CN105269322A - Five-shaft-linkage automatic drilling and milling platform for machining installation plane of vertical fin part connector - Google Patents
Five-shaft-linkage automatic drilling and milling platform for machining installation plane of vertical fin part connector Download PDFInfo
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- CN105269322A CN105269322A CN201410319229.1A CN201410319229A CN105269322A CN 105269322 A CN105269322 A CN 105269322A CN 201410319229 A CN201410319229 A CN 201410319229A CN 105269322 A CN105269322 A CN 105269322A
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Abstract
A five-shaft-linkage automatic drilling and milling platform for machining an installation plane of a vertical fin part connector is characterized by comprising a frame assembly, an upper plane guide rail assembly and a five-shaft machining system. The frame assembly serves as the main bearing component for the upper plane guide rail assembly and the five-shaft machining system and is fixedly connected with the ground. The upper plane guide rail assembly is located on the frame assembly and serves as the movement guiding device of the five-shaft machining system. The five-shaft machining system is provided with a five-shaft-linkage mechanism and can meet the functions of plane milling, hole machining and hole reaming of products. The five-shaft-linkage automatic drilling and milling platform has the advantages that the machining and assembly accuracy of products is guaranteed, the number of detachable parts is reduced, the operation space for workers is increased, labor intensity of workers is relieved, labor cost is reduced, production efficiency is improved, and environmental pollution is reduced.
Description
Technical field
The present invention relates to aircraft vertical fin component joints mounting plane process and assemble field, particularly one to utilize five-axle linkage automatic control system to complete the milling of aircraft vertical fin component joints mounting plane to bore integrated processing platform.
Background technology
The processing of aircraft vertical fin component joints mounting plane and assembling, because the parts that will install are larger, and jiont treatment face does not compensate, to product plane degree, the position degree of size and installing hole requires high, therefore traditional processing method jiont treatment surface parts is gone up separately Digit Control Machine Tool processing (difference according to measured value and theoretical value), installing hole then needs design bushing plate (detachably) to process, thus cause whole type frame locator more, numerous and diverse, operating space is limited, and resetting often, machining accuracy certainly will be affected, lower efficiency, strengthen cost etc.
In order to solve the problem, need to design a kind of aircraft vertical fin component joints mounting plane processing five-axle linkage and automatically controlling to bore milling method and platform, raising the efficiency while guarantee precision, reduce human resources, reduce environmental pollution.
Summary of the invention
Have in view of that, the object of this invention is to provide a kind of aircraft vertical fin component joints mounting plane processing five-axle linkage automatic drill milling platform, raise the efficiency while guarantee required precision, reduce human resources, reduce environmental pollution.
The present invention is a kind of aircraft vertical fin component joints mounting plane processing five-axle linkage automatic drill milling platform, comprises type frame assembly, upper flat guide assembly and five-axis robot system; Described type frame assembly is fixed on ground as the primary load bearing component of upper flat guide assembly and five-axis robot system, upper rail plane is seated on type frame assembly, as linear motion guide device and the driving mechanism of five-axis robot system, described five-axis robot system self can meet the function of product milling plane and system, fraising with five-axle linkage mechanism.
Further, described type frame assembly comprises the underframe assemblies fixed on the ground, is fixed on 8 support post assemblies on underframe assemblies, and is fixed on the upper beam assembly on support post assembly; Upper flat guide assembly comprises 2 connecting plates and 2 linear guides pairs that are fixedly connected with type frame assembly, for five-axis robot system provides 2 servomotors and 2 motion lead screw pair of driving force; Five-axis robot system comprises supporting traverse, 2 cross slide waies, 2 longitudinal rails, processing dynamics head, automatically tool magazine, suctions are cut system, collected and cut case, servomotor, ball screw, control cabinet and control panel; Five-axis robot system self can meet the function of product milling plane and system, fraising with five-axle linkage mechanism.
Further, five-axis robot system architecture part has horizontal and vertical two groups of linear guides secondary, and power head mechanism part has universal rotary mechanism, can meet the function that processing head realizes five-axle linkage.
The invention has the beneficial effects as follows: a kind of vertical fin component joints mounting plane processing five-axle linkage automatic drill milling platform of the present invention, the milling plane of processed parts, system, fraising integration processing can be realized, can raise the efficiency while guarantee precision, reduce human resources, reduce environmental pollution.
