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 PDF

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Publication number
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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glass cover
edge
special tool
air motor
milling cutter
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CN115533173B (en
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刘晓东
张春振
康晓峰
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Shenyang Aircraft Industry Group Co Ltd
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Shenyang Aircraft Industry Group Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C3/00Milling particular work; Special milling operations; Machines therefor
    • B23C3/12Trimming or finishing edges, e.g. deburring welded corners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23CMILLING
    • B23C9/00Details or accessories so far as specially adapted to milling machines or cutter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, 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
    • B23Q17/00Arrangements for observing, indicating or measuring on machine tools
    • B23Q17/22Arrangements for observing, indicating or measuring on machine tools for indicating or measuring existing or desired position of tool or work

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Milling Processes (AREA)

Abstract

The invention belongs to the technical field of aviation assembly, and provides a special tool for milling an edge of a cabin glass cover and a using method thereof. The special tool for milling the edges of the cabin glass covers comprises a locking handle, a pneumatic motor, a size adjusting mechanism, a forming milling cutter, a pressing wheel, an end face guide wheel, a fixed guide wheel and a dial indicator. The invention introduces the concepts of handheld pneumatic type adjustable precision profiling machining and assembling in the field assembling process of the airplane for the first time. The problems that the requirement on the machining precision of a single part is too high, the elastic deformation of a large-size part has great influence on the assembly precision, the strength of a manual repair worker is high, the efficiency is low, the quality is poor and the like are solved. The research proves the feasibility and the obvious advantages of the on-site adoption of the adjustable precision copying machining and assembling concept, has great popularization significance in other assembling links, and has a promoting effect on the progress of the airplane assembling process.

Description

一种座舱玻璃罩铣边专用工具及使用方法A special tool for edge milling of cockpit glass cover and its use method

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 bottom plate 1, a handle 2, a locking handle, an air motor 4, a quick connector 5, a dust removal interface 6, a size adjustment mechanism 7, a chip baffle 9, a forming Milling cutter 10, pressing wheel 11, end face guide wheel 12, fixed guide wheel 13 and dial indicator 14; base plate 1 is a T-shaped plate, including horizontal side and vertical side; handle 2 is installed on the upper surface of base plate 1 horizontal side; There is a through slot on the vertical side; the air motor 4 is installed on the vertical side of the bottom plate 1, the dust removal interface 6 and the forming milling cutter 10 are installed on the other vertical side of the bottom plate 1; the dust removal interface 6 is funnel-shaped, and the forming milling cutter 10 packs Covering the inside of the dust removal interface 6, the dust removal interface 6 is connected to a vacuum cleaner for dust removal; one end of the air motor 4 is connected to the forming milling cutter 10 to drive it to rotate, and the other end of the air motor 4 is provided with a quick connector 5 for connecting to the air duct; the installation of the air motor 4 The bottom of the seat is connected with a size adjustment mechanism 7, and the size adjustment mechanism 7 is a lead screw for adjusting the position of the air motor 4; the mounting seat of the air motor 4 and the dust removal interface 6 form a semi-closed structure; the pressing wheel 11 and the fixed guide wheel 13 are respectively Installed on the ends of both sides of the horizontal side of the bottom plate 1; every two pressing wheels 11 form a group and are installed on the lever mechanism. The center of the lever mechanism is a mandrel, and the pressing wheel 11 takes the mandrel as the rotation center; locking The handle is a threaded structure, and a compression spring is connected between it and the lever mechanism; adjust the locking handle to squeeze the compression spring, which indirectly acts on the lever mechanism, and the pressing wheel 11 is further squeezed on the glass cover; the end guide wheel 12 is installed on the bottom plate 1 Both ends of the horizontal side are located between the pinch wheel 11 and the fixed guide wheel 13; the chip baffle 9 is vertically installed on the outside of the pinch wheel 11 on the horizontal side of the bottom plate 1, on the one hand, it prevents glass debris from splashing, on the other hand, it is compatible with the molding The milling cutter 10 protective cover forms a semi-closed structure, so that debris is more easily sucked out by the vacuum cleaner.

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 dial indicator 14 is installed on the horizontal side of the base plate 1 , and its end is in contact with the mounting seat of the air motor 4 .

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 air motor 4 and the forming milling cutter 10 are connected by fixing screws 15, and the fixing screws 15 are removed to replace the forming milling cutter 10. The purpose of adjusting the air motor is realized by adjusting the size adjustment mechanism 7, and finally the processing thickness accuracy of the cockpit glass cover is adjusted.

