Compressor
11549513 ยท 2023-01-10
Assignee
Inventors
Cpc classification
F04D29/584
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/266
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2240/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/582
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/026
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/5806
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/002
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/0646
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/522
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2250/51
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D25/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D25/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/58
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A compressor comprising: a stator assembly comprising a plurality of stator elements; a rotor assembly comprising a shaft to which is mounted at least one bearing, a permanent magnet and an impeller; a support body; and an outer can comprising an air inlet. The support body comprises a hollow elongate central part to which is mounted the at least one bearing, and inside which the magnet is positioned, the elongate central part comprising a plurality of openings, and the air inlet of the outer can is axially aligned at least partially with the plurality of openings in the elongate central part.
Claims
1. A compressor comprising: a stator assembly comprising a plurality of stator elements; a rotor assembly comprising a shaft to which is mounted at least one bearing, a permanent magnet and an impeller; a support body; and an outer can comprising an air inlet; wherein the support body comprises a hollow elongate central part to which is mounted the at least one bearing, inside which the magnet is positioned, and at least a part of the stator elements are radially external to the hollow elongate central part, the elongate central part comprising a plurality of openings, and wherein the air inlet of the outer can and the plurality of openings in the elongate central part are each disposed on a surface that is parallel with respect to an axial direction of the shaft.
2. The compressor of claim 1, wherein the air inlet comprises at least one opening such that air enters the compressor in a direction having both axial and radial components.
3. The compressor of claim 1, wherein the outer can is spaced apart from the support body to form an annular airflow pathway.
4. The compressor of claim 3, wherein the stator elements are positioned with respect to the plurality of openings, and are fixed to the support body such that they are cooled by airflows on an inside and outside of the support body.
5. The compressor of claim 1, wherein a printed circuit board is mounted to an end of the outer can proximate the air inlet.
6. The compressor of claim 5, wherein one or more electric components mounted to the printed circuit board (PCB) extend from the PCB and into a space behind the air inlet.
7. The compressor of claim 1, wherein, in use, air flows through the compressor both inside the support body, and outside the support body.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In order that the present invention may be more readily understood, embodiments of the invention will now be described, by way of example, with reference to the following accompanying drawings, in which:
(2)
(3)
(4)
DETAILED DESCRIPTION OF THE INVENTION
(5)
(6) The rotor assembly 12 comprises a shaft 30 on which is mounted a magnet 32, a first balancing ring 34 and a second balancing ring 36. When the rotor assembly 12 is assembled, a pair of bearings are mounted on the shaft 30 on either side of the core 32 and balancing rings 34, 36. In
(7) When the stator elements 16, 18, 20 and 22 are located in respective openings in the support body 14, at least a portion of the opening is still open, and not restricted by the stator element. This allows an airflow to pass the stator element, through the opening, and into the support body. When the compressor is in use, this airflow can be used to cool the rotor assembly 12 located inside the support body 14, and in particular the magnet 32.
(8)
(9) An outer can 130 is positioned around the outside of the compressor 100. It is supported by the support body 116 by being mounted via hub 132 to the outside surface of the bearing seat 120. An air inlet 134 is provided in the outer can 130 to allow air to be drawn in by the compressor 100 during use. Mounted to the outer surface of the other bearing seat 122 is a shroud 136 which surrounds the impeller 114. The outer casing 130 is also mounted to shroud 136. Air passages 138 are provided around or through the shroud 136 to allow air to be drawn through the compressor 100 by the impeller 114. The hub 132 also acts as a winding termination block to which windings of the stator elements 102, 104 can be connected in order to receive current.
(10) As can be seen from
(11) After passing the stator elements 102, 104, airflow B passes back out of the support body 116 and rejoins airflow A. The combined airflows are then drawn past the shroud 136 by the impeller 114, and out of the compressor 100 as airflow C.
(12)
(13) As can be seen from
(14) Whilst particular embodiments have thus far been described, it will be understood that various modifications may be made without departing from the scope of the invention as defined by the claims.