CN110802407A - Hub clamp for airplane hub assembly line and application method thereof - Google Patents
Hub clamp for airplane hub assembly line and application method thereof Download PDFInfo
- Publication number
- CN110802407A CN110802407A CN201911310198.2A CN201911310198A CN110802407A CN 110802407 A CN110802407 A CN 110802407A CN 201911310198 A CN201911310198 A CN 201911310198A CN 110802407 A CN110802407 A CN 110802407A
- Authority
- CN
- China
- Prior art keywords
- hub
- pressing
- connecting rod
- bottom plate
- clamp
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P21/00—Machines for assembling a multiplicity of different parts to compose units, with or without preceding or subsequent working of such parts, e.g. with programme control
- B23P21/002—Machines for assembling a multiplicity of different parts to compose units, with or without preceding or subsequent working of such parts, e.g. with programme control the units stationary whilst being composed
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
- B25B11/02—Assembly jigs
Abstract
The invention discloses a hub clamp for an aircraft hub assembly line and an application method thereof, wherein the clamp comprises a base, a clamping mechanism and a hub mounting plate, the clamping mechanism comprises a multi-link mechanism, a locking mechanism and a hub pressing claw which are connected with the multi-link mechanism, the multi-link mechanism is arranged on the base and is provided with a plurality of free ends, each free end is respectively and vertically connected with the hub pressing claw, and the base is provided with a central circular hole, an annular guide groove concentric with the central circular hole and a straight guide groove along the radial direction of the annular guide groove; the articulated shaft between each connecting rod of many link mechanism is located annular guide way, and the lower extreme of wheel hub pressure claw is located straight guide way, makes wheel hub pressure claw and the connecting rod of its connection form slider-crank mechanism, and the wheel hub mounting panel has the central round hole with base concentric line, and the lock is fixed in the base upper end, and each wheel hub pressure claw stretches out outside the wheel hub mounting panel, can self-centering clamp the wheel hub of different specifications. When the clamp clamps the hub and transmits the bearing to be pressed, the hub does not need to be turned over, and the production efficiency can be greatly improved.
Description
Technical Field
The invention relates to an automatic production line of an airplane hub, in particular to a hub clamp for an airplane hub assembly line and an application method thereof.
Background
In the field of hub production and processing and assembly, parts such as bearings and bolts of a hub are assembled, the hub is mainly manually placed on a fixed working table or a fixed fixture body for assembly, and the assembled hub is placed into a finished product area manually or by a manipulator after the assembly is finished.
The related patents of the existing hub clamp mainly focus on the processing of the hub and the automatic conveying of the hub.
ZL201621342032.0 a wheel hub carries double-layered anchor clamps discloses can realize automatic handling, guarantee wheel hub apparent quality's wheel hub carries double-layered anchor clamps in wheel hub transport technical field, and its structure includes ring flange, anchor clamps frame, wheel rail anchor clamps, and wherein wheel hub anchor clamps include clamping mechanism, prevent the mechanism that falls, are equipped with the wheel hub anchor clamps of two symmetries on the anchor clamps frame, can carry two wheel hubs simultaneously.
201711407432.4A hub clamp discloses a hub clamp capable of adjusting and clamping hubs of different models in the technical field of vehicle tooling, the structure of the hub clamp comprises a mounting seat, a hub platform, a plurality of slide rails, a horizontal telescopic mechanism and a clamping mechanism, a clamping groove is formed in the clamping mechanism, the height of the hub platform and the clamping mechanism can be adjusted, the clamping radius of the clamping mechanism can be adjusted, and the clamping of the hubs of different models can be realized.
201520499740.4A hub anchor clamps discloses the hub anchor clamps of the wheel hub of a kind of fixed multiple specification and fixed drilling machine in automobile wheel hub processing field, its structure mainly includes the base, the backing plate, the curb plate, the slide bar, the base plate, a fixed base, the dead lever, fixed knob etc., wheel hub places on the base plate, it is fixed to press from both sides tight through the slidable fixed strip, install the slide on the side, install the lifter on the slide, install the mount pad that can fix the drilling machine on the lifter, can improve the machining precision of wheel hub when drilling.
201620162246.3A novel hub clamp comprises a case, a support shaft, a clamping device, a rotary linkage device, an auxiliary pressing device and the like, which realizes the fixation of hubs with different sizes, is convenient for renovating the inner and outer diameters of the hubs, and is especially suitable for the tyre removing operation of tyre hubs.
To sum up, most hub clamps are used for carrying hubs at present, but are not suitable for material circulation of the hubs at different stations of an automatic assembly line, or are only used for assembling hub parts on a certain fixed platform or equipment, and meanwhile, the hubs need to be turned over when bearings on the other side of the hubs are installed, so that the hub clamps are complex in operation, high in labor intensity and low in working efficiency.
In other words, in the current bearing assembly technology of the hub, although there are hub clamps which can adapt to various specifications, there is no tooling device which can be circulated on an automatic production line and is suitable for hub assembly.
Disclosure of Invention
The invention aims to provide a hub clamp which can clamp hubs of different specifications to flow among different stations of an automatic assembly production line and can greatly improve the hub assembly efficiency and an application method thereof.
The invention provides a hub clamp for an aircraft hub assembly line, which comprises a base, a clamping mechanism and a hub mounting plate, wherein the clamping mechanism comprises a multi-link mechanism, a locking mechanism and a hub pressing claw which are connected with the multi-link mechanism; the articulated shaft between each connecting rod of many link mechanism is located annular guide way, and the lower extreme of wheel hub pressure claw is located straight guide way, makes wheel hub pressure claw and the connecting rod of its connection form slider-crank mechanism, and the wheel hub mounting panel has the central round hole with base concentric line, and the lock is fixed in the base upper end, and each wheel hub pressure claw stretches out outside the wheel hub mounting panel, can self-centering clamp the wheel hub of different specifications.
In the real-time mode of the technical scheme, the base comprises a base body formed by surrounding the bottom plate and the side plate frame, and a guide bearing and a buffer block are installed on the side plate frame, the bottom surface of the bottom plate is a smooth surface, the lower end of the side plate frame is connected to the periphery of the upper surface of the bottom plate, the guide bearing is vertically embedded in a vertical installation hole in the side plate frame, the outer edge of the guide bearing is located outside the outer wall of the side plate frame, and the buffer block is fixed on the outer wall of the side plate frame.
In a real-time mode of the technical scheme, the bottom plate is a rectangular plate with the central circular hole, the side plate frames are rectangular frames, the annular guide grooves are two concentric with the central circular hole, the guide bearings are symmetrically connected in the vertical mounting holes in one pair of side plates of the side plate frames, and the buffer blocks are symmetrically connected to the outer walls of the other pair of side plates on the bottom plate.
In a real-time mode of the above technical solution, there are four straight guide grooves, which are arranged in the radial direction of the upper surface of the bottom plate corresponding to the annular guide grooves and are respectively located at the middle positions in the length and width directions of the upper surface of the bottom plate, and each straight guide groove extends from the edge of the upper surface of the bottom plate to the central circular hole until approaching the small-diameter annular guide groove.
In a real-time mode of the technical scheme, the multi-connecting-rod mechanism comprises four groups of two connecting rod mechanisms which are hinged with each other, each group of two connecting rod mechanisms comprises a long connecting rod and a short connecting rod which are hinged with each other end to end, the long connecting rods of the four groups of two connecting rod mechanisms are hinged with each other in a clockwise or anticlockwise direction in sequence, and the outer ends of the short connecting rods are provided with round holes.
In a real-time mode of the above technical solution, when the multi-link mechanism is installed on the bottom plate, lower ends of hinge shafts between the long links and the short links are inserted into the large-diameter annular guide groove on the bottom plate, and lower ends of hinge shafts between the long links are inserted into the small-diameter annular guide groove.
In a real-time mode of the technical scheme, the hub pressing claw comprises a pressing head, a guide rod, a pressing cushion pad and a pressing block, the pressing head is of a 7-shaped structure, the guide rod is connected to the lower end of a vertical arm of the pressing head, the width of the guide rod is smaller than that of the pressing head, the lower end of the guide rod is an insertion column matched with a round hole in the outer end of the short connecting rod, the pressing cushion pad is connected to the inner side of the vertical arm of the pressing head, the width of the upper end section of the pressing cushion pad is consistent with that of the vertical arm of the pressing head, the width of the lower end section of the pressing cushion pad is consistent with that of the guide rod, the outer end of.
