CN206683818U - A kind of planet carrier class part dynamic balance running device - Google Patents
A kind of planet carrier class part dynamic balance running device Download PDFInfo
- Publication number
- CN206683818U CN206683818U CN201720429437.6U CN201720429437U CN206683818U CN 206683818 U CN206683818 U CN 206683818U CN 201720429437 U CN201720429437 U CN 201720429437U CN 206683818 U CN206683818 U CN 206683818U
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- China
- Prior art keywords
- mandrel
- ring flange
- taper nut
- rate taper
- planet carrier
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Abstract
The utility model provides a kind of planet carrier class part dynamic balance running device, including mandrel, ring flange and rate taper nut, wherein:Ring flange is fixedly connected on mandrel, and flange side surface is vertical with mandrel axis, and ring flange is coaxial with mandrel;Rate taper nut is connected through a screw thread with mandrel, rate taper nut end face is vertical with mandrel axis, rate taper nut is coaxial with mandrel, with mandrel relative motion can occur for rate taper nut in the axial direction, rate taper nut periphery is the conical surface of the drift angle direction towards ring flange, planet carrier class part is fixed on into the enterprising action balance of mandrel by rate taper nut and ring flange to test, realizes and dynamic balance running is carried out without seam or the planet carrier class part of support for spline and both ends to inside.
Description
Technical field
Field of gears is the utility model is related to, more specifically to a kind of planet carrier class part dynamic balance running device.
Background technology
Planet carrier class part is indispensable part in Gear Planet Transmission, be mainly to connect planetary gear and sun gear, from
And transmit moment of torsion.Machinery rotate in, especially high speed rotate in, due to part material inequality with and blank lack
Fall into, caused error in processing and assembling, or even just there are many factors such as asymmetrical geometry during design, on part
Larger centrifugal intertia force can be produced caused by each small particle, it can not only cause the work of axle, gear member and bearing
Make worsening condition, and the size and Orientation of centrifugal intertia force is all that necessarily periodically variable is presented, when these periodicity
The centrifugal intertia force of change is applied in mechanical system, it is easy to is caused vibrations, is produced noise, accelerates axle, bearing and gear
The abrasion of part, sexual behavior event can be damaged so as to shorten mechanical life, when serious.Therefore, to try to eliminate centrifugal intertia force
The harmful effect to caused by mechanical system, must just dynamic balance running be carried out to this kind of part, reach the balance essence of permission
Grade is spent, or the mechanical oscillation amplitude because caused by is dropped in allowed limits, so as to improve life of product and performance.
It is flat that existing technology can only have seam with screw or the planet carrier class part for having shaft extension to support to enter action to both ends
Weighing apparatus experiment, mainly add flange type servicing unit or direct shaft extension to support positioning using the seam at both ends, be placed on testing stand
Carry out dynamic balance running;If seam or bearing length are too short, corresponding interference fit shaft sleeve is just designed, is placed on testing stand
On with axle sleeve come be positioned into action balance experiment.However, such inside parts is spline, and planet of the both ends without seam or support
For frame, it due to being limited by design of part, can not be arranged on dynamic balance test stand, increase the tired of dynamic balance running
Difficulty, and then have impact on the product duration.
Therefore, how dynamic balance running is carried out without seam or the planet carrier class part of support for spline and both ends to inside,
The problem of becoming those skilled in the art's urgent need to resolve.
Utility model content
In view of this, the purpose of this utility model is to provide planet carrier class part dynamic balance running device, passes through taper
Planet carrier class part is fixed on the enterprising action balance of mandrel and tested by nut and ring flange, and it is spline and both ends to realize to inside
Dynamic balance running is carried out without seam or the planet carrier class part of support.
To achieve the above object, the utility model provides following technical scheme:
A kind of planet carrier class part dynamic balance running device, it is characterised in that including mandrel, ring flange and rate taper nut,
Wherein:
The ring flange is fixedly connected on the mandrel;
The rate taper nut is connected through a screw thread with the mandrel, and the rate taper nut periphery is drift angle direction towards institute
State the conical surface of ring flange.
Preferably, the ring flange is boss and convex surface facing the rate taper nut, and the first rate taper nut external diameter is more than the
One flange external diameter, the first rate taper nut external diameter be the rate taper nut conical surface maximum outside diameter, the first flange dish external diameter
For the external diameter on the less face of cylinder of the ring flange.
Preferably, there are several mounting holes the rate taper nut end face.
Preferably, the mounting hole is screwed hole.
Preferably, the ring flange is welded on the mandrel.
Preferably, the mandrel welds the step cutting pattern for being more than both sides at the ring flange for external diameter, and step width etc.
In the ring flange both ends of the surface distance.
