CN206824431U - A kind of aerospace partses Special reforming equipment - Google Patents

A kind of aerospace partses Special reforming equipment Download PDF

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Publication number
CN206824431U
CN206824431U CN201720354563.XU CN201720354563U CN206824431U CN 206824431 U CN206824431 U CN 206824431U CN 201720354563 U CN201720354563 U CN 201720354563U CN 206824431 U CN206824431 U CN 206824431U
Authority
CN
China
Prior art keywords
singlechip controller
eccentric wheel
support post
support baseboard
fixing groove
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
Application number
CN201720354563.XU
Other languages
Chinese (zh)
Inventor
李先民
石繁
叶胜蓝
尚小忠
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangxi Chang zhe Albert Aviation Equipment Technology Co. Ltd.
Original Assignee
Longnan County Productivity Promotion Center
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Longnan County Productivity Promotion Center filed Critical Longnan County Productivity Promotion Center
Priority to CN201720354563.XU priority Critical patent/CN206824431U/en
Application granted granted Critical
Publication of CN206824431U publication Critical patent/CN206824431U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of aerospace partses Special reforming equipment, including support baseboard and control panel, the upper surface of support baseboard is installed with support post, the top of support post is fixed with load bearing cross beam, support baseboard upper surface is inlaid with fixing groove, eccentric wheel and power transmission shaft are installed in fixing groove, are connected with rotary electric machine, the top of eccentric wheel is socketed with Work piece fixing platform and fixed spring folder;The center of load bearing cross beam, which is worn, is connected to lifting shaft, and the top of lifting shaft is provided with press rods, and bottom is welded with pressure block, and the bar end of press rods is socketed with travelling gear, and travelling gear is connected with compression pump;The inside of control panel is provided with singlechip controller, and singlechip controller is connected with data collecting card, power governor and motor driver.The utility model processing is simple, and precision is high, simple to operate effective, and is avoided that influence of personnel's technological disparity to product, meets the manufacturing technology requirement of aviation parts.

