CN206692296U - A kind of transmission device of Multi Role Aircraft - Google Patents
A kind of transmission device of Multi Role Aircraft Download PDFInfo
- Publication number
- CN206692296U CN206692296U CN201621404927.2U CN201621404927U CN206692296U CN 206692296 U CN206692296 U CN 206692296U CN 201621404927 U CN201621404927 U CN 201621404927U CN 206692296 U CN206692296 U CN 206692296U
- Authority
- CN
- China
- Prior art keywords
- connecting rod
- lifting body
- rod lifting
- transmission device
- central shaft
- 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.)
- Expired - Fee Related
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- Transmission Devices (AREA)
Abstract
A kind of transmission device of Multi Role Aircraft, power gear drive central shaft to make revolution and rotated by terminal pad, and the top of rotary shaft is discoid, and its periphery passes through through hole installing connecting rods lifting body；Connecting rod lifting body bottom installation jacking block, jacking block move in the groove of cylindrical cam, realize the up and down motion of connecting rod lifting body；Line shaft drives rotating gear I to rotate from above with contiguous block, and it drives rotating gear II to rotate, and rotating gear II passes through key connection with connecting rod lifting body.When device works, while connecting rod lifting body is revolved round the sun by central shaft, rotation is acted by the band of rotating gear I, while a kind of resultant motion is combined into up and down motion, the mould above connecting rod lifting body is set to control tank body or cover motion, to reach the purpose of capping.The transmission device is by the double dynamical self-movement for realizing revolution and rotation, and speed is easy to adjust, while the route being driven shortens, and rotary inertia diminishes, it is easier to installation and maintenance.
Description
Technical field
It the utility model is related to food package, more particularly to a kind of transmission device of Multi Role Aircraft.
Background technology
At present, the packaging for having many both at home and abroad all uses tinplate can, there is one between the tank body and cover of can
The process of capping, the process generally covered is completed by multi-functional combination machine, because combination machine has needed
Into enter fill, send the processes such as lid, positioning, crimping, discharging, in order to complete these actions in a table apparatus, so the transmission of device
Process is more complicated.The transmission device used at this stage is such (referring to Fig. 5), and fixing axle 20 is fixed with body to be kept prohibiting
Only, power gear I 22 is fixed by terminal pad I 23 and rotating cylinder 24, and power gear is connected by bearing 21 with fixing axle 20,
Fixed gear 25 is fixed in fixing axle 20 by key, and transition gear 26 is arranged on rotating cylinder, with turning for rotating cylinder
Dynamic drivening rod lifting body I 27 rotates, using single power, the rotating speed of connecting rod lifting body I 27 and turning for rotating cylinder 24
The ratio between speed is constant, and the route being driven is long, and top is more complicated.
A kind of transmission device for Multi Role Aircraft that the utility model refers to by double dynamical by realizing revolution and rotation
Self-movement, speed is easy to adjust, while the route being driven shortens, and rotary inertia diminishes, it is easier to installation and maintenance.
Utility model content
Weak point present in regarding to the issue above, the utility model provide a kind of transmission device of Multi Role Aircraft.
To achieve the above object, the utility model provides a kind of transmission device of Multi Role Aircraft, including：
Central shaft, the top of the central shaft is discoid, processing through hole at the periphery of the disk, in the disk
Groove is processed at the heart, is fixedly connected below the central shaft by terminal pad with power teeth crop rotation；
The central shaft is fixed in frame by top combination bearing body and bottom combination bearing body；
Cylindrical cam, the cylindrical cam are arranged in the frame；
Connecting rod lifting body, the connecting rod lifting body are arranged on the through hole, below the connecting rod lifting body
To jack block, the jacking block is arranged in the cam groove of the cylindrical cam；
Line shaft, the line shaft are driven by actuating unit above, and the line shaft is arranged on by double-row bearing
The groove；
The line shaft is fixedly connected by contiguous block with rotating gear I, and the rotating gear I is carried out with rotating gear II
Rotation connection, the rotating gear II are connected with the connecting rod lifting body.
Further improved as the utility model, be spline below the central shaft, the central shaft passes through the flower
Key is connected with the terminal pad.
Further improve as the utility model, positioned below the terminal pad by pressing plate.
Further improved as the utility model, the structure of the top combination bearing body and the bottom combination bearing body
Unanimously, including plane bearing is connected by bearing holder (housing, cover) with roller bearing, and the outside of the roller bearing is fixed by gland.