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 face guide wheels 12 are of ball bearing structure, which roll and rub against the upper surface of the cockpit glass cover during processing to prevent parts from being scratched by tools during processing; 4 fixed guide wheels 13 play the role of limiting the position of the cockpit glass cover. A rubber sheath is installed on the handle 2 to avoid hand abrasion of the operator due to long-term hand-held processing.

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 front locking handle 3 and a rear locking handle 8 . The dust removal interface 6 is installed with an industrial vacuum cleaner to absorb glass debris during processing, so as to avoid being inhaled by the operator and causing lung diseases.

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;Step 1. Loosen the locking handle, the end guide wheel 12 is tightly attached to the front edge of the cabin cover, and lock the compression handle on the front edge of the cockpit cover;

步骤2.舱罩缓慢推动,于成型铣刀10处切削;Step 2. Slowly push the canopy and cut at 10 places with the forming milling cutter;

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;Step 3. After the cut edge enters the pressing wheel area, lock the pressing handle there;

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。Step 4. Measure the cut part, calculate the remaining allowance, adjust the cutting amount of the tool, and cut again.

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 step 1, the cutting accuracy is adjusted, specifically: install the dial indicator 14 to the tool measurement position, adjust the size adjustment mechanism 7, observe the number displayed by the dial indicator, and adjust the forming milling cutter 10 to the target position.

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 front locking handle 3 and the rear locking handle 8 of the tool, and place the tool on the front edge of the cockpit glass cover; the guide wheel 12 on the end surface of the tool is closely attached to the front edge of the cockpit glass cover, and then lock the front locking handle 3;

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 rear locking handle 8 after the cut edge enters the area of the rear pressing wheel.

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 display dial indicator 14 to the tool measurement position. During daily use of the tool, the dial indicator is taken off to prevent the dial indicator 14 from being damaged.

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 air motor 4 mount.

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 size adjustment mechanism 7, observe the number displayed on the dial indicator 14, and adjust the forming milling cutter 10 to a suitable position.

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 air motor 4 mounting base, and pay attention to the uniform and reliable force.

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 dial gauge 14.

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 special limit wrench 16 and the special fastening wrench 17 includes the following steps;

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 screws 15, and take out the air motor 4 and the forming milling cutter 10 as a whole.

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 special limit wrench 16 and the special tightening wrench 17 to loosen the collet, take out the forming milling cutter 10, replace it with a new forming milling cutter 10 and re-lock it. The positioning surface on the forming milling cutter 10 should be close to the washer and the chuck.

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 milling cutter 10 after the cutter has been replaced, and tighten the locking screw 15 firmly.

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 milling cutter 10 and whether the rotation is inflexible.

5.完成成型铣刀10更换。5. Complete the replacement of the forming milling cutter 10 .

Claims (6)

