CN204867839U - Rotary compressor's assembly fixture - Google Patents
Rotary compressor's assembly fixture Download PDFInfo
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- CN204867839U CN204867839U CN201520508828.8U CN201520508828U CN204867839U CN 204867839 U CN204867839 U CN 204867839U CN 201520508828 U CN201520508828 U CN 201520508828U CN 204867839 U CN204867839 U CN 204867839U
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- frame
- positioning seat
- resilient sleeve
- rotary compressor
- assembly
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Abstract
The utility model discloses a rotary compressor's assembly fixture. Rotary compressor includes first, second frame, and two frames are fixed respectively on compressor housing's inner surface, and the second frame is used for supporting the upper portion of bent axle. The assembly fixture of compressor includes positioning system and clamping system. Positioning system is including fixed core subassembly and positioning seat from top to bottom, and casing stator assembly part overcoat is on fixed core subassembly, and well casing centre gripping is equipped with down the location platform in order to fix a position first frame on the lower positioning seat between upper and lower positioning seat, goes up to be equipped with on the positioning seat and fixes a position in order to fix a position the second frame. The clamping system is used for pressing from both sides tight first frame and second frame. According to the utility model discloses an assembly fixture has guaranteed assembly precision and decide to coordinate the homogeneity between the rotor, makes that wearing and tearing are little between each bearing and the bent axle, the noise is little, and during crankshaft rotation moment of torsion low power dissipation, amount of unbalance is little in the motor clearance, realizes the close clearance and assembles.
Description
Technical field
The utility model relates to compressor process equipment field, especially relates to a kind of assembly tooling of rotary compressor.
Background technology
Compressor industry generally adopts directly that the mode be weldingly fixed on housing fixes compression member by compression assembly, to form electric machine rotor gap.But because assembling conjunction size is more, in assembling process, between each part or between part and frock clamp, often there is dimensional interference.Again because the impact of welding stress, the electric machine rotor gap after having welded often changes, and causes machine air gap amount of unbalance to worsen, and compressor performance reduces.
For solving the problem, Ge great compressor manufacturer and correlative study institutes have all carried out a large amount of work, wherein, adopt the fixing method of dual-gripper to be seen in patent and bibliographical information successively to the sub-assembly of compression assembly and rotor.In actual production, for some novel dual-support structures of rotary compressor, its assembly tooling and corresponding assembly method not yet improve.
Utility model content
The application is intended to solve the technical problem existed in prior art.For this reason, the utility model aims to provide a kind of assembly tooling of rotary compressor, to ensure the assembly precision of the rotary compressor of dual-support structure.
According to the assembly tooling of rotary compressor of the present utility model, described rotary compressor comprises: shell, bent axle, base bearing, supplementary bearing, cylinder, stator, the first frame and the second frame, described shell comprises the middle shell of up/down perforation, the periphery wall of described first frame is fixed on the aperture surface of described middle shell, the periphery wall of described second frame is fixed on the aperture surface of described middle shell, and described second frame is for supporting the top of described bent axle, wherein, the internal perisporium that described stator is fixed on described middle shell forms housing stator assemblies, the assembly tooling of described rotary compressor comprises: navigation system, described navigation system comprises: fixed core assembly, upper positioning seat and lower positioning seat, be enclosed within outside the diameter of stator bore face of described housing stator assemblies on described fixed core assembly, the upper and lower end face of described middle shell is clamped between described upper positioning seat and described lower positioning seat, the upper surface of described lower positioning seat is provided with and extend into lower positioning table in described middle shell to locate described first frame, the lower surface of described upper positioning seat is provided with and extend into upper positioning table in described middle shell to locate described second frame, clamping system, described clamping system is used for described first frame being clamped in described lower positioning table and described second frame being clamped in described upper positioning table.
According to the assembly tooling of rotary compressor of the present utility model, fixture system with the diameter of stator bore face of housing stator assemblies for benchmark positions two of the rotary compressor of dual-support structure frames and clamps, ensure that the assembly precision of the first frame and the second frame, ensure that between the stator of electric machine assembly and rotor, interval is even, make that the wearing and tearing between each bearing and bent axle are little, noise is little, and moment of torsion when making crankshaft rotating is low in energy consumption, machine air gap amount of unbalance is little, realize small―gap suture assembling.
In certain embodiments, described fixed core assembly comprises: stiff shaft, the outer peripheral face of described stiff shaft be male cone (strobilus masculinus) at least partially; Resilient sleeve, be enclosed within outside described resilient sleeve on described stiff shaft, described stiff shaft can move up and down relative to described resilient sleeve, the inner conical surface being formed as matching with described male cone (strobilus masculinus) at least partially of the internal perisporium of described resilient sleeve, be enclosed within outside described stator in described resilient sleeve, described resilient sleeve to be configured to when described stiff shaft moves towards one end that the cross-sectional area of described inner conical surface reduces described resilient sleeve radially elasticity open only to be against on described diameter of stator bore face.Thus, fixed core modular construction is simple, processing ease, and can realize good location, the clamping of housing stator assemblies.
Particularly, described resilient sleeve is provided with and hollows out groove.Thus, resilient sleeve is more prone to radial direction and opens after being squeezed, and improves the control sensitivity of fixed core assembly further.
More specifically, the described groove that hollows out at least comprises multiple first pilot trench and multiple second pilot trench that are arranged alternately, described first pilot trench and the second pilot trench extend respectively vertically, described multiple first pilot trench is through towards the upper surface of described resilient sleeve, and described multiple second pilot trench is through towards the lower surface of described resilient sleeve.Thus, improve further resilient sleeve be squeezed after radial deformability.
In certain embodiments, described clamping system comprises: lower platen, and described lower platen stretches out from the periphery wall lower end of described resilient sleeve, and the lower surface of described lower platen is only against on the upper surface of described first frame.
In certain embodiments, described clamping system comprises: the first rotary cylinder, described first rotary cylinder is located on described lower positioning seat, the piston rod of described first rotary cylinder extend in described middle shell, and the free end of the piston rod of described first rotary cylinder is formed as the first jaw and is clamped in described first frame.
In certain embodiments, described clamping system comprises: upper clamping piece, and described upper clamping piece can be located on described upper positioning seat up or down, and the lower end of described upper clamping piece to extend into downwards in described middle shell and is only against on the lower surface of described second frame.
In certain embodiments, described clamping system comprises: the second rotary cylinder, described second rotary cylinder is located on described upper positioning seat, the piston rod of described second rotary cylinder extend in described middle shell, and the free end of the piston rod of described second rotary cylinder is formed as the second jaw and is clamped in described second frame.
In certain embodiments, one end of described stiff shaft connects driver, and the other end of described stiff shaft is connected on described upper positioning seat or described lower positioning seat by locating shaft.Thus, the rigidity of a whole set of tool locating system is strengthened.
In certain embodiments, the assembly tooling of rotary compressor also comprises the guide pillar be positioned at outside described middle shell, described upper positioning seat and described lower positioning seat are located on described guide pillar respectively, and described upper positioning seat described guide pillar relative at least one in described lower positioning seat is removable.Thus, the accuracy of positioning seat and lower positioning seat relative position in guarantee, improves assembly precision.
Additional aspect of the present utility model and advantage will part provide in the following description, and part will become obvious from the following description, or be recognized by practice of the present utility model.
Accompanying drawing explanation
Above-mentioned and/or additional aspect of the present utility model and advantage will become obvious and easy understand from accompanying drawing below combining to the description of embodiment, wherein:
Fig. 1 is the structural representation of the rotary compressor according to the utility model embodiment;
Fig. 2 is location and the clamping schematic diagram of the rack frock of rotary compressor according to the utility model embodiment;
Fig. 3 is the assembly tooling structural representation of the rotary compressor according to the utility model embodiment;
Fig. 4 is the rotary compressor assembly tooling structural representation according to another embodiment of the utility model;
Fig. 5 is the structural representation of the stiff shaft according to the utility model embodiment;
Fig. 6 is the structural representation of the resilient sleeve according to the utility model embodiment.
Reference numeral:
100: rotary compressor;
1: exhaust manifolds; 2: upper shell; 3: middle shell; 4: stator; 5: rotor; 6: bent axle; 7: base bearing; 8: cylinder; 9: supplementary bearing; 10: lower house; 13: balance weight; 14: reservoir;
A: shell; B: electric machine assembly; C: compression assembly; V: container cavity;
11: lower support structure; 111: the first frames;
12: upper support structure; 121: the second frames; 122: auxiliary bearing;
The upper surface of the F1: the first frame; The lower surface of the F2: the first frame;
The lower surface of the F3: the second frame;
F5: diameter of stator bore face; F7: the first locating surface; F8: the second locating surface;
304: housing stator assemblies;
200: assembly tooling;
210: navigation system;
211: fixed core assembly; 2111: stiff shaft; Z1: male cone (strobilus masculinus); 2112: resilient sleeve; Z2: inner conical surface; K: hollow out groove; K1: the first pilot trench; K2: the second pilot trench; K3: bottom outlet;
212: upper positioning seat; 213: upper positioning table; 214: lower positioning seat; 215: lower positioning table; 216: circumferential alignment pin; 217: axis hole;
220: clamping system; 221: lower platen; 222: the first rotary cylinders; 2221: the first jaws; 223: upper clamping piece; 224: the second rotary cylinders; 2241: the second jaws;
230: auxiliary supporting system; 231: locating shaft; 232: locating hole; 233: centre bore;
240: guidance system; 241: guide pillar; 242: guide pin bushing.
Detailed description of the invention
Be described below in detail embodiment of the present utility model, the example of described embodiment is shown in the drawings, and wherein same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the utility model, and can not be interpreted as restriction of the present utility model.
In description of the present utility model, it will be appreciated that, term " " center ", " longitudinal direction ", " transverse direction ", " length ", " width ", " thickness ", " on ", D score, " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end ", " interior ", " outward ", " clockwise ", " counterclockwise ", " axis ", " radial direction ", orientation or the position relationship of the instruction such as " circumference " are based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as restriction of the present utility model.
In addition, term " first ", " second " only for describing object, and can not be interpreted as instruction or hint relative importance or imply the quantity indicating indicated technical characteristic.Thus, be limited with " first ", the feature of " second " can express or impliedly comprise one or more these features.In description of the present utility model, except as otherwise noted, the implication of " multiple " is two or more.
In description of the present utility model, unless otherwise clearly defined and limited, term " installation ", " being connected ", " connection ", " fixing " should be interpreted broadly, and such as, can be fixedly connected with, also can be removably connect, or integral; Can be mechanical connection, also can be electrical connection; Can be directly be connected, also indirectly can be connected by intermediary, can be the connection of two element internals or the interaction relationship of two elements.For the ordinary skill in the art, concrete condition the concrete meaning of above-mentioned term in the utility model can be understood.
In the utility model, unless otherwise clearly defined and limited, fisrt feature second feature it " on " or D score can comprise the first and second features and directly contact, also can comprise the first and second features and not be directly contact but by the other characterisation contact between them.And, fisrt feature second feature " on ", " top " and " above " comprise fisrt feature directly over second feature and oblique upper, or only represent that fisrt feature level height is higher than second feature.Fisrt feature second feature " under ", " below " and " below " comprise fisrt feature immediately below second feature and tiltedly below, or only represent that fisrt feature level height is less than second feature.
Below with reference to Fig. 1-Fig. 6, the assembly tooling 200 according to the rotary compressor of the utility model embodiment is described.
Particularly, as shown in Figure 1, rotary compressor 100 comprises: shell A, electric machine assembly B and compression assembly C.Shell A is airtight container, limits container cavity V in shell A.Electric machine assembly B and compression assembly C is all located in shell A, and namely electric machine assembly B and compression assembly C is all located in container cavity V.In the example illustrated in figure 1, shell A comprises middle shell 3, upper shell 2 and lower house 10, and middle shell 3 is formed as the tubular of upper and lower both ends open, i.e. middle shell 3 up/down perforation, and upper shell 2 and lower house 10 are located at the two ends up and down of middle shell 3 respectively.Rotary compressor 100 also comprises exhaust manifolds 1, and exhaust manifolds 1 to be located on shell A and to be communicated with container cavity V, and in the example of fig. 1, exhaust manifolds 1 are connected on upper shell 2.
As shown in Figure 1, electric machine assembly B is positioned at the top of compression assembly C, and electric machine assembly B comprises stator 4 and coordinates the rotor 5 rotated with stator 4.Stator 4 is fixed on shell A, and rotor 5 is located in stator 4 rotationally.
As shown in Figure 1, compression assembly C comprises bent axle 6, cylinder assembly, supplementary bearing 9, base bearing 7, piston and slide plate (scheming not shown) etc., cylinder assembly can comprise one or more cylinder 8, when cylinder 8 is multiple, is provided with dividing plate between adjacent two cylinders 8.Wherein, bent axle 6 runs through cylinder assembly and is enclosed within outside rotor 5 on bent axle 6, bent axle 6 be fixedly connected with rotor 5 with rotor 5 synchronous rotary.Base bearing 7 and supplementary bearing 9 are located at the two ends up and down of cylinder assembly respectively, base bearing 7 and/or supplementary bearing 9 are provided with the steam vent (scheming not shown) being communicated with cylinder interior space, and bent axle 6 coordinates to be located at rotationally in shell A with base bearing 7 and supplementary bearing 9 respectively.Be located to piston eccentric rotary in cylinder 8, bent axle 6 is connected with piston with driven plunger eccentric rotary, and bent axle 6 drives piston rotation and refrigerant in compression cylinder 8.Rotary compressor 100 also provides refrigerant to be compressed by reservoir 14, and reservoir 14 is connected with cylinder 8.Cylinder interior space is divided into high pressure chest and low pressure chamber by slide plate 11, compression refrigerant in piston rotation process, and the pressure in high pressure chest is raised, and when pressure is increased to the external pressure slightly larger than compression assembly C, namely pressurized gas refrigerant discharges by steam vent.
Be eccentric system due to bent axle 6 and by the piston of bent axle 6 driven rotary, during rotation, larger vibration can be caused, therefore in the design, usually also need end face configuration balance weight 13 at rotor 5 to offset mass eccentricity.
According to the rotary compressor 100 of the utility model embodiment, as depicted in figs. 1 and 2, also comprise the first frame 111 and the second frame 121, the periphery wall of the first frame 111 is fixed on the aperture surface of middle shell 3, and the part of base bearing 7, supplementary bearing 9 or other compression assemblies C such as cylinder 8 or dividing plate is fixedly connected in the first frame 111.The periphery wall of the second frame 121 is fixed on the aperture surface of middle shell 3, and the second frame 121 is for supporting the top of bent axle 6.
That is, the lower end of compression assembly C is fixed on shell A by the first frame 111, and the first frame 111 forms the lower support structure 11 of the sub-assembly of compression assembly C and rotor 5.Second frame 121 is supported on the upper end of bent axle 6, and the second frame 121 forms the upper support structure 12 of the sub-assembly of compression assembly C and rotor 5.The sub-assembly that the rotor 5 of compression assembly C and electric machine assembly B is formed is connected on the shell A of compressor by lower support structure 11 and upper support structure 12.
In the utility model embodiment, using the first frame 111 as above stated assembly lower end with the transition piece between shell A, using the second frame 121 as above stated assembly upper end with the transition piece between shell A, after ensureing that assembling completes, the sub-assembly of the rotor 5 of compression assembly C and electric machine assembly B and the relative position of stator 4 can not change, thus the flexure eliminated when rotor 5 rotates swings, very low electric machine rotor gap amount of unbalance can be ensured simultaneously, make the wearing and tearing between each bearing and bent axle 6 little, noise is little, moment of torsion when bent axle 6 rotates is low in energy consumption, machine air gap amount of unbalance is little.
In some concrete examples, upper support structure 12 also comprises auxiliary bearing 122, and auxiliary bearing 122 is fixed on the upper surface of the second frame 121, and the top being enclosed within bent axle 6 outside auxiliary bearing 122 is to support bent axle 6.
Wherein, when assembling rotary compressor 100, the internal perisporium first stator 4 being fixed on middle shell 3 forming housing stator assemblies 304, and then the first frame 111, second frame 121 is located, is connected on housing stator assemblies 304.
The assembly tooling 200 of rotary compressor described in the utility model, solution be the assembly tooling 200 how the first frame 111, second frame 121 is located by connecting on housing stator assemblies 304.
According to the assembly tooling 200 of the rotary compressor of the utility model embodiment, as shown in Figure 3 and Figure 4, comprising: navigation system 210 and clamping system 220.
Wherein, as shown in Figure 3 and Figure 4, navigation system 210 comprises: fixed core assembly 211, upper positioning seat 212 and lower positioning seat 214, be enclosed within fixed core assembly 211 outside the diameter of stator bore face F5 of housing stator assemblies 304, the upper and lower end face of middle shell 3 is clamped between upper positioning seat 212 and lower positioning seat 214, the upper surface of lower positioning seat 214 is provided with and extend into lower positioning table 215 in middle shell 3 to locate the first frame 111, the lower surface of upper positioning seat 212 is provided with and extend into upper positioning table 213 in middle shell 3 to locate the second frame 121, clamping system 220 is for being clamped in lower positioning table 215 by the first frame 111 and the second frame 121 being clamped in upper positioning table 213.
Here, aperture surface refers to the internal face of respective members, in the following description, perpendicular with the aperture surface of component, is commonly referred to as with the central axis of this component perpendicular.
Wherein, housing stator assemblies 304 with fixed core assembly 211 for reference for assembling, the upper surface of lower positioning table 215 is the first locating surface F7, the lower surface of upper positioning table 213 is the second locating surface F8, and the first locating surface F7, the second locating surface F8 form the assembling and positioning face of the first frame 111, second frame 121.Like this, owing to being enclosed within fixed core assembly 211 outside the diameter of stator bore face F5 of housing stator assemblies 304, therefore, after the positional precision that ensure that the first locating surface F7, the second locating surface F8 and fixed core assembly 211, after having assembled, the assembly precision of the diameter of stator bore face F5 of the relative housing stator assemblies 304 of the first frame 111, second frame 121 can also just be ensured.
Wherein, upper positioning seat 212 and lower positioning seat 214 are respectively arranged with circumferential alignment pin 216, circumferential alignment pin 216 on upper positioning seat 212 is location second frame 121 in circumference, circumferential alignment pin 216 on lower positioning seat 214 is location first frame 111 in circumference, avoids the first frame 111, second frame 121 rotational displacement.
According to the assembly tooling 200 of the rotary compressor of the utility model embodiment, fixture system with the diameter of stator bore face F5 of housing stator assemblies 304 for two frames of benchmark to the rotary compressor 100 of dual-support structure position and clamp, ensure that the assembly precision of the first frame 111 and the second frame 121, ensure the stator 4 of electric machine assembly B and coordinate evenly between rotor 5, make that the wearing and tearing between each bearing and bent axle 6 are little, noise is little, and moment of torsion when making bent axle 6 rotate is low in energy consumption, machine air gap amount of unbalance is little, realize small―gap suture assembling.
In certain embodiments, as shown in figures 3 to 6, fixed core assembly 211 comprises: stiff shaft 2111 and resilient sleeve 2112, wherein, stiff shaft 2111 is axle core, be enclosed within outside resilient sleeve 2112 on stiff shaft 2111, and be enclosed within resilient sleeve 2112 outside housing stator assemblies 304, form the positioning form of overcoat successively.
Wherein, only be against on the F5 of diameter of stator bore face when resilient sleeve 2112 is radially opened, can ensure that the central shaft of diameter of stator bore face F5 and stiff shaft 2111 is to overlapping, like this, when location afterwards, navigation system 210, positions the first frame 111, second frame 121 for positioning datum with diameter of stator bore face F5.That is, a set of expansion core clamping device that the location of housing stator assemblies 304 and clamping are is benchmark with diameter of stator bore face F5.
Particularly, as shown in figures 3 to 6, the outer peripheral face of stiff shaft 2111 be male cone (strobilus masculinus) Z1 at least partially, be enclosed within stiff shaft 2111 outside resilient sleeve 2112, stiff shaft 2111 can move up and down relative to resilient sleeve 2112, the inner conical surface Z2 being formed as matching with male cone (strobilus masculinus) Z1 at least partially of the internal perisporium of resilient sleeve 2112, resilient sleeve 2112 to be configured to when stiff shaft 2111 moves towards one end that the cross-sectional area of inner conical surface Z2 reduces resilient sleeve 2112 radially elasticity open, resilient sleeve 2112 is only against on the F5 of diameter of stator bore face when radially elasticity is opened.Thus, fixed core assembly 211 structure is simple, processing ease, and can realize good location, the clamping of housing stator assemblies 304.
Wherein, the male cone (strobilus masculinus) Z1 of stiff shaft 2111 is substantially identical with the tapering of the inner conical surface Z2 of resilient sleeve 2112, thus ensures that the male cone (strobilus masculinus) Z1 of resilient sleeve 2112 is close on the inner conical surface Z2 of resilient sleeve 2112 at least partially.Here, when moving towards one end that the cross-sectional area of the inner conical surface Z2 of resilient sleeve 2112 reduces at stiff shaft 2111, stiff shaft 2111 compresses axially resilient sleeve 2112, and resilient sleeve 2112 elastic deformation occurs and opens to radial direction.Therefore resilient sleeve 2112 and stiff shaft 2111 snug fit, resilient sleeve 2112 can be out of shape immediately when stiff shaft 2111 moves axially, thus improve the sensitivity of control.In the example shown in Fig. 3 and Fig. 6, the outer peripheral face of resilient sleeve 2112 is the face of cylinder, and inner conical surface Z2 and external cylindrical surface are coaxially arranged.Alternatively, resilient sleeve 2112 is spring steel.
More specifically, one end of stiff shaft 2111 connects driver (scheming not shown), stiff shaft 2111 is pulled to move during drive operation downwards, the male cone (strobilus masculinus) Z1 of stiff shaft 2111 contacts with the inner conical surface Z2 of resilient sleeve 2112, promote resilient sleeve 2112 radial direction to open, the external cylindrical surface of resilient sleeve 2112 contacts with diameter of stator bore face F5, with clamping body stator assemblies 304.
Advantageously, upper positioning seat 212 or lower positioning seat 214 are provided with axis hole 217, and stiff shaft 2111 extend in middle shell 3 through axis hole 217.Axis hole 217 can limit stiff shaft 2111 moving axially along axis hole 217 with coordinating of stiff shaft 2111, improves the control accuracy of stiff shaft 2111.Wherein, the orientation assemble face on the central axis of axis hole 217 and corresponding upper positioning seat 212 or lower positioning seat 214 is perpendicular.
In certain embodiments, as shown in Figure 1-Figure 3, auxiliary bearing 122 matches with bent axle 6 through after the second frame 121, and the upper surface of the second frame 121 is orientation assemble faces of location auxiliary bearing 122.Because base bearing 7, supplementary bearing 9 or cylinder 8 in compression assembly C are fixedly connected in the first frame 111, in the example of fig. 1, the lower surface F2 of the first frame 111 is the orientation assemble face of compression assembly C.
Like this, for bent axle 6 after ensureing to install is arranged with auxiliary bearing 122 is concentric, will ensure during installation that the first frame 111 parallels with the second frame 121, in the example of especially Fig. 1, the lower surface F2 of the first frame 111 is parallel with the upper surface of the second frame 121.
When assembling, also to ensure the first frame 111 and the second frame 121 aperture surface F5 perpendicular to stator 4 simultaneously, namely in the example of fig. 1, the lower surface F2 of the first frame 111 and the central axis of stator 4 perpendicular, the upper surface of the second frame 121 and the central axis of stator 4 perpendicular.Specifically, when mounted, first frame 111 and the second frame 121 all with the aperture surface F5 of stator 4 for locating surface, ensure that the corresponding orientation assemble face of the first frame 111 and the second frame 121 is all perpendicular with the central axis of stator 4, like this, also just can ensure to install rear rotor 5 and stator 4 better can coaxial cooperation, ensures gap uniformity between rotor 5 and stator 4.
Particularly, compression assembly C by with the diameter of stator bore face S5 of electric machine assembly B feel relieved install after be connected in the first frame 111, the central axis of the central axis of compression assembly C and stator 4 can be made like this to be located along the same line, and namely bent axle 6 coaxially can be arranged with stator 4.When bent axle 6 coordinates with auxiliary bearing 122, auxiliary bearing 122 is wanted first to be connected in the second frame 121 after aligning again, like this, can ensure that the central axis of auxiliary bearing 122 and the central axis of bent axle 6 are located along the same line.After said method assembling, can make coaxially to arrange between rotor 5 and stator 4, ensure gap uniformity between stator 4 and rotor 5.
In certain embodiments, as shown in Figure 6, resilient sleeve 2112 is provided with and hollows out groove k, that is, resilient sleeve 2112 cuts out a part on perisporium, like this, resilient sleeve 2112 is more prone to radial direction and opens after being squeezed, and improves the control sensitivity of fixed core assembly 211 further.
Particularly, hollow out the groove k outer peripheral face of through resilient sleeve 2112 and inner peripheral surface diametrically, like this, resilient sleeve 2112 radial direction is opened and is more prone to.
More specifically, as shown in Figure 6, hollow out groove k and at least comprise the multiple first pilot trench k1 and multiple second pilot trench k2 that are arranged alternately, first pilot trench k1 and the second pilot trench k2 extends respectively vertically, multiple first pilot trench k1 is through towards the upper surface of resilient sleeve 2112, and multiple second pilot trench k2 is through towards the lower surface of resilient sleeve 2112.Thus, improve further resilient sleeve 2112 be squeezed after radial deformability.
In some concrete examples, as shown in Figure 6, what resilient sleeve 2112 is provided with more than 6 staggered hollows out groove k, non-through one end of each first pilot trench k1 and the second pilot trench k2 is provided with bottom outlet k3, the diameter of bottom outlet k3 is greater than the groove width hollowing out groove k accordingly, and advantageously, bottom outlet k3 is circular port.
In certain embodiments, the end face of resilient sleeve 2112 is only against in the first frame 111 or the second frame 121 after tool locating completes, advantageously, the end face contacted with corresponding frame of resilient sleeve 2112 and the central axis of inner conical surface Z2 perpendicular, that is, resilient sleeve 2112 also achieves the function of clamping frame while location.
In a specific embodiment, as shown in Figure 3, clamping system 220 comprises: lower platen 221, and lower platen 221 stretches out from the periphery wall lower end of resilient sleeve 2112, and the lower surface of lower platen 221 is only against on the upper surface F1 of the first frame 111.That is, the first frame 111 can be compressed by the form of frame for movement, wherein, is located at by lower platen 221 in resilient sleeve 2112, and lower platen 221 is mobile with the movement of resilient sleeve 2112.When stiff shaft 2111 moves down, resilient sleeve 2112 is driven to open and move in the same way, to compress the first frame 111 be positioned on lower positioning seat 214.Thus, the simple compression of the first frame 111 can be realized, reduced the number of the part of assembly tooling 200 simultaneously, reduce the cost of assembly tooling 200.
Wherein, lower platen 221 can be integrally formed in resilient sleeve 2112, and lower platen 221 also can be formed as individual part and be fixed in resilient sleeve 2112.
Certainly, the utility model is not limited thereto, such as shown in Figure 4, clamping system 220 can comprise: the first rotary cylinder 222, first rotary cylinder 222 is located on lower positioning seat 214, the piston rod of the first rotary cylinder 222 extend in middle shell 3, and the free end of the piston rod of the first rotary cylinder 222 is formed as the first jaw 2221 and is clamped in the first frame 111.That is, the first frame 111 is clamped by pneumatic structure, and in addition, the first frame 111 also clamps by hydraulic structure.
In certain embodiments, as shown in Figure 3, clamping system 220 comprises: upper clamping piece 223, and upper clamping piece 223 can be located on positioning seat 212 up or down, and the lower end of upper clamping piece 223 to extend into downwards in middle shell 3 and is only against on the lower surface F3 of the second frame 121.That is, the second frame 121 also can be compressed by frame for movement, thus, reduces the cost of assembly tooling 200 further.
Particularly, as shown in Figure 3, upper positioning seat 212 is provided with the screwed hole of up/down perforation, and upper clamping piece 223 comprises feed screw nut's structure, and the threaded portion of screw mandrel is engaged in screwed hole, drives screw mandrel to move up and down during nut rotation.
Certainly, the utility model is not limited thereto, such as shown in Figure 4, clamping system 220 comprises: the second rotary cylinder 224, second rotary cylinder 224 is located on positioning seat 212, the piston rod of the second rotary cylinder 224 extend in middle shell 3, and the free end of the piston rod of the second rotary cylinder 224 is formed as the second jaw 2241 and is clamped in the second frame 121.That is, the second frame 121 is also by pneumatic structure clamping, and in addition, the second frame 121 also clamps by hydraulic structure.
In certain embodiments, as shown in Figure 3, the other end of stiff shaft 2111 is connected on upper positioning seat 212 or lower positioning seat 214 by locating shaft 231, and that is, one end not connecting driver of stiff shaft 2111 is supported by locating shaft 231.
Particularly, in the example of fig. 3, upper clamping piece 223 is provided with the locating hole 232 of up/down perforation, the top of stiff shaft 2111 is provided with the centre bore 233 arranged vertically, locating shaft 231 is placed in locating hole 232 from above, the lower end of locating shaft 231 extend in centre bore 233, thus locating shaft 231 is connected between positioning seat 212 and stiff shaft 2111.
Locating shaft 231 and accordingly locating hole 232, centre bore 233 form auxiliary supporting system 230.The axis of locating hole 232, locating shaft 231 overlaps with stiff shaft 2111 center line of navigation system 210, during frock work, locating shaft 231 one end is inserted in the centre bore 233 of stiff shaft 2111, and the other end is bearing on positioning seat 212, strengthens the rigidity of a whole set of tool locating system 210.
In certain embodiments, as shown in Figure 3, the assembly tooling 200 of rotary compressor also comprises the guide pillar 241 be positioned at outside middle shell 3, and upper positioning seat 212 and lower positioning seat 214 are located on guide pillar 241 respectively, and upper positioning seat 212 guide pillar 241 relative at least one in lower positioning seat 214 is removable.
Here, guide pillar 241 constitutes the guidance system 240 of assembly tooling 200, and when upper positioning seat 212 and lower positioning seat 214 relative movement, corresponding positioning seat moves along guide pillar 241, in guarantee, positioning seat 212 and the accuracy of lower positioning seat 214 relative position, improve assembly precision.
Particularly, guidance system 240 also comprises guide pin bushing 242, and guide pin bushing 242 is located on positioning seat 212 and/or lower positioning seat 214, and guide pillar 241 is engaged in guide pin bushing 242.
Advantageously, clamp after Workpiece fixing, namely in assembling process, be first positioned on lower positioning table 215, upper positioning table 213 respectively by the first frame 111, second frame 121, then clamping system 220 works the first frame 111, second frame 121 to be fixedly clamped respectively.
For ease of understanding, describe the assembly method according to the rotary compressor 100 of the utility model embodiment below with reference to Fig. 3, Fig. 4, wherein, rotary compressor 100 adopts the assembly tooling 200 according to the utility model above-described embodiment.
According to the assembly method of the rotary compressor 100 of the utility model embodiment, comprise the steps:
S1: respectively the first frame 111 to be positioned on lower positioning seat 214 and the second frame 121 is positioned on upper positioning seat 212, being enclosed within outside housing stator assemblies 304 on fixed core assembly 211, and the lower surface of middle shell 3 being positioned on lower positioning seat 214;
S2: clamping system 220 works, to be clamped on lower positioning seat 214 and upper positioning seat 212 respectively by the first frame 111, second frame 121;
S3: so that the second frame 121 is placed in middle shell 3 downwards on the upper surface upper positioning seat 212 being placed on middle shell 3;
S4: the first frame 111, second frame 121 is separately fixed on middle shell 3;
S5: after fixedly completing, withdraws housing stator assemblies 304 by assembly tooling 200.
That is, in above-mentioned assembly method, using diameter of stator bore face F5 as positioning reference plane, achieve the correct location of the first frame 111, second frame 121, ensure the assembly precision of rotary compressor 100.
It should be noted that, the first frame 111, second frame 121 described in literary composition is convenient in order to describe, and the clamping of two frames and permanent order can be exchanged.
In addition, also it should be noted that, above-mentioned first frame 111, second frame 121 is respectively equipped with groove of giving up the throne (scheming not shown), after fixedly completing in step s 5, clamping device in second frame 121 rotates to groove place of giving up the throne, then go up positioning seat 212 when moving up, the clamping device on positioning seat 212 can be driven to exit middle shell 3 from this groove of giving up the throne.In like manner, the clamping device in the first frame 111 also rotates to groove place of giving up the throne accordingly after fixedly completing, and then when being taken off from lower positioning seat 214 by workpiece, the clamping device on lower positioning seat 214 exits middle shell 3 from this groove of giving up the throne simultaneously.
Thus, according to the assembly method of the rotary compressor 100 of the utility model embodiment, step is simple, rigorous, by the correct location by the first frame 111, second frame 121, ensure the assembly precision of rotary compressor 100, meet the object that moment of torsion is low in energy consumption, machine air gap amount of unbalance is little when wearing and tearing between each bearing and bent axle 6 are little, noise is little, bent axle 6 rotates after making to have the compressor assembling of dual-support structure, and ensure that the reliability of compressor is good.
Below with reference to the specific embodiment shown in Fig. 3 and Fig. 4, describe the assembly method of rotary compressor 100 in detail, it is to be appreciated that in different embodiment, identical label shows that element is identical, or two elements have identical function.
Embodiment one
As shown in Figure 3, in embodiment one, the assembly method step of rotary compressor 100 is as follows:
S1: respectively the first frame 111 is positioned on the first locating surface F7 on lower positioning seat 214, second frame 121 is positioned on the second locating surface F8 of upper positioning seat 212, be enclosed within outside housing stator assemblies 304 in resilient sleeve 2112, and the lower surface of middle shell 3 be positioned on lower positioning seat 214;
S2: clamping system 220 works, wherein, upper clamping piece 223 on upper positioning seat 212 moves up, so that the second frame 121 is clamped on upper positioning table 213, on lower positioning seat 214, stiff shaft 2111 moves down, so that the diameter of stator bore face F5 of housing stator assemblies 304 is pressed on the outer surface of resilient sleeve 2112, and by the lower platen 221 in resilient sleeve 2112, first frame 111 is clamped on lower positioning table 215;
S3: upper positioning seat 212 moves down along guide pillar 241, until upper positioning seat 212 moves and is only against the upper end of middle shell 3, drives the second frame 121 to be placed in middle shell 3 downwards simultaneously;
S4: the first frame 111, second frame 121 is welded on middle shell 3 respectively;
S5: after having welded, unclamps stiff shaft 2111 and upper clamping piece 223, is moved up by upper positioning seat 212, so that the workpiece assembled is taken out of lower positioning seat 214, completes operation work.
Embodiment two
As shown in Figure 4, in embodiment two, the assembly method step of rotary compressor 100 is as follows:
S1: respectively the first frame 111 is positioned on the first locating surface F7 on lower positioning seat 214, second frame 121 is positioned on the second locating surface F8 of upper positioning seat 212, be enclosed within outside housing stator assemblies 304 in resilient sleeve 2112, and the lower surface of middle shell 3 be positioned on lower positioning seat 214;
S2: clamping system 220 works, first frame 111 is clamped on lower positioning table 215 by the first rotary cylinder 222, second frame 121 is clamped on upper positioning table 213 by the second rotary cylinder 224, to be clamped on lower positioning seat 214 and upper positioning seat 212 respectively by the first frame 111, second frame 121; One end that stiff shaft 2111 reduces towards the cross-sectional area of inner conical surface Z2 is moved, and resilient sleeve 2112 radially elasticity opens only to be against on the F5 of diameter of stator bore face, clamps housing stator assemblies 304.
S3: upper positioning seat 212 moves down, until upper positioning seat 212 moves and is only against the upper end of middle shell 3, drives the second frame 121 to be placed in middle shell 3 downwards simultaneously;
S4: the first frame 111, second frame 121 is welded on middle shell 3 respectively;
S5: after having welded, unclamps stiff shaft 2111 and the first rotary cylinder 222, second rotary cylinder 224, is moved up by upper positioning seat 212, so that the workpiece assembled is taken out of lower positioning seat 214, complete operation work.
In the description of this description, specific features, structure, material or feature that the description of reference term " embodiment ", " some embodiments ", " example ", " concrete example " or " some examples " etc. means to describe in conjunction with this embodiment or example are contained at least one embodiment of the present utility model or example.In this manual, identical embodiment or example are not necessarily referred to the schematic representation of above-mentioned term.And the specific features of description, structure, material or feature can combine in an appropriate manner in any one or more embodiment or example.
Although illustrate and described embodiment of the present utility model, those having ordinary skill in the art will appreciate that: can carry out multiple change, amendment, replacement and modification to these embodiments when not departing from principle of the present utility model and aim, scope of the present utility model is by claim and equivalents thereof.
Claims (10)
1. the assembly tooling of a rotary compressor, it is characterized in that, described rotary compressor comprises: shell, bent axle, base bearing, supplementary bearing, cylinder, stator, the first frame and the second frame, described shell comprises the middle shell of up/down perforation, the periphery wall of described first frame is fixed on the aperture surface of described middle shell, the periphery wall of described second frame is fixed on the aperture surface of described middle shell, and described second frame is for supporting the top of described bent axle;
Wherein, the internal perisporium that described stator is fixed on described middle shell forms housing stator assemblies;
The assembly tooling of described rotary compressor comprises:
Navigation system, described navigation system comprises: fixed core assembly, upper positioning seat and lower positioning seat, be enclosed within outside the diameter of stator bore face of described housing stator assemblies on described fixed core assembly, the upper and lower end face of described middle shell is clamped between described upper positioning seat and described lower positioning seat, the upper surface of described lower positioning seat is provided with and extend into lower positioning table in described middle shell to locate described first frame, and the lower surface of described upper positioning seat is provided with and extend into upper positioning table in described middle shell to locate described second frame;
Clamping system, described clamping system is used for described first frame being clamped in described lower positioning table and described second frame being clamped in described upper positioning table.
2. the assembly tooling of rotary compressor according to claim 1, is characterized in that, described fixed core assembly comprises:
Stiff shaft, the outer peripheral face of described stiff shaft be male cone (strobilus masculinus) at least partially;
Resilient sleeve, be enclosed within outside described resilient sleeve on described stiff shaft, described stiff shaft can move up and down relative to described resilient sleeve, the inner conical surface being formed as matching with described male cone (strobilus masculinus) at least partially of the internal perisporium of described resilient sleeve, be enclosed within outside described stator in described resilient sleeve, described resilient sleeve to be configured to when described stiff shaft moves towards one end that the cross-sectional area of described inner conical surface reduces described resilient sleeve radially elasticity open only to be against on described diameter of stator bore face.
3. the assembly tooling of rotary compressor according to claim 2, is characterized in that, described resilient sleeve is provided with and hollows out groove.
4. the assembly tooling of rotary compressor according to claim 3, it is characterized in that, the described groove that hollows out at least comprises multiple first pilot trench and multiple second pilot trench that are arranged alternately, described first pilot trench and the second pilot trench extend respectively vertically, described multiple first pilot trench is through towards the upper surface of described resilient sleeve, and described multiple second pilot trench is through towards the lower surface of described resilient sleeve.
5. the assembly tooling of rotary compressor according to claim 2, it is characterized in that, described clamping system comprises: lower platen, and described lower platen stretches out from the periphery wall lower end of described resilient sleeve, and the lower surface of described lower platen is only against on the upper surface of described first frame.
6. the assembly tooling of rotary compressor according to claim 1, it is characterized in that, described clamping system comprises: the first rotary cylinder, described first rotary cylinder is located on described lower positioning seat, the piston rod of described first rotary cylinder extend in described middle shell, and the free end of the piston rod of described first rotary cylinder is formed as the first jaw and is clamped in described first frame.
7. the assembly tooling of rotary compressor according to claim 1, it is characterized in that, described clamping system comprises: upper clamping piece, described upper clamping piece can be located on described upper positioning seat up or down, and the lower end of described upper clamping piece to extend into downwards in described middle shell and is only against on the lower surface of described second frame.
8. the assembly tooling of rotary compressor according to claim 1, it is characterized in that, described clamping system comprises: the second rotary cylinder, described second rotary cylinder is located on described upper positioning seat, the piston rod of described second rotary cylinder extend in described middle shell, and the free end of the piston rod of described second rotary cylinder is formed as the second jaw and is clamped in described second frame.
9. the assembly tooling of rotary compressor according to claim 2, is characterized in that, one end of described stiff shaft connects driver, and the other end of described stiff shaft is connected on described upper positioning seat or described lower positioning seat by locating shaft.
10. the assembly tooling of rotary compressor according to claim 1, it is characterized in that, also comprise the guide pillar be positioned at outside described middle shell, described upper positioning seat and described lower positioning seat are located on described guide pillar respectively, and described upper positioning seat described guide pillar relative at least one in described lower positioning seat is removable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520508828.8U CN204867839U (en) | 2015-07-13 | 2015-07-13 | Rotary compressor's assembly fixture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520508828.8U CN204867839U (en) | 2015-07-13 | 2015-07-13 | Rotary compressor's assembly fixture |
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| Publication Number | Publication Date |
|---|---|
| CN204867839U true CN204867839U (en) | 2015-12-16 |
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| CN201520508828.8U Withdrawn - After Issue CN204867839U (en) | 2015-07-13 | 2015-07-13 | Rotary compressor's assembly fixture |
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| CN (1) | CN204867839U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104959742A (en) * | 2015-07-13 | 2015-10-07 | 广东美芝制冷设备有限公司 | Assembly fixture of rotation type compressor and assembly method |
-
2015
- 2015-07-13 CN CN201520508828.8U patent/CN204867839U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104959742A (en) * | 2015-07-13 | 2015-10-07 | 广东美芝制冷设备有限公司 | Assembly fixture of rotation type compressor and assembly method |
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| AV01 | Patent right actively abandoned |
Granted publication date: 20151216 Effective date of abandoning: 20180717 |
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