Accompanying drawing explanation
Fig. 1 is integral shaft mapping of the present invention;
Fig. 2 is type frame assembly axonometric drawing of the present invention;
Fig. 3 is upper flat guide assembly axonometric drawing of the present invention;
Fig. 4 is five-axis robot system axonometric drawing of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing and illustrative examples, the present invention is described further:
Fig. 1 is integral shaft mapping of the present invention, and as shown in Figure 1, a kind of vertical fin component joints mounting plane processing five-axle linkage automatic drill milling platform of the present embodiment comprises type frame assembly (1), upper flat guide assembly (2) and five-axis robot system (3); Described type frame assembly (1) fixes on the ground, upper flat guide assembly (2) is fixed on type frame assembly (1), five-axis robot system (3) is processing primary load bearing parts with type frame assembly (1), above flat guide assembly (2) is guiding mechanism, coordinates the function that the five-axis simultaneous structure of self realizes the milling plane of parts and system, fraising.
In the present embodiment, Fig. 2 is type frame assembly axonometric drawing of the present invention, as shown in Figure 2, described type frame assembly (1) comprises underframe assemblies (1-01) and fixes on the ground, 8 support post assemblies (1-02) are fixed on underframe assemblies (1-01), and upper beam assembly (1-03) is fixed on support post assembly (1-02); The body junction component of type frame assembly adopts the square tube of 300mm × 300mm × 12mm specification, to ensure rigidity and the intensity of main body frame, ground utilizes ground and the design of shockproof ditch, reduces the vibrations because machining produces to greatest extent, thus reduces the external influence factors of machining accuracy.
In the present embodiment, Fig. 3 is upper flat guide assembly axonometric drawing of the present invention, as shown in Figure 3, described upper flat guide assembly (2) comprises 2 connecting plates (2-01) and 2 linear guides (2-02) that are fixedly connected with type frame assembly (1), form 2 servomotors (2-03) and 2 motion lead screw pair (2-04) of motion driving mechanism, driving mechanism is that five-axis robot system (3) provides linear reciprocal movement power.
In the present embodiment, Fig. 4 is five-axis robot system axonometric drawing of the present invention, as shown in Figure 4, described five-axis robot system (3) comprises supporting traverse (3-01), 2 cross slide waies (3-02), 2 longitudinal rails (3-03), processing dynamics head (3-04), automatic tool magazine (3-05), system (3-06) is cut in suction, case (3-07) cut by collection, servomotor (3-08), ball screw (3-09), control cabinet (3-10) and control panel (3-11), this five-axis robot system architecture part has horizontal and vertical two groups of linear guides secondary, power head mechanism part has universal rotary mechanism, the function that processing head realizes five-axle linkage can be met.
In the present embodiment, the function achieved by vertical fin component joints mounting plane processing platform: realize milling flat, brill, fraising integration; The flatness of aluminium alloy and titanium alloy material and the finishing requirements of hole location can be met.
Scheme Choice: according to assembling instructions for use, fine finishining paralell is located at the upper mounting plate surface of general assembly type frame, take seamless being rigidly connected, use five-shaft numerical control process equipment, realize milling flat, drilling, fraising institutional operation, this cover processing platform contains row cuts (vacuum adsorption type), cooling (air-cooled), on-line measurement, compensation data, correction and automatic tool changer, can realize mechanical, electrical, liquid automated job function truly.
Assembling process:
Utilize laser tracker assembly jig assembly (1), ensure that its top surface plane degree controls within the scope of 0.1mm, and utilize large span bridge leveling ruler, repair grinding frame upper surface flatness within 0.02mm, to eliminate the gap between installed surface as far as possible, reach the requirement of seamless link.
The technical requirement that five-axis robot system (3) presses numerically controlled processing equipment under frame is assembled and after debugging, be connected on type frame assembly (1) according to reference for installation, use the depth of parallelism, the flatness between bridge leveling ruler inspection processing platform guide rail in installation process, ensure instructions for use.
After installation, the error produced when the on-line measurement system utilizing five-axis robot system (3) to carry carrys out checkout equipment debugging, then carries out correction-compensation in a program.
Due to the quantity of this parts product needed drilling and dimensions more, simultaneously in order to reduce the resetting error produced in feed process as far as possible, reduce the weight of number of cutters and tool magazine, so adopt the cutter of the one that drills and reams.
Claims (5)
1. a vertical fin component joints mounting plane processing five-axle linkage automatic drill milling platform, its method is: in type frame, install a 5-shaft linkage numerical control system of processing, the milling completing aircraft vertical fin component joints mounting plane bores integration processing, to meet the installation requirement of aircraft vertical fin component joints.
2. according to claim 1, it is characterized in that described automatic drill milling platform comprises type frame assembly (1), the upper flat guide assembly (2) be connected with type frame assembly (1) and the five-axis robot system (3) be seated on upper flat guide assembly (2).
3. according to claim 2, it is characterized in that, described type frame assembly (1) comprises underframe assemblies (1-01), is fixed on 8 support post assemblies (1-02) on underframe assemblies (1-01), and is fixed on the upper beam assembly (1-03) on support post assembly (1-02) top.
4. according to claim 2, it is characterized in that, described upper flat guide assembly (2) comprises 2 connecting plates (2-01) and 2 linear guides (2-02) that are fixedly connected with type frame assembly (1), forms 2 servomotors (2-03) and 2 motion lead screw pair (2-04) of motion driving mechanism.
5. according to claim 2, it is characterized in that, described five-axis robot system (3) comprises supporting traverse (3-01), 2 cross slide waies (3-02), 2 longitudinal rails (3-03), processing dynamics head (3-04), automatically tool magazine (3-05), suctions are cut system (3-06), collected and cut case (3-07), servomotor (3-08), ball screw (3-09), control cabinet (3-10) and control panel (3-11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410319229.1A CN105269322A (en) | 2014-07-07 | 2014-07-07 | Five-shaft-linkage automatic drilling and milling platform for machining installation plane of vertical fin part connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410319229.1A CN105269322A (en) | 2014-07-07 | 2014-07-07 | Five-shaft-linkage automatic drilling and milling platform for machining installation plane of vertical fin part connector |
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| Publication Number | Publication Date |
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| CN105269322A true CN105269322A (en) | 2016-01-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410319229.1A Pending CN105269322A (en) | 2014-07-07 | 2014-07-07 | Five-shaft-linkage automatic drilling and milling platform for machining installation plane of vertical fin part connector |
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| CN (1) | CN105269322A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112676839A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| CN113247297A (en) * | 2021-06-28 | 2021-08-13 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1562557A (en) * | 2004-03-31 | 2005-01-12 | 沈阳工业学院 | Elevated platform type automatic processing center of lathe and milling machine of five shafts |
| JP2005230945A (en) * | 2004-02-18 | 2005-09-02 | Kawahara:Kk | Device for simultaneously machining deep hole and outer periphery for long workpiece |
| CN102566439A (en) * | 2011-12-27 | 2012-07-11 | 中航沈飞民用飞机有限责任公司 | Space orientation computing method for numerical control bracket |
| CN102649231A (en) * | 2012-05-11 | 2012-08-29 | 福建泉州洛江振丰模配制造有限公司 | Bridge gantry non-ferrous metal and composite material machining center |
| CN203064207U (en) * | 2013-01-28 | 2013-07-17 | 上海上飞飞机装备制造有限公司 | Airframe general assembly frame |
| CN203621559U (en) * | 2013-12-10 | 2014-06-04 | 中航成飞民用飞机有限责任公司 | Perforating equipment of large spar assembly |
-
2014
- 2014-07-07 CN CN201410319229.1A patent/CN105269322A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005230945A (en) * | 2004-02-18 | 2005-09-02 | Kawahara:Kk | Device for simultaneously machining deep hole and outer periphery for long workpiece |
| CN1562557A (en) * | 2004-03-31 | 2005-01-12 | 沈阳工业学院 | Elevated platform type automatic processing center of lathe and milling machine of five shafts |
| CN102566439A (en) * | 2011-12-27 | 2012-07-11 | 中航沈飞民用飞机有限责任公司 | Space orientation computing method for numerical control bracket |
| CN102649231A (en) * | 2012-05-11 | 2012-08-29 | 福建泉州洛江振丰模配制造有限公司 | Bridge gantry non-ferrous metal and composite material machining center |
| CN203064207U (en) * | 2013-01-28 | 2013-07-17 | 上海上飞飞机装备制造有限公司 | Airframe general assembly frame |
| CN203621559U (en) * | 2013-12-10 | 2014-06-04 | 中航成飞民用飞机有限责任公司 | Perforating equipment of large spar assembly |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112676839A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| CN112676839B (en) * | 2020-12-17 | 2021-12-03 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| CN113247297A (en) * | 2021-06-28 | 2021-08-13 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
| CN113247297B (en) * | 2021-06-28 | 2021-12-10 | 成都飞机工业（集团）有限责任公司 | Integrated system for machining and testing large part of machine body |
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Application publication date: 20160127 |