Description

A kind of aerospace partses Special reforming equipment
Technical field
Aviation part shaping technique field is the utility model is related to, specially a kind of aerospace partses Special reforming equipment.
Background technology
Aerospace partses are typically designed that complicated, functional requirement is strict, it is necessary to meet rigidity, intensity, fatigue, airtight, reliability Deng requirement.With the continuous growth of usage time, or the impact in operation is excessive, and numerous parts are under huge pressure Deformation is produced, the production work that part deformation then can be to single unit system can all impact, the even meeting of sometimes small deviation Cause huge loss;It is excessively unrestrained if directly abandoned for deformation part but the cost of aerospace partses is all costly Take, typically can all carry out corresponding shaping corrective operations, so as to realize recycling;And existing shaping device be mostly half from For dynamicization, it is necessary to be operated by artificial experience, operating efficiency is low and precision can not ensure, it is impossible to meets actual production need well Ask.
Utility model content
To achieve the above object, the utility model provides following technical scheme:A kind of aerospace partses Special reforming equipment, bag Support baseboard and control panel are included, the upper surface both sides of the support baseboard are installed with support post, the support post Rotatable connection forms parallel construction on support baseboard, and the top of support post is installed with load bearing cross beam, support post Middle support baseboard upper surface is inlaid with fixing groove, is provided with eccentric wheel in the fixing groove, in the wheel shaft of the eccentric wheel The heart is socketed with power transmission shaft, and the power transmission shaft passes from the cell wall of fixing groove, and the other end of power transmission shaft is connected with rotary electric machine, partially The top of heart wheel is socketed with Work piece fixing platform, and the both sides of the Work piece fixing platform are welded with fixed spring folder;The load bearing cross beam Center wear and be connected to lifting shaft, the top of the lifting shaft is provided with press rods, and the bottom of lifting shaft is welded with pressure block, described The bar end of press rods is socketed with travelling gear, and the travelling gear other end is connected with compression pump;The control panel it is interior Portion is provided with singlechip controller, and the data input pin of the singlechip controller is connected with data collecting card, signal output part It is connected with power governor and motor driver.
As a kind of preferable technical scheme of the utility model, the singlechip controller uses MSP430 family chips, And the power pins of singlechip controller are connected with accessory power supply, input/output terminal is connected with liquid crystal display and matrix keyboard group Into minimum system.
As a kind of preferable technical scheme of the utility model, the input of the data collecting card is connected with pressure sensing Device and position sensor, the pressure sensor are fixed on pressure block, and position sensor is fixed on Work piece fixing platform.
As a kind of preferable technical scheme of the utility model, the power governor is connected to the control terminal of compression pump, The motor driver is connected to rotary electric machine control terminal.
Compared with prior art, the beneficial effects of the utility model are:The aerospace partses Special reforming equipment, passes through setting Eccentric wheel, be driven using rotary electric machine, lead to rotary shaft band movable eccentric wheel and rotate, then to the height of Work piece fixing platform from By adjusting, meet that difference treats the specification requirement of shaping workpiece;By setting lifting shaft, using compression pump as pressure-driven, pass through Stress control lifting shaft moves up and down, and then drives pressure block to carry out shaping operation to part;By setting control panel, with list Piece machine controller is control core, carries out data acquisition with data collecting card control pressure sensor and position sensor, utilizes Singlechip controller, power governor and motor driver is controlled to be driven control to compression pump and rotary electric machine respectively, from And closed loop feedback regulation is formed, improve the safety and stability performance of shaping operation;The utility model can realize automated part shaping Operation, processing is simple, and precision is high, simple to operate effective, and is avoided that influence of personnel's technological disparity to product, meets boat The manufacturing technology requirement of empty parts.
Brief description of the drawings
Fig. 1 is the utility model structure diagram;
Fig. 2 is control panel internal module structural representation.
In figure:1- support baseboards;2- support posts;3- load bearing cross beams;4- fixing grooves;5- eccentric wheels;6- power transmission shafts;7- works Part fixed station;8- lifting shafts;9- press rods;10- pressure blocks;11- travelling gears;12- compression pumps;13- control panels;14- turns Dynamic motor;15- singlechip controllers;16- power governors;17- motor drivers;18- accessory power supplys;19- liquid crystal displays; 20- matrix keyboards;21- pressure sensors;22- position sensors;23- data collecting cards;24- fixed springs are pressed from both sides.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made The every other embodiment obtained, belong to the scope of the utility model protection.
Embodiment:
Fig. 1 and Fig. 2 are referred to, the utility model provides a kind of technical scheme:A kind of aerospace partses Special reforming equipment, bag Support baseboard 1 and control panel 13 are included, the upper surface both sides of the support baseboard 1 are installed with support post 2, the support Column 2, which is rotatably connected on support baseboard 1, forms parallel construction, and the top of support post 2 is installed with load bearing cross beam 3, branch The upper surface of support baseboard 1 for supportting the centre of column 2 is inlaid with fixing groove 4, and eccentric wheel 5 is provided with the fixing groove 4, described inclined The wheel shaft center of heart wheel 5 is socketed with power transmission shaft 6, and the power transmission shaft 6 passes from the cell wall of fixing groove 4, the other end of power transmission shaft 6 Rotary electric machine 14 is connected with, the top of eccentric wheel 5 is socketed with Work piece fixing platform 7, and the both sides of the Work piece fixing platform 7 are welded with admittedly Determine spring clip 24;The center of the load bearing cross beam 3, which is worn, is connected to lifting shaft 8, and the top of the lifting shaft 8 is provided with press rods 9, rises The bottom of drop axle 8 is welded with pressure block 10, and the bar end of the press rods 9 is socketed with travelling gear 11, the travelling gear 11 The other end is connected with compression pump 12;The inside of the control panel 13 is provided with singlechip controller 15, the single-chip microcomputer control The data input pin of device 15 is connected with data collecting card 23, and signal output part is connected with power governor 16 and motor driver 17;
The singlechip controller 15 uses MSP430 family chips, and the power pins of singlechip controller 15 are connected with Accessory power supply 18, input/output terminal is connected with liquid crystal display 19 and matrix keyboard 20 forms minimum system;The data acquisition The input of card 23 is connected with pressure sensor 21 and position sensor 22, and the pressure sensor 21 is fixed on pressure block 10 On, position sensor 22 is fixed on Work piece fixing platform 7;The power governor 16 is connected to the control terminal of compression pump 12, institute State motor driver 17 and be connected to the control terminal of rotary electric machine 14.
Specifically used mode and advantage:The support baseboard 1 is used to support fixed whole device, and the support post 2 is used In the fixed load bearing cross beam 3 of support, the fixing groove 4 is used to place eccentric wheel 5, and the eccentric wheel 5 is driven by power transmission shaft 6, when turning When dynamic motor 14 rotates, band movable eccentric wheel 5 rotates, so as to lift or put down Work piece fixing platform 7, the Work piece fixing platform 7 The workpiece of shaping is treated for placing, the fixed spring folder 24 is used to fix workpiece;The press rods 10 by travelling gear 11 with Compression pump 12 is connected, and when the compression pump 12 works, pump rod pushes force, drives press rods 9 to push, and then drives lifting shaft 8 are pushed, and pressure block 10 is pushed by impact, and compacting shaping is carried out to part;
The control panel 13 is used to realize that adjust automatically operates, and the singlechip controller 15 is supplied by accessory power supply 18 Electricity, the matrix keyboard 20 are used to be operated parameter setting, and the liquid crystal display 19 can be with real-time display parameter, the pressure Force snesor 21 gathers the pressure that current pressure block 10 applies, and the position sensor 22 is used to gather Work piece fixing platform 7 and pressure The relative position of power block 10, the data value collected are fed through single-chip microcomputer control after data pick-up is converted into data signal Device 15, the singlechip controller 15 carry out analysis judgement according to the signal received, see whether meet setting value, if discontented Foot, then the pressure value that power governor 16 adjusts compression pump 12 is obtained, or rotary electric machine 14 is adjusted using motor driver 17 Rotating speed, and then adjust relative position, improve plastic precision and efficiency.
The aerospace partses Special reforming equipment, by setting eccentric wheel, is driven using rotary electric machine, leads to rotary shaft band Movable eccentric wheel rotates, then freely adjust to the height of Work piece fixing platform, the different specification requirements for treating shaping workpiece of satisfaction;It is logical Setting lifting shaft is crossed, using compression pump as pressure-driven, is moved up and down by Stress control lifting shaft, and then drives pressure block pair Part carries out shaping operation;By setting control panel, using singlechip controller as control core, with data acquisition card control pressure Force snesor and position sensor carry out data acquisition, using singlechip controller, control power governor and motor driver Control is driven to compression pump and rotary electric machine respectively, so as to form closed loop feedback regulation, the safety for improving shaping operation is steady Qualitative energy;The utility model can realize automated part shaping operation, and processing is simple, and precision is high, simple to operate effective, and Influence of personnel's technological disparity to product is avoided that, meets the manufacturing technology requirement of aviation parts.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and And in the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation Involved claim.

Claims (4)

  1. A kind of 1. aerospace partses Special reforming equipment, it is characterised in that:It is described including support baseboard (1) and control panel (13) The upper surface both sides of support baseboard (1) are installed with support post (2), and support post (2) rotatable connection is at support bottom Parallel construction is formed on plate (1), the top of support post (2) is installed with load bearing cross beam (3), the centre of support post (2) Support baseboard (1) upper surface be inlaid with fixing groove (4), eccentric wheel (5), the eccentric wheel are installed in the fixing groove (4) (5) wheel shaft center is socketed with power transmission shaft (6), and the power transmission shaft (6) passes from the cell wall of fixing groove (4), power transmission shaft (6) The other end is connected with rotary electric machine (14), and the top of eccentric wheel (5) is socketed with Work piece fixing platform (7), the Work piece fixing platform (7) Both sides be welded with fixed spring folder (24);The center of the load bearing cross beam (3), which is worn, is connected to lifting shaft (8), the lifting shaft (8) Top press rods (9) are installed, the bottom of lifting shaft (8) is welded with pressure block (10), the bar end set of the press rods (9) Travelling gear (11) is connected to, travelling gear (11) other end is connected with compression pump (12);The control panel (13) it is interior Portion is provided with singlechip controller (15), and the data input pin of the singlechip controller (15) is connected with data collecting card (23), signal output part is connected with power governor (16) and motor driver (17).
  2. A kind of 2. aerospace partses Special reforming equipment according to claim 1, it is characterised in that:The singlechip controller (15) MSP430 family chips are used, and the power pins of singlechip controller (15) are connected with accessory power supply (18), input is defeated Go out end and be connected with liquid crystal display (19) and matrix keyboard (20) composition minimum system.
  3. A kind of 3. aerospace partses Special reforming equipment according to claim 1, it is characterised in that:The data collecting card (23) input is connected with pressure sensor (21) and position sensor (22), and the pressure sensor (21) is fixed on pressure On block (10), position sensor (22) is fixed on Work piece fixing platform (7).
  4. A kind of 4. aerospace partses Special reforming equipment according to claim 1, it is characterised in that:The power governor (16) control terminal of compression pump (12) is connected to, the motor driver (17) is connected to rotary electric machine (14) control terminal.
CN201720354563.XU 2017-04-06 2017-04-06 A kind of aerospace partses Special reforming equipment Expired - Fee Related CN206824431U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720354563.XU CN206824431U (en) 2017-04-06 2017-04-06 A kind of aerospace partses Special reforming equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720354563.XU CN206824431U (en) 2017-04-06 2017-04-06 A kind of aerospace partses Special reforming equipment

Publications (1)

Publication Number Publication Date
CN206824431U true CN206824431U (en) 2018-01-02

Family

ID=60768130

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720354563.XU Expired - Fee Related CN206824431U (en) 2017-04-06 2017-04-06 A kind of aerospace partses Special reforming equipment

Country Status (1)

Country Link
CN (1) CN206824431U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111496019A (en) * 2020-04-30 2020-08-07 瑞安市荣海机电有限公司 Device for eliminating curved surface deformation of front frame of O L ED display
CN113083943A (en) * 2021-03-25 2021-07-09 贵州安吉航空精密铸造有限责任公司 Method for correcting appearance of large casting

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111496019A (en) * 2020-04-30 2020-08-07 瑞安市荣海机电有限公司 Device for eliminating curved surface deformation of front frame of O L ED display
CN111496019B (en) * 2020-04-30 2022-02-15 安徽亿普拉斯科技有限公司 Device for eliminating curve deformation of front frame of OLED display
CN113083943A (en) * 2021-03-25 2021-07-09 贵州安吉航空精密铸造有限责任公司 Method for correcting appearance of large casting

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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: 20180903

Address after: 333000 south side of Wu Tong Road, Jingdezhen high tech Zone, Jingdezhen, Jiangxi (Hesheng science and technology business incubator)

Patentee after: Jiangxi Chang zhe Albert Aviation Equipment Technology Co. Ltd.

Address before: 341700 room 8207, Longnan County, Longnan County, Ganzhou, Jiangxi.

Patentee before: Longnan County Productivity Promotion Center

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: 20180102

Termination date: 20190406