CN205554691U - Automatic closing cap device of aircraft box - Google Patents
Automatic closing cap device of aircraft box Download PDFInfo
- Publication number
- CN205554691U CN205554691U CN201620350288.XU CN201620350288U CN205554691U CN 205554691 U CN205554691 U CN 205554691U CN 201620350288 U CN201620350288 U CN 201620350288U CN 205554691 U CN205554691 U CN 205554691U
- Authority
- CN
- China
- Prior art keywords
- capping
- frame
- closing cap
- plate
- aircraft box
- 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
Links
Landscapes
- Vacuum Packaging (AREA)
Abstract
The utility model discloses an automatic closing cap device of aircraft box, it includes and frame (1) is equipped with lifting bottom plate (713) on frame (1), and the one side of lifting bottom plate (713) is equipped with two pole cylinder (721), and the tip of two pole cylinder (721) is equipped with angle aluminium extension frame (722), and the inboard face of angle aluminium extension frame (722) is equipped with closing cap sucking disc group (723), closing cap sucking disc group (723) top is equipped with closing cap cylinder (724), and closing cap cylinder (724) below is equipped with capping movable plate (725), and the both sides of capping movable plate (725) are equipped with the capping side plate washer (726) that is the form of buckling. The utility model discloses can realize the automatic closing cap of aircraft box, have characteristics rational in infrastructure, that work efficiency is high, small, cheap.
Description
Technical field
This utility model relates to a kind of aircraft box automatic capping device, in particular with sucker,
Baffle plate and pneumatic element achieve the complete automatic sealing of aircraft box.
Background technology
Aircraft box folding machine in the market is the most all that volume is relatively big and can only fold and fly
The first half of machine box, folding and the capping of latter half can only be by manually completing.Almost do not have
The device having complete set can be fully achieved the complete folding of aircraft box.And along with in recent years
Carry out the application development of pneumatic element, set up the cost of a set of pneumatic means the most significantly under
Fall.And the structure of pneumatic means is very simple, medium is air, compared to hydraulic pressure, aerofluxus
Process simple, and more clean and safe.And the Reliability comparotive of pneumatic means is high, use
Life-span is long, and general air-operated solenoid valve is more than 30,000,000 times service life, and part all has
There are versatility, easy maintenance.Therefore the aircraft box automatic sealing of a employing pneumatics is researched and developed
Device, becomes problem urgently to be resolved hurrily.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of aircraft box automatic sealing
Device, this utility model can realize the automatic sealing of aircraft box, has rational in infrastructure, work
The feature that efficiency is high, volume is little, cheap.
The technical solution of the utility model: aircraft box automatic capping device, including frame, frame
Being provided with lifting base plate, the side of lifting base plate is provided with double-rod cylinder, and the end of double-rod cylinder sets
Having aluminum corner brace to extend frame, the inboard face of aluminum corner brace elongation frame is provided with capping sucker group；In capping sucker group
Side is provided with capping cylinder, is provided with capping movable plate, the both sides of capping movable plate below capping cylinder
It is provided with the capping side plate washer in bending.
In above-mentioned aircraft box automatic capping device, described lifting base plate is W shape profile plate.
In aforesaid aircraft box automatic capping device, described lifting base plate is provided with side and fixes
Plate.
Compared with prior art, drive when this utility model starts and be fixed on double-rod cylinder elongation,
Aluminum corner brace elongation frame is connected with the double-rod cylinder of stroke 75mm, and vacuum generator starts, and is fixed on
Capping sucker group on aluminum corner brace elongation frame picks up carton, is sent to be fixed on frame section material frame
W type lifting base plate on, wait next step action.Electromagnetic valve is restarted, and stretches with double-rod cylinder
Long, two panels capping side plate washer first contacts the capping of aircraft box and is folded, with baffle plate bracing frame
The aircraft lid face baffle plate being connected is pressed down, will press, a piece of lid under the lid face of aircraft box
Face movable plate is connected with two panels capping side plate washer L-type connector, owing to keeping off in aircraft lid face
During pressing under plate, two panels capping side plate washer retrains lid side so that it is complete jackknife action.
This utility model can realize the automatic sealing of aircraft box, have rational in infrastructure, work efficiency is high,
The feature that volume is little, cheap.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
With embodiment, this utility model is further described below in conjunction with the accompanying drawings, but does not make
For the foundation that this utility model is limited.
