The present application claims the benefit of Chinese Patent Application No. 202420037517.7 filed on Jan. 8, 2024, the contents of which are incorporated herein by reference in their entirety.
The present application relates to the field of BLDC motors, in particular to a high-speed BLDC motor with a stable bearing structure.
A BLDC motor is an electromagnetic device for converting or transmitting electric energy according to the law of electromagnetic induction. The BLDC motor generally includes a housing, a stator assembly, a rotor assembly and a rotating shaft, and the rotor assembly rotates relative to the stator assembly by means of the rotating shaft. The rotational friction force is usually reduced by means of a bearing member, currently, the specific bearing member used by the BLDC motor is such that a spring is mounted between two bearing assemblies, and the pre-tightening force is applied to two bearing outer rings by means of the compression force of the spring. Due to the low machining precision of end faces of the spring, two bearings are prone to deviation in actual situations, which easily causes nonuniform stress on steel balls of the bearings at the speed of 110,000-150,000 rpm, causes fatigue failure after long-term (2,000 h) operation, accelerates the abrasion of a bearing track, and affects the service life of the BLDC motor.
In order to overcome the defects and shortcomings in the prior art, the present application provides a high-speed BLDC motor with a stable bearing structure, which solves the technical problem of shortening of the service life of a BLDC motor due to nonuniform stress on steel balls of bearings due to relative eccentricity of the bearings due to machining errors of end faces when a spring is assembled between two bearing assemblies in the existing high-speed BLDC motor technology.
In order to achieve the above purpose, the present application is achieved by the following technical solution: the high-speed BLDC motor with the stable bearing structure comprises a stator assembly, a rotor assembly, a rotating shaft, a bearing member and a shaft sleeve, where the bearing member comprises a first bearing and a second bearing, the first bearing comprises a first bearing inner ring and a first bearing outer ring, the second bearing comprises a second bearing inner ring and a second bearing outer ring, two end faces of the shaft sleeve are in contact with end faces of the first bearing inner ring and the second bearing inner ring respectively, and adhesives are provided on contact surfaces of the first bearing inner ring and the second bearing inner ring with the rotating shaft.
Preferably, the first bearing and the second bearing are provided on the same side of the rotor assembly.
Preferably, the first bearing outer ring has a displacement of 0.01-0.015 mm relative to the first bearing inner ring, and the second bearing outer ring has a displacement of 0.01-0.015 mm relative to the second bearing inner ring.
Preferably, a distance between the first bearing outer ring and the second bearing outer ring is 0.02-0.03 mm shorter than a distance between the first bearing inner ring and the second bearing inner ring.
Preferably, the bearing member is provided in a bearing chamber, and the bearing chamber is provided with a boss for applying a support force to the bearing member.
Preferably, the boss has a thickness of 0.2-1 mm.
Preferably, the high-speed BLDC motor further comprises a housing, where an end face of the housing is provided with ventilation grooves.
Preferably, each of the ventilation grooves has a diameter of 1-5 mm.
Preferably, the shaft sleeve is made of metal.
Compared with the prior art, the present application has the beneficial effects as follows:
In order to explain embodiments of the present application or technical solutions in the prior art more clearly, drawings needed in descriptions of the embodiments or the prior art will be briefly introduced below.
Reference numerals: 1—stator assembly; 2—rotor assembly; 3—rotating shaft; 4—bearing member; 41—first bearing; 411—first bearing inner ring; 412—first bearing outer ring; 42—second bearing; 421—second bearing inner ring; 422—second bearing outer ring; 5—shaft sleeve; 6—bearing chamber; 61—boss; 7—housing; and 71—ventilation groove.
The present application is further explained in conjunction with the drawings of the specification and particular embodiments below. However, the described embodiments are merely part of embodiments of the present application, not all of them. On the basis of the embodiments of the present application, all other embodiments obtained by those of ordinary skill in the art without involving any inventive effort should fall within the scope of protection of the present application.
Reference is made to
Further, the first bearing outer ring 412 has a displacement of 0.01 mm relative to the first bearing inner ring 411, the second bearing outer ring 422 has a displacement of 0.01 mm relative to the second bearing inner ring 421, and a distance between the first bearing outer ring 412 and the second bearing outer ring 422 is 0.02 mm shorter than a distance between the first bearing inner ring 411 and the second bearing inner ring 421.
Further, the boss 61 has a thickness of 0.2 mm.
Further, each of the ventilation grooves 71 has a diameter of 1 mm.
Reference is made to
Further, the first bearing outer ring 412 has a displacement of 0.015 mm relative to the first bearing inner ring 411, the second bearing outer ring 422 has a displacement of 0.015 mm relative to the second bearing inner ring 421, and a distance between the first bearing outer ring 412 and the second bearing outer ring 422 is 0.03 mm shorter than a distance between the first bearing inner ring 411 and the second bearing inner ring 421.
Further, the boss 61 has a thickness of 1 mm.
Further, each of the ventilation grooves 71 has a diameter of 5 mm.
The embodiments listed above are merely particular embodiments of the present application. Obviously, the present application is not limited to the above embodiments, and there may be many similar modifications. All transformations that would have been directly derived from or associated with the content disclosed herein by those of ordinary skill in the art should be considered to fall within the scope of protection of the present application.
Number | Date | Country | Kind |
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202420037517.7 | Jan 2024 | CN | national |