CN110498058A - Hole guiding method suitable for laminated structure of closed angle area - Google Patents
Hole guiding method suitable for laminated structure of closed angle area Download PDFInfo
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- CN110498058A CN110498058A CN201910714995.0A CN201910714995A CN110498058A CN 110498058 A CN110498058 A CN 110498058A CN 201910714995 A CN201910714995 A CN 201910714995A CN 110498058 A CN110498058 A CN 110498058A
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- laminated structure
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- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000010276 construction Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000005553 drilling Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H7/00—Marking-out or setting-out work
- B25H7/04—Devices, e.g. scribers, for marking
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Length-Measuring Instruments Using Mechanical Means (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Abstract
Description
技术领域technical field
本申请涉及飞机装配技术领域,特别是一种适用于叠层结构单面封闭区域闭角孔位的引孔方法。The present application relates to the technical field of aircraft assembly, and in particular, to a hole guiding method suitable for closed-angle holes in a single-sided closed area of a laminated structure.
背景技术Background technique
在飞机装配领域,通常针对一些类似于闭角T型角片叠层结构处的划线制孔时,由于角片闭角区域制孔没有施工空间,所以需要在T型角片闭角区域表面先用铅笔划出孔的边距位置,然后借助钢板尺将T型件表面孔位的线引至下表面,最终从下表面开敞区域进行制孔。目前,对于闭角区域制孔工具一般选用直角风钻、偏心风钻,因使用要求、使用场合的不同存在不同的种类,以满足不同的制孔需求。但是,某些区域结构复杂,空间的局限性使得制孔环境的可操作性变差,在某些特殊情况下,例如空间单面封闭的区域,靠近边缘的闭角区域叠层结构,通用的制孔工具无法满足闭角区域制孔要求,并且没有操作施工空间,需要进行划线引孔,在普通划线引孔的过程中由于需要将闭角区上表面的线通过人眼的观察引至下表面,在这个过程中由于视觉的误差以及钢板尺的误差,造成了孔位的偏离,使得上下表面的孔位不在同心位置,从而影响了后续制孔的质量和效率,故需要一种特制的引孔器及引孔方法用以完成空间闭角区域叠层结构的引孔工作。In the field of aircraft assembly, it is usually necessary to make holes on the surface of the closed corner area of the T-shaped corner piece because there is no construction space for making holes in the laminated structure of the closed-angle T-shaped corner piece. First use a pencil to mark the edge position of the hole, then use a steel ruler to lead the line of the hole position on the surface of the T-shaped piece to the lower surface, and finally make the hole from the open area of the lower surface. At present, right-angle pneumatic drills and eccentric pneumatic drills are generally used for hole-making tools in the closed-angle area. There are different types due to different use requirements and application occasions to meet different hole-making needs. However, the structure of some areas is complex, and the limitation of space makes the operability of the hole-making environment worse. The hole-making tool cannot meet the hole-making requirements in the closed-angle area, and there is no room for operation and construction, so it is necessary to scribe the hole. To the lower surface, in this process, due to the visual error and the error of the steel ruler, the hole position deviates, so that the hole position on the upper and lower surfaces is not concentric, thus affecting the quality and efficiency of the subsequent hole making, so a The specially made hole guide and hole guide method are used to complete the hole guide work of the laminated structure in the space closed-angle area.
发明内容SUMMARY OF THE INVENTION
为了解决上述问题,本申请的目的在于提供一种适用于闭角区域叠层结构的引孔方法。In order to solve the above problems, the purpose of the present application is to provide a hole guiding method suitable for the stacked structure in the closed-angle area.
一种适用于闭角区域叠层结构的引孔方法,所述闭角区域为固定在叠层结构上方的角片的闭角区域,该方法即使用引孔器在叠层结构的上下表面划出待制孔的孔位,并从叠层结构下方进行反向制孔。引孔器结构包括导杆、固定测量块、滑动测量块,固定测量块固定在导杆前端,并与导杆垂直,固定测量块上设有刻度线,滑动测量块垂直穿在导杆上并可沿导杆滑动,滑动测量块上设有与固定测量块完全一致的刻度线。A hole guide method suitable for a laminated structure in a closed-angle area, the closed-angle area is the closed-angle area of a corner sheet fixed above the laminated structure, and the method is to use a hole guide to draw the upper and lower surfaces of the laminated structure. The hole position of the hole to be made is drawn, and the reverse hole making is carried out from the bottom of the laminated structure. The hole guide structure includes a guide rod, a fixed measuring block, and a sliding measuring block. The fixed measuring block is fixed at the front end of the guide rod and is perpendicular to the guide rod. It can be slid along the guide rod, and the sliding measuring block is provided with a scale line that is exactly the same as the fixed measuring block.
引孔步骤如下:The drilling steps are as follows:
1、在叠层结构上表面角片的闭角区域划出所需制孔的初孔的孔位;1. Draw the hole position of the initial hole for the required hole in the closed-angle area of the surface corner sheet on the laminated structure;
2、将固定测量块的下表面贴住角片的闭角区域,并将固定测量块的刻度线对准所划出的孔位;2. Stick the lower surface of the fixed measuring block to the closed-angle area of the corner piece, and align the scale line of the fixed measuring block with the drawn hole position;
3、将滑动测量块沿导杆向上方推动,直至滑动测量块上表面贴住叠层结构的下方;3. Push the sliding measuring block upward along the guide rod until the upper surface of the sliding measuring block is attached to the bottom of the laminated structure;
4、读取固定测量块表面刻度线数据,根据固定测量块的数据,在滑动测量块的刻度尺上读出该数据,并根据该数据在叠层结构的下方划出孔位;4. Read the scale line data on the surface of the fixed measuring block, read the data on the scale of the sliding measuring block according to the data of the fixed measuring block, and draw the hole position under the laminated structure according to the data;
5、根据所划出的孔位,从叠层结构的下方沿着叠层结构法向反向制孔。5. According to the marked hole positions, make holes from the bottom of the laminated structure along the normal direction of the laminated structure in the reverse direction.
该引孔方法适用于闭角区域叠层结构,引孔器的引孔操作具有良好的适用性,解决了普通纯手工划线引孔孔位不准确的问题,尤其针对闭角区域空间受限影响施工的情况,该方法使用简便,且易于操作,从而提高装配区域孔位的准确性,提升了装配现场的装配效率。The hole guiding method is suitable for the laminated structure in the closed-angle area, and the hole-guiding operation of the hole-guiding device has good applicability. Affecting the construction situation, the method is easy to use and easy to operate, thereby improving the accuracy of hole positions in the assembly area and improving the assembly efficiency on the assembly site.
下面结合附图和实施例对本发明进一步说明。The present invention will be further described below in conjunction with the accompanying drawings and embodiments.
附图说明Description of drawings
图1引孔器的结构示意图Figure 1 Schematic diagram of the structure of the hole guide
图2引孔器使用示意图Figure 2 Schematic diagram of the use of the hole guide
图中编号说明:1导杆、2、固定测量块 3滑动测量块、4刻度线Number description in the figure: 1 guide rod, 2, fixed measuring block 3 sliding measuring block, 4 scale line
具体实施方式Detailed ways
在飞机结构中,闭角边缘区域为固定在叠层结构上方的角片的闭角区域。如图1所示,引孔器包括导杆1、固定测量块2、滑动测量块3,以及在测量块上的刻度线4,固定测量块2固定在导杆1前端,并与导杆1垂直,固定测量块3上设有刻度线4,滑动测量块3垂直穿在导杆1上并可沿导杆1滑动,滑动测量块3上设有与固定测量块2完全一致的刻度线4。In aircraft construction, the closed-angle edge region is the closed-angle region of the corner piece fixed above the laminate structure. As shown in Figure 1, the hole guide includes a guide rod 1, a fixed measuring block 2, a sliding measuring block 3, and a scale line 4 on the measuring block. The fixed measuring block 2 is fixed at the front end of the guide rod 1, and is connected with the guide rod 1 Vertical, there is a scale line 4 on the fixed measuring block 3, the sliding measuring block 3 is vertically penetrated on the guide rod 1 and can slide along the guide rod 1, and the sliding measuring block 3 is provided with a scale line 4 that is completely consistent with the fixed measuring block 2 .
如图2所示,使用该引孔器进行引孔的方法,操作过程为:As shown in Figure 2, the method of using the hole guide to guide holes, the operation process is as follows:
1.在角片的闭角区域划出所需制孔的初孔的孔位;1. In the closed-angle area of the corner piece, mark the hole position of the initial hole for the required hole;
2.将固定测量块2的下表面贴住角片的闭角区域,并将固定测量块2 的刻度线对准所划出的孔位;2. Stick the lower surface of the fixed measuring block 2 against the closed-angle area of the corner piece, and align the scale line of the fixed measuring block 2 with the drawn hole position;
3.将滑动测量块3沿导杆1向上方推动,直至滑动测量块3上表面贴住叠层结构的下方;3. Push the sliding measuring block 3 upward along the guide rod 1 until the upper surface of the sliding measuring block 3 is attached to the bottom of the laminated structure;
4.读取固定测量块2表面刻度线数据,根据固定测量块2的数据,在滑动测量块3的刻度尺4上读出该数据,并根据该数据在叠层结构的下方划出孔位;4. Read the scale line data on the surface of the fixed measuring block 2, read the data on the scale 4 of the sliding measuring block 3 according to the data of the fixed measuring block 2, and draw a hole position under the laminated structure according to the data ;
5.根据所划出的孔位,从叠层结构的下方沿着叠层结构法向反向制孔。5. According to the marked hole positions, make holes in the reverse direction along the normal direction of the laminated structure from below the laminated structure.
该方法可以解决实际操作中因区域开敞性差而导致的孔位不准确、制孔偏差、以及操作性差等问题,该方法使用简单,操作方便,提高了装配的准确度,提升了装配效率。The method can solve the problems of inaccurate hole position, hole-making deviation, and poor operability caused by poor area openness in actual operation.
Claims (8)
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CN201910714995.0A CN110498058A (en) | 2019-08-02 | 2019-08-02 | Hole guiding method suitable for laminated structure of closed angle area |
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Citations (7)
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US4601618A (en) * | 1985-02-27 | 1986-07-22 | The Boeing Company | Pilot hole locator and drill guide and method |
CN1695852A (en) * | 2005-05-12 | 2005-11-16 | 赵赫 | Optical coordinae type bench drill |
CN201693217U (en) * | 2010-03-16 | 2011-01-05 | 沈阳飞机工业(集团)有限公司 | Arch-shaped hole digger |
CN203578859U (en) * | 2013-11-28 | 2014-05-07 | 上海航天精密机械研究所 | Special guide hole device for horseshoe-shaped structure member |
CN203830775U (en) * | 2014-04-18 | 2014-09-17 | 中航沈飞民用飞机有限责任公司 | Track type equidistant perpendicular drilling device |
US20180208328A1 (en) * | 2017-01-25 | 2018-07-26 | The Boeing Company | Method and system for joining structures |
CN208800829U (en) * | 2018-08-20 | 2019-04-30 | 中国商用飞机有限责任公司 | Adjustable perforator |
-
2019
- 2019-08-02 CN CN201910714995.0A patent/CN110498058A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4601618A (en) * | 1985-02-27 | 1986-07-22 | The Boeing Company | Pilot hole locator and drill guide and method |
CN1695852A (en) * | 2005-05-12 | 2005-11-16 | 赵赫 | Optical coordinae type bench drill |
CN201693217U (en) * | 2010-03-16 | 2011-01-05 | 沈阳飞机工业(集团)有限公司 | Arch-shaped hole digger |
CN203578859U (en) * | 2013-11-28 | 2014-05-07 | 上海航天精密机械研究所 | Special guide hole device for horseshoe-shaped structure member |
CN203830775U (en) * | 2014-04-18 | 2014-09-17 | 中航沈飞民用飞机有限责任公司 | Track type equidistant perpendicular drilling device |
US20180208328A1 (en) * | 2017-01-25 | 2018-07-26 | The Boeing Company | Method and system for joining structures |
CN208800829U (en) * | 2018-08-20 | 2019-04-30 | 中国商用飞机有限责任公司 | Adjustable perforator |
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Application publication date: 20191126 |