CN113236755B - Planet carrier installation method, planetary reducer fluctuation compensation method and planetary reducer - Google Patents

Planet carrier installation method, planetary reducer fluctuation compensation method and planetary reducer Download PDF

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CN113236755B
CN113236755B CN202110786003.2A CN202110786003A CN113236755B CN 113236755 B CN113236755 B CN 113236755B CN 202110786003 A CN202110786003 A CN 202110786003A CN 113236755 B CN113236755 B CN 113236755B
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bearing
ring
planet carrier
ring body
buffer ring
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CN113236755A (en
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郝鸣
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Jiangsu Guomao Reducer Group Co ltd
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Jiangsu Guomao Reducer Group Co ltd
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/08—General details of gearing of gearings with members having orbital motion
    • F16H57/082—Planet carriers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/06—Elastic or yielding bearings or bearing supports, for exclusively rotary movement by means of parts of rubber or like materials
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/0006—Vibration-damping or noise reducing means specially adapted for gearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H57/023—Mounting or installation of gears or shafts in the gearboxes, e.g. methods or means for assembly
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/0006—Vibration-damping or noise reducing means specially adapted for gearings
    • F16H2057/0012—Vibration-damping or noise reducing means specially adapted for gearings for reducing drive line oscillations
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/08—General details of gearing of gearings with members having orbital motion
    • F16H2057/085—Bearings for orbital gears

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Retarders (AREA)

Abstract

The invention relates to the technical field of speed reducers, in particular to a planet carrier installation method, which comprises a first bearing, wherein the first bearing is coaxially arranged with a planet carrier, an inner ring of the first bearing is attached to a cylindrical peripheral section on the planet carrier, an outer ring of the first bearing is attached to a cylindrical inner section on an inner gear, and the inner gear is meshed with a planet gear corresponding to the planet carrier. According to the invention, the planet carrier is limited, so that the operation stability between the planet wheel and the inner gear is improved. Meanwhile, the invention also discloses a planetary reducer fluctuation compensation method and a planetary reducer, which adopt the planet carrier installation method and have the same technical effect.

Description

Planet carrier installation method, planetary reducer fluctuation compensation method and planetary reducer
Technical Field
The invention relates to the technical field of speed reducers, in particular to a planet carrier installation method, a planet reducer fluctuation compensation method and a planet reducer.
Background
The planetary reducer has the characteristics of large transmission ratio, large bearing capacity, high efficiency, stable operation and the like, and is widely applied to the fields of metallurgy, mines, hoisting and transportation, electric power, energy, building materials, light industry, traffic and the like.
Aiming at the existing planetary reducer, in order to improve the motion stability of a planetary gear, the machining precision of the planetary gear and an internal gear meshed with the planetary gear is improved, so that the machining process is controlled more strictly, or a more excellent installation process is provided, so that the installation of each part of the planetary reducer is more stable and controllable; by the adoption of the mode, operation fluctuation in the working process of the planetary speed reducer is reduced, so that noise is reduced, and the operation stability of the planetary speed reducer is improved.
However, in the actual production process, the improvement difficulty of the machining process and the installation process is high, and after the effect reaches a certain degree, further optimization is difficult to realize, so that the performance of the planetary reducer is improved to reach the bottleneck.
In view of the above problems, the present designer is actively making research and innovation based on the practical experience and professional knowledge that is rich over many years in engineering application of such products, so as to create a planet carrier installation method, a planetary reducer fluctuation compensation method and a planetary reducer, so that the planetary reducer has higher practicability.
Disclosure of Invention
The invention provides a planet carrier installation method, so as to solve the requirement of improving the performance of the planetary reduction in the background technology, and the invention also requests to protect a planetary reducer fluctuation compensation method and a planetary reducer, and has the same technical effect.
In order to achieve the purpose, the invention adopts the technical scheme that:
the planet carrier installation method comprises the following steps:
set up first bearing, first bearing and the coaxial setting of planet carrier, just first bearing inner circle with the laminating of cylindric peripheral section on the planet carrier, the laminating of cylindric inside section on first bearing outer lane and the internal gear, the internal gear with the planet wheel meshing that the planet carrier corresponds.
Furthermore, the first bearing and the internal gear are fixed in a clearance fit mode, an elastic buffer ring is arranged, the elastic buffer ring surrounds the periphery of the first bearing, is attached to the outer side of the first bearing, and is arranged in a first mounting groove formed in the internal gear in a pressed state.
Furthermore, the elastic buffer ring is set to be a combined structure of an inner buffer ring and an outer buffer ring;
the inner buffer ring comprises a hollow cylindrical inner ring body and a plurality of annular convex edges arranged on the outer side of the inner ring body, the annular convex edges are arranged in parallel along the axial direction of the inner ring body, and two sides of the inner ring body and the side wall of the first mounting groove are arranged at intervals;
the outer buffer ring comprises a hollow cylindrical outer ring body and support ring bodies protruding from two edges of the inner side of the outer ring body, and the two support ring bodies are symmetrically arranged;
the support ring body comprises a side surface and an abutting surface;
the side surface and the side wall of the first mounting groove are arranged at intervals, and the outer ring body retracts inwards relative to the side surface;
the binding surface is connected with the side surface, is a curved surface and is bound with the inner ring body;
each annular convex edge is positioned between the two support ring bodies, the annular convex edges and the outer ring body are arranged at intervals before the first bearing is installed and works, the interval distance is smaller than the gap distance between the first bearing and the inner gear, and the outer buffer ring is in a pressed state under the extrusion of the inner buffer ring on the support ring bodies.
Further, the clearance between the first bearing and the internal gear is controlled to be 0.05-0.3 mm.
The planetary reducer fluctuation compensation method comprises the following steps:
arranging a first bearing and an elastic buffer ring;
the first bearing is coaxially arranged with the planet carrier, the inner ring of the first bearing is attached to the cylindrical peripheral section on the planet carrier, the outer ring of the first bearing is attached to the cylindrical inner section on the inner gear, and the inner gear is meshed with the planet gear corresponding to the planet carrier;
the elastic buffer ring is attached to the outer side of a second bearing used for supporting the end part of the shaft body and is arranged in a second mounting groove arranged on a fixing structure for mounting the second bearing, and the shaft body indirectly outputs power for the rotation of the planet carrier;
and the second bearing is fixed with the fixed structure in a clearance fit mode.
Furthermore, the elastic buffer ring is set to be a combined structure of an inner buffer ring and an outer buffer ring;
the inner buffer ring comprises a hollow cylindrical inner ring body and a plurality of annular convex edges arranged on the outer side of the inner ring body, the annular convex edges are arranged in parallel along the axial direction of the inner ring body, and two sides of the inner ring body and the side wall of the second mounting groove are arranged at intervals;
the outer buffer ring comprises a hollow cylindrical outer ring body and support ring bodies protruding from two edges of the inner side of the outer ring body, and the two support ring bodies are symmetrically arranged;
the support ring body comprises a side surface and an abutting surface;
the side surface and the side wall of the second mounting groove are arranged at intervals, and the outer ring body retracts inwards relative to the side surface;
the binding surface is connected with the side surface, is a curved surface and is bound with the inner ring body;
each annular convex edge is positioned between the two support ring bodies, the annular convex edges and the outer ring body are arranged at intervals before the second bearing is installed and works, the interval distance is smaller than the gap distance between the second bearing and the fixed structure, and the outer buffer ring is in a compressed state under the extrusion of the inner buffer ring to the support ring bodies.
Further, a second elastic buffer ring is arranged;
the second elastic buffer ring is arranged around the periphery of the first bearing, attached to the outer side of the first bearing and arranged in a first mounting groove formed in the inner gear in a pressed state.
The planet carrier installation method is adopted to install the planet carrier.
The planet carrier is mounted on the planet carrier by adopting the planet carrier mounting method.
The planetary reducer adopts the planetary reducer fluctuation compensation method to mount the planet carrier and the shaft body.
The invention has the advantages that
According to the invention, the planet carrier is limited, so that the operation stability between the planet wheel and the inner gear is improved. Meanwhile, the invention also discloses a planet speed reducer fluctuation compensation method, and by adopting the planet carrier installation method, on the basis of alleviating the fluctuation transmitted to the outside by the planet carrier, the original installation mode of the second bearing at the end part of the shaft body is changed, the second bearing can be radially buffered by the arrangement of the elastic buffer ring, the planet carrier is limited from the outside, the compensation allowance is provided for the end part of the shaft body from the inside, and the running stability of the speed reducer is greatly improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments described in the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a schematic view of a first bearing according to an embodiment;
FIG. 2 is a schematic view of the second embodiment with an additional elastic buffer ring;
FIG. 3 is a partial enlarged view of the first mounting groove;
FIG. 4 is a cross-sectional and partially enlarged view of the elastomeric damping ring;
FIG. 5 is a partial cross-sectional view of the inner damping ring;
FIG. 6 is a partial cross-sectional view of the outer cushion ring;
FIG. 7 is a schematic view (including a partial enlargement) of the installation of the resilient bumper ring relative to the first mounting groove;
FIG. 8 is a schematic view (including partial enlargement) of the axial displacement of the inner damping ring relative to the outer damping ring;
FIG. 9 is a schematic view showing an arrangement of a first bearing and an elastic buffer ring according to a third embodiment;
FIG. 10 is an enlarged view of the top of FIG. 9;
FIG. 11 is a schematic view illustrating the mounting of the shaft and the fixing structure;
FIG. 12 is a partial enlarged view of the fixing structure and the first mounting groove;
FIG. 13 is a schematic view showing an arrangement of a first bearing and an elastic buffer ring according to a fourth embodiment;
FIG. 14 is a schematic view showing an arrangement of a first bearing and two elastic buffer rings according to a fifth embodiment;
reference numerals: 1. a first bearing; 2. a planet carrier; 3. an internal gear; 31. a first mounting groove; 4. a planet wheel; 5. a shaft body; 6. an elastic buffer ring; 61. an inner buffer ring; 61a, an inner ring body; 61b, an annular convex edge; 62. an outer cushion ring; 62a, an outer ring body; 62b, a support ring body; 62b1, side; 62b2, a joint surface; 7. a second bearing; 8. a fixed structure; 81. and a second mounting groove.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only and do not represent the only embodiments.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Example one
As shown in fig. 1, in the method for mounting the planet carrier 2, a first bearing 1 is provided, the first bearing 1 and the planet carrier 2 are coaxially arranged, an inner ring of the first bearing 1 is attached to a cylindrical peripheral section on the planet carrier 2, an outer ring of the first bearing 1 is attached to a cylindrical inner section on the inner gear 3, and the inner gear 3 is engaged with the planet gear 4 corresponding to the planet carrier 2.
In this embodiment, provide one kind through restricting planet carrier 2 to improve the mode of operating stability between planet wheel 4 and the internal gear 3, through the implementation of above-mentioned mode, aim at reduces the processing and the installation degree of difficulty of planet wheel 4 and internal gear 3, thereby reduces the manufacturing cost of product on the one hand, improves the stability of planetary reducer operation simultaneously.
Example two
The method for installing the planet carrier 2 comprises the steps of arranging the first bearing 1, wherein the first bearing 1 and the planet carrier 2 are coaxially arranged, an inner ring of the first bearing 1 is attached to a cylindrical peripheral section on the planet carrier 2, an outer ring of the first bearing 1 is attached to a cylindrical inner section on the inner gear 3, and the inner gear 3 is meshed with a planet gear 4 corresponding to the planet carrier 2. The contents of this portion are the same as those of the first embodiment, and the technical effects are not described herein again.
As shown in fig. 2 and 3, on the basis of the above structure, the first bearing 1 and the internal gear 3 are fixed by clearance fit, and an elastic buffer ring 6 is provided, wherein the elastic buffer ring 6 is disposed around the periphery of the first bearing 1, attached to the outer side of the first bearing 1, and disposed in a first mounting groove 31 disposed on the internal gear 3 in a pressed state.
The bearing is fixed in a relatively conventional mode through an interference fit mode, a standard size table is provided for the installation of the bearing, but in the invention, the planet carrier 2 is different from parts such as shafts and the like which are conventionally supported by the bearing, so for the installation requirement of the first bearing 1, a new mode is provided in the embodiment, namely, the elastic buffer ring 6 is added, and through the arrangement of the elastic buffer ring 6, when the operation of the first bearing 1 fluctuates, the vibration and the like caused by the fluctuation can be alleviated through the buffer effect of the elastic buffer ring 6 in a pressed state, so that the operation stability of the planetary reducer is improved.
As a preferable mode of the second embodiment, as shown in fig. 4 to 6, the elastic buffer ring 6 is provided as a combined structure of an inner buffer ring 61 and an outer buffer ring 62; the inner buffer ring 61 comprises a hollow cylindrical inner ring body 61a and a plurality of annular convex edges 61b arranged on the outer side of the inner ring body 61a, the annular convex edges 61b are arranged in parallel along the axial direction of the inner ring body 61a, and two sides of the inner ring body 61a are arranged at intervals with the side wall of the first mounting groove 31; the outer buffer ring 62 comprises an outer ring body 62a in a hollow cylindrical shape and support ring bodies 62b protruding from two edges of the inner side of the outer ring body 62a, and the two support ring bodies 62b are symmetrically arranged; the support ring body 62b includes a side surface 62b1 and an abutment surface 62b 2; the side surface 62b1 is spaced apart from the side wall of the first mounting groove 31, and the outer ring body 62a is retracted inward relative to the side surface 62b 1; the abutting surface 62b2 is connected to the side surface 62b1, and the abutting surface 62b2 is a curved surface and is abutted against the inner ring 61 a.
Each annular protruding edge 61b is located between the two support ring bodies 62b, and before the first bearing 1 is installed and works, the annular protruding edges 61b and the outer ring body 62a are arranged at intervals, the interval distance is smaller than the gap distance between the first bearing 1 and the inner gear 3, and the outer buffer ring 62 is pressed by the inner buffer ring 61 under the extrusion of the support ring bodies 62 b.
As shown in fig. 7, in the state shown in the figure, the first bearing 1 is not operated yet, and therefore, the deviation of the installation position occurs without being affected by the operation of the speed reducer, and a predetermined gap exists between the first bearing 1 and the internal gear 3, and the gap is generated by the clearance fit between the first bearing 1 and the internal gear 3, wherein the range of the gap is preferably controlled to be 0.05 to 0.3mm, so that the fluctuation which may occur in the first bearing 1 is effectively controlled, the gap is filled by the inner ring 61a, the inner ring 61a and the bearing are tightly attached by the elastic force generated by the outer cushion ring 62, and the edge of the inner ring 61a is also properly pressed at this time.
In the above preferred solution, the fluctuation generated when the planet carrier 2 drives the first bearing 1 is buffered by two stages:
primary buffering: for the buffering of the non-laminated small range of the first bearing 1 and the inner gear 3, the buffering is mainly realized by the deformation of the outer buffering ring 62 concentrated on the supporting ring bodies 62b at the two sides and the deformation of the inner buffering ring 61 concentrated on the edges at the two sides, the fluctuation of the first bearing 1 is alleviated by the deformation, thereby improving the stability of the operation, under the condition of stable product quality, the probability of the micro fluctuation of the first bearing 1 is higher, therefore, the high-frequency buffering with more sensitivity can be realized by the small range concentration of the deformation, the two sides of the inner ring 61a and the side wall of the first installation groove 31 are arranged at intervals, and the side surface 62b1 of the supporting ring body 62b and the side wall of the first installation groove 31 are arranged at intervals to reduce the friction force, so that the sensitivity is ensured.
Of course, the annular flange 61b and the inner ring 61a are relatively pressed during the damping process, but since there is no initial pressing therebetween, the force for supporting the first bearing 1 generated during the wave motion is negligible.
Secondary buffering: the purpose of buffering in a large range when the first bearing 1 collides with the internal gear 3 is to alleviate the hard impact between the first bearing 1 and the internal gear 3, and the purpose is realized by large deformation extrusion between each annular convex edge 61b and the outer ring body 62a, and the two-stage buffering mode is matched with the buffering mode in the one-stage buffering, so that the collision between the first bearing 1 and the internal gear 3 is flexible, the noise generation and the large fluctuation of the structure are effectively reduced, and the fluctuation generation probability is small, so that even though the deformation recovery sensitivity of multiple parts is low, the one-stage buffering is not greatly influenced.
In the secondary damping process, in addition to the radial fluctuation, the axial fluctuation inevitably occurs due to the large vibration, and in the above embodiment, the buffer of the first bearing 1 in the axial direction can also be achieved simultaneously by the annular flanges 61b being arranged at intervals from the two support ring bodies 62b, with the roots fixed and the ends free, as shown in fig. 8, the axial damping may be provided by play of the inner ring 61a relative to the outer damping ring 62, and the slight bending of the annular convex edge 61b, the invention selects the separately arranged inner and outer buffer rings, so that in the axial buffer process, the influence of the structural stability of the radial damping is reduced because of the change in the relative position of the two in this direction, i.e. excessive changes in shape in one direction caused by the material being stretched in the other direction are avoided.
EXAMPLE III
As shown in fig. 9 to 12, the method for compensating for the fluctuation of the planetary reducer comprises the following steps: arranging a first bearing 1 and an elastic buffer ring 6; the first bearing 1 and the planet carrier 2 are coaxially arranged, the inner ring of the first bearing 1 is attached to the cylindrical peripheral section on the planet carrier 2, the outer ring of the first bearing 1 is attached to the cylindrical inner section on the inner gear 3, and the inner gear 3 is meshed with the planet gear 4 corresponding to the planet carrier 2; the elastic buffer ring 6 is attached to the outer side of the second bearing 7 for supporting the end part of the shaft body 5, and is arranged in a second mounting groove 81 arranged on a fixed structure 8 for mounting the second bearing 7, and the shaft body 5 indirectly outputs power for the rotation of the planet carrier 2; wherein, the second bearing 7 is fixed with the fixed structure 8 by clearance fit.
In the present embodiment, the method for mounting the planet carrier 2 in the first embodiment is adopted, but this method only alleviates the fluctuation transmitted to the outside of the planet carrier 2, and the fluctuation is necessarily transmitted to the axial direction, so that the fluctuation may be brought to the relative position relationship between the planet wheel 4 and the shaft body 5, in order to solve the above problem, the planetary reducer is further optimized in the present embodiment, the original mounting method of the second bearing 7 at the end of the shaft body 5 is changed, and the second bearing 7 can be buffered in the radial direction through the arrangement of the elastic buffer ring 6. In this embodiment, the planet carrier 2 is limited from the outside, and the compensation allowance is provided for the end part of the shaft body 5 from the inside, so that the running stability of the speed reducer is greatly improved.
As a preference of the present embodiment, the elastic buffer ring 6 is provided as a combined structure of the inner buffer ring 61 and the outer buffer ring 62; the inner buffer ring 61 comprises a hollow cylindrical inner ring body 61a and a plurality of annular convex edges 61b arranged on the outer side of the inner ring body 61a, the annular convex edges 61b are arranged in parallel along the axial direction of the inner ring body 61a, and two sides of the inner ring body 61a and the side wall of the second mounting groove 81 are arranged at intervals; the outer buffer ring 62 comprises an outer ring body 62a in a hollow cylindrical shape and support ring bodies 62b protruding from two edges of the inner side of the outer ring body 62a, and the two support ring bodies 62b are symmetrically arranged; the support ring body 62b includes a side surface 62b1 and an abutment surface 62b 2; the side surface 62b1 is spaced apart from the side wall of the second mounting groove 81, and the outer ring body 62a is inwardly retracted relative to the side surface 62b 1; the abutting surface 62b2 is connected to the side surface 62b1, and the abutting surface 62b2 is a curved surface and is abutted against the inner ring 61 a.
Each annular protruding edge 61b is located between the two support ring bodies 62b, and before the second bearing 7 is installed and works, the annular protruding edges 61b and the outer ring body 62a are arranged at intervals, the interval distance is smaller than the gap distance between the second bearing 7 and the fixed structure 8, and the outer buffer ring 62 is in a compressed state under the extrusion of the inner buffer ring 61 on the support ring bodies 62 b.
The working mode of the elastic buffer ring 6 in the preferred embodiment can be described in the second embodiment, and is not described herein again.
Example four
As shown in fig. 13, the planetary reducer ripple compensating method adopts the method of mounting the carrier 2 according to the second embodiment.
In this embodiment, the radial direction of the planet carrier 2 is limited to a certain extent, and on this basis, the elastic buffer ring 6 is provided to provide a compensation margin, so that the speed reducer fluctuates in a more flexible manner within a controlled reasonable range, and the running stability of the speed reducer is greatly improved.
EXAMPLE five
As shown in fig. 14, in the planetary reducer fluctuation compensation method, a second elastic buffer ring 6 is provided on the basis of the third embodiment; the second elastic buffer ring 6 is disposed around the periphery of the first bearing 1, attached to the outer side of the first bearing 1, and disposed in a first mounting groove 31 formed in the inner gear 3 in a pressed state.
In the embodiment, the advantages of the third embodiment and the fourth embodiment are combined, but in this way, the range of the two clearance fits is preferably controlled to be 0.05-0.15 mm, so that the shaft body 5 is prevented from generating excessive disturbance.
EXAMPLE six
The planet carrier 2 is mounted on the planet carrier of the first embodiment or the second embodiment by the planet carrier mounting method.
EXAMPLE seven
The planetary reduction gear adopts the planetary reduction gear fluctuation compensation method in the third or fifth embodiment to mount the carrier 2 and the shaft body 5.
It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1.行星架安装方法，其特征在于：1. The planet carrier installation method is characterized in that: 设置第一轴承，所述第一轴承与所述行星架同轴设置，且所述第一轴承内圈与所述行星架上的圆柱状的外围段贴合，所述第一轴承外圈与内齿轮上圆柱状的内侧段贴合，所述内齿轮与所述行星架对应的行星轮啮合；A first bearing is arranged, the first bearing is arranged coaxially with the planet carrier, the inner ring of the first bearing is fitted with the cylindrical peripheral section on the planet carrier, and the outer ring of the first bearing is The cylindrical inner section of the internal gear is fitted, and the internal gear meshes with the planet gear corresponding to the planet carrier; 令所述第一轴承与所述内齿轮之间通过间隙配合的方式固定，并设置弹性缓冲环，所述弹性缓冲环围绕所述第一轴承外围设置，并与所述第一轴承外侧贴合，且成受压状态设置于所述内齿轮上所设置的第一安装槽内；The first bearing and the internal gear are fixed by means of clearance fit, and an elastic buffer ring is arranged. The elastic buffer ring is arranged around the periphery of the first bearing and fits with the outside of the first bearing. , and is placed in the first installation groove set on the internal gear in a pressurized state; 将所述弹性缓冲环设置为内缓冲环和外缓冲环的组合结构；Setting the elastic buffer ring as a combined structure of an inner buffer ring and an outer buffer ring; 所述内缓冲环包括空心圆柱体状的内环体，以及设置于所述内环体外侧的若干环状凸沿，各所述环状凸沿沿所述内环体的轴线方向并列设置，所述内环体两侧与所述第一安装槽侧壁间隔设置；The inner buffer ring includes a hollow cylinder-shaped inner ring body, and a plurality of annular convex edges arranged on the outside of the inner ring body, and each annular convex edge is arranged side by side along the axis direction of the inner ring body, Both sides of the inner ring body are spaced apart from the side walls of the first installation groove; 所述外缓冲环包括空心圆柱体状的外环体，以及在所述外环体内侧两边缘凸出的支撑环体，两所述支撑环体对称设置；The outer buffer ring includes a hollow cylindrical outer ring body, and a support ring body protruding from two edges inside the outer ring body, and the two support ring bodies are symmetrically arranged; 所述支撑环体包括侧面和贴合面；The support ring body includes a side surface and a fitting surface; 所述侧面与所述第一安装槽侧壁间隔设置，所述外环体相对于所述侧面向内缩进；The side surface is spaced from the side wall of the first installation groove, and the outer ring body is indented inward relative to the side surface; 所述贴合面与所述侧面连接，所述贴合面为曲面，且与所述内环体贴合设置；the bonding surface is connected with the side surface, the bonding surface is a curved surface, and is arranged to fit with the inner ring body; 各所述环状凸沿位于两支撑环体之间，且在所述第一轴承安装完成且工作前，所述环状凸沿与所述外环体间隔设置，且间隔距离小于所述第一轴承与所述内齿轮之间的间隙距离，所述外缓冲环在所述内缓冲环对所述支撑环体的挤压下成受压状态。Each of the annular protruding edges is located between the two supporting ring bodies, and before the first bearing is installed and operated, the annular protruding edges and the outer ring body are spaced apart, and the spacing distance is smaller than the first bearing. The clearance distance between a bearing and the internal gear, the outer buffer ring is in a compressed state under the pressing of the inner buffer ring to the support ring body. 2.根据权利要求1所述的行星架安装方法，其特征在于，所述第一轴承与所述内齿轮之间间隙控制在0.05~0.3mm之间。2 . The planet carrier installation method according to claim 1 , wherein the clearance between the first bearing and the internal gear is controlled to be between 0.05 and 0.3 mm. 3 . 3.行星减速机波动补偿方法，其特征在于：3. The planetary reducer fluctuation compensation method is characterized in that: 设置第一轴承和弹性缓冲环；Set the first bearing and the elastic buffer ring; 所述第一轴承与行星架同轴设置，且所述第一轴承内圈与所述行星架上的圆柱状的外围段贴合，所述第一轴承外圈与内齿轮上圆柱状的内侧段贴合，所述内齿轮与所述行星架对应的行星轮啮合；The first bearing is arranged coaxially with the planet carrier, and the inner ring of the first bearing is fitted with the cylindrical peripheral section on the planet carrier, and the outer ring of the first bearing is connected to the inner cylindrical inner side of the inner gear. The segments fit together, and the inner gear meshes with the planet gear corresponding to the planet carrier; 所述弹性缓冲环与用于对轴体端部进行支撑的第二轴承外侧贴合，且设置于对所述第二轴承进行安装的固定结构上所设置的第二安装槽内，所述轴体为所述行星架的转动间接输出动力；The elastic buffer ring is attached to the outer side of the second bearing used for supporting the end of the shaft body, and is arranged in the second installation groove provided on the fixing structure for installing the second bearing. The body is the indirect output power of the rotation of the planet carrier; 其中，所述第二轴承与所述固定结构之间通过间隙配合的方式固定；Wherein, the second bearing and the fixing structure are fixed by means of clearance fit; 将所述弹性缓冲环设置为内缓冲环和外缓冲环的组合结构；Setting the elastic buffer ring as a combined structure of an inner buffer ring and an outer buffer ring; 所述内缓冲环包括空心圆柱体状的内环体，以及设置于所述内环体外侧的若干环状凸沿，各所述环状凸沿沿所述内环体的轴线方向并列设置，所述内环体两侧与所述第二安装槽侧壁间隔设置；The inner buffer ring includes a hollow cylinder-shaped inner ring body, and a plurality of annular convex edges arranged on the outside of the inner ring body, and each annular convex edge is arranged side by side along the axis direction of the inner ring body, Both sides of the inner ring body are spaced apart from the side walls of the second installation groove; 所述外缓冲环包括空心圆柱体状的外环体，以及在所述外环体内侧两边缘凸出的支撑环体，两所述支撑环体对称设置；The outer buffer ring includes a hollow cylindrical outer ring body, and a support ring body protruding from two edges inside the outer ring body, and the two support ring bodies are symmetrically arranged; 所述支撑环体包括侧面和贴合面；The support ring body includes a side surface and a fitting surface; 所述侧面与所述第二安装槽侧壁间隔设置，所述外环体相对于所述侧面向内缩进；the side surface is spaced apart from the side wall of the second installation groove, and the outer ring body is indented inward relative to the side surface; 所述贴合面与所述侧面连接，所述贴合面为曲面，且与所述内环体贴合设置；the bonding surface is connected with the side surface, the bonding surface is a curved surface, and is arranged to fit with the inner ring body; 各所述环状凸沿位于两支撑环体之间，且在所述第二轴承安装完成且工作前，所述环状凸沿与所述外环体间隔设置，且间隔距离小于所述第二轴承与所述固定结构之间的间隙距离，所述外缓冲环在所述内缓冲环对所述支撑环体的挤压下成受压状态。Each of the annular protruding edges is located between the two supporting ring bodies, and before the second bearing is installed and operated, the annular protruding edges and the outer ring body are spaced apart, and the spacing distance is smaller than the first bearing. The gap distance between the two bearings and the fixed structure, the outer buffer ring is in a compressed state under the pressing of the inner buffer ring to the support ring body. 4.根据权利要求3所述的行星减速机波动补偿方法，其特征在于，设置第二个弹性缓冲环；4. The planetary reducer fluctuation compensation method according to claim 3, wherein a second elastic buffer ring is provided; 第二个所述弹性缓冲环围绕所述第一轴承外围设置，并与所述第一轴承外侧贴合，且成受压状态设置于所述内齿轮上所设置的第一安装槽内。The second elastic buffer ring is arranged around the periphery of the first bearing, is in contact with the outer side of the first bearing, and is arranged in the first installation groove provided on the internal gear in a pressurized state. 5.行星减速机，其特征在于，采用如权利要求1或2所述的行星架安装方法，对行星架进行安装。5. The planetary reducer is characterized in that, the planet carrier is installed by adopting the planet carrier mounting method as claimed in claim 1 or 2. 6.行星减速机，其特征在于，采用如权利要求3或4所述的行星减速机波动补偿方法，对所述行星架及轴体进行安装。6 . The planetary reducer, characterized in that the planet carrier and the shaft body are installed by adopting the method for compensating for the fluctuation of the planetary reducer according to claim 3 or 4 .
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