hollow rotor shaft forms a portion of the coolant path and interconnects a volume between the inner and outer housings with a low pressure cavity containing the pump member. A controller is positioned within the controller cavity in heat transfer relation with the partition wall.
An electric pump includes an outer housing having a motor cavity and a controller cavity separated by a partition wall. An inner housing is positioned within the motor cavity of the outer housing. One of the inner and outer housings includes radially extending ribs positioned adjacent to the other of the inner and outer housing to define a coolant flow path between the inner and outer housings. An electric motor is positioned within the inner housing and includes a stator and a rotor, where the rotor is fixed to a solid rotor shaft for driving a pump member. A cylindrical sleeve separates the stator and the rotor. An area between the sleeve and the rotor forms a portion of the coolant path and interconnects a volume between the inner and outer housings with a low pressure cavity containing the pump member. A controller is positioned within the controller cavity in heat transfer relation with the partition wall.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only of selected embodiments and not all possible implementations, and are not intended to limit the scope of the present disclosure.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Example embodiments will now be described more fully with reference to the accompanying drawings.
Pump 10 includes an outer housing 26 and an inner housing 28 arranged to allow fluid pumped by impeller 18 to pass between inner housing 28 and outer housing 26 to cool controller 22. A sleeve 30 is positioned to surround rotor assembly 16 and define a sealed stator cavity 32 in which stator assembly 14 is positioned. Fluid pumped by impeller 18 does not enter stator cavity 32 or contact stator assembly 14. A cap 36 includes an inlet 38 and an outlet 40. A mid-plate 44 cooperates with cap 36 to define an impeller cavity 46 where impeller 18 is rotatably positioned. Fasteners 48 couple cap 36 and mid-plate 44 to outer housing 26. First, second and third o-rings 52, 54 and 56 seal an interface between cap 36 and mid-plate 44, a joint between mid-plate 44 and outer housing 26, and an interface between mid-plate 44 and inner housing 28.
Rotor assembly 16 includes a plurality of permanent magnets (not shown) encapsulated by a shell 62. All of the rotor assembly components are fixed to rotor shaft 20. A first bushing 66 is positioned within a counterbore 68 formed in mid-plate 44 to support a first end 69 of rotor shaft 20 for rotation. An elastomeric member 70 and a plate 72 function to prevent shock loads being transferred to bushing 66. A second bushing 76 is positioned within a bore 78 of inner housing 28 to support a second end 80 of rotor shaft 20 for rotation.
Sleeve 30 sealingly engages mid-plate 44 and inner housing 28 to define stator cavity 32 as well as a rotor cavity 82. A first o-ring 84 is positioned between an inner circumferential surface of sleeve 30 and an outer circumferential surface of a boss 86 of mid-plate 44. Another o-ring 88 is positioned within a groove 90 formed within inner housing 28 to sealingly engage an end face 92 of sleeve 30. The overall length of sleeve 30 is defined to assure that a compressive load acts on o-ring 88 when cap 36 and mid-plate 44 are coupled to outer housing 26 via fasteners 48. This arrangement assures that pumped fluid does not enter stator cavity 32.
Stator assembly 14 includes a coil 100 and a plurality of plates 102 closely fitted to an inner cylindrical wall 104 of inner housing 28. Wires from coil 100 extend through apertures 108 formed in radially extending flanges 110 of sleeve 30.
Inner housing 28 includes a substantially cylindrically shaped wall 114 having an inner cylindrical surface 104 and an outer cylindrical surface 116. A bottom 118 closes one end of cylindrical wall 114. Mid-plate 44 closes the opposite end. A central aperture 120 extends through bottom 118 and is in receipt of one end of rotor shaft 20. Other apertures 124 are coaxially aligned with apertures 108 of sleeve 30 to allow wires from the windings to pass therethrough. It is contemplated that inner housing 28 is formed from a metal using a casting process.
Outer housing 26 may also be a metal casting. Outer housing 26 includes a substantially cylindrically shaped wall 128 with a substantially cylindrical inner surface 130. A partition wall 132 caps cylindrical wall 128 and separates a cooling cavity 136 from a controller cavity 138. An end cap 139 is coupled to outer housing 26 with a plurality of fasteners 141 to define controller cavity 138. A plurality of radially inwardly extending ribs 140 define a coolant flow path 142 best shown in
Ribs 140a radially inwardly protrude from surface 130 and axially extend from an inner surface 144 of partition wall 132 to a mating surface 146 formed at the end of outer housing 26. Another set of inwardly protruding ribs, identified at reference numerals 140b, are shorter than ribs 140a, extend from surface 144 and terminate at ends 150 spaced apart from mating surface 146. The long (140a) and short (140b) ribs are positioned circumferentially spaced apart from one another in an alternating pattern to define a singular continuous and circuitous flow path 142. Ribs 140a and 140b also include radially extending and axially protruding portions extending above surface 144. The external features of inner housing 28, including outer surface 116 and bottom 118, are sized to mate with and be positioned substantially adjacent to the innermost surfaces of ribs 140a, 140b. As such, inner housing 28 cooperates with outer housing 26 to define fluid flow path 142. It should be appreciated that in an alternate configuration, some or all of ribs 140 may be formed on inner housing 28 instead of outer housing 26.
Outer housing 26 also includes passages 158, 160 and 162 shaped as concentric rings axially protruding from surface 144. O-ring seals 163 are positioned between the inner and outer concentric rings to sealingly engage bottom 118 of inner housing 28. Apertures 164, 166 and 168 extend through partition wall 132 to allow wires of stator assembly 14 to extend into controller cavity 138. Seals 163 function to restrict ingress of pumped fluid into stator cavity 32 and controller cavity 138.
As best shown in
Coolant fluid flow path 142 provides pressurized fluid to inlet 154 and axially across inner surface 130. The fluid turns 90 degrees to flow across inner surface 144 and around passage 158. Path 142 turns 90 degrees once again to direct coolant flow axially across surface 130 in an opposite direction. Flow continues across cylindrical surface 130 and turns 180 degrees around end 150 of rib 140b and across mid-plate 44. This circuitous pattern is repeated until pressurized fluid reaches a blind recess 172 (
Controller 22 is mounted to a portion 178 of partition wall 132 having an increased thickness. The increased thickness portion acts as a heat sink for energy emitted by elements such as MOSFETs of controller 22. Fluid flow path 142 includes many portions of surface 144 being in direct contact with the pumped fluid. Heat is transferred from controller 22 to the fluid passing across partition 132.
Another flow path exists to lubricate bushings 66 and 76. As shown in
An inner housing 320 includes a cylindrical portion 322 having radially outwardly extending ribs 324 as well as an integrally formed mid-plate 326. The ribs may alternatively be formed on outer housing 302. A sleeve 330 includes a cylindrical portion 332 and an integrally formed flange portion 334. Flange portion 334 closes an open end of cylindrically-shaped portion 322 of inner housing 320. A seal 340 is located at the joint interconnecting inner housing 320 and flange portion 334. Cylindrical portion 332 of sleeve 330 axially extends to engage partition wall 304 to at least partially define lower reservoir 310.
A rotor shaft 342 of pump is no longer hollow as described in relation to the previous arrangements. Rotor shaft 342 is solid and fluid does not flow therethrough.
More particularly, high pressure fluid is provided to inlet 350 through fluid passageway 356a and on either side of a wall 360a. Fluid continues to flow through passageways 356i and 356b around another set of ribs, down through passageways 356c and 356h, back up along passageways 356d and 356g, and returning through passageways 356f and 356e. Internal ports 362, 364 allow coolant to enter lower reservoir 310. Slots 308 allow coolant to enter bearing cavity 312. Coolant within cavity 312 may lubricate the interface between a bearing or bushing 370 and solid rotor shaft 342. The fluid flow path continues from lower reservoir 310 around rotor 248, inside of sleeve 330 until the fluid reaches a cavity 372. Fluid within cavity 372 may also lubricate the interface between a bearing or bushing 374 and solid rotor shaft 342. Coolant flows from cavity 372 through a plurality of passageways 376 extending through mid-plate 326 to provide a portion of the fluid path no longer provided through rotor shaft 342. A plurality of outlets 378 are circumferentially spaced apart from one another and extend through an impeller 380 to further define a portion of the coolant flow path. Outlets 378 terminate at a low pressure zone within impeller 380 such that increased temperature coolant is combined with the fluid being pumped from pump 300.
The foregoing description of the embodiments has been provided for purposes of illustration and description. It is not intended to be exhaustive or to limit the disclosure. Individual elements or features of a particular embodiment are generally not limited to that particular embodiment, but, where applicable, are interchangeable and can be used in a selected embodiment, even if not specifically shown or described. The same may also be varied in many ways. Such variations are not to be regarded as a departure from the disclosure, and all such modifications are intended to be included within the scope of the disclosure.
This application claims the benefit of U.S. Provisional Application No. 61/376,740, filed on Aug. 25, 2010. The entire disclosure of the above application is incorporated herein by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/CA11/00961 | 8/24/2011 | WO | 00 | 6/19/2013 |
Number | Date | Country | |
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61376740 | Aug 2010 | US |