1.一种座舱玻璃罩铣边专用工具,其特征在于,该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。1. A special tool for milling edge of cockpit glass cover, characterized in that, the special tool for milling edge of cockpit glass cover includes base plate (1), handle (2), locking handle, air motor (4), quick connector (5) , dust removal interface (6), size adjustment mechanism (7), chip guard (9), forming milling cutter (10), pressure wheel (11), end face guide wheel (12), fixed guide wheel (13) and sub table (14); the base plate (1) is a T-shaped plate, including horizontal and vertical sides; the handle (2) is installed on the upper surface of the horizontal side of the base plate (1); the vertical side has a through slot; the air motor (4 ) is installed on the vertical side of the bottom plate (1), and the dust removal interface (6) and the forming milling cutter (10) are installed on the other vertical side of the bottom plate (1); the dust removal interface (6) is funnel-shaped, and the forming milling cutter (10 ) is wrapped inside the dust removal interface (6), and the dust removal interface (6) is connected to a vacuum cleaner for dust removal; one end of the air motor (4) is connected to the forming milling cutter (10) to drive it to rotate, and the other end of the air motor (4) is provided with a quick connector ( 5), used to connect the air duct; the bottom of the mounting seat of the air motor (4) is connected to the size adjustment mechanism (7), and the size adjustment mechanism (7) is a lead screw for adjusting the position of the air motor (4); the air motor (4) ) and the dust removal interface (6) to form a semi-closed structure; the pinch wheel (11) and the fixed guide wheel (13) are respectively installed at the ends of the bottom plate (1) on both sides of the horizontal side; every two pinch wheels (11) is a group, is installed on the lever mechanism, and the center of the lever mechanism is a mandrel, and the pinch wheel (11) is the center of rotation with the mandrel; The locking handle is a threaded structure, which connects a compression spring with the lever mechanism; Adjust the locking handle to squeeze the compression spring, which acts indirectly on the lever mechanism, and the pressure wheel (11) is further squeezed on the glass cover; the end face guide wheel (12) is installed at both ends of the horizontal side of the bottom plate (1), Between the pinch wheel (11) and the fixed guide wheel (13); the chip baffle (9) is vertically installed on the outside of the pinch wheel (11) on the horizontal side of the base plate (1). 2.根据权利要求1所述的座舱玻璃罩铣边专用工具,其特征在于,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。2. The special tool for edge milling of the cockpit glass cover according to claim 1, characterized in that a dial indicator (14) is installed on the horizontal side of the bottom plate (1), and its end is connected with the mounting seat of the air motor (4) touch. 3.根据权利要求1所述的座舱玻璃罩铣边专用工具,其特征在于,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)。3. The special tool for edge milling of the cockpit glass cover according to claim 1, characterized in that, the air motor (4) and the forming milling cutter (10) are connected by a fixing screw (15), and the fixing screw (15) is removed , realize changing forming milling cutter (10). 4.根据权利要求1所述的座舱玻璃罩铣边专用工具,其特征在于,所述端面导向轮(12)为滚珠轴承结构;把手(2)上安装橡胶护套。4. The special tool for edge milling of the cockpit glass cover according to claim 1, characterized in that, the end surface guide wheel (12) is a ball bearing structure; a rubber sheath is installed on the handle (2). 5.一种座舱玻璃罩铣边专用工具的使用方法,其特征在于,包括步骤如下:5. A method for using a special tool for edge milling of a cockpit glass cover, characterized in that the steps are as follows: 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;Step 1. Loosen the locking handle, the end guide wheel (12) is tightly attached to the front edge of the cabin cover, and lock the compression handle on the front edge of the cockpit cover; 步骤2.舱罩缓慢推动,于成型铣刀(10)处切削;Step 2. Slowly push the canopy and cut it at the forming milling cutter (10); 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;Step 3. After the cut edge enters the pressing wheel area, lock the pressing handle there; 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。Step 4. Measure the cut part, calculate the remaining allowance, adjust the cutting amount of the tool, and cut again. 6.根据权利要求5所述的座舱玻璃罩铣边专用工具的使用方法,其特征在于,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。6. The method of using the special tool for edge milling of the cockpit glass cover according to claim 5, characterized in that the cutting accuracy is adjusted before the step 1, specifically: install the dial indicator (14) to the tool measurement position, adjust The size adjustment mechanism (7) observes the number displayed on the dial indicator, and adjusts the forming milling cutter (10) to the target position.
CN202211243462.7A 2022-10-12 2022-10-12 A special tool for milling edge of cockpit glass cover and use method thereof Active CN115533173B (en)

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CN104139199A (en) * 2014-07-28 2014-11-12 江西金品铜业科技有限公司 Copper strip edge-milling device
CN106363216A (en) * 2016-11-29 2017-02-01 四川凌峰航空液压机械有限公司 Milling method of high-precision cylindrical hydraulic oil separation groove
CN111940802A (en) * 2020-08-17 2020-11-17 沈阳飞机工业(集团)有限公司 Milling tool for margin of aluminum alloy skin of airplane
CN213827191U (en) * 2020-10-09 2021-07-30 中威航空材料有限公司 Edge milling device with cloth bag dust removal mechanism

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
CN104139199A (en) * 2014-07-28 2014-11-12 江西金品铜业科技有限公司 Copper strip edge-milling device
CN106363216A (en) * 2016-11-29 2017-02-01 四川凌峰航空液压机械有限公司 Milling method of high-precision cylindrical hydraulic oil separation groove
CN111940802A (en) * 2020-08-17 2020-11-17 沈阳飞机工业(集团)有限公司 Milling tool for margin of aluminum alloy skin of airplane
CN213827191U (en) * 2020-10-09 2021-07-30 中威航空材料有限公司 Edge milling device with cloth bag dust removal mechanism

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