CN107378507B - Aviation part numerical control processing production line - Google Patents
Aviation part numerical control processing production line Download PDFInfo
- Publication number
- CN107378507B CN107378507B CN201710579458.0A CN201710579458A CN107378507B CN 107378507 B CN107378507 B CN 107378507B CN 201710579458 A CN201710579458 A CN 201710579458A CN 107378507 B CN107378507 B CN 107378507B
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- numerical control
- station
- control processing
- assembly station
- production line
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Classifications
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- 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
- B23P23/00—Machines or arrangements of machines for performing specified combinations of different metal-working operations not covered by a single other subclass
- B23P23/06—Metal-working plant comprising a number of associated machines or apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q1/00—Members which are comprised in the general build-up of a form of machine, particularly relatively large fixed members
- B23Q1/25—Movable or adjustable work or tool supports
- B23Q1/64—Movable or adjustable work or tool supports characterised by the purpose of the movement
- B23Q1/66—Worktables interchangeably movable into operating positions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
- B23Q3/06—Work-clamping means
- B23Q3/08—Work-clamping means other than mechanically-actuated
- B23Q3/088—Work-clamping means other than mechanically-actuated using vacuum means
Abstract
The present invention relates to a kind of aviation part numerical control processing production lines, and tooling assembly station is arranged on ground, horizontal digital-control machining center is arranged on several linearly symmetrical numerical control processing stations of the two sides of tooling assembly station, numerical control processing station；In the top of numerical control processing station and tooling assembly station, one perforative truss is set, truss is equipped with mobile boom hoisting, it is equipped with central control server in the outside of numerical control processing station, controls each horizontal digital-control machining center and the conversion of boom hoisting position respectively by system command.The production line is lifted using truss, the time for making full use of numerical control processing and part to assemble in tooling, rational allocation numerical control device, it solves the problems, such as that aviation part is wide in variety, batch is small to be difficult to have enough to meet the need in intelligent production line, realize the production line of production and processing installation digital automation, working efficiency is not only improved, but also reduces staffing, reduces operating error.
Description
Technical field
The present invention relates to a kind of aviation part numerical control processing production lines, belong to aviation High-speed Computer number control manufacturing batch production neck
Domain.
Background technique
Restricting aeronautical product field of machining at present and forming the greatest problem of complete intelligent production line is exactly aviation part
It is wide in variety, small in batches.For these reasons, in aeronautical product field of machining, it is difficult by using shapes such as robot, row framves
Formula has enough to meet the need crawl, the absorption of multinomial part in whole production line.So being difficult to be formed as automobile and mobile phone industry big
Scale full-automation production line.
The processing of aeronautical product part at present uses external programming, the side of each one machining center of numerical control worker operation
Formula.It is excessive to result in the leading time in this way, and machining center effective run time exists simultaneously a large amount of artificial behaviour less than 40%
Hidden danger of quality caused by making mistakes.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of aviation part numerical control processing production line, which uses purlin
Frame lifting, the time for making full use of numerical control processing and part to assemble in tooling, rational allocation numerical control device solves aviation zero
Part is wide in variety, batch is small is difficult to the problem of having enough to meet the need in intelligent production line, realizes the life of production and processing installation digital automation
Producing line not only improves working efficiency, but also reduces staffing, reduces operating error.
In order to solve the above problem, the specific technical solution of the present invention is as follows: a kind of aviation part numerical control processing production line,
Tooling assembly station is arranged in ground, in several linearly symmetrical numerical control processing stations of the two sides of tooling assembly station, number
It controls and horizontal digital-control machining center is set on processing stations；It is arranged one in the top of numerical control processing station and tooling assembly station to pass through
The truss worn, truss are equipped with mobile boom hoisting, are equipped with central control server in the outside of numerical control processing station, pass through
System command controls each horizontal digital-control machining center and the conversion of boom hoisting position respectively.
Three coordinate measurement machines are equipped on the straight line where numerical control processing station.
The tooling assembly station quantity is three, intermediate main assembly station, and both sides are respectively to spread assistant engineer position.
Aviation part system operation methods are processed using production line, it is characterised in that the following steps are included:
1) by CNC program, the tool position in tool magazine requires to be arranged in MES manufacturing enterprise production process according to technological procedure
In execution system；
2) mounting tool: the accommodating tool fixture on main assembly station, and parts to be processed is located on frock clamp,
Frock clamp controls boom hoisting and is lifted into secondary station together with fitting turnover normotopia；And continue on main assembly station
On clamping other set part to be processed to corresponding frock clamp；
3) lifting is in place: when there is idle numerical control processing station, and detecting in secondary station there is clamping tooling folder
After the part of tool, boom hoisting is controlled by central control server, ready frock clamp is transported to together with part idle
Numerical control processing station on, and by operator confirm position it is errorless after, boom hoisting is operated by central control server and falls work
Dress verifies flatness, verticality and setting origin by system program automatically；
4) it processes part: by central control server system self-closing safety door, being transferred in MES system and corresponding zero
The processing program of part woollen setting simultaneously starts to process；During processing, machining state, the knife of part are observed in MES system
The abrasion situation of tool cuts that show that machining center is completed in the but liquid state of cooling and spindle motor loading condition and center display screen surplus
Remaining time and machining state are completed by remote monitoring system；
5) after showing machining center completion and voice system prompt in the center display screen of central control server, operation system
System automatically opens safety door, and part is transported to three coordinate detection machines and detected, controlled again after detection by control boom hoisting
Boom hoisting processed is transported to main assembly station from three coordinates detection seat in the plane, unloads part；
6) whether the part for confirming that main assembly station unloads continues next process, if it is desired, main assembly station is from new
Clamping parts, part is transported to paving assistant engineer's bit platform by boom hoisting, and is waited and be transplanted on the numerical control processing station that would sit idle for
On, repeat step 3)~5), until entire part completion of processing.
The frock clamp is interchangeable vacuum platform, and horizontal digital-control machining center is equipped with and puts down to interchangeable mutual vacuum
The positioning device and forced locking device of platform.
The aviation part numerical control processing production line uses linear distributing numerical control processing station, carries out convenient for upper truss
Lifting improves the turn around time of part the entire production line, while tooling assembly station is arranged in centre, to make and frock clamp
The part assembled can be lifted once, and be accurately positioned, and the time of numerically-controlled machine tool Set and Positioning early period is saved, therefore be improved
Whole production efficiency.
Straight line where numerical control processing station is equipped with three coordinate measurement machines, after a numerical control processing stations, needs
It is detected on to three coordinate measurement machines, to guarantee the qualification rate of part.
Tooling assembly station quantity is three, intermediate main assembly station, and both sides are respectively to spread assistant engineer position, in order to tooling
After fixture and component assembly are good, await orders in secondary station, and main assembly station continues another part of clamping, to significantly mention
The clamping efficiency of high part, and it is not take up the time of numerical control processing, to further increase processing efficiency.
Production line processes aviation part system operation methods and uses above-mentioned steps, will be to be processed by main Operational preparation station
Then parts fixation completes part to be processed by the mode of the hanged vacuum processing platform of Lift-on/Lift-off System and exists on vacuum processing platform
Turnover in whole production line, to solve, aviation part is wide in variety, batch is small is difficult to have enough to meet the need in intelligent production line
Problem.
The machining center is specific customization, no stationary work-table face, it is desirable that equipment, which has to have between vacuum processing platform, determines
Position device and forced locking device, and have good interchangeability between each machining center and each vacuum processing platform.
Frock clamp is interchangeable vacuum platform, and horizontal digital-control machining center is equipped with and determines interchangeable vacuum platform
Position device and forced locking device save the expense of tooling, while interchangeable vacuum platform positioning accuracy is high, guarantee adding for part
Working medium amount.
Detailed description of the invention
Fig. 1 is the top view of aviation part numerical control processing production line.
Fig. 2 is the main view of aviation part numerical control processing production line.
Fig. 3 is single numerical control processing station working state schematic representation.
Fig. 4 is tooling assembly station structural schematic diagram.
Specific embodiment
As shown in Figure 1, a kind of aviation part numerical control processing production line, is arranged tooling assembly station 2 on ground, fills in tooling
Several linearly symmetrical numerical control processing stations 1 of two sides with station 2, setting horizontal digital-control adds on numerical control processing station 1
Work center, the horizontal digital-control machining center is without stationary work-table face, it is desirable that equipment has and has positioning between interchangeable mutual vacuum platform
Device and forced locking device, and have good interchangeability between each machining center and each vacuum processing platform, to realize each
The clamping of specification part；In the top of numerical control processing station 1 and tooling assembly station 2, one perforative truss 3, truss 3 are set
It is equipped with mobile boom hoisting 5, central control server 4 is equipped in the outside of numerical control processing station 1, passes through system command point
Each horizontal digital-control machining center and the conversion of boom hoisting position are not controlled.
Three coordinate measurement machines 6 are equipped on the straight line where numerical control processing station 1, part is completed whole in numerical control machining center
It is a need manufacturing procedure after, directly detected on three coordinate measurement machines, to ensure that the quality of product, avoid Same Part
There is identical mistake in the same process, that is, guarantees the ex factory pass rate of part.
2 quantity of tooling assembly station is three, intermediate main assembly station 21, and both sides are respectively to spread assistant engineer position
22, main assembly station 21 is used to carry out part in tooling assembly or disassembly, and the part assembled is transferred to paving assistant engineer
Position 22 on, wait it is to be processed, wherein main assembly station 21 use automatic turning platform, it is parallel to the ground, it is easy to setup and disassembly zero
Part, 90 degree of the part assembled overturnings are directly landed in paving assistant engineer position 22, wait to be processed to realize vertical lifting.Truss 3
Paving assistant engineer position 22 is sling to horizontal digital-control machining center, and passes through positioning device and forced locking device positioning and locking.
Aviation part system operation methods are processed using production line, comprising the following steps:
1) by CNC program, the tool position in tool magazine requires to be arranged in MES manufacturing enterprise production process according to technological procedure
In execution system, it includes remote operating system, long-range monitoring that the entire production line, which executes system by MES manufacturing enterprise production process,
System, production data acquisition system, intelligent production plan arrangement and Real time optimal dispatch system, speech prompting system, thus real
Now whole automatic production line；
2) mounting tool: the accommodating tool fixture on main assembly station 21, and parts to be processed is located in frock clamp
On on main assembly station 21 be equipped with benchmark centering control device, exact position of the part on frock clamp may be implemented, from
And the processing step of origin is looked for when saving processing part, then frock clamp is together with fitting turnover normotopia, and controls boom hoisting 5
It is lifted into secondary station 22；And continue clamping other set part to be processed on main assembly station 21 to corresponding tooling
On fixture；
3) lifting is in place: when there is idle numerical control processing station 1, and detecting there is clamping tooling in secondary station 22
After the part of fixture, boom hoisting 5 is controlled by central control server 4, ready frock clamp is transported to together with part
On idle numerical control processing station 1, and by operator confirm position it is errorless after, boom hoisting is operated by central control server and is fallen
Lower tooling verifies flatness, verticality and setting origin by system program automatically；
4) it processes part: by central control server system self-closing safety door, being transferred in MES system and corresponding zero
The processing program of part woollen setting simultaneously starts to process；During processing, machining state, the knife of part are observed in MES system
The abrasion situation of tool cuts that show that machining center is completed in the but liquid state of cooling and spindle motor loading condition and center display screen surplus
Remaining time and machining state are completed by remote monitoring system；
5) after showing machining center completion and voice system prompt in the center display screen of central control server, operation system
System automatically opens safety door, and part is transported to three coordinate detection machines 5 and detected by control boom hoisting 5, after detection again
It controls boom hoisting 5 and is transported to main assembly station 21 from three coordinate detection machines 5, unload part；
Whether the part for confirming that main assembly station 21 unloads continues next process, if it is desired, main assembly station 21 from
New clamping parts, part is transported to paving assistant engineer's bit platform 22 by boom hoisting, and is waited and be transplanted on the numerical control processing that would sit idle for
On station 1, step 3)~5 are repeated), until entire part completion of processing.
Claims (3)
1. a kind of system operation methods of aviation part numerical control processing production line processing aviation part,
The structure of production line are as follows: on ground, tooling assembly station (2) are set, it is linearly right in the two sides of tooling assembly station (2)
Claim to be distributed several numerical control processing stations (1), horizontal digital-control machining center is set on numerical control processing station (1)；In numerical control processing
A perforative truss (3) is arranged in the top of station (1) and tooling assembly station (2), and truss (3) is equipped with mobile rising and lifts
(5) are set, central control server (4) is equipped in the outside of numerical control processing station (1), is controlled respectively by system command each horizontal
Numerical control machining center and the conversion of boom hoisting position；Wherein tooling assembly station (2) quantity is three, intermediate main assembly station
(21), both sides are respectively to spread assistant engineer position (22)；
It is characterized in that operating method the following steps are included:
1) by CNC program, the tool position in tool magazine requires setting to execute in MES manufacturing enterprise production process according to technological procedure
In system；
2) mounting tool: the accommodating tool fixture on main assembly station (21), and parts to be processed is located on frock clamp,
Frock clamp controls boom hoisting (5) and is lifted on secondary station (22) together with fitting turnover normotopia；And in main assembly station
(21) continue on clamping other set part to corresponding frock clamp to be processed on；
3) lifting is in place: when there is idle numerical control processing station (1), and detecting there is clamping tooling on secondary station (22)
After the part of fixture, boom hoisting (5) are controlled by central control server (4), ready frock clamp is defeated together with part
Be sent on idle numerical control processing station (1), and by operator confirm position it is errorless after, lifting is operated by central control server
Device falls tooling, verifies flatness, verticality and setting origin automatically by system program；
4) it processes part: by central control server system self-closing safety door, being transferred in MES system and corresponding part hair
Expect the processing program of setting and starts to process；During processing, the machining state of part, cutter are observed in MES system
Abrasion situation, cut show in the but liquid state of cooling and spindle motor loading condition and center display screen machining center complete residue when
Between and machining state, completed by remote monitoring system；
5) after showing machining center completion and voice system prompt in the center display screen of central control server, operating system is certainly
Dynamic to open safety door, part is transported to three coordinate detection machines (5) and detected by control boom hoisting (5), after detection again
It controls boom hoisting (5) and is transported to main assembly station (21) from three coordinate detection machine (5) positions, unload part；
6) whether the part for confirming that main assembly station (21) is unloaded continues next process, if it is desired, main assembly station (21)
From new clamping parts, part is transported to paving assistant engineer's bit platform (22) by boom hoisting, and is waited and be transplanted on the numerical control that would sit idle for
On processing stations (1), step 3)~5 are repeated), until entire part completion of processing.
2. the system operation methods of aviation part numerical control processing production line processing aviation part as described in claim 1, special
Sign is: the frock clamp is interchangeable vacuum platform, and horizontal digital-control machining center is equipped with and puts down to interchangeable vacuum
The positioning device and forced locking device of platform.
3. the system operation methods of aviation part numerical control processing production line processing aviation part as described in claim 1, special
Sign is: three coordinate measurement machines (6) are equipped on the straight line where numerical control processing station (1).
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| Application Number | Priority Date | Filing Date | Title |
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| CN201710579458.0A CN107378507B (en) | 2017-07-17 | 2017-07-17 | Aviation part numerical control processing production line |
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| CN201710579458.0A CN107378507B (en) | 2017-07-17 | 2017-07-17 | Aviation part numerical control processing production line |
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| CN107378507B true CN107378507B (en) | 2019-04-26 |
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| CN110202388B (en) * | 2019-05-17 | 2021-12-03 | 成都飞机工业（集团）有限责任公司 | Automatic production line and production method for small-size parts |
| CN110587343A (en) * | 2019-10-08 | 2019-12-20 | 中国航空工业集团公司洛阳电光设备研究所 | Tool clamp capable of being replaced and installed quickly and using method thereof |
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| CN112496766B (en) * | 2020-11-12 | 2022-04-01 | 浙江泰鸿万立科技股份有限公司 | Automatic production line system for vehicle body parts |
| CN113385957A (en) * | 2021-06-01 | 2021-09-14 | 东莞长盈精密技术有限公司 | Clamping jig and machining method |
| CN114770133A (en) * | 2021-12-20 | 2022-07-22 | 重庆长安工业(集团)有限责任公司 | Flexible automatic manufacturing system for plate parts |
| CN115156925B (en) * | 2022-07-29 | 2023-05-16 | 中国电子科技集团公司第三十八研究所 | Small-size flexible precision machining production line |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103753227A (en) * | 2014-01-21 | 2014-04-30 | 重庆大江工业有限责任公司 | Machining production line and machining method for axle housing component |
| CN104259774A (en) * | 2014-09-09 | 2015-01-07 | 黄河科技学院 | Plane wing titanium alloy thin-wall web efficient numerical control machining technology |
| CN204308562U (en) * | 2014-11-03 | 2015-05-06 | 柳州市东川机械制造有限公司 | Anchor clipper automatic production line |
| CN104816202A (en) * | 2015-05-22 | 2015-08-05 | 江西佳时特数控技术有限公司 | Flexible machining production line based on numerically-controlled machine tools |
| CN104985443A (en) * | 2015-07-08 | 2015-10-21 | 龙口市丛林铝材有限公司 | Flexible manufacturing system of aluminum alloy hot extruding die |
-
2017
- 2017-07-17 CN CN201710579458.0A patent/CN107378507B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103753227A (en) * | 2014-01-21 | 2014-04-30 | 重庆大江工业有限责任公司 | Machining production line and machining method for axle housing component |
| CN104259774A (en) * | 2014-09-09 | 2015-01-07 | 黄河科技学院 | Plane wing titanium alloy thin-wall web efficient numerical control machining technology |
| CN204308562U (en) * | 2014-11-03 | 2015-05-06 | 柳州市东川机械制造有限公司 | Anchor clipper automatic production line |
| CN104816202A (en) * | 2015-05-22 | 2015-08-05 | 江西佳时特数控技术有限公司 | Flexible machining production line based on numerically-controlled machine tools |
| CN104985443A (en) * | 2015-07-08 | 2015-10-21 | 龙口市丛林铝材有限公司 | Flexible manufacturing system of aluminum alloy hot extruding die |
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