Further improved as the utility model, the rotating gear II is connected with the connecting rod lifting body by flat key
Connect.
Further improved as the utility model, positioning fixture is installed above the connecting rod lifting body.
The beneficial effects of the utility model are：
1. using the double dynamical self-movement for realizing revolution and rotation, speed is easy to adjust, makes the versatility of device stronger,
By the regulation to friction speed, make the seaming effect of can more preferable.
2. the route for making transmission using double-power mechanism shortens, device is simple, convenient to install and maintain.
3. due to the rotation without figure cylinder, rotary inertia is set to diminish, when there is fortuitous event, braking is more convenient.
4. central shaft is positioned using combination bearing body, make the radial direction of central shaft and will not axially shift.
Brief description of the drawings
Fig. 1 is a kind of front view of the transmission device of Multi Role Aircraft of the utility model；
Fig. 2 is the partial enlarged drawing at A positions in Fig. 1；
Fig. 3 is the sectional view of part centre axle；
Fig. 4 is Fig. 3 top view；
Fig. 5 is the front view of existing transmission device.
In figure：1st, central shaft；101st, spline；102nd, groove；103rd, through hole；2nd, terminal pad；3rd, power gear；4th, bottom group
Close bearing body；41st, plane bearing；42nd, bearing holder (housing, cover)；43rd, roller bearing；44th, gland；5th, frame；6th, cylindrical cam；7th, upper group
Close bearing body；8th, block is jacked；9th, connecting rod lifting body；10th, double-row bearing；11st, line shaft；12nd, contiguous block；13rd, rotating gear
Ⅰ；14th, rotating gear II；20th, fixing axle；21st, bearing；22nd, power gear I；23rd, terminal pad I；24th, rotating cylinder；25th, it is solid
Fixed gear；26th, transition gear；27th, connecting rod lifting body I.
Embodiment
As shown in figure 1, a kind of transmission device of Multi Role Aircraft described in the utility model embodiment, including：Central shaft 1
Top is discoid, is fixedly connected below central shaft 1 by terminal pad 2 with power gear 3；Central shaft 1 passes through spline
101 are connected with terminal pad 2, are positioned below terminal pad 2 by pressing plate.Central shaft 1 passes through top combination bearing body 7 and bottom group
Bearing body 4 is closed to be fixed in frame 5；Cylindrical cam 6 is arranged in frame 5；Connecting rod lifting body 9 is arranged at through hole 103, even
It is jacking block 8 below bar lifting body 9, jacking block 8 is arranged in the cam groove of cylindrical cam 6；Line shaft 11 is by upper
The actuating unit in face is driven, and line shaft is arranged at groove 102 by double-row bearing 10；Line shaft 11 by contiguous block 12 with
Rotating gear I 13 is fixedly connected, and rotating gear I 13 is rotatablely connected with rotating gear II 14, rotating gear II 14 and connecting rod
Lifting body 9 is rotatablely connected.Rotating gear II 14 is connected with connecting rod lifting body 9 by flat key.Above connecting rod lifting body 9
Positioning fixture is installed.
As shown in Fig. 2 top combination bearing body 7 is consistent with the structure of bottom combination bearing body 4, including plane bearing 41 is logical
Cross bearing holder (housing, cover) 42 to be connected with roller bearing 43, the outside of roller bearing 43 is fixed by gland 44.
As shown in Figure 3-4, the top of central shaft 1 is discoid that through hole 103, the center of disk are processed at the periphery of disk
Place processes groove 102, is spline 101 below central shaft 1.
As shown in figure 5, being the front view of existing transmission device, fixing axle 20 is bolted with body, power gear I
22 are fixed by terminal pad I 23 and rotating cylinder 24, and power gear is connected by bearing 21 with fixing axle 20, passes through power gear
Rotational band move rotating cylinder realize revolution.Fixed gear 25 is fixed in fixing axle 20 by key, and transition gear 26 is arranged on
On rotating cylinder, the little gear below transition gear is rotatablely connected with fixed gear 25, gear wheel and connecting rod jack above
Structure I 27 is rotatablely connected, and with the rotation of rotating cylinder, fixed gear 25 passes through the drivening rod lifting body I 27 of transition gear 26
Realize rotation.
Using the double dynamical self-movement for realizing revolution and rotation, speed is easy to adjust, makes the versatility of device stronger, leads to
The regulation to friction speed is crossed, makes the seaming effect of can more preferable.The route for making transmission using double-power mechanism shortens, device letter
It is single, it is convenient to install and maintain.Due to the rotation without figure cylinder, rotary inertia is set to diminish, when there is fortuitous event, braking is more
It is convenient.Central shaft is positioned using combination bearing body, is made the radial direction of central shaft and will not axially be shifted.
When specifically used, the utility model is understood for convenience, is described with reference to accompanying drawing；
When device works, power gear drives central axis by terminal pad, and connecting rod lifting body is arranged on central shaft
Through hole, realize revolution, jacking block is arranged in the cam groove of cylindrical cam, while the connecting rod lifting body is revolved round the sun
Realize and move up and down, line shaft is driven by actuating unit above, and line shaft is fixed by contiguous block and rotating gear I to be connected
Connect, rotating gear I is rotatablely connected with rotating gear II, and rotating gear II is rotatablely connected with connecting rod lifting body.By dynamic
The rotation drivening rod lifting body of power axle makees rotation, finally realizes the resultant motion of a kind of revolution, rotation and up and down motion, makes
Positioning fixture control tank body or cover motion above connecting rod lifting body, to reach the purpose of capping.
Preferred embodiment of the present utility model is the foregoing is only, is not limited to the utility model, for this
For the technical staff in field, the utility model can have various modifications and variations.It is all in the spirit and principles of the utility model
Within, any modification, equivalent substitution and improvements made etc., it should be included within the scope of protection of the utility model.
Claims (6)
- A kind of 1. transmission device of Multi Role Aircraft, it is characterised in that including：Central shaft (1), the top of the central shaft (1) is discoid, and through hole (103) is processed at the periphery of the disk, described Groove (102) is processed at the center of disk, is fixed below the central shaft (1) by terminal pad (2) and power gear (3) Connection；The central shaft (1) is fixed in frame (5) by top combination bearing body (7) and bottom combination bearing body (4)；Cylindrical cam (6), the cylindrical cam (6) are arranged in the frame (5)；Connecting rod lifting body (9), the connecting rod lifting body (9) are arranged on the through hole (103) place, the connecting rod lifting body (9) it is jacking block (8) below, the jacking block (8) is arranged in the cam groove of the cylindrical cam (6)；Line shaft (11), the line shaft (11) are driven by actuating unit above, and the line shaft passes through double-row bearing (10) it is arranged on the groove (102) place；The line shaft (11) is fixedly connected by contiguous block (12) with rotating gear I (13), the rotating gear I (13) with from Rotating disk II (14) is rotatablely connected, and the rotating gear II (14) is connected with the connecting rod lifting body (9).
- A kind of 2. transmission device of Multi Role Aircraft according to claim 1, it is characterised in that：Under the central shaft (1) Face is spline (101), and the central shaft (1) is connected by the spline (101) with the terminal pad (2).
- A kind of 3. transmission device of Multi Role Aircraft according to claim 2, it is characterised in that：Under the terminal pad (2) Face is positioned by pressing plate.
- A kind of 4. transmission device of Multi Role Aircraft according to claim 1, it is characterised in that：The top combination bearing body (7) it is consistent with the structure of the bottom combination bearing body (4), including plane bearing (41) passes through bearing holder (housing, cover) (42) and roller bearing (43) connect, the outside of the roller bearing (43) is fixed by gland (44).
- A kind of 5. transmission device of Multi Role Aircraft according to claim 1, it is characterised in that：The rotating gear II (14) It is connected with the connecting rod lifting body (9) by flat key.
- A kind of 6. transmission device of Multi Role Aircraft according to claim 5, it is characterised in that：The connecting rod lifting body (9) positioning fixture is installed above.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621404927.2U CN206692296U (en) | 2016-12-20 | 2016-12-20 | A kind of transmission device of Multi Role Aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621404927.2U CN206692296U (en) | 2016-12-20 | 2016-12-20 | A kind of transmission device of Multi Role Aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206692296U true CN206692296U (en) | 2017-12-01 |
Family
ID=60439050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621404927.2U Expired - Fee Related CN206692296U (en) | 2016-12-20 | 2016-12-20 | A kind of transmission device of Multi Role Aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206692296U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106744574A (en) * | 2016-12-20 | 2017-05-31 | 舟山市普陀博达机械制造有限公司 | A kind of transmission device of Multi Role Aircraft |
-
2016
- 2016-12-20 CN CN201621404927.2U patent/CN206692296U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106744574A (en) * | 2016-12-20 | 2017-05-31 | 舟山市普陀博达机械制造有限公司 | A kind of transmission device of Multi Role Aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20171201 Termination date: 20181220 |