In a real-time mode of the technical scheme, each side wall of the side plate frame is disconnected at each straight guide groove, the fracture is in a splayed shape with a large opening end facing inwards, the guide rod of the hub pressing claw is located in the fracture, and the insertion column at the lower end of the guide rod penetrates through the round hole at the outer end of the short connecting rod and then is inserted into the straight guide groove.
In a real-time mode of the above technical scheme, the locking mechanism includes a connecting lever connecting rod and a driving member, one end of the connecting lever connecting rod is hinged to a short connecting rod of one of the two link mechanisms of the link mechanism, the driving member is connected to the other end of the connecting lever connecting rod, and a corner of the connecting lever connecting rod is hinged to the bottom plate.
In a real-time mode of the technical scheme, the hub mounting plate is a rectangular plate with the same plane size as the base bottom plate, the bottom surface of the hub mounting plate is provided with a central round hole and an annular guide groove which correspond to the bottom plate, a radial stroke groove of the hub pressing claw is arranged on the hub mounting plate corresponding to the straight guide groove, and a guide rod of the hub pressing claw is positioned in the stroke groove; the hub mounting plate is also provided with a driving member movement stroke groove; and the upper ends of the hinged shafts between the long connecting rods and the short connecting rods of the multi-connecting-rod mechanism are inserted into corresponding annular guide grooves on the hub mounting plate.
The invention provides a method for clamping an airplane hub by using the clamp, which comprises the following steps:
(1) mounting the multi-link mechanism on a rectangular bottom plate of a base;
(2) connecting the locking mechanism and the hub pressing claw to the multi-link mechanism;
(3) buckling a hub mounting plate on a rectangular side frame of the base and fastening the hub mounting plate and the rectangular side frame, wherein a pressing head of a hub pressing claw and a pressing cushion pad extend out of the hub mounting plate;
(4) placing the hub on the hub mounting plate;
(5) pulling a handle of the locking mechanism to enable the multi-link mechanism to drive each wheel hub pressing claw to slide along the value guide groove on the rectangular bottom plate until the pressing cushion pad of each wheel hub pressing claw abuts against the edge of the wheel hub;
(6) the screw rod connected with the pressing block for rotating the hub pressing claw is used for pressing the hub by the bottom surface of the pressing block.
According to the invention, the clamping mechanism capable of automatically centering is arranged between the base and the hub mounting plate, hubs with different specifications can be clamped through the clamping mechanism, and the axial center line of the hub and the central round holes on the base and the hub mounting plate share the same axial center line, so that the press-fitting assembly process of bearings at two ends of the hub can be realized without changing the direction of the hub. The wheel hub is clamped through the tool, the conveying belt of the automatic assembly production line can convey the wheel hub to each station for press mounting and assembling of bearings at two ends of the wheel hub, the wheel hub does not need to be turned over in the prior art, and production efficiency can be greatly improved. The self-centering clamping principle of the clamping mechanism is as follows: the lower end of each hinged shaft between the long connecting rods of the multi-connecting rod mechanism is inserted into a small-diameter annular guide groove on the rectangular bottom plate, the lower end of each hinged shaft between the long connecting rods and the short connecting rods is inserted into a large-diameter annular guide groove, when a handle of the locking mechanism is pulled, the crank arm connecting rods of the locking mechanism pull the multi-connecting rod mechanism, so that the short connecting rods of the multi-connecting rod mechanism and a crank block mechanism formed by wheel hub pressing claws slide along each straight guide groove on the rectangular bottom plate simultaneously until each wheel hub pressing claw presses the wheel hub tightly at the same time, and the axial center line of the wheel hub is superposed with the center round holes of the rectangular bottom.
Drawings
Fig. 1 is a schematic view of a front view of a usage state according to an embodiment of the present invention.
FIG. 2 is a top view of the FIG. 1 schematic (without the workpiece hub shown).
FIG. 3 is a top view of the multi-bar linkage assembly of FIG. 1 assembled with a base.
Fig. 4 is a bottom schematic view of the hub mounting plate of fig. 2.
Fig. 5 is a schematic axial side structure diagram of the use state of the present embodiment.
Fig. 6 is a schematic axial side structure diagram of the clamping mechanism of the present embodiment.
Fig. 7 is a schematic axial side structure view of the hub pressing claw of the embodiment.
Detailed Description
As can be seen from fig. 1 to 3, the hub fixture for the aircraft hub assembly line disclosed in the present embodiment includes a base 1, a clamping mechanism 2, and a hub mounting plate 3.
As can be seen from fig. 1 to 3, the base 1 of the present embodiment is a rectangular base, and includes a rectangular bottom plate 11, a side plate frame 12, a guide bearing 13, and a buffer block 14.
The side plate frame 12 is a rectangular frame and is connected to the periphery of the upper surface of the rectangular bottom plate 11, the guide bearings 13 are symmetrically installed in vertical installation holes of a pair of side walls of the side plate frame 12, and the outer sides of the other pair of side walls of the side plate frame are symmetrically connected with the buffer blocks 14. When this anchor clamps are carrying wheel hub circulation on the logistics line, the direction bearing of both sides plays the direction and reduces the effect of resistance. When the clamp carries a hub to move on a production line to collide with a front blocking mechanism or a rear clamp collides with the front clamp, the buffer blocks at the front end and the rear end play roles in buffering, energy absorption and vibration reduction.
As can be seen from fig. 1 and 3, the rectangular bottom plate 11 has a central circular hole 111, and a small-diameter annular guide groove 112 and a large-diameter annular guide groove 113 concentrically surrounding the central circular hole. The upper surface of the rectangular bottom plate is also symmetrically provided with four straight guide grooves 114 along the length direction and the width direction, and each straight guide groove passes through the large-diameter annular guide groove and is close to the small-diameter annular guide groove.
As can be seen in connection with fig. 1 to 3, the clamping mechanism 2 comprises a multi-link mechanism 21, a locking mechanism 22 and a hub pressing claw 23.
As can be seen from fig. 3, the multi-link mechanism 21 includes four sets of two-link mechanisms, each set of two-link mechanism includes a long link 211 and a short link 212 hinged end to end, the long links of each set of two-link mechanism are hinged in turn clockwise or counterclockwise, and the free ends of the short links have round holes.
As shown in fig. 3, when the multi-link mechanism 21 is mounted on the rectangular base plate 11, the lower ends of the hinge shafts between the long links and the short links are inserted into the large-diameter annular guide groove 113 on the rectangular base plate, and the lower ends of the hinge shafts between the long links are inserted into the small-diameter annular guide groove 112. And the upper end of each articulated shaft extends out of the multi-link mechanism.
As can be seen from fig. 1 to 3, the locking mechanism 22 includes a connecting lever 221 and a driving handle 222, wherein the inner end of the connecting lever is hinged to any one of the short links 212, the driving handle is connected to the outer end of the connecting lever, and the corner of the connecting lever 221 is hinged to the rectangular bottom plate 11 through a hinge shaft.
The corresponding side wall of the side plate frame 12 of the base 1 is provided with a mounting and moving groove of the outer end of the crank arm connecting rod 221.
As can be seen from fig. 1 to 7, there are four hub holding-down claws 23, and each hub holding-down claw 23 includes a holding-down head 231, a guide rod 232, a holding-down cushion 233, a holding-down piece 234, and a screw 235. The compression head 231 is of a 7-shaped configuration. The guide rod 232 is connected to the lower end of the vertical arm of the compression head, the width of the guide rod is smaller than that of the compression head, and the lower end of the guide rod is a plug-in column matched with the circular hole in the outer end of the short connecting rod 212. The compression cushion 233 is attached to the inside of the compression head vertical arm, with its upper end section having a width corresponding to the compression head vertical arm width and its lower end section having a width corresponding to the guide bar width. The outer end of the horizontal arm of the pressing head 231 is connected with a vertical screw rod 235, the lower end of the screw rod penetrates through the horizontal arm and then is connected with a pressing block 234, and the screw rod is rotated to adjust the height position of the pressing block.
Each side wall of the side plate frame 12 is disconnected corresponding to each straight guide groove 114, the fracture is in a splayed shape with a large opening end facing inwards, the guide rod 232 of the hub pressing claw 23 is positioned in the fracture, and the insertion column at the lower end of the guide rod 232 penetrates through the round hole at the outer end of the short connecting rod 212 and then is inserted into the straight guide groove 114.
As can be seen from fig. 1, 2 and 4, the hub mounting plate 3 is a rectangular plate having the same plane size as the rectangular bottom plate 11, and the lower surface thereof has a central circular hole and large and small annular guide grooves corresponding to those of the rectangular bottom plate 11.
The hub mounting plate 3 is further provided with a hub pressing claw mounting groove 31 corresponding to the position of the straight guide groove 114 on the rectangular bottom plate 11, the length of the hub pressing claw mounting groove 31 is the same as that of the straight guide groove, the width of the hub pressing claw mounting groove is slightly larger than that of the guide rod 232, and the hub pressing claw mounting groove 31 penetrates through the thickness of the hub mounting plate 3.
The hub mounting plate 3 is also provided with a locking mechanism movement stroke groove 32.
During assembly of the device, the multi-link mechanism 21 is firstly installed on the rectangular bottom plate 11, the locking mechanism 22 and the hub pressing claw 23 are installed on the multi-link mechanism 21, and then the hub installation plate 3 is buckled on the rectangular side frame 12 and fastened through screws. After the hub mounting plate 3 is fixed, the pressing head 231 and the pressing cushion 232 of the hub pressing claw 23 extend out of the hub mounting plate 3. After the hub LG is placed on the hub mounting plate 3, the handle of the locking mechanism 22 is pulled, so that the multi-link mechanism 21 drives each hub pressing claw 23 to slide along the straight guide groove 114 on the rectangular bottom plate 11 until the pressing cushion 232 of each hub pressing claw 23 abuts against the edge of the hub, and then the screw 235 connected with the pressing block 234 is rotated, so that the bottom surface of the pressing block 234 presses the hub.
The self-centering principle of the clamping mechanism is as follows: the lower end of each hinged shaft between the long connecting rods of the multi-connecting rod mechanism is inserted into a small-diameter annular guide groove on the rectangular bottom plate, the lower end of each hinged shaft between the long connecting rods and the short connecting rods is inserted into a large-diameter annular guide groove, when a handle of the locking mechanism is pulled, the crank arm connecting rods of the locking mechanism pull the multi-connecting rod mechanism, so that the short connecting rods of the multi-connecting rod mechanism and a crank block mechanism formed by wheel hub pressing claws slide along each straight guide groove on the rectangular bottom plate simultaneously until each wheel hub pressing claw presses the wheel hub tightly at the same time, and the axial center line of the wheel hub is superposed with the center round holes of the rectangular bottom.
Claims (10)
1. A wheel hub anchor clamps for aircraft wheel hub assembly line which characterized in that: the clamping mechanism comprises a multi-link mechanism, a locking mechanism and a hub pressing claw which are connected with the multi-link mechanism, the multi-link mechanism is arranged on the base and is provided with a plurality of free ends, each free end is respectively and vertically connected with the hub pressing claw, and the base is provided with a central round hole, an annular guide groove concentric with the central round hole and a straight guide groove along the radial direction of the annular guide groove; the articulated shaft between each connecting rod of many link mechanism is located annular guide way, and the lower extreme of wheel hub pressure claw is located straight guide way, makes wheel hub pressure claw and the connecting rod of its connection form slider-crank mechanism, and the wheel hub mounting panel has the central round hole with base concentric line, and the lock is fixed in the base upper end, and each wheel hub pressure claw stretches out outside the wheel hub mounting panel, can self-centering clamp the wheel hub of different specifications.
2. A hub clamp for an aircraft hub assembly line according to claim 1, wherein: the base includes the pedestal that bottom plate and side plate frame enclose and installs guide bearing and buffer block on the curb plate frame, and the bottom surface of bottom plate is the smooth surface, and the lower extreme of side plate frame is connected in the upper surface periphery of bottom plate, and guide bearing inlays along vertical in the vertical mounting hole of inlaying on the side plate frame, and guide bearing's outer fringe is located outside the outer wall of side plate frame, and the buffer block is fixed in the outer wall of side plate frame.
3. A hub clamp for an aircraft hub assembly line according to claim 2, wherein: the bottom plate is a rectangular plate with the central round hole, the side plate frame is a rectangular frame, the annular guide grooves are concentric with the central round hole, the guide bearings are symmetrically connected in vertical mounting holes in a pair of side plates of the side plate frame, and the buffer blocks are symmetrically connected to the outer walls of the other pair of side plates on the bottom plate.
4. A hub clamp for an aircraft hub assembly line according to claim 3, wherein: the four straight guide grooves are arranged on the upper surface of the bottom plate in the radial direction corresponding to the annular guide grooves and are respectively positioned in the middle positions of the upper surface of the bottom plate in the length and width directions, and each straight guide groove extends from the edge of the upper surface of the bottom plate to the central circular hole until being close to the small-diameter annular guide groove.
5. A hub clamp for an aircraft hub assembly line according to claim 4, wherein: the multi-connecting-rod mechanism comprises four groups of two connecting rod mechanisms which are hinged with each other, each group of two connecting rod mechanisms comprises a long connecting rod and a short connecting rod which are hinged end to end, the long connecting rods of the four groups of two connecting rod mechanisms are sequentially hinged in a clockwise or anticlockwise direction, and the outer ends of the short connecting rods are provided with round holes; when the multi-link mechanism is installed on the bottom plate, the lower ends of hinged shafts between the long connecting rods and the short connecting rods are inserted into the large-diameter annular guide groove on the bottom plate, and the lower ends of the hinged shafts between the long connecting rods are inserted into the small-diameter annular guide groove.
6. A hub clamp for an aircraft hub assembly line according to claim 1, wherein: the hub pressing claw comprises a pressing head, a guide rod, a pressing cushion pad and a pressing block, the pressing head is of a 7-shaped structure, the guide rod is connected to the lower end of a vertical arm of the pressing head, the width of the guide rod is smaller than that of the pressing head, an inserting column matched with a round hole in the outer end of the short connecting rod is arranged at the lower end of the guide rod, the pressing cushion pad is connected to the inner side of the vertical arm of the pressing head, the width of the upper end section of the pressing cushion pad is consistent with that of the vertical arm of the pressing head, the width of the lower end section of the pressing cushion pad is consistent with that of the guide rod, the outer end.
7. A hub clamp for an aircraft hub assembly line according to claim 6, wherein: each side wall of the side plate frame is disconnected at each straight guide groove, the fracture is in a splayed shape with a large opening end facing inwards, the guide rod of the hub pressing claw is positioned in the fracture, and the insertion column at the lower end of the guide rod penetrates through the round hole at the outer end of the short connecting rod and then is inserted into the straight guide groove.
8. A hub clamp for an aircraft hub assembly line according to claim 3, wherein: the locking mechanism comprises a crank arm connecting rod and a driving component, one end of the crank arm connecting rod is hinged with a short connecting rod of one of the two connecting rod mechanisms of the connecting rod mechanism, the driving component is connected to the other end of the crank arm connecting rod, and corners of the crank arm connecting rod are hinged on the bottom plate.
9. A hub clamp for an aircraft hub assembly line according to claim 1, wherein: the hub mounting plate is a rectangular plate with the same plane size as the base bottom plate, the bottom surface of the hub mounting plate is provided with a central round hole and an annular guide groove which correspond to the bottom plate, a radial stroke groove of a hub pressing claw is arranged on the hub mounting plate corresponding to the straight guide groove, and a guide rod of the hub pressing claw is positioned in the stroke groove; the hub mounting plate is also provided with a driving member movement stroke groove; and the upper ends of the hinged shafts between the long connecting rods and the short connecting rods of the multi-connecting-rod mechanism are inserted into corresponding annular guide grooves on the hub mounting plate.
10. A method of clamping an aircraft hub with the clamp of claim 1, comprising the steps of:
(1) mounting the multi-link mechanism on a rectangular bottom plate of a base;
(2) connecting the locking mechanism and the hub pressing claw to the multi-link mechanism;
(3) buckling a hub mounting plate on a rectangular side frame of the base and fastening the hub mounting plate and the rectangular side frame, wherein a pressing head of a hub pressing claw and a pressing cushion pad extend out of the hub mounting plate;
(4) placing the hub on the hub mounting plate;
(5) pulling a handle of the locking mechanism to enable the multi-link mechanism to drive each wheel hub pressing claw to slide along the value guide groove on the rectangular bottom plate until the pressing cushion pad of each wheel hub pressing claw abuts against the edge of the wheel hub;
(6) the screw rod connected with the pressing block for rotating the hub pressing claw is used for pressing the hub by the bottom surface of the pressing block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911310198.2A CN110802407A (en) | 2019-12-18 | 2019-12-18 | Hub clamp for airplane hub assembly line and application method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911310198.2A CN110802407A (en) | 2019-12-18 | 2019-12-18 | Hub clamp for airplane hub assembly line and application method thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110802407A true CN110802407A (en) | 2020-02-18 |
Family
ID=69493265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201911310198.2A Pending CN110802407A (en) | 2019-12-18 | 2019-12-18 | Hub clamp for airplane hub assembly line and application method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110802407A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111730674A (en) * | 2020-06-30 | 2020-10-02 | 菏泽岸绿装饰有限公司 | Foamed plastic chisel for industrial design |
| CN115464391A (en) * | 2022-08-15 | 2022-12-13 | 珠海智新自动化科技有限公司 | Clamping device and rotary driving mechanism assembling equipment |
-
2019
- 2019-12-18 CN CN201911310198.2A patent/CN110802407A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111730674A (en) * | 2020-06-30 | 2020-10-02 | 菏泽岸绿装饰有限公司 | Foamed plastic chisel for industrial design |
| CN115464391A (en) * | 2022-08-15 | 2022-12-13 | 珠海智新自动化科技有限公司 | Clamping device and rotary driving mechanism assembling equipment |
| CN115464391B (en) * | 2022-08-15 | 2024-04-09 | 珠海智新自动化科技有限公司 | Clamping device and rotary driving mechanism assembling equipment |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109367327B (en) | Industrial fixed truckle automatic assembly equipment | |
| CN109500599B (en) | Automatic assembling equipment for piston assembly | |
| CN112475066A (en) | Full-automatic rivet pressing robot | |
| CN110802407A (en) | Hub clamp for airplane hub assembly line and application method thereof | |
| CN109227123B (en) | High-efficient lock body spring bolt equipment | |
| CN108274232B (en) | Automatic assembling machine for motor component of dust collector | |
| US20020170333A1 (en) | Hemming machine with movable die cartridges | |
| CN109202356A (en) | H profile steel overturns centering body | |
| KR101984303B1 (en) | Apparatus for centering nut hole and bolt hole of tire wheel | |
| CN103639787A (en) | Clamping working platform for precise fan-shaped ceramic part | |
| CN109514243B (en) | Screw machine | |
| CN211991755U (en) | Hub clamp for airplane hub assembly line | |
| CN111761018A (en) | Full-automatic drilling riveting machine | |
| CN108098295B (en) | Automobile headrest support rod assembling device | |
| CN104589055B (en) | A kind of vehicle dormer window produces equipment | |
| CN112247558A (en) | A lock nut material loading screws up device for piston assembly production | |
| CN208644595U (en) | Screw automatic assembling machine | |
| CN116276028A (en) | Automatic assembly production line and process for automobile door hinge | |
| CN107350418B (en) | Automatic assembling machine for magnetic sheet framework | |
| CN220387805U (en) | Double riveting machine for riveting automobile components | |
| CN112739195A (en) | Intelligent manufacturing equipment for power circuit board | |
| CN218808899U (en) | Mould processing and carrying device | |
| CN108015542B (en) | Headlight lens assembly mechanism | |
| CN213080837U (en) | Copying positioning device for automobile flange | |
| CN110774006A (en) | G type card automatic molding equipment |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination |