CN207723409U - A kind of light aerocraft shell riveting jig - Google Patents
A kind of light aerocraft shell riveting jig Download PDFInfo
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- CN207723409U CN207723409U CN201721635901.3U CN201721635901U CN207723409U CN 207723409 U CN207723409 U CN 207723409U CN 201721635901 U CN201721635901 U CN 201721635901U CN 207723409 U CN207723409 U CN 207723409U
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- traversing
- vertical shift
- riveting
- pedestal
- sliding rail
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Abstract
The utility model discloses a kind of light aerocraft shell riveting jigs, it includes pedestal, pedestal top is provided with detent mechanism, riveting mechanism, testing agency, control mechanism and operation panel, and testing agency's face detent mechanism setting, riveting mechanism is between detent mechanism and testing agency；Detent mechanism includes u-bracket, and u-bracket upper end is fixed with positioning plate, and boss is provided at left and right sides of positioning plate, telescopic block is provided on boss；Positioning plate one end vertical with the left and right sides is provided with fixed lobe, and the other end is provided with mobile protrusion, and mobile protrusion is connect with the driving mechanism being fixed in u-bracket；Riveting mechanism includes moving assembly and is arranged riveted joint on moving assembly top；Moving assembly includes the installation frame being fixedly connected with pedestal, and installation frame top is provided with transverse-moving mechanism and vertical shift mechanism, and transverse-moving mechanism includes traversing motor, and the output shaft of traversing motor is connect with traversing belt group.
Description
Technical field：
The utility model is related to assembled fixture technical fields, and in particular to a kind of light aerocraft shell riveting jig.
Background technology：
Light aerocraft refers to maximum take-off weight and is less than 5700 kilograms of aircraft, and light aerocraft has light, safety, using wanting
Ask it is low, can be in meadow landing, easily operated, cheap advantage, due to its small volume, construction is relatively easy, gradually quilt
Applied to leisure and business travel.With the exploitation of novel synthetic material, the shell of light aerocraft is firmer, light and handy so that
Flight energy consumption and stability, the safety all highers of light aerocraft.The shell of light aerocraft is spliced by polylith sheet metal component
, it in process of production, needs to rivet different case members, this will use and arrive riveting jig, existing riveting
Jig structure is complicated, and stability is poor, it is difficult to meet high-precision positioning needs.
Utility model content：
The purpose of this utility model provides a kind of outer shell rivething of light aerocraft and controls aiming at the deficiencies in the prior art
Tool.
The technology solution of the utility model is as follows：
A kind of light aerocraft shell riveting jig comprising pedestal, pedestal top be provided with detent mechanism, riveting mechanism,
Testing agency, control mechanism and operation panel, the setting of testing agency face detent mechanism, riveting mechanism be located at detent mechanism with
Between testing agency；Detent mechanism includes u-bracket, and u-bracket upper end is fixed with positioning plate, the left and right sides setting of positioning plate
There is boss, telescopic block is provided on boss；Positioning plate one end vertical with the left and right sides is provided with fixed lobe, other end setting
There are mobile protrusion, mobile protrusion to be connect with the driving mechanism being fixed in u-bracket；Riveting mechanism includes moving assembly and sets
Set the riveted joint on moving assembly top；Moving assembly includes the installation frame being fixedly connected with pedestal, and installation frame top is set
It is equipped with transverse-moving mechanism and vertical shift mechanism, transverse-moving mechanism includes traversing motor, and the output shaft of traversing motor is connect with traversing belt group,
It is provided with transverse slide rail on the inside of traversing belt group, is slided on transverse slide rail and is provided with traversing sliding block, traversing sliding block and traversing skin
Band group connection；Vertical shift mechanism includes vertical shift motor, and the output shaft of vertical shift motor is connect with vertical shift belt group, outside vertical shift belt group
Side is provided with vertical shift slide rail, is slided in vertical shift slide rail and is provided with vertical shift sliding block, and vertical shift auxiliary sliding rail is provided on traversing sliding block, is indulged
It moves on sliding block and is provided with traversing auxiliary sliding rail, slide plate slides are mounted on vertical shift auxiliary sliding rail and traversing auxiliary sliding rail, under slide plate
Portion is provided with assists sliding rail and the traversing vertical shift sliding slot for assisting sliding rail to be respectively cooperating with and traversing sliding slot with vertical shift；Slide plate top is arranged
There are riser, riser top to be provided with hoisting belts component, lifting motor is connect with hoisting belts component, and the side of riser is fixed with
Side panel is provided with lifting sliding rail on side panel, and lifting slider, lifting slider and hoisting belts component are provided on lifting sliding rail
It connects, riveting head bracket is installed on lifting slider, riveted joint is mounted on riveting head bracket.
Installation frame includes the bottom plate and cylinder being fixedly connected with pedestal.
Testing agency includes elevating mechanism, angle-adjusting mechanism and camera, and camera is fixed on angle by holder
On adjustment mechanism, angle-adjusting mechanism is further fixed with elevating mechanism, and elevating mechanism is fixedly connected with pedestal.
Driving mechanism is telescopic cylinder, and the piston rod of telescopic cylinder is connect with mobile protrusion, and pressure is provided in mobile protrusion
Force snesor, pressure sensor are electrically connected with control mechanism.
Control mechanism is electrically connected with testing agency, detent mechanism, riveting mechanism, operation panel.
Pedestal lower part is provided with column, and the bottom end of column is provided with detachable ground anchor, and detachable ground anchor includes ground feet support
And the cushion pad in ground feet support lower end is set.
The beneficial effects of the utility model are：The utility model is simple in structure, can be carried out to airplane skin accurate
Positioning, while coordinating the riveting operation of riveting mechanism completion airplane skin.
Description of the drawings：
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of riveting mechanism；
Fig. 3 is the structural schematic diagram of moving assembly；
Fig. 4 is the structural schematic diagram of detent mechanism.
Specific implementation mode：
It is right below in conjunction with the accompanying drawings in order to keep the above objects, features, and advantages of the utility model more obvious and easy to understand
Specific embodiment of the present utility model is described in detail.
As shown in Figs 1-4, a kind of light aerocraft shell riveting jig comprising pedestal 10,10 top of pedestal are provided with fixed
Position mechanism 6, riveting mechanism 5, testing agency 30, control mechanism 40 and operation panel 20,30 face detent mechanism of testing agency
6 settings, riveting mechanism 5 is between detent mechanism 6 and testing agency 30；Detent mechanism 6 includes u-bracket 60, u-bracket 60
Upper end is fixed with positioning plate 61, and the left and right sides of positioning plate 61 is provided with boss 611, telescopic block 612 is provided on boss 611；
The one end vertical with the left and right sides of positioning plate 61 is provided with fixed lobe 621, and the other end is provided with mobile protrusion 622, and movement is convex
622 are played to connect with the driving mechanism 63 being fixed in u-bracket 60；Riveting mechanism 5 includes moving assembly and is arranged in movement
The riveted joint 7 on component top；Moving assembly includes the installation frame being fixedly connected with pedestal 10, and installation frame top is provided with cross
Telephone-moving structure and vertical shift mechanism, transverse-moving mechanism include traversing motor 530, and the output shaft of traversing motor 530 connects with traversing belt group 531
It connecing, the inside of traversing belt group 531 is provided with transverse slide rail 532, is slided on transverse slide rail 532 and is provided with traversing sliding block 533,
Traversing sliding block 533 is connect with traversing belt group 531；Vertical shift mechanism includes vertical shift motor 520, the output shaft of vertical shift motor 520 with
Vertical shift belt group 521 connects, and the outside of vertical shift belt group 521 is provided with vertical shift slide rail 522, and setting is slided in vertical shift slide rail 522
There is vertical shift sliding block 523, vertical shift auxiliary sliding rail 551 is provided on traversing sliding block 533, traversing auxiliary is provided on vertical shift sliding block 523
Sliding rail 552, slide plate 55 are slidably mounted on vertical shift auxiliary sliding rail 551 and traversing auxiliary sliding rail 552, and 55 lower part of slide plate is provided with
Sliding rail 551 and the traversing vertical shift sliding slot for assisting sliding rail 552 to be respectively cooperating with and traversing sliding slot are assisted with vertical shift；55 top of slide plate is arranged
There are riser 543, riser top to be provided with hoisting belts component 541, lifting motor 540 is connect with hoisting belts component 541, is stood
The side of plate is fixed with side panel, and lifting sliding rail 542 is provided on side panel, lifting slider 56 is provided on lifting sliding rail 542,
Lifting slider 56 is connect with hoisting belts component 541, and riveting head bracket 560 is equipped on lifting slider 56, and riveted joint 7 is installed
On riveting head bracket 560.
Installation frame includes the bottom plate 512 being fixedly connected with pedestal 10 and cylinder 511.
Testing agency 30 includes elevating mechanism, angle-adjusting mechanism and camera, and camera is fixed on angle by holder
It spends on adjustment mechanism, angle-adjusting mechanism is further fixed with elevating mechanism, and elevating mechanism is fixedly connected with pedestal.
Driving mechanism 63 is telescopic cylinder, and the piston rod of telescopic cylinder is connect with mobile protrusion 622, in mobile protrusion 622
It is provided with pressure sensor, pressure sensor is electrically connected with control mechanism.
Control mechanism 40 is electrically connected with testing agency 30, detent mechanism 6, riveting mechanism 5, operation panel 20.
10 lower part of pedestal is provided with column, and the bottom end of column is provided with detachable ground anchor 101, and detachable ground anchor 101 includes
Ground feet support and cushion pad in ground feet support lower end is set.
The embodiment rather than limits the present invention the utility model is illustrated.Any this field
Technical staff can modify to the embodiment, therefore this practicality under the spirit and scope without prejudice to the utility model
Novel rights protection scope, should be as listed by the claim of the utility model.
Claims (6)
1. a kind of light aerocraft shell riveting jig, it is characterised in that：It includes pedestal (10), and pedestal (10) top is provided with fixed
Position mechanism (6), riveting mechanism (5), testing agency (30), control mechanism (40) and operation panel (20), testing agency (30)
Face detent mechanism (6) is arranged, and riveting mechanism (5) is located between detent mechanism (6) and testing agency (30)；Detent mechanism (6)
Including u-bracket (60), u-bracket (60) upper end is fixed with positioning plate (61), is provided at left and right sides of positioning plate (61) convex
Platform (611) is provided with telescopic block (612) on boss (611)；Positioning plate (61) one end vertical with the left and right sides is provided with fixation
Raised (621), the other end are provided with mobile raised (622), mobile protrusion (622) and the driving being fixed in u-bracket (60)
Mechanism (63) connects；Riveting mechanism (5) includes moving assembly and is arranged riveted joint (7) on moving assembly top；Mobile group
Part includes the installation frame being fixedly connected with pedestal (10), and installation frame top is provided with transverse-moving mechanism and vertical shift mechanism, traversing
Mechanism includes traversing motor (530), and the output shaft of traversing motor (530) is connect with traversing belt group (531), traversing belt group
(531) it is provided with transverse slide rail (532) on the inside of, is slided on transverse slide rail (532) and is provided with traversing sliding block (533), traversing cunning
Block (533) is connect with traversing belt group (531)；Vertical shift mechanism includes vertical shift motor (520), the output shaft of vertical shift motor (520)
It is connect with vertical shift belt group (521), vertical shift slide rail (522), vertical shift slide rail (522) is provided on the outside of vertical shift belt group (521)
Upper sliding is provided with vertical shift sliding block (523), and vertical shift auxiliary sliding rail (551), vertical shift sliding block are provided on traversing sliding block (533)
(523) traversing auxiliary sliding rail (552) is provided on, slide plate (55) is slidably mounted on vertical shift auxiliary sliding rail (551) and traversing auxiliary
On sliding rail (552), slide plate (55) lower part is provided with to be respectively cooperating with vertical shift auxiliary sliding rail (551) and traversing auxiliary sliding rail (552)
Vertical shift sliding slot and traversing sliding slot；Slide plate (55) top is provided with riser (543), and riser top is provided with hoisting belts component
(541), lifting motor (540) is connect with hoisting belts component (541), and the side of riser is fixed with side panel, is set on side panel
It is equipped with lifting sliding rail (542), lifting slider (56), lifting slider (56) and hoisting belts group are provided on lifting sliding rail (542)
Part (541) connects, and riveting head bracket (560) is equipped on lifting slider (56), and riveted joint (7) is mounted on riveting head bracket
(560) on.
2. a kind of light aerocraft shell riveting jig according to claim 1, it is characterised in that：Installation frame includes and bottom
The bottom plate (512) and cylinder (511) that seat (10) is fixedly connected.
3. a kind of light aerocraft shell riveting jig according to claim 1, it is characterised in that：Testing agency (30) includes
Elevating mechanism, angle-adjusting mechanism and camera, camera are fixed on by holder on angle-adjusting mechanism, and angle adjusts machine
Structure is further fixed with elevating mechanism, and elevating mechanism is fixedly connected with pedestal.
4. a kind of light aerocraft shell riveting jig according to claim 1, it is characterised in that：Driving mechanism (63) is to stretch
Contracting cylinder, the piston rod of telescopic cylinder are connect with mobile raised (622), are provided with pressure sensor on mobile protrusion (622), are pressed
Force snesor is electrically connected with control mechanism.
5. a kind of light aerocraft shell riveting jig according to claim 1, it is characterised in that：Control mechanism (40) and inspection
Mechanism (30), detent mechanism (6), riveting mechanism (5), operation panel (20) is surveyed to be electrically connected.
6. a kind of light aerocraft shell riveting jig according to claim 1, it is characterised in that：Pedestal (10) lower part is arranged
There are column, the bottom end of column to be provided with detachable ground anchor (101), detachable ground anchor (101) includes that ground feet support and setting exist
The cushion pad of ground feet support lower end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721635901.3U CN207723409U (en) | 2017-11-30 | 2017-11-30 | A kind of light aerocraft shell riveting jig |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721635901.3U CN207723409U (en) | 2017-11-30 | 2017-11-30 | A kind of light aerocraft shell riveting jig |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207723409U true CN207723409U (en) | 2018-08-14 |
Family
ID=63089133
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721635901.3U Active CN207723409U (en) | 2017-11-30 | 2017-11-30 | A kind of light aerocraft shell riveting jig |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207723409U (en) |
-
2017
- 2017-11-30 CN CN201721635901.3U patent/CN207723409U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190723 Address after: 312500 No. 1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee after: Wanfeng Aircraft Industry Co., Ltd. Address before: 312500 No. 1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee before: Wanfeng Aviation Industry Co Ltd |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220221 Address after: 312500 No.1-3 (building 1-5), Aofeng Road, Wozhou Town, Xinchang County, Shaoxing City, Zhejiang Province Patentee after: Zhejiang Wanfeng Aircraft Manufacturing Co.,Ltd. Address before: 312500 No.1 Aofeng Road, Xinchang Industrial Park, Xinchang County, Shaoxing City, Zhejiang Province Patentee before: Wanfeng Aircraft Industry Co.,Ltd. |