CN115533173A - Special tool for milling edges of cabin glass covers and using method - Google Patents
Special tool for milling edges of cabin glass covers and using method Download PDFInfo
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- CN115533173A CN115533173A CN202211243462.7A CN202211243462A CN115533173A CN 115533173 A CN115533173 A CN 115533173A CN 202211243462 A CN202211243462 A CN 202211243462A CN 115533173 A CN115533173 A CN 115533173A
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- 238000003801 milling Methods 0.000 title claims abstract description 51
- 239000011521 glass Substances 0.000 title claims abstract description 47
- 238000000034 method Methods 0.000 title claims abstract description 25
- 239000000428 dust Substances 0.000 claims description 18
- 230000006835 compression Effects 0.000 claims description 8
- 238000007906 compression Methods 0.000 claims description 8
- 238000005259 measurement Methods 0.000 claims description 3
- 230000005489 elastic deformation Effects 0.000 abstract description 3
- 238000003754 machining Methods 0.000 abstract 3
- 230000001737 promoting effect Effects 0.000 abstract 1
- 238000012545 processing Methods 0.000 description 19
- 238000010586 diagram Methods 0.000 description 13
- 238000009434 installation Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 208000019693 Lung disease Diseases 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical group COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- 229920005372 Plexiglas® Polymers 0.000 description 1
- 238000005299 abrasion Methods 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
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- 230000007547 defect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C3/00—Milling particular work; Special milling operations; Machines therefor
- B23C3/12—Trimming or finishing edges, e.g. deburring welded corners
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23C—MILLING
- B23C9/00—Details or accessories so far as specially adapted to milling machines or cutter
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- 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
- B23Q17/00—Arrangements for observing, indicating or measuring on machine tools
- B23Q17/22—Arrangements for observing, indicating or measuring on machine tools for indicating or measuring existing or desired position of tool or work
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Abstract
Description
技术领域technical field
本发明涉及航空装配技术领域,尤其涉及一种座舱玻璃罩铣边专用工具及使用方法。The invention relates to the technical field of aviation assembly, in particular to a special tool for edge milling of a cockpit glass cover and a use method thereof.
背景技术Background technique
飞机座舱玻璃安装精度,对飞机隐身指标的实现意义重大。同时飞机座舱玻璃的安装质量也关乎着飞行员的生命安全。但因座舱盖玻璃零件的加工精度、座舱盖骨架的加工及装配精度、装配过程中的误差积累等因素,导致安装座舱盖玻璃时需反复调整打磨座舱盖玻璃边缘,加工效率极低,操作者劳动强度大,因此需要研究一种经济快捷的加工方式对座舱盖玻璃边缘处进行加工。The installation accuracy of aircraft cockpit glass is of great significance to the realization of aircraft stealth indicators. At the same time, the installation quality of aircraft cockpit glass is also related to the safety of pilots. However, due to factors such as the processing accuracy of the canopy glass parts, the processing and assembly accuracy of the canopy frame, and the accumulation of errors in the assembly process, it is necessary to repeatedly adjust and polish the edge of the canopy glass when installing the canopy glass, and the processing efficiency is extremely low. The labor intensity is high, so it is necessary to study an economical and quick processing method to process the edge of the canopy glass.
飞机驾驶舱玻璃罩为有机玻璃类材料,厚度为16mm,形状类似于椭圆体局部形状。需要沿舱罩边缘加工出规定形状、尺寸,以方便进行下道安装工序。考虑到玻璃舱罩形状复杂、尺寸较大、自身弹性变形较大等不利因素,设计时采用多组固定导向轮支撑,多组压紧轮压紧,利用驾驶舱罩自身内圆导向,使用气动马达驱动成型铣刀对驾驶舱罩外侧边缘进行铣削加工。同时因为材料自身的特性,加工时会产生大量碎屑粉尘,在结构设计时增加除尘功能。The glass cover of the aircraft cockpit is a plexiglass material with a thickness of 16mm and a shape similar to the partial shape of an ellipsoid. It is necessary to process the specified shape and size along the edge of the canopy to facilitate the next installation process. Considering the unfavorable factors such as complex shape, large size, and large elastic deformation of the glass canopy, multiple sets of fixed guide wheels are used for support in the design, and multiple sets of compression wheels are used for compression. A motor-driven form milling cutter mills the outside edge of the canopy. At the same time, due to the characteristics of the material itself, a large amount of debris and dust will be generated during processing, and the dust removal function is added in the structural design.