It can be seen from the above technical proposal that the utility model provides a kind of planet carrier class part dynamic balance running dress
Put, including mandrel, ring flange and rate taper nut, wherein:Ring flange is fixedly connected on mandrel, flange side surface and mandrel axis
Vertically, ring flange and mandrel are coaxial;Rate taper nut is connected through a screw thread with mandrel, and rate taper nut end face is vertical with mandrel axis,
Rate taper nut is coaxial with mandrel, and relative motion can occur with mandrel in the axial direction for rate taper nut, and rate taper nut periphery is top
Planet carrier class part is fixed on the enterprising action of mandrel by rate taper nut and ring flange and put down by angular direction towards the conical surface of ring flange
Weighing apparatus experiment, realize and dynamic balance running is carried out without seam or the planet carrier class part of support for spline and both ends to inside.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only
It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is a kind of specific knot of the embodiment 1 of planet carrier class part dynamic balance running device disclosed in the utility model
Structure schematic diagram;
Fig. 2 is the tool of mandrel and ring flange in a kind of planet carrier class part dynamic balance running device disclosed in the utility model
Body structure chart;
Fig. 3 is the specific knot of rate taper nut in a kind of planet carrier class part dynamic balance running device disclosed in the utility model
Composition.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The all other embodiment obtained, belong to the scope of the utility model protection.
It is a kind of tool of the embodiment 1 of the dynamic balance running device of planet carrier class part 4 disclosed in the utility model such as Fig. 1
Body structural representation, the present apparatus include mandrel 1, ring flange 2 and rate taper nut 3, wherein:
Ring flange 2 is fixedly connected on mandrel 1, and the end face of ring flange 2 is vertical with the axis of mandrel 1, and ring flange 2 and mandrel 1 are same
Axle.
Rate taper nut 3 is connected through a screw thread with mandrel 1, and the end face of rate taper nut 3 is vertical with the axis of mandrel 1, rate taper nut 3 with
Mandrel 1 is coaxial, and with mandrel 1 relative motion can occur for rate taper nut 3 in the axial direction, and the periphery of rate taper nut 3 is drift angle direction
Towards the conical surface of ring flange 2, the maximum outside diameter of rate taper nut 3 is more than the inner spline gear outside diameter circle of planet carrier class part 4, taper spiral shell
Mother 3 uses less taper, and can increase the inner spline gear tip circle of planet carrier class part 4 has the contact area of the conical surface, fixes part
Obtain more firm.To ensure the coaxial requirement of rate taper nut 3 and mandrel 1, positioning precision, the conical surface and core of rate taper nut 3 are improved
Axle 1 is Combined machining.
The distance of first end face of mandrel and the second end face of mandrel be more than first flange side surface and the second end face of mandrel away from
From the first end face of mandrel is the end face of the side of 1 mounting flange of mandrel 2, and the second end face of mandrel is that mandrel 1 connects conic nut one
The end face of side, first flange side surface are end face in small distance with the first end face of mandrel on ring flange.
The distance of second end face of mandrel and the first end face of mandrel is more than the first rate taper nut end face and the first end face of mandrel
Distance, the first rate taper nut end face are end face in small distance with the second end face of mandrel on rate taper nut 3.
In summary, a kind of dynamic balance running device of planet carrier class part 4 is present embodiments provided, to planet carrier class zero
When part 4 carries out dynamic balance running, planet carrier class part 4 rotates rate taper nut 3, made between ring flange 2 and rate taper nut 3
Rate taper nut 3 moves relative to mandrel 1 to ring flange 2, because the maximum outside diameter of rate taper nut 3 is more than flower in planet carrier class part 4
Key teeth outside diameter circle, final rate taper nut 3 are tightly fitted on ring flange 2.Because rate taper nut 3 and mandrel 1 are coaxial, and ring flange
2 end faces have that the axis of mandrel 1 is vertical, so planet carrier class part 4 is also coaxial with mandrel 1, mandrel 1 can be arranged on testing stand,
It is achieved thereby that dynamic balance running is carried out without seam or the planet carrier class part 4 of support for spline and both ends to inside.
For further optimization this programme, ring flange 2 is boss and convex surface facing rate taper nut 3, the first rate taper nut external diameter
More than first flange dish external diameter, the first rate taper nut external diameter is the maximum outside diameter of the conical surface of rate taper nut 3, and first flange dish external diameter is
The external diameter on the 2 less face of cylinder of ring flange.First flange dish external diameter is that the less gap in gap coordinates with inner spline gear tip circle, such as
H8/h8.It is easy when carrying out dynamic balance running because rate taper nut 3 and the contact area of the internal splines of planet carrier class part 4 are smaller
Circular runout is produced, the ring flange 2 of boss structure can be such that the boss structure of ring flange 2 inserts in planet carrier class part 4, because coordinating
Gap is small, thus when can reduce experiment part circular runout.
There are several mounting holes for further optimization this programme, the end face of rate taper nut 3, mounting hole can be through hole or blind hole,
If mounting hole is blind hole, blind hole is on the end face of the first rate taper nut 3.Rod-like piece can be inserted in mounting hole, be easy to rotate
Rate taper nut 3.Mounting hole can use screwed hole, in screwed rod-like piece advances through hole, will can make in rotation rate taper nut 3
When, rod-like piece does not skid off from hole.
It is welded on for further optimization this programme, ring flange 2 on mandrel 1.Ring flange 2 is fixed on by the way of welding
On mandrel 1, compared with other connected modes, it can eliminate and be shaken caused by gap.And use a process processing method after welding
Blue disk 2 and mandrel 1 it is cylindrical, can both reduce the cylindrical bounce of seam, and ensure that hanging down for the end face of ring flange 2 and the axis of mandrel 1
Straight degree.
Further to optimize this programme, it is more than the step cutting pattern of both sides, and step at the welding flange 2 of mandrel 1 for external diameter
Width is equal to the both ends of the surface distance of ring flange 2.Step cutting pattern is the welding position of ring flange 2, the positioning being easy in welding process.
And deformation of the mandrel 1 because of welding generation can also be reduced using this structure.
In summary, the dynamic balance running device of planet carrier class part 4 that the present embodiment provides has the following advantages:(1) pass through
Planet carrier class part 4 is fixed on 1 enterprising action balance of mandrel and tested by rate taper nut 3 and ring flange 2, and it is flower to realize to inside
Key and both ends carry out dynamic balance running without seam or the planet carrier class part 4 of support.(2) rate taper nut 3 uses less taper,
Increasing the inner spline gear tip circle of planet carrier class part 4 has the contact area of the conical surface, part is fixed more firm.(3) taper spiral shell
The conical surface of mother 3 and the Combined machining of mandrel 1, ensure that the coaxial requirement of rate taper nut 3 and mandrel 1, improve positioning precision.(4)
The ring flange 2 of boss structure can be such that the boss structure of ring flange 2 inserts in planet carrier class part 4, because fit clearance is small, so can
The circular runout of part when reducing experiment.(5) mounting hole uses screwed hole, can by screwed rod-like piece advances through hole
When being easy to rotate rate taper nut 3, and rotating rate taper nut 3, rod-like piece does not skid off from hole.(6) will by the way of welding
Ring flange 2 is fixed on mandrel 1, compared with other connected modes, can be eliminated and be shaken caused by gap.And one is used after welding
Individual process processing ring flange 2 and mandrel 1 it is cylindrical, can both reduce the cylindrical bounce of seam, and ensure that the end face of ring flange 2 and core
The perpendicularity of the axis of axle 1.(7) multi-diameter shaft is used, is easy to the positioning of welding, and reduces the thermal deformation of mandrel 1 in welding process.
Each embodiment is described by the way of progressive in this specification, what each embodiment stressed be with it is other
The difference of embodiment, between each embodiment identical similar portion mutually referring to.
The foregoing description of the disclosed embodiments, professional and technical personnel in the field are enable to realize or new using this practicality
Type.A variety of modifications to these embodiments will be apparent for those skilled in the art, determine herein
The General Principle of justice can be realized in other embodiments in the case where not departing from spirit or scope of the present utility model.Cause
This, the utility model is not intended to be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The most wide scope consistent with features of novelty.
Claims (6)
- A kind of 1. planet carrier class part dynamic balance running device, it is characterised in that including mandrel, ring flange and rate taper nut, its In:The ring flange is fixedly connected on the mandrel;The rate taper nut is connected through a screw thread with the mandrel, and the rate taper nut periphery is drift angle direction towards the method The conical surface of blue disk.
- 2. device as claimed in claim 1, it is characterised in that the ring flange is boss and convex surface facing the taper spiral shell Mother, the first rate taper nut external diameter are more than first flange dish external diameter, the first rate taper nut external diameter be the rate taper nut conical surface most Big external diameter, the first flange dish external diameter are the external diameter on the less face of cylinder of the ring flange.
- 3. device as claimed in claim 2, it is characterised in that there are several mounting holes the rate taper nut end face.
- 4. device as claimed in claim 3, it is characterised in that the mounting hole is screwed hole.
- 5. device as claimed in claim 4, it is characterised in that the ring flange is welded on the mandrel.
- 6. device as claimed in claim 5, it is characterised in that the mandrel welds is more than both sides at the ring flange for external diameter Step cutting pattern, and step width is equal to the ring flange both ends of the surface distance.
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CN201720429437.6U CN206683818U (en) | 2017-04-21 | 2017-04-21 | A kind of planet carrier class part dynamic balance running device |
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CN201720429437.6U CN206683818U (en) | 2017-04-21 | 2017-04-21 | A kind of planet carrier class part dynamic balance running device |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108036896A (en) * | 2017-12-26 | 2018-05-15 | 沈阳透平机械股份有限公司 | Wind tunnel compressor rotor hub balanced controls and wheel hub balance method |
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2017
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108036896A (en) * | 2017-12-26 | 2018-05-15 | 沈阳透平机械股份有限公司 | Wind tunnel compressor rotor hub balanced controls and wheel hub balance method |
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