Patent Application
20130177405
This disclosure relates to a turbomachine for use in a fluid system, for example, used in cooling. More particularly, the disclosure relates to a fluid separation configuration for maintaining wet and dry sides within the turbomachine.
One aerospace cooling system incorporates a pump that circulates a coolant through a power electronics cooling system. A propylene glycol/water (PGW) mix is used as coolant, which is electrically conductive.
The pump includes a rotor assembly and a stator assembly separated by a sleeve, which provides wet and dry sides. The rotor assembly and its supporting bearings are provided on the wet side, and the stator assembly is provided on the dry side. The sleeve must prevent the coolant from migrating to the dry side since the electrically conductive coolant can short the stator assembly. To this end, a seal is arranged at either axial end of the sleeve between an inner diameter of the sleeve, on the wet side, and the pump's housing.
A turbomachine includes a motor including a rotor assembly and a stator assembly. A sleeve fluidly separates the rotor assembly from the stator assembly. The sleeve has first and second ends axially spaced from one another. In one example, first and second seals are arranged at the first end and fluidly separate the rotor assembly from the stator assembly. The second seal is arranged downstream from the first seal relative to the rotor assembly.
In another example, the sleeve includes wet and dry sides. A first seal is arranged at the first end on the wet side. A drain is provided in the housing and arranged in a region downstream from the first seal. The drain fluidly connects the region to an exterior of the housing.
One example method of assembling the turbomachine 12 includes installing the seals 48, 50 between the sleeve 42 and the housing 20 at the wet side 45 on first and second opposing ends of the sleeve 42. Seals 56, 58 are installed between the sleeve 42 and housing 20 on the dry side 47 of the sleeve 42 at the first and second ends. The sleeve 42 is arranged within the housing 12 to fluidly separate the rotor assembly 22 from the stator assembly 32.
A cooling system includes a turbomachine having a housing enclosing a rotor assembly and a stator assembly. The rotor assembly is configured to communicate with a conductive fluid. A sleeve separates the rotor assembly and the stator assembly. A seal engages the sleeve and is configured to retain the conductive fluid on a first side of the sleeve. A drain is provided in the housing arranged fluidly downstream from the seal.
The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
A fluid system 10 is schematically shown in
An example turbomachine 12 is illustrated in
A stator assembly 32 is arranged about the rotor assembly 22 and includes windings 34. An electrical connector 36 is electrically connected to the windings 34. Current through the windings 34 excites the permanent magnets 26 and imparts rotation to the rotor assembly 22 to rotationally drive a pumping element 40, which may be an impeller or gerotor, arranged at an end of the shaft 24. A resolver assembly 38 may be used to measure the degrees of rotation of the rotor assembly 22, as desired.
A sleeve 42, cylindrical in shape, is arranged between the rotor assembly 22 and the stator assembly 32 to separate first and second sides 45, 47 that respectively correspond to wet and dry sides. In one example, the shaft 24 is hollow providing a portion of a fluid passage that permit the coolant to flow from the pumping element 40 and within the first side 45 to lubricate and cool the bearings 28, 30, which may be provided by an integrated journal and thrust bearing in the example. Coolant must be prevented from migrating to the second side 47 if electrically conductive, such as PGW, which would short the stator assembly 32. The sleeve 42 includes an inner surface 44 and an outer surface 46 respective at the first and second sides 45, 47. First and second seals 48, 50 are arranged at axially opposing ends of the sleeve 42 on the wet side to provide a seal between the sleeve 42 and the housing 20. In the example illustrated, housing portion 20C includes a first groove 52 that receives the first seal 48 and housing portion 20B includes a second groove 54 that receives the second seal 50.
In applications where it is desirable to reduce the weight of the turbomachine 12 as much as possible, a plastic sleeve 42 may be utilized. In one example, the sleeve 42 is constructed from polyether ether ketone (PEEK). A plastic sleeve may be subject to deflection under pressure of the coolant on the first side 45. As the sleeve 42 deflects, it may be possible that some coolant may migrate past the first and second seals 48, 50. To this end, additional seals may be used to prevent further migration of the coolant into the second side 47. For example, a third seal 56 is arranged in a third groove 62 in the third housing portion 20C radially outwardly from the first seal 48 and downstream from the first seal 48 to provide a seal between the outer surface 46 and the housing 20.
The resolver assembly 38 includes a fourth groove 64 receiving a fourth seal 58 that seals relative to the outer surface 46. A fifth groove 66 in the housing portion 20A includes a fifth seal 60 that seals relative to the resolver assembly 38. The fourth and fifth seals 58, 60 are arranged downstream from the second seal 50. In the example, first, second, third, fourth and fifth seals 48, 50, 56, 58, 60 are elastomeric O-rings constructed from a material compatible with PGW, for example.
To relieve the pressure and evacuate any fluid that might leak past the first and second seals 48, 50, first and second drains 68, 70 are provided at either end of the sleeve 42. The first drain 68 is provided in a region between the first and third seals 48, 56 and fluidly connects the region to an exterior of the housing 20. The second drain 70 is provided in a region between the second and fifth seals 50, 60 and fluidly connects the region to the exterior of the housing 20. Thus, coolant that leaks past the first and second seal 48, 50 is permitted to drain from the housing 20 and overboard, thereby preventing the coolant from building pressure behind the third, fourth and fifth seals 56, 58, and 60. In this manner, undesired sleeve deflection is reduced.
One example method of assembling the turbomachine 12 includes installing the seals 48, 50 between the sleeve 42 and the housing 20 on the wet side 45 at first and second opposing ends of the sleeve 42. Seals 56, 58 are installed between the sleeve 42 and housing 20 on the dry side 47 of the sleeve 42 at the first and second ends. The sleeve 42 is arranged within the housing 12 to fluidly separate the rotor assembly 22 from the stator assembly 32.
Although an example embodiment has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.