Embodiment: aircraft box automatic capping device, as shown in Figure 1, including frame 1, machine
Frame 1 is provided with lifting base plate 713, and the side of lifting base plate 713 is provided with double-rod cylinder 721,
The end of double-rod cylinder 721 is provided with aluminum corner brace elongation frame 722, the inboard face of aluminum corner brace elongation frame 722
It is provided with capping sucker group 723；Capping sucker group 723 is arranged over covering cylinder 724, capping
Being provided with capping movable plate 725 below cylinder 724, the both sides of capping movable plate 725 are provided with in curved
The capping side plate washer 726 of folding shape.Described lifting base plate 713 is W shape profile plate.Described
Lifting base plate 713 is provided with side fixed plate 714.Utility model works principle is as follows: electricity
Magnet valve starts, and drives and is fixed on double-rod cylinder elongation, aluminum corner brace elongation frame and stroke 75mmDouble
Bar cylinders, vacuum generator starts, and the capping sucker group being fixed on aluminum corner brace elongation frame is inhaled
Play carton, be sent on the W type lifting base plate that is fixed on frame section material frame, wait next
Step action.Electromagnetic valve is restarted, and extends with double-rod cylinder, and two panels capping side plate washer first contacts and flies
The capping of machine box is also folded, and the aircraft lid face baffle plate being connected with baffle plate bracing frame is and then
Under press, will press under the lid face of aircraft box, a piece of capping movable plate and two panels capping side plate washer are used
L-type connector is connected, during pressure under the baffle plate of aircraft lid face, and two panels capping side plate washer
Retrain lid side so that it is complete jackknife action.
Claims (3)
1. an aircraft box automatic capping device, it is characterised in that: include frame (1), machine
Frame (1) is provided with lifting base plate (713), and the side of lifting base plate (713) is provided with double-rod gas
Cylinder (721), the end of double-rod cylinder (721) is provided with aluminum corner brace elongation frame (722), and aluminum corner brace is stretched
The inboard face of long frame (722) is provided with capping sucker group (723)；In capping sucker group (723)
Side is provided with capping cylinder (724), and capping cylinder (724) lower section is provided with capping movable plate (725),
The both sides of capping movable plate (725) are provided with capping side plate washer (726) in bending.
Aircraft box automatic capping device the most according to claim 1, it is characterised in that:
Described lifting base plate (713) is W shape profile plate.
Aircraft box automatic capping device the most according to claim 1, it is characterised in that:
Described lifting base plate (713) is provided with side fixed plate (714).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350288.XU CN205554691U (en) | 2016-04-22 | 2016-04-22 | Automatic closing cap device of aircraft box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350288.XU CN205554691U (en) | 2016-04-22 | 2016-04-22 | Automatic closing cap device of aircraft box |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205554691U true CN205554691U (en) | 2016-09-07 |
Family
ID=56806307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620350288.XU Expired - Fee Related CN205554691U (en) | 2016-04-22 | 2016-04-22 | Automatic closing cap device of aircraft box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205554691U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628302A (en) * | 2017-01-09 | 2017-05-10 | 安徽杰瑞信息科技有限公司 | Packaging robot for food production |
-
2016
- 2016-04-22 CN CN201620350288.XU patent/CN205554691U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628302A (en) * | 2017-01-09 | 2017-05-10 | 安徽杰瑞信息科技有限公司 | Packaging robot for food production |
| CN106628302B (en) * | 2017-01-09 | 2018-11-16 | 安徽杰瑞信息科技有限公司 | A kind of packaging robot for food production |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205554691U (en) | Automatic closing cap device of aircraft box | |
| CN206728388U (en) | A kind of removable chip mounter | |
| CN202798384U (en) | Motor back end cover pressing-in device | |
| CN104931739B (en) | A kind of closing device of circuit board testing interface | |
| CN105270425B (en) | Intermediate mechanical case vacuumizes and pressue device and its application method | |
| CN104234938A (en) | Double-loop-bar vertical wind power generator capable of ascending and descending | |
| CN204660827U (en) | A kind of Acetabula device | |
| CN204082447U (en) | Two loop bar lifting/lowering type vertical wind power generator | |
| CN209080380U (en) | A kind of metal key-press switch full page is from film device | |
| CN206092318U (en) | Energy -efficient air compressor | |
| CN208856475U (en) | The material conveying device of FCT test machine | |
| CN202529826U (en) | Automatic CIP (cleaning in place) device | |
| CN207239632U (en) | A kind of full-automatic frame disassembly machine of solar photovoltaic assembly aluminium | |
| CN202169720U (en) | Carton forming machine with bonding mechanisms | |
| CN202895744U (en) | Hydraulic machine travelling table air source automatic docking device | |
| CN207618082U (en) | A kind of PE bags of shedding mechanism | |
| CN206466712U (en) | From buffering negative pressure suction disc device | |
| CN208628801U (en) | The rotor and main shaft press-fitting tool of steam turbine and generator | |
| CN206494515U (en) | A kind of battery core feeding clamps modified gear | |
| CN201014468Y (en) | Air sealed wind door | |
| CN2818961Y (en) | Synchronized coal-shoot spray operating valve of hydraulic moving stand | |
| CN209491497U (en) | A kind of novel nail extracting device | |
| CN205393789U (en) | Laser engraving machine smoke and dust cleaning device | |
| CN205362110U (en) | Corrugated container board hole descaling machine for package printing | |
| CN202732267U (en) | Air compressing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160907 Termination date: 20170422 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |