CN209115394U - Blade and internal rotor integral structure and blade and the integrated blower of internal rotor - Google Patents

Blade and internal rotor integral structure and blade and the integrated blower of internal rotor Download PDF

Info

Publication number
CN209115394U
CN209115394U CN201821848071.7U CN201821848071U CN209115394U CN 209115394 U CN209115394 U CN 209115394U CN 201821848071 U CN201821848071 U CN 201821848071U CN 209115394 U CN209115394 U CN 209115394U
Authority
CN
China
Prior art keywords
blade
rotor
integral structure
internal rotor
installation
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201821848071.7U
Other languages
Chinese (zh)
Inventor
彭兵
薛佳运
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yi Kun Power Technology (shanghai) Co Ltd
Original Assignee
Yi Kun Power Technology (shanghai) Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Yi Kun Power Technology (shanghai) Co Ltd filed Critical Yi Kun Power Technology (shanghai) Co Ltd
Priority to CN201821848071.7U priority Critical patent/CN209115394U/en
Application granted granted Critical
Publication of CN209115394U publication Critical patent/CN209115394U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model discloses a kind of blade and internal rotor integral structure and blade and the integrated blower of internal rotor, the blade and internal rotor integral structure include: rotor hub, rotational installation and disk-shaped setting, the rotor hub is provided with hollow-out parts, the hollow-out parts are circumferentially arranged, and the rotor hub is divided into inner ring and outer ring;Multiple blades are located in the hollow-out parts, and inner end and the inner ring of each blade are fixed, and outer end is fixed with the outer ring, so that the blade and the rotor hub are along radial arrangement;And permanent magnet and rotor core, set on the outer end of the outer ring.The blade and the rotor hub are along radial arrangement, thus blade will not occupy additional axial space, the axial dimension of the blade and the integrated blower of internal rotor be accomplished smaller.

Description

Blade and internal rotor integral structure and blade and the integrated blower of internal rotor
Technical field
The utility model relates to blower technical field, in particular to a kind of blade and internal rotor integral structure and blade with The integrated blower of internal rotor.
Background technique
The installation of traditional fan blade needs to install blade in machine shaft, and the axial direction for needing to extend rotor axis of electric is long The installation to realize blade is spent, causes the axial dimension of blower longer, is unsatisfactory for the vehicle-mounted equal small erecting bed of axial bulk It closes, causes conventional fan difficult to install.If fan blade is the requirement for meeting short axial size, need motor fan blade The stator exterior in motor is designed, rotor and fan blade part are carried out by folding connection, blower leaf by special construction Piece needs to wrap up the rotor part of blower motor to meet the requirement of axial small size;By outside the stator of interior rotor blower fan Portion designs a rotor hub cover, and fan blade is integrated in the outside of rotor hub cover, and interior will be turned by special construction Son is connected with rotor hub cover, to realize the purpose for reducing axial dimension.Obviously, this kind of structure only partly reduces axial Size, the part that internal rotor is connected with external rotor hubcap occupy the axial dimension of motor, also, fan blade rotation by Shaft drives, and is fixed rotating shaft, needs the installation in the end cover designs bearing of motor, inevitably increase blower axial direction ruler It is very little.This kind of mode causes motor rotor construction complicated, and in high-power blower application, processing technology difficulty is larger, Wu Faman Foot requires.
Utility model content
The main purpose of the utility model is to propose a kind of blade and internal rotor integral structure and blade and internal rotor one The blower of body, rotor hub and blade are distributed radially completely, thus blade will not occupy additional axial space, so that The axial dimension of the blade and the integrated blower of internal rotor can be accomplished smaller.
To achieve the above object, the utility model proposes a kind of blades and internal rotor integral structure, comprising:
Rotor hub, rotational installation and disk-shaped setting, the rotor hub are provided with hollow-out parts, and the hollow-out parts are along week To setting, the rotor hub is divided into inner ring and outer ring;
Multiple blades, be located at the hollow-out parts in, inner end and the inner ring of each blade are fixed, outer end with it is described Outer ring is fixed, so that the blade and the rotor hub are along radial arrangement;And
Permanent magnet and rotor core, set on the outer end of the outer ring.
Preferably, the multiple blade and the rotor hub are integrally formed.
Preferably, the multiple blade is housed in completely in the hollow-out parts.
Preferably, the rotor core is arranged in a ring and fixing sleeve is set to the periphery of the outer ring, the rotor core Equipped with along multiple mounting grooves axially through setting:
The multiple permanent magnet is set as multiple and correspondence is installed on the multiple mounting groove;
The two side ends of the rotor core are respectively equipped with pressing ring, and two pressing rings carry out the multiple permanent magnet axial Limit.
Preferably, the blade and internal rotor integral structure further include further include multiple studs, it is the multiple double Header stud correspondence is connect with the multiple permanent magnet, and is extended from the both ends of the multiple permanent magnet, and with described two pressures Circle connection.
Preferably, the outer ring outer peripheral surface and annular stop platform, the circumferential surface of the annular stop platform are convexly equipped with close to one end Multiple first installation bases are equipped with, each installation base is equipped with the first mounting hole;
The position of the outer ring outer peripheral surface and the close other end is sheathed on a rotor spacing collar, the week of the rotor spacing collar Face is equipped with multiple the second installation bases corresponding with first installation base, and each second installation base is equipped with the Two mounting holes, by passing through second mounting hole between the multiple second installation base and the multiple first installation base It is fixedly mounted with the spiro connecting piece of first mounting hole;
The rotor core and described two pressing rings are set between the rotor spacing collar and the annular stop platform, and by The rotor spacing collar and the annular stop platform carry out axial limiting.
Preferably, the blade and internal rotor integral structure further include:
Installation axle, the installation axle is vertically to arrangement, and the lower end of the installation axle is fixing end, to be installed on blade On the lower cover of the integrated blower of internal rotor;
The rotor hub rotational installation is in the installation axle.
Preferably, the rotor hub has the mounting hole being set in the installation axle, is equipped with axis in the mounting hole It holds, the rotor hub is rotatablely installed by the bearing in the installation axle.
Preferably, the installation axle is in overstriking setting from top to bottom.
The utility model also provides a kind of blade and the integrated blower of internal rotor, comprising: blade is integrated with internal rotor Structure, the blade and internal rotor integral structure, comprising:
Rotor hub, rotational installation and disk-shaped setting, the rotor hub are provided with hollow-out parts, and the hollow-out parts are along week To setting, the rotor hub is divided into inner ring and outer ring;
Multiple blades, be located at the hollow-out parts in, inner end and the inner ring of each blade are fixed, outer end with it is described Outer ring is fixed, so that the blade and the rotor hub are along radial arrangement;And
Permanent magnet and rotor core, set on the outer end of the outer ring.