发明内容Contents of the invention
为了提高飞机座舱盖玻璃装配质量及加工效率,降低操作者劳动强度,对座舱盖玻璃装配过程进行具体工艺分析,探讨预留精加工余量采用工具进行手动修磨的可行性,设计了一种座舱玻璃罩铣边专用工具,并提出了使用方法及加工流程,用于加工飞机座舱玻璃罩边缘厚度,保证飞机座舱玻璃罩装配质量。In order to improve the quality and processing efficiency of aircraft canopy glass assembly and reduce the labor intensity of operators, a specific process analysis of the canopy glass assembly process was carried out, and the feasibility of using tools for manual grinding with reserved finishing allowance was designed. A special tool for edge milling of the cockpit glass cover, and the use method and processing flow are proposed, which are used to process the edge thickness of the aircraft cockpit glass cover to ensure the assembly quality of the aircraft cockpit glass cover.
本发明的技术方案:一种座舱玻璃罩铣边专用工具,包括底板1、把手2、锁紧手柄、气动马达4、快速接头5、除尘接口6、尺寸调整机构7、挡屑板9、成型铣刀10、压紧轮11、端面导向轮12、固定导向轮13和百分表14;底板1为T形板,包括水平侧和竖直侧;把手2安装于底板1水平侧上表面;竖直侧开有通槽;气动马达4安装于底板1竖直侧一面,除尘接口6、成型铣刀10安装于底板1竖直侧另一面;除尘接口6为漏斗状,成型铣刀10包覆于除尘接口6内部,除尘接口6连接吸尘器用于除尘;气动马达4一端连接成型铣刀10带动其转动,气动马达4另一端设置快速接头5,用于连接风管;气动马达4的安装座底部连接尺寸调整机构7,尺寸调整机构7为丝杠,用于调整气动马达4位置;气动马达4的安装座与除尘接口6,形成半封闭结构;压紧轮11和固定导向轮13分别安装于底板1水平侧两侧的端部;每两个压紧轮11为一组,安装于杠杆机构上,杠杆机构中心为一芯轴,压紧轮11以芯轴为旋转中心;锁紧手柄为螺纹结构,其与杠杆机构间连接压缩弹簧;调整锁紧手柄挤压压缩弹簧,间接作用在杠杆机构上,压紧轮11进而挤压在玻璃罩上;端面导向轮12安装于底板1水平侧两端,且位于压紧轮11和固定导向轮13间;挡屑板9垂直安装于底板1水平侧的压紧轮11外侧,其一方面防止玻璃碎屑飞溅,另一方面与成型铣刀10防护罩形成半封闭结构,使碎屑更容易被吸尘器吸出。The technical solution of the present invention: a special tool for edge milling of the cockpit glass cover, including a
所述底板1水平侧安装一百分表14,其端部与气动马达4的安装座接触。A
所述气动马达4和成型铣刀10间通过固定螺钉15连接,拆卸固定螺钉15,实现更换成型铣刀10。通过调整尺寸调整机构7实现调整气动马达的目的,最终实现调整座舱玻璃罩的加工厚度精度。The
所述端面导向轮12为滚珠轴承结构,加工时与座舱玻璃罩上表面滚动摩擦,防止零件加工时被工具划伤;4个固定导向轮13起限制座舱玻璃罩位置的作用。把手2上安装橡胶护套,避免由于长期手持加工时造成操作者手部磨伤。The end
所述锁紧手柄包括前锁紧手柄3和后锁紧手柄8。所述除尘接口6通过安装工业吸尘器,实现吸附加工过程中的玻璃碎屑,避免被操作者吸入引起肺部疾病。The locking handle includes a
一种座舱玻璃罩铣边专用工具的使用方法,包括步骤如下:A method for using a special tool for edge milling a cockpit glass cover, comprising the following steps:
步骤1.松开锁紧手柄,端面导向轮12与舱罩前端边缘贴紧,锁紧驾驶舱罩前端边缘的压紧手柄;
步骤2.舱罩缓慢推动,于成型铣刀10处切削;
步骤3.切削完成的边缘进入到压紧轮区域后锁紧该处压紧手柄;
步骤4.测量切过的部分,计算剩余余量,调整工具切削量,再次进行切削。
所述步骤1之前进行切削精度调整,具体为;安装百分表14至工具测量位置,调整尺寸调整机构7,观察百分表显示数量,调整成型铣刀10至目的位置。Before the
使用高压气体驱动,设计用于铣削飞机驾驶舱玻璃罩边缘,提高驾驶舱安装精度,改善机体整体空气动力学性能,减轻装配人员劳动强度、降低减少施工过程中人为因素导致的错误机率、减少加工缺陷。Driven by high-pressure gas, it is designed to mill the edge of the glass cover of the aircraft cockpit, improve the installation accuracy of the cockpit, improve the overall aerodynamic performance of the airframe, reduce the labor intensity of assemblers, reduce the error rate caused by human factors in the construction process, and reduce processing defect.
本发明的有益效果:本发明的工具首次在飞机现场装配过程中引入了手持气动式可调精度仿形加工、装配的理念。解决了单一零件加工精度要求过高,大尺寸零件弹性变形对装配精度影响较大,及手工修配工强度大、效率低、质量差等问题。本次研制证实了现场采用可调精度仿形加工、装配理念的可行性及具有的明显优势,在其它装配环节具有极大推广意义。对飞机装配工艺的进步具有推动作用。Beneficial effects of the present invention: the tool of the present invention introduces the concept of hand-held pneumatic adjustable precision profiling processing and assembly in the on-site assembly process of aircraft for the first time. It solves the problems of excessively high processing precision requirements for a single part, large-scale parts elastic deformation has a great influence on assembly precision, and manual repairers with high strength, low efficiency, and poor quality. This development has confirmed the feasibility and obvious advantages of adopting adjustable precision profiling processing and assembly concepts on site, and has great promotion significance in other assembly links. It has a driving effect on the progress of aircraft assembly technology.
附图说明Description of drawings
图1为座舱盖玻璃加工位置示意图;(a)为整体示意图;(b)为细节图;Figure 1 is a schematic diagram of the processing position of the canopy glass; (a) is an overall schematic diagram; (b) is a detailed diagram;
图2为座舱玻璃罩铣边专用工具加工原理示意图;Figure 2 is a schematic diagram of the processing principle of the special tool for edge milling of the cockpit glass cover;
图3为座舱玻璃罩铣边专用工具后侧示意图;Figure 3 is a schematic diagram of the rear side of the special tool for edge milling of the cockpit glass cover;
图4为座舱玻璃罩铣边专用工具前侧示意图;Figure 4 is a schematic diagram of the front side of the special tool for edge milling of the cockpit glass cover;
图5为座舱玻璃罩铣边专用工具加工状态示意图;Figure 5 is a schematic diagram of the processing state of the special tool for edge milling of the cockpit glass cover;
图6为座舱玻璃罩铣边专用工具切削精度调整方法俯视图;Fig. 6 is a top view of the cutting precision adjustment method of the special tool for edge milling of the cockpit glass cover;
图7为座舱玻璃罩铣边专用工具切削精度调整方法示意图;Fig. 7 is a schematic diagram of the cutting accuracy adjustment method of the special tool for edge milling of the cockpit glass cover;
图8为座舱玻璃罩铣边专用工具刀具更换方法示意图;Fig. 8 is a schematic diagram of the tool replacement method of the special tool for edge milling of the cockpit glass cover;
图9为座舱玻璃罩铣边专用工具刀具示意图。Fig. 9 is a schematic diagram of a special tool for edge milling of the cockpit glass cover.
图中:1-底板;2-把手;3-前锁紧手柄;4-气动马达;5-快速接头;6-除尘接口;7-尺寸调整机构;8-后锁紧手柄;9-挡屑板;10-成型铣刀;11-压紧轮;12-端面导向轮;13-固定导向轮;14-百分表;15-固定螺钉;16-专用限位扳手;17-专用紧固扳手。In the figure: 1-bottom plate; 2-handle; 3-front locking handle; 4-air motor; 5-quick connector; 6-dust removal interface; 7-size adjustment mechanism; 8-rear locking handle; Plate; 10-forming milling cutter; 11-pressing wheel; 12-end guide wheel; 13-fixed guide wheel; 14-percent indicator; 15-fixing screw; 16-special limit wrench; .
具体实施方式detailed description
图5为座舱玻璃罩铣边专用工具加工状态示意图;包括步骤如下,Figure 5 is a schematic diagram of the processing state of the special tool for milling the glass cover of the cockpit; the steps are as follows,
1.清理好工作区域,确保清洁没有干涉物品。1. Clean up the working area to ensure that there are no interfering objects.
2.将准备加工的座舱玻璃罩放置在工装架上。2. Place the cockpit glass cover to be processed on the tooling rack.
3.将工具前锁紧手柄3、后锁紧手柄8松开,工具放置在座舱玻璃罩前端边缘;工具端面导向轮12与座舱玻璃罩前端边缘贴紧后锁紧前锁紧手柄3;3. Loosen the
4.握稳工具手柄,启动工具,稳定匀速的缓缓推动工具沿驾驶舱罩内弧面向前切削。4. Hold the tool handle firmly, start the tool, and slowly push the tool at a steady and uniform speed to cut forward along the inner arc of the cockpit cover.
5.切削完成的边缘进入到后压紧轮区域后锁紧后锁紧手柄8。5. Lock the
6.切削完成,将工具取下,清除工作区域及工具上的切屑。6. After the cutting is completed, remove the tool and remove chips from the working area and the tool.
7.测量切过的部分,计算剩余余量,调整工具切削量,再次进行切削。根据余量大小和精度要求,切削可分多次进行。7. Measure the cut part, calculate the remaining allowance, adjust the cutting amount of the tool, and cut again. According to the size of the allowance and the precision requirements, the cutting can be divided into several times.
8.检查切面尺寸及精度符合要求。8. Check that the size and precision of the cut surface meet the requirements.
图6、图7为工具切削精度调整方法示意图,工具切削精度调整方法,包括步骤如下;Figure 6 and Figure 7 are schematic diagrams of the method for adjusting the cutting precision of the tool, and the method for adjusting the cutting precision of the tool includes the following steps;
1.将调整显示百分表14安装到工具测量位置。日常使用工具时,百分表取下,防止百分表14损坏。1. Install the adjustment
2.轻轻松开气动马达4安装座的固定螺钉。2. Gently loosen the set screw of the
3.拧动尺寸调整机构7,观察百分表14显示数量,调整成型铣刀10到合适位置。3. Turn the
4.拧紧气动马达4安装座的固定螺钉,注意用力均匀,可靠。4. Tighten the fixing screws of the
5.检查工具,轻轻转动刀具观察有无干涉。5. Check the tool, turn the tool slightly to see if there is any interference.
6.调整完成,取下百分表14。6. After the adjustment is completed, remove the
图8、图9为工具刀具更换方法示意图,专用限位扳手16和专用紧固扳手17进行刀具更换方法包括步骤如下;Fig. 8 and Fig. 9 are schematic diagrams of the tool replacement method, and the tool replacement method with the
1.松开四个固定螺钉15,将气动马达4和成型铣刀10整体取出。1. Loosen the four fixing
2.使用专用限位扳手16和专用紧固扳手17将夹头松开,将成型铣刀10取出,更换新成型铣刀10并重新锁紧。成型铣刀10上定位面应与垫圈和夹头贴紧。2. Use the
3.将更换完刀具的气动马达与成型铣刀10重新安装,并坚固锁紧螺钉15。3. Reinstall the air motor and the forming
4.手动检查成型铣刀10转动有无干涉及转动不灵活现象。4. Manually check whether there is interference in the rotation of the forming
5.完成成型铣刀10更换。5. Complete the replacement of the forming
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2022
- 2022-10-12 CN CN202211243462.7A patent/CN115533173B/en active Active
Patent Citations (6)
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| US20110214302A1 (en) * | 2010-03-04 | 2011-09-08 | Makita Corporation | Cutting tools |
| CN103801744A (en) * | 2014-02-21 | 2014-05-21 | 庄世良 | Industrial pneumatic edge milling machine |
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