Patent Application
20170117776
The subject matter disclosed herein relates to motors, and more particularly, to a stator for a motor with laminations to facilitate cooling.
Environmental control systems can utilize electric motors to pressurize and move air for use within the cabin of an aircraft. The electric motor of the environmental control system, as well as other motors, may utilize air cooling to cool the motor during operation. Often air cooling may not provide for sufficient cooling of the motor during certain operating conditions.
According to an embodiment, a laminated stator for a motor includes a first plurality of stator laminations with a first electrical conductivity and a first thermal conductivity, and a second plurality of stator laminations with a second electrical conductivity and a second thermal conductivity, wherein the second electrical conductivity is lower than the first electrical conductivity, the second thermal conductivity is higher than the first thermal conductivity, and the second plurality of stator laminations are disposed throughout the first plurality of stator laminations.
According to an embodiment, an environmental control system cooled by an airflow includes a motor cooling inlet to receive the airflow, and a motor including a rotor, and a laminated stator to receive the airflow from the motor cooling inlet, including a first plurality of stator laminations with a first electrical conductivity and a first thermal conductivity, and a second plurality of stator laminations with a second electrical conductivity and a second thermal conductivity, wherein the second electrical conductivity is lower than the first electrical conductivity, the second thermal conductivity is higher than the first thermal conductivity, and the second plurality of stator laminations are disposed throughout the first plurality of stator laminations.
Technical function of the embodiments described above includes a second plurality of stator laminations with a second electrical conductivity and a second thermal conductivity, wherein the second electrical conductivity is lower than the first electrical conductivity and the second thermal conductivity is higher than the first thermal conductivity.
Other aspects, features, and techniques of the embodiments will become more apparent from the following description taken in conjunction with the drawings.
The subject matter is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other features, and advantages of the embodiments are apparent from the following detailed description taken in conjunction with the accompanying drawings in which like elements are numbered alike in the FIGURES:
Referring now to the drawings,
During operation, the motor 110 can generate heat. In the illustrated embodiment, airflow 102 can be utilized to air cool the motor 110. In the illustrated embodiment, airflow 102 is received from the compressor inlet 106 and is directed to the motor cooling inlet 108. The airflow 102 can flow through the motor stator 112 and exit through the cooling exit 104. In certain embodiments, the amount of airflow 102 is limited by operating conditions, such as high speed, high altitude operating conditions, which may not provide adequate cooling of the motor 110. In these operating conditions, conventional motors 110 may exceed target operating temperatures affecting reliability and performance. Advantageously, the stator 112 can include cooling lamination layers to increase heat transfer to remove heat from the stator 112.
In
In the illustrated embodiment, the conductive lamination layers 120 and the cooling lamination layers 122 are stacked to form the motor stator 112. The conductive lamination layers 120 and the cooling lamination layers 122 can be bonded together to form the laminated stator 112.
In the illustrated embodiment, the conductive lamination layers 120 allow for normal electromagnetic operation of the motor stator 112. In the illustrated embodiment, a plurality of conductive lamination layers 120 can be layered or stacked to form the stator 112. Generally, the conductive lamination layers 120 have a high electrical conductivity and a relatively low thermal conductivity relative to the cooling lamination layers 122. In the illustrated embodiment, the conductive lamination layers 120 can be electrical steel, such as Arnon, or other suitable materials for forming a motor stator 112. During operation, the conductive lamination layers 120 can generate heat due to the electrical energy passing through the conductive lamination layers. In the illustrated embodiment, the conductive lamination layers 120 may conduct some heat to be removed by the airflow 102, however during typical operation the use of the conductive lamination layers 120 introduces additional heat into the stator 112.
In the illustrated embodiment, the cooling lamination layers 122 can transfer and dissipate heat generated by the motor stator 112, and in particular the heat generated by the conductive lamination layers 120. In the illustrated embodiment, the cooling lamination layers 122 can be formed from annealed pyrolytic graphite. Advantageously, annealed pyrolytic graphite has a relatively high thermal conductivity (1700 W/m-K). Further, annealed pyrolytic graphite can provide generally anisotropic heat transfer. In other embodiments, the cooling lamination layers 122 can be formed from any suitable material with a low electrical conductivity and a high thermal conductivity relative to the conductive lamination layers 120. The heat generated by the conductive lamination layers 120 can be dissipated and moved out to the fins 124, 126 (as shown in
In the illustrated embodiment, the conductive lamination layers 120 and the cooling lamination layers 122 can have the same lamination shape 123. Advantageously, since the conductive lamination layers 120 and the cooling lamination layers 122 have the same lamination shape 123 ease of processing and assembly can be facilitated. After assembly, the conductive lamination layers 120 and the cooling lamination layers 122 can be glued and or bonded to form the stator 112.
In certain embodiments, the ratio of conductive lamination layers 120 to cooling lamination layers 122 can be twenty conductive lamination layers 120 to one cooling lamination layer 122. Based on a twenty to one ratio of conductive lamination layer 120 and the cooling lamination layer 122, this results in equivalent radial direction thermal conductivity of 113.2 W/m-K. In other embodiments, the ratio can be any suitable ratio to allow for suitable electrical and thermal performance of the stator 112. In certain embodiments, the thickness of each of the conductive lamination layers 120 and the cooling lamination layers 122 can be selected for desired thermal and electrical characteristics. In the illustrated embodiment, the length of the stator 112 is affected by the number of cooling lamination layers 122 in the stator 112. The introduction of cooling lamination layers 122 may lengthen the stator 112.
In the illustrated embodiment, the introduction of cooling lamination layers 122 allows for more effective cooling of motors 110 utilizing air cooling from an airflow 102. In certain embodiments, such as a motor 110 for use in an environmental control system 100, operating temperatures have been reduced from 236.9 C to 211 C, for worst case cooling and electrical load conditions, allowing for greater reliability of the motor 110.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the embodiments. While the description of the present embodiments has been presented for purposes of illustration and description, it is not intended to be exhaustive or limited to the embodiments in the form disclosed. Many modifications, variations, alterations, substitutions or equivalent arrangement not hereto described will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the embodiments. Additionally, while various embodiments have been described, it is to be understood that aspects may include only some of the described embodiments. Accordingly, the embodiments are not to be seen as limited by the foregoing description, but are only limited by the scope of the appended claims.