In technical solution provided by the utility model, multiple blades are located in the hollow-out parts of rotor hub, each leaf The inner end of piece and the inner ring of the rotor hub are fixed, and outer end and the outer ring of the rotor hub are fixed, so that the blade With the rotor hub along radial arrangement, thus blade will not occupy additional axial space, so that the blade and interior turn The axial dimension of the integrated blower of son can be accomplished smaller.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor Under, the structure that can also be shown according to these attached drawings obtains other attached drawings.
Fig. 1 is the solid after the cutting of an embodiment of blade provided by the utility model and the integrated blower of internal rotor Schematic diagram;
Fig. 2 is the schematic perspective view of the blade and internal rotor integral structure and lower cover in Fig. 1;
Fig. 3 is blade and internal rotor integral structure perspective exploded view in Fig. 1.
Drawing reference numeral explanation:
The embodiments will be further described with reference to the accompanying drawings for the realization, functional characteristics and advantage of the utility model aim.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describing, it is clear that described embodiment is only a part of the embodiment of the utility model, rather than all Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise Under every other embodiment obtained, fall within the protection scope of the utility model.
It is to be appreciated that if related in the utility model embodiment directionality instruction (such as upper and lower, left and right, it is preceding, Afterwards ...), then directionality instruction is only used for explaining opposite between each component under a certain particular pose (as shown in the picture) Positional relationship, motion conditions etc., if the particular pose changes, directionality instruction is also correspondingly changed correspondingly.
In addition, if relating to the description of " first ", " second " etc. in the utility model embodiment, " first ", " the Two " etc. description is used for description purposes only, and is not understood to indicate or imply its relative importance or is implicitly indicated meaning The quantity of the technical characteristic shown." first " is defined as a result, the feature of " second " can explicitly or implicitly include at least one A this feature.It in addition, the technical solution between each embodiment can be combined with each other, but must be with ordinary skill Based on personnel can be realized, this technical side will be understood that when the combination of technical solution appearance is conflicting or cannot achieve The combination of case is not present, also not within the protection scope of the requires of the utility model.
It please refers to Fig.1 to Fig.3, the utility model also provides a kind of blade and the integrated blower 100 of internal rotor, including outer Stator module 1 and blade and internal rotor integral structure 2, specifically, in the present embodiment, the external stator component 1 is in a ring Setting, the blade and internal rotor integral structure 2 are set to the inside of the external stator component 1, are in the external stator component 1 Internal and external cycle setting.The main improvement of the design is to improve the blade and internal rotor integral structure 2, subsequent knot Fig. 1 to Fig. 3 is closed the blade and internal rotor integral structure 2 is specifically introduced.
The blade and internal rotor integral structure 2 include rotor hub 21, multiple blades 22 and permanent magnet 23 and turn Sub- iron core 24, the rotor hub 21 is rotatablely installed and disk-shaped setting, the rotor hub 21 are provided with hollow-out parts 210, institute It is circumferentially arranged to state hollow-out parts 210, the rotor hub 21 is divided for inner ring 21a and outer ring 21b;22, the multiple blade In in the hollow-out parts 210, inner end and the inner ring 21a of each blade 22 are fixed, and outer end and the outer ring 21b are solid Fixed, so that the blade 22 and the rotor hub 21 are along radial arrangement, the permanent magnet 23 and rotor core 24 are set to The outer end of the outer ring 21b.
In technical solution provided by the utility model, multiple blades 22 are located in the hollow-out parts 210 of rotor hub 21, each The inner end of the blade 22 and the inner ring 21a of the rotor hub 21 are fixed, and the outer ring 21b of outer end and the rotor hub is solid Calmly, so that the blade 22 and the rotor hub 21 are along radial arrangement, thus blade 22 will not occupy additional axial direction Space accomplishes the axial dimension of the blade and the integrated blower 100 of internal rotor smaller.
In order to maximumlly reduce the axial dimension of the blade Yu internal rotor integral structure 2, in the utility model In embodiment, the multiple blade 22 is housed in completely in the hollow-out parts 210, so that the multiple blade 22 does not account for additionally According to the axial dimension of the rotor hub 21.
The multiple blade 22 and the rotor hub 21 are connected as one by the design, for this purpose, in the rotor hub In 21 rotation processes, the rotor hub 21 can be born compared with noticeable effort, which includes axial force and radial force, especially The effect of radial force is so that the rotational stability of the rotor hub 21 is subjected to biggish test, for this purpose, in the utility model In embodiment, the multiple blade 22 and the rotor hub 21 are integrally formed, avoided thus because of the multiple blade 22 Undesirable influence further is caused on the stability of the rotor hub 21 using split settings with the rotor hub 21, when Right the design is without being limited thereto, it is clear that the rotor hub 21 and the multiple blade 22 can also use split settings and group connects It is integrated, then the structure assembled at this time wants firm and mitigates the influence to the stability of the rotor hub 21 as far as possible.
The permanent magnet 23 and rotor core 24 are set to the outer end of the outer ring 21b, specific mounting means with no restrictions, In the embodiments of the present invention, the rotor core 24 is arranged in a ring and fixing sleeve is set to the periphery of the outer ring 21b, The rotor core 24 is equipped with along multiple mounting grooves axially through setting, and the permanent magnet 23 is set as multiple and corresponding installation In the multiple mounting groove, the two side ends of the rotor core 24 are respectively equipped with pressing ring 25, and two pressing rings 25 are to described Multiple permanent magnets 23 carry out axial limiting.Pacified by the way that the multiple mounting groove axially opened up is arranged for the multiple permanent magnet 23 Dress mainly considers the multiple permanent magnet 23 and is easy abjection radially, and by the side wall of the mounting groove to described more A permanent magnet 23 is limited, and carries out axial limiting to the multiple permanent magnet 23 by described two pressing rings 25 simultaneously, and And some structures are set on described two pressing rings 25, to pass through the adjustable rotor hub 21 of described two pressing rings 25 Dynamic balancing.
Further, in the embodiments of the present invention, the blade further includes multiple with internal rotor integral structure 2 Studs 26, the multiple studs 26 correspondence are connect with the multiple permanent magnet 23, and from the multiple permanent magnet 23 Both ends extend, and connect with described two pressing rings 25.The multiple 23 one side of permanent magnet is limited in described more by correspondence In a mounting groove, on the other hand it is connect by the multiple studs 26 correspondence with described two pressing rings 25, for this purpose, described more A permanent magnet 23 in 21 rotation process of rotor hub, on the one hand held by the rotor core 24 by generated radial force Load, is on the other hand undertaken by described two pressing rings 25, so that the stability of the rotor hub 21 is more preferable.
The specific fixed form of the rotor core 24 and outer ring 21b with no restrictions, in the utility model
In embodiment, the outer ring 21b outer peripheral surface and annular stop platform 212, the annular stop are convexly equipped with close to one end The circumferential surface of platform 212 is equipped with multiple first installation bases 213, and each installation base 213 is equipped with the first mounting hole, the outer ring The position of 21b outer peripheral surface and the close other end is sheathed on a rotor spacing collar 27, sets on the outer peripheral surface of the rotor spacing collar 27 There are multiple second installation bases 271 corresponding with first installation base 213, is set on each second installation base 271 There is the second mounting hole, it is described by passing through between the multiple second installation base 271 and the multiple first installation base 213 The spiro connecting piece of second mounting hole and first mounting hole is fixedly mounted, and the rotor core 24 and described two pressing rings 25 are set to Between the rotor spacing collar 27 and the annular stop platform 212, and by the rotor spacing collar 27 and the annular stop platform 212 carry out axial limiting, and keyway arrangements are equipped between the inside of the rotor core 24 and the outer peripheral surface of the outer ring 21b Carry out circumferential limit.
In the embodiments of the present invention, the blade and internal rotor integral structure 2 further include installation axle 28, described For installation axle 28 vertically to arrangement, the lower end of the installation axle 28 is fixing end, integrated with internal rotor to be installed on blade Blower 100 lower cover 3 on;The rotational installation of rotor hub 21 is in the installation axle 28.Under right angle setting environment, lead to The firm installation that the fixed mode in lower end achieves that internal rotor component is crossed, and the lower end of the installation axle 28 is fixedly mounted on The lower cover 3, rather than lower cover 3 is rotatably installed in using installation axle 28, and then be arranged not necessarily at the lower cover 3 Bearing 29 is installed for the installation axle 28, and then lower cover 3 can be set more simple, and lower end is fixed, and upper end suspends, and Unnecessary setting upper end cover.
Further, the rotor hub 21 has the mounting hole that is set in the installation axle 28, in the mounting hole Equipped with bearing 29, the rotor hub 21 is rotatablely installed by the bearing 29 in the installation axle 28.The multiple bearing 29 Additional axial space is prevented take up positioned at the annular gap, so that the blade and the integrated blower 100 of internal rotor can To further decrease.
Also, mounting structure of the installation axle 28 as the internal rotor component, is fixed, the installation axle using lower end single-point 28 can, easier circular runouts poorer further away from lower end supporting point intensity, thus in order to enhance the installation axle 28 intensity and Stability avoids installation axle 28 in the internal rotor component rotation process, radial direction to deform and cause it is described in turn It moves component circular runout and influences stability, the installation axle 28 is set as being set as overstriking setting under, it is of course also possible to It is to set the internal rotor component and 22 at least one of them of the blade to be set as aggravating setting from top to bottom, and make The center of gravity for the rotating member that the internal rotor component and the blade 22 form makes the rotation of rotating member closer to lower supporting point Stability is good.
The above is only the preferred embodiment of the present invention, and therefore it does not limit the scope of the patent of the utility model, Under all utility models in the utility model are conceived, equivalent structure made based on the specification and figures of the utility model Transformation, or directly/be used in other related technical areas indirectly and be included in the scope of patent protection of the utility model.

Claims (10)

1. a kind of blade and internal rotor integral structure characterized by comprising
Rotor hub, is rotatablely installed and disk-shaped setting, the rotor hub are provided with hollow-out parts, and the hollow-out parts are circumferentially set It sets, the rotor hub is divided into inner ring and outer ring;
Multiple blades are located in the hollow-out parts, and inner end and the inner ring of each blade are fixed, outer end and the outer ring It is fixed, so that the blade and the rotor hub are along radial arrangement;And
Permanent magnet and rotor core, set on the outer end of the outer ring.
2. blade as described in claim 1 and internal rotor integral structure, which is characterized in that the multiple blade and described turn Sub- wheel hub is integrally formed.
3. blade as described in claim 1 and internal rotor integral structure, which is characterized in that the multiple blade accommodates completely In the hollow-out parts.
4. blade as described in claim 1 and internal rotor integral structure, which is characterized in that the rotor core is set in a ring It sets and fixing sleeve is set on the periphery of the outer ring, the rotor core is equipped with along multiple mounting grooves axially through setting:
The permanent magnet is set as multiple and correspondence is installed on the multiple mounting groove;
The two side ends of the rotor core are respectively equipped with pressing ring, and two pressing rings carry out axial limit to the multiple permanent magnet Position.
5. blade as claimed in claim 4 and internal rotor integral structure, which is characterized in that it further include multiple studs, The multiple studs correspondence is connect with the multiple permanent magnet, and is extended from the both ends of the multiple permanent magnet, and with Described two pressing ring connections.
6. blade as claimed in claim 5 and internal rotor integral structure, which is characterized in that the outer ring outer peripheral surface and close One end is convexly equipped with annular stop platform, and the circumferential surface of the annular stop platform is equipped with multiple first installation bases, each installation base It is equipped with the first mounting hole;
The outer ring outer peripheral surface and a rotor spacing collar is sheathed on close to the position of the other end, on the circumferential surface of the rotor spacing collar Equipped with multiple the second installation bases corresponding with first installation base, each second installation base is equipped with the second peace Hole is filled, by passing through second mounting hole and institute between the multiple second installation base and the multiple first installation base The spiro connecting piece for stating the first mounting hole is fixedly mounted;
The rotor core and described two pressing rings are set between the rotor spacing collar and the annular stop platform, and described Rotor spacing collar and the annular stop platform carry out axial limiting.
7. blade as claimed in claim 6 and internal rotor integral structure, which is characterized in that further include:
Installation axle, for the installation axle vertically to arrangement, the lower end of the installation axle is fixing end, to be installed on blade with it is interior On the lower cover of the integrated blower of rotor;
The rotor hub rotational installation is in the installation axle.
8. blade as claimed in claim 7 and internal rotor integral structure, which is characterized in that the rotor hub, which has, to be arranged Mounting hole in the installation axle, the mounting hole is interior to be equipped with bearing, and the rotor hub is rotatablely installed by the bearing In the installation axle.
9. blade as claimed in claim 7 and internal rotor integral structure, which is characterized in that the installation axle is in from top to bottom Overstriking setting.
10. a kind of blade and the integrated blower of internal rotor, which is characterized in that including as described in any one of claim 1 to 9 Blade and internal rotor integral structure.
CN201821848071.7U 2018-11-09 2018-11-09 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor Active CN209115394U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821848071.7U CN209115394U (en) 2018-11-09 2018-11-09 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821848071.7U CN209115394U (en) 2018-11-09 2018-11-09 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor

Publications (1)

Publication Number Publication Date
CN209115394U true CN209115394U (en) 2019-07-16

Family

ID=67204501

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821848071.7U Active CN209115394U (en) 2018-11-09 2018-11-09 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor

Country Status (1)

Country Link
CN (1) CN209115394U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109340180A (en) * 2018-11-09 2019-02-15 仪坤动力科技(上海)有限公司 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor
CN112583223A (en) * 2020-12-18 2021-03-30 中北大学 Ducted fan device integrated with permanent magnet synchronous disc type flat wire motor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109340180A (en) * 2018-11-09 2019-02-15 仪坤动力科技(上海)有限公司 Blade and internal rotor integral structure and blade and the integrated blower of internal rotor
CN112583223A (en) * 2020-12-18 2021-03-30 中北大学 Ducted fan device integrated with permanent magnet synchronous disc type flat wire motor
CN112583223B (en) * 2020-12-18 2022-02-08 中北大学 Ducted fan device integrated with permanent magnet synchronous disc type flat wire motor
WO2022126736A1 (en) * 2020-12-18 2022-06-23 中北大学 Ducted fan device integrated with permanent magnet synchronous disc-type flat wire electric motor
US11897623B2 (en) 2020-12-18 2024-02-13 North University Of China Ducted fan device integrated with permanent magnet synchronous disc flat wire motor

Similar Documents

Publication Publication Date Title
CN209115394U (en) Blade and internal rotor integral structure and blade and the integrated blower of internal rotor
CN203707950U (en) Motor with thrust bearing
JP2012087748A (en) Blower fan
CN109340180A (en) Blade and internal rotor integral structure and blade and the integrated blower of internal rotor
CN205429898U (en) Motor, power device and unmanned vehicles
CN109340259A (en) A kind of permanent-magnet suspension bearing bearing radial and axial load
CN102312846A (en) Air Blast fan
CN209414210U (en) A kind of blade and the integrated blower of internal rotor
CN209654265U (en) A kind of mounting structure and blower of blade and internal rotor integral fan
TWI516685B (en) Balanceable fan
CN209414209U (en) Blade and internal rotor integral structure and blower with fixing axle
CN205657532U (en) Motor structure and model aeroplane and model ship aircraft that has this structure
CN109372773A (en) A kind of blade and the integrated blower of internal rotor
CN207134939U (en) Coaxial motor and unmanned vehicle
CN108667247A (en) A kind of bi-motor stacking motor and its cooking machine
CN206712587U (en) Rotor mounting structure and blower fan system
CN109281852A (en) A kind of mounting structure and blower of blade and internal rotor integral fan
CN104393728A (en) Double-stator motor
CN103219810B (en) Motor and motor rotor thereof
CN208401711U (en) A kind of bi-motor stacking motor and its cooking machine
CN109578332A (en) The manufacturing method of wheel portion, impeller, air supply device and air supply device
CN204497938U (en) A kind of external rotor electric machine
CN109209952A (en) Blade and internal rotor integral structure and blower with fixing axle
CN106033917B (en) Inner rotor motor
CN107546910A (en) A kind of balance block structure of automotive electronics cooling water pump motor

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant