WO2022011522A1 - 一种用于飞机客舱玻璃组件清洁与组装的辅助工装 - Google Patents

一种用于飞机客舱玻璃组件清洁与组装的辅助工装 Download PDF

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Publication number
WO2022011522A1
WO2022011522A1 PCT/CN2020/101750 CN2020101750W WO2022011522A1 WO 2022011522 A1 WO2022011522 A1 WO 2022011522A1 CN 2020101750 W CN2020101750 W CN 2020101750W WO 2022011522 A1 WO2022011522 A1 WO 2022011522A1
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WIPO (PCT)
Prior art keywords
rubber
main shaft
frame
glass
sealing sleeve
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PCT/CN2020/101750
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English (en)
French (fr)
Inventor
顾辉
张伟光
王德超
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山东太古飞机工程有限公司
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Publication of WO2022011522A1 publication Critical patent/WO2022011522A1/zh

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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
    • B64F5/30—Cleaning aircraft
    • 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
    • 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
    • B64F5/40—Maintaining or repairing aircraft

Definitions

  • the invention relates to the technical field of aircraft cabin glass maintenance, in particular to an auxiliary tool for cleaning and assembling of aircraft cabin glass components.
  • the maintenance of aircraft cabin glass belongs to the routine work of aircraft regular inspection.
  • the purpose of this work is to check the damage to the inner and outer layers of the glass during the operation cycle of the aircraft, so as to avoid excessive glass damage and increase the risk of aircraft operation.
  • the glass has too many scratches and the depth exceeds the limit, it will be repaired manually or replaced with a new glass directly.
  • Before reinstalling the glass its components need to be cleaned, one is to ensure the transparency of the glass, and the other is to carry out a secondary inspection during the cleaning process to avoid omissions.
  • the glass assembly is composed of inner glass, outer glass, middle support ring, and rubber sealing sleeve. After cleaning the four parts with glass water and air gun, they are assembled.
  • the present invention provides a tool that effectively avoids secondary pollution to the inner and outer glass during assembly and improves tooling efficiency.
  • An auxiliary tool for cleaning and assembling of glass components in an aircraft cabin comprising:
  • the rack is composed of a left frame vertically arranged at the left end, a right frame vertically arranged at the right end, and a middle bracket connected to the left frame and the right frame, and the left frame, the right frame and the middle frame are formed in the top view direction H-shaped structure;
  • the guide rail I is horizontally arranged in the left frame along the front-rear direction;
  • Guide rail II horizontally arranged in the right frame along the front-rear direction;
  • the rubber sealing sleeve is fixed in the middle frame by the fixing device.
  • the outer ends of the middle frame and located at the four arc corners of the rubber sealing sleeve are respectively provided with rubber skin flanging mechanisms.
  • the rubber skins on the front and rear sides of the arc corners of the rubber sealing sleeve are respectively turned to the outside;
  • Two sliding blocks II are provided with sliding holes II matching the guide rail I, and the two sliding blocks II are located at the front and rear ends of the intermediate frame respectively;
  • Two sliders I are provided with sliding holes I matching the guide rail II, and the two sliders I are located at the front and rear ends of the intermediate frame respectively;
  • a main shaft is arranged along the left and right direction between the slider I and the slider II on the same side, a number of rubber suction cups are arranged on the main shaft, and a circle matching the outer diameter of the main shaft is respectively set in the slider I and the slider II.
  • the two ends of the main shaft are respectively rotated and installed in the corresponding circular holes on the same side, the inner glass is adsorbed and fixed by the rubber suction cup at one end, and the outer glass is adsorbed and fixed by the rubber suction cup at the other end;
  • the spindle locking device is arranged on the sliding block I. When the spindle rotates 90°, the spindle locking device locks and fixes the spindle relative to the sliding block I.
  • the above-mentioned fixing device includes a fixing rod horizontally arranged at the right end of the middle frame, a fixing rod vertically arranged at the lower end of the middle frame, a movable rod slidably inserted in the upper end of the middle frame along the vertical direction, and slidably inserted along the horizontal direction.
  • the movable rod at the left end of the intermediate frame, the inner end of the fixed rod is provided with a plug, the plug is inserted into the groove provided along the circumferential direction in the middle part of the rubber sealing sleeve, and the middle part of the movable rod is provided with a circular ring.
  • the boss, the spring I is sleeved on the movable rod, its upper end is connected with the middle frame, and its lower end is connected with the boss, the inner end of the movable rod is provided with a plug, under the elastic force of the spring I, the plug is inserted into the middle of the rubber sealing sleeve
  • the head ends of the four plugs are in contact with the outer ends of the support rings that are clamped in the card grooves in the card grooves arranged in the circumferential direction.
  • the above-mentioned rubber leather flanging mechanism has two clamping arms, the two clamping arms are hinged to form an X shape through a pin shaft, the tail ends of the clamping arms are connected by a clamping arm spring, and the head end of the clamping arm is provided with a rubber sealing sleeve.
  • the arc clamp rods match the curvature of the arc corners
  • the two sides of the two clamp arms are respectively provided with brackets fixed on the middle frame
  • the inner end of the bracket is provided with a rubber block
  • the rubber block is provided with
  • the corresponding circular arc corners are perpendicular to the chute, in the chute, there are several sockets that match the outer diameter of the pin shaft at intervals along its length direction, and the pin shafts on both sides of the two clamping arms are respectively inserted on the same side corresponding to each other.
  • the two arc clamp rods are clamped on the front and rear sides of the arc corner of the rubber sealing sleeve respectively, and the arc clamp rod turns the rubber skin on the same side outwards and clamps tight.
  • the above-mentioned main shaft locking device includes a locking handle and a sliding rod
  • the main shaft is provided with a through hole along its axial direction
  • the guide rail II is provided with a long hole along its length direction
  • the head end of the main shaft is provided with an external thread I.
  • the head end of the main shaft passes through the long hole
  • the sliding rod is inserted into the through hole of the main shaft along the axial direction of the main shaft.
  • the nut II is provided with a round hole.
  • the head end of the sliding rod passes through the circular hole of the nut II and is connected to the locking handle. I contact, the outer end of the slider I is provided with two card slots matching the thickness of the locking handle, and the two card slots are arranged in a cross shape. in the card slot.
  • the head end of the movable rod is provided with an external thread II, and a hexagonal nut is screwed on the external thread II.
  • the beneficial effects of the present invention are as follows: the inner layer glass is adsorbed and fixed on the main shaft on one side through the rubber sucker, the outer layer glass is adsorbed and fixed on the main shaft on the other side through the rubber sucker, and then the main shaft is rotated to make the outer glass and the inner layer glass They are all rotated to the horizontal state. After the rotation is in place, the main shaft is locked and fixed by the main shaft locking device. At this time, the inner glass and outer glass can be easily cleaned. After the cleaning is completed, the main shaft is unlocked and the main shaft is rotated 90° , at this time, both the inner glass and the outer glass are rotated to the vertical state, and the main shaft is locked and fixed by the main shaft locking device again.
  • the rubber skin flanging mechanism turns the rubber skins on the front and rear sides of the four arc corners of the rubber sealing sleeve to the outside respectively in the middle frame, the inner glass and the outer glass are slid into the opening of the rubber sealing sleeve. , and then contact the effect of the rubber skin flanging mechanism on the rubber skin. After the rubber skin returns to the original state, the inner glass and the outer glass are wrapped and fixed. After the fixing device is released, the installed glass assembly can be removed from the intermediate frame, which improves the cleaning and installation efficiency of the aircraft cabin glass, and effectively avoids the contamination of the glass during the installation process.
  • Fig. 1 is the three-dimensional structure schematic diagram of the present invention
  • Fig. 2 is the three-dimensional structure schematic diagram of the main shaft part of the present invention.
  • Fig. 3 is the three-dimensional structure schematic diagram of the rubber sealing sleeve part of the present invention.
  • Fig. 4 is the three-dimensional structure schematic diagram of the movable rod part of the present invention.
  • Fig. 5 is the three-dimensional structure schematic diagram of the clamp arm part of the present invention.
  • An auxiliary tool for cleaning and assembling an aircraft cabin glass assembly comprising: a frame, which consists of a left frame 1 vertically arranged at the left end, a right frame 2 vertically arranged at the right end, and a frame connected to the left frame 1 and the left frame.
  • the middle bracket 3 of the right frame 2 is formed, and the left frame 1, the right frame 2 and the middle frame 3 form an H-shaped structure in the top view direction;
  • the guide rail I 6 is horizontally arranged in the left frame 1 along the front and rear directions;
  • the direction is horizontally arranged in the right frame 2;
  • the rubber sealing sleeve 9 is fixed in the middle frame 3 by the fixing device, and the outer ends of the middle frame 3 and located at the four arc corners of the rubber sealing sleeve 9 are respectively provided with rubber skins.
  • the rubber skin flanging mechanism turns the rubber skins on the front and rear sides of the arc corner of the corresponding rubber sealing sleeve 9 to the outside respectively;
  • Sliding hole II 18, two sliders II 17 are located at the front and rear ends of the middle frame 3 respectively;
  • two sliders I 15 are internally provided with sliding holes I 20 matching the guide rail II 7, and two sliders I 15 They are respectively located at the front and rear ends of the intermediate frame 3; between the slider I 15 and the slider II 17 on the same side, a main shaft 4 is arranged along the left and right direction, and a number of rubber suction cups 5 are arranged on the main shaft 4.
  • the slider I 15 and the slider II 17 are respectively provided with circular holes 19 that match the outer diameter of the main shaft 4.
  • Both ends of the main shaft 4 are respectively rotated and installed in the corresponding circular holes 19 on the same side.
  • the suction cup 5 is adsorbed and fixed with the outer glass 32; and the main shaft locking device is arranged on the slider I 15.
  • the main shaft locking device locks and fixes the main shaft 4 relative to the slider I 15.
  • the inner glass 8 is adsorbed and fixed on the main shaft 4 on one side through the rubber suction cup 5, and the outer glass 32 is adsorbed and fixed on the main shaft 4 on the other side through the rubber suction cup 5, and then the main shaft 4 is rotated to make the outer glass 32. Both the inner glass 8 and the inner glass 8 are rotated to the horizontal state.
  • the main shaft 4 is locked and fixed by the main shaft locking device.
  • the inner glass 8 and the outer glass 32 can be easily cleaned.
  • the main shaft 4 is released.
  • the main shaft 4 is rotated 90°, at this time the inner glass 8 and the outer glass 32 are both rotated to the vertical state, and the main shaft 4 is locked and fixed by the main shaft locking device again. Then move the main shaft 4 inward, so that the main shaft 4 slides along the guide rail I 6 through the slider II 17, and slides along the guide rail II 7 through the slider I 15.
  • the rubber skin flanging mechanism in the middle frame 3 turns the rubber skins on the front and rear sides of the four arc corners of the rubber sealing sleeve 9 to the outside respectively, the inner glass 8 and the outer glass 32 are slid into the rubber sealing. In the opening of the sleeve 9, the action of the rubber skin flanging mechanism on the rubber skin is then contacted. After the rubber skin returns to the original state, the inner glass 8 and the outer glass 32 are wrapped and fixed. After the fixing device is released, the installed glass assembly can be removed from the intermediate frame 3, which improves the cleaning and installation efficiency of the aircraft cabin glass, and effectively avoids the contamination of the glass during the installation process.
  • the fixing device can be the following structure, which includes a fixing rod 12 arranged horizontally at the right end of the middle frame 3, a fixing rod 12 vertically arranged at the lower end of the middle frame 3, and a movable rod slidably inserted at the upper end of the middle frame 3 along the vertical direction 29 and the movable rod 29 slidably inserted in the left end of the middle frame 3 along the horizontal direction, the inner end of the fixed rod 12 is provided with a plug 31, and the plug 31 is inserted into the groove 27 provided in the circumferential direction in the middle part of the rubber sealing sleeve 9, and the movable rod
  • the middle part of the rod 29 is provided with a circular boss 30, the spring I 14 is sleeved on the movable rod 29, its upper end is connected with the intermediate frame 3, and its lower end is connected with the boss 30, and the inner end of the movable rod 29 is provided with a plug 31.
  • the plug 31 Under the elastic force of the spring I 14, the plug 31 is inserted into the groove 27 provided in the circumferential direction in the middle part of the rubber sealing sleeve 9, and the head ends of the four plugs 31 are clamped in the groove 27. contact with the outer ends.
  • the movable rods 29 on the upper and left sides of the middle frame 3 are pulled outward to compress the spring I 14, and the rubber sealing head 9 is placed in the middle frame 3, and its lower end passes through the fixed rod 12 at the lower end of the middle frame 3.
  • the plug 31 above is inserted into the card slot 27, the plug 31 on the fixed rod 12 on the right end of the middle frame 3 is inserted into the card slot 27, and then the movable rod 29 is released, so that under the elastic force of the spring I 14, the plug on the movable rod 29 31 is inserted into the upper and left ends of the card grooves 27 in the rubber sealing sleeve to realize clamping and fixing in four directions: up, down, left and right.
  • the rubber sealing sleeve 9 can be taken out after the movable rod 29 is pulled outside to disengage the plug 31 from the card slot 27 , which is simple and convenient to use.
  • the rubber leather flanging mechanism can be of the following structure, which includes two clamping arms 11, the two clamping arms 11 are hinged to form an X shape through the pin shaft 34, the tail end of the clamping arm 11 is connected by the clamping arm spring 35, the head of the clamping arm 11 is connected
  • the end is provided with a circular arc clamp rod 36 that matches the curvature of the circular arc corner of the rubber sealing sleeve 9
  • the two sides of the two clamping arms are respectively provided with brackets 10 fixed on the middle frame 3, and the inner end of the bracket 10 is provided with rubber.
  • the rubber block 37 is provided with a chute 38 perpendicular to the corresponding arc corner, the chute 38 is spaced along its length direction with a number of sockets 39 that match the outer diameter of the pin shaft 34, two clamping arms
  • the pin shafts 34 on both sides of 11 are respectively inserted into the corresponding jacks 39 on the same side, and the two arc clamp rods 36 are clamped respectively on the front and rear sides of the circular arc corner of the rubber sealing sleeve 9 under the elastic force of the clamp arm spring 35.
  • the circular arc clamp rod 36 opens the rubber skin on the same side outwards and clamps it.
  • the two clamping arms 11 are pressed inward to compress the clamping arm springs 35, so that the two arc clamping rods 36 are opened.
  • the rubber block 37 is made of rubber material, so the pin shaft 34 squeezes and deforms each socket 39 when moving, so that it can be moved into the corresponding socket 39, so that the arc clamp rod 36 can clamp the rubber skin of the slot 27.
  • the rubber skins are turned over by moving each clamp arm 11 .
  • the main shaft locking device can be the following structure, which includes a locking handle 16 and a sliding rod 22, a through hole is provided in the main shaft 4 along its axial direction, a long hole is provided in the guide rail II 7 along its length direction, and the head end of the main shaft 4 is provided with a External thread I 21, the head end of the main shaft 4 passes through the long hole, the sliding rod 22 is inserted into the through hole of the main shaft 4 along the axial direction of the main shaft 4, the sliding rod 22 is provided with a threaded section, and the nut I 24 is screwed to the thread On the segment, the nut II 25 is screwed on the external thread I 21, the nut II 25 is provided with a round hole, the head end of the sliding rod 22 passes through the round hole of the nut II 25 and is connected and fixed with the locking handle 16, and the spring II 23 is set In the sliding rod 22, one end is in contact with the nut II 25, and the other end is in contact with the nut I 24.
  • the outer end of the slider I 15 is provided with two card slots 26 that match the thickness of the locking handle 16.
  • the slots 26 are arranged in a cross shape, and when the locking handle 16 is rotated 90 degrees, it is inserted into the corresponding slot 26 .
  • the locking handle 16 is inserted into the horizontal card slot 26.
  • the main shaft 4 is rotated until the inner glass 8 and the outer glass 32, which are adsorbed and fixed by the rubber suction cup 5, are in a horizontal state, and the glass can be easily cleaned at this time.
  • pull out the locking handle 16 pull out the locking handle 16, and drive the sliding rod 22 to slide outward along the through hole in the main shaft 4. Since the head end of the main shaft 4 is fixed with a nut II 25, the sliding rod 22 moves when sliding outward.
  • the nut I 24 squeezes the spring II 23, so that the locking handle 16 is detached from the horizontal card slot 26, and then the main shaft 4 is rotated by 90° by rotating the locking handle 16, so as to drive the inner glass 8 and the outer glass 32 from The horizontal device is rotated to the vertical state, and the locking handle 16 is released after the rotation is in place.
  • the locking handle 16 is inserted into the card slot 26 in the vertical state to realize the locking of the main shaft 4 rotating in place to ensure that it is in a vertical position.
  • the inner glass 8 and the outer glass 32 in the straight state are in the vertical state.
  • the head end of the movable rod 29 is provided with an external thread II 33, and a hexagonal nut 13 is screwed on the external thread II 33.
  • the movable rod 29 can be easily pulled through the hexagonal nut 13, so that the plug 31 can be disengaged from the card slot 27, which improves the convenience of operation.

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  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Securing Of Glass Panes Or The Like (AREA)
  • Window Of Vehicle (AREA)

Abstract

一种用于飞机客舱玻璃组件清洁与组装的辅助工装，内层玻璃和外层玻璃清洁完成后，解除主轴的锁止，将主轴转动90°，此时内层玻璃和外层玻璃均转动至竖直状态，再次通过主轴锁止装置将主轴锁止固定。由于橡胶皮翻边机构在中间框架中将橡胶密封套四个圆弧拐角处前后两侧的橡胶皮分别向外侧翻开，因此将内层玻璃和外层玻璃滑动装入橡胶密封套的开口中，之后解除橡胶皮翻边机构对橡胶皮的作用，橡胶皮恢复原始状态后将内层玻璃和外层玻璃包裹固定。之后解除固定装置后即可将安装好的玻璃组件从中间框架中拆下，提高了飞机客舱玻璃的清洁和安装的效率，有效避免了安装过程中对玻璃的污染。

Description

一种用于飞机客舱玻璃组件清洁与组装的辅助工装 技术领域
本发明涉及飞机客舱玻璃维护技术领域，具体涉及一种用于飞机客舱玻璃组件清洁与组装的辅助工装。
背景技术
飞机客舱玻璃的维护属于飞机定检的例行工作，该工作目的在于检查飞机运行周期内造成的玻璃内、外层的损伤情况，避免玻璃损伤超限，增加飞机运行风险。当发现玻璃出现划痕过多，以及深度超限时，将对其进行人工修复或者直接更换新玻璃。在重新安装玻璃前需要对其组件进行清洁，一是为了保证玻璃的透明度，二是在清洁的过程中进行二次检查，避免出现遗漏。玻璃组件由内层玻璃，外层玻璃，中间支撑圆环，橡胶密封套组成，将四个部件用玻璃水及风枪洗净吹干后，进行组装，由于安装时需要将橡胶固定套的固定胶皮翻起才能使内、外层玻璃插入，但是这个过程工作人员需要极其小心的操作，避免在安装过程中杂质、手印等污染物留在内、外层玻璃的内侧，进而造成二次返工，该工作又去缺乏专用工具，极大的浪费工作人员时间，工作效率低下。
发明内容
本发明为了克服以上技术的不足，提供了一种有效避免在进行组装时对内、外层玻璃二次污染，提高工装效率的工装。
本发明克服其技术问题所采用的技术方案是：
一种用于飞机客舱玻璃组件清洁与组装的辅助工装，包括：
机架，其由竖直设置于左侧端的左框架、竖直设置于右侧端的右框架以及连接于左框架与右框架的中间支架构成，左框架、右框架与中间框架在俯视方向上形成H形结构；
导轨Ⅰ，沿前后方向水平设置于左框架中；
导轨Ⅱ，沿前后方向水平设置于右框架中；
橡胶密封套，通过固定装置固定于中间框架中，所述中间框架中且位于橡胶密封套的四个圆弧拐角处的外侧端分别设置有橡胶皮翻边机构，橡胶皮翻边机构将对应的橡胶密封套的圆弧拐角处前后两侧的橡胶皮分别向外侧翻开；
两个滑块Ⅱ，其内部设置有与导轨Ⅰ相匹配的滑孔Ⅱ，两个滑块Ⅱ分别位于中间框架的前后两端；
两个滑块Ⅰ，其内部设置有与导轨Ⅱ相匹配的滑孔Ⅰ，两个滑块Ⅰ分别位于中间框架的前后 两端；
同侧的滑块Ⅰ与滑块Ⅱ之间沿左右方向设置有主轴，所述主轴上设置有若干橡胶吸盘，所述滑块Ⅰ与滑块Ⅱ中分别设置有与主轴外径相匹配的圆孔，主轴两端分别转动安装于同侧对应的圆孔中，一端橡胶吸盘吸附固定有内层玻璃，另一端的橡胶吸盘吸附固定有外层玻璃；以及
主轴锁止装置，设置于滑块Ⅰ上，当主轴转动90°后主轴锁止装置将主轴相对滑块Ⅰ锁止固定。
进一步的，上述固定装置包括水平设置于中间框架右侧端的固定杆、竖直设置于中间框架下端的固定杆、沿竖直方向滑动插装于中间框架上端的活动杆以及沿水平方向滑动插装于中间框架左侧端的活动杆，所述固定杆的内侧端设置有插头，所述插头插入橡胶密封套中间部位沿圆周方向设置的卡槽中，所述活动杆中部位设置有圆环形的凸台，弹簧Ⅰ套装于活动杆上，其上端与中间框架相连接，其下端与凸台相连，所述活动杆的内侧端设置有插头，在弹簧Ⅰ的弹力下，插头插入橡胶密封套中间部位沿圆周方向设置的卡槽中，四个插头的头端与卡置于卡槽中的支撑圆环的外侧端相接触。
进一步的，上述橡胶皮翻边机构两个夹臂，两个夹臂通过销轴铰接形成X形，夹臂的尾端通过夹臂弹簧相连，所述夹臂的头端设置有与橡胶密封套的圆弧拐角曲率相匹配的圆弧夹杆，两个夹臂的两侧分别设置有固定于中间框架上的支架，所述支架的内侧端设置有橡胶块，所述橡胶块中设置有与对应的圆弧拐角相垂直的滑槽，所述滑槽中延其长度方向间隔设置有若干与销轴外径相匹配的插孔，两个夹臂两侧的销轴分别插装于同侧对应的插孔中，在夹臂弹簧的弹力下两个圆弧夹杆分别夹紧于橡胶密封套圆弧拐角处前后两侧，且圆弧夹杆将同侧的橡胶皮向外翻开后夹紧。
进一步的，上述主轴锁止装置包括锁定手柄以及滑杆，所述主轴内沿其轴向设置有通孔，所述导轨Ⅱ中延其长度方向设置有长孔，主轴的头端设置有外螺纹Ⅰ，主轴的头端穿过长孔，滑杆沿主轴的轴向插装于主轴的通孔中，滑杆上设置有螺纹段，螺母Ⅰ旋合于螺纹段上，螺母Ⅱ旋合于外螺纹Ⅰ上，螺母Ⅱ中设置有圆孔，滑杆的头端穿过螺母Ⅱ的圆孔后与锁定手柄连接固定，弹簧Ⅱ套装于滑杆，其一端与螺母Ⅱ相接触，其另一端与螺母Ⅰ相接触，所述滑块Ⅰ的外侧端设置有两个与锁定手柄厚度相匹配的卡槽，两个卡槽相互呈十字形设置，当锁定手柄旋转90度后，其插装于对应的卡槽中。
为了方便操作，活动杆的头端设置有外螺纹Ⅱ，所述外螺纹Ⅱ上旋合有六角螺母。
本发明的有益效果是：将内层玻璃通过橡胶吸盘吸附固定于一侧的主轴上，将外层 玻璃通过橡胶吸盘吸附固定于另一侧的主轴上，之后转动主轴使外侧玻璃和内层玻璃均转动至水平状态，转动到位后通过主轴锁止装置将主轴锁止固定，此时可以方便对内层玻璃和外层玻璃进行清洁，清洁完成后，解除主轴的锁止，将主轴转动90°，此时内层玻璃和外层玻璃均转动至竖直状态，再次通过主轴锁止装置将主轴锁止固定。之后向内侧移动主轴，使主轴通过滑块Ⅱ沿导轨Ⅰ滑动，通过滑块Ⅰ沿导轨Ⅱ滑动。由于橡胶皮翻边机构在中间框架中将橡胶密封套四个圆弧拐角处前后两侧的橡胶皮分别向外侧翻开，因此将内层玻璃和外层玻璃滑动装入橡胶密封套的开口中，之后接触橡胶皮翻边机构对橡胶皮的作用，橡胶皮恢复原始状态后将内层玻璃和外层玻璃包裹固定。之后解除固定装置后即可将安装好的玻璃组件从中间框架中拆下，提高了飞机客舱玻璃的清洁和安装的效率，有效避免了安装过程中对玻璃的污染。
附图说明
图1为本发明的立体结构示意图；
图2为本发明的主轴部位的立体结构示意图；
图3为本发明的橡胶密封套部位的立体结构示意图；
图4为本发明的活动杆部位的立体结构示意图；
图5为本发明的夹臂部位的立体结构示意图；
图中，1.左框架 2.右框架 3.中间框架 4.主轴 5.橡胶吸盘 6.导轨Ⅰ 7.导轨Ⅱ 8.内层玻璃 9.橡胶密封套 10.支架 11.夹臂 12.固定杆 13.六角螺母 14.弹簧Ⅰ 15.滑块Ⅰ 16.锁定手柄 17.滑块Ⅱ 18.滑孔Ⅱ 19.圆孔 20.滑孔Ⅰ 21.外螺纹Ⅰ 22.滑杆 23.弹簧Ⅱ 24.螺母Ⅰ 25.螺母Ⅱ 26.卡槽 27.卡槽 28.支撑圆环 29.活动杆 30.凸台 31.插头 32.外层玻璃 33.外螺纹Ⅱ 34.销轴 35.夹臂弹簧 36.圆弧夹杆 37.橡胶块 38.滑槽 39.插孔。
具体实施方式
下面结合附图1、附图2对本发明做进一步说明。
一种用于飞机客舱玻璃组件清洁与组装的辅助工装，包括：机架，其由竖直设置于左侧端的左框架1、竖直设置于右侧端的右框架2以及连接于左框架1与右框架2的中间支架3构成，左框架1、右框架2与中间框架3在俯视方向上形成H形结构；导轨Ⅰ 6，沿前后方向水平设置于左框架1中；导轨Ⅱ 7，沿前后方向水平设置于右框架2中；橡胶密封套9，通过固定装置固定于中间框架3中，中间框架3中且位于橡胶密封套9的四个圆弧拐角处的外侧端分别设置有橡胶皮翻边机构，橡胶皮翻边机构将对应的橡胶密封套9的圆弧拐角处前后两侧的橡胶皮分别向外侧翻开；两个滑块Ⅱ 17，其内部设置有与导轨Ⅰ 6相匹配的 滑孔Ⅱ 18，两个滑块Ⅱ 17分别位于中间框架3的前后两端；两个滑块Ⅰ 15，其内部设置有与导轨Ⅱ 7相匹配的滑孔Ⅰ 20，两个滑块Ⅰ 15分别位于中间框架3的前后两端；同侧的滑块Ⅰ 15与滑块Ⅱ 17之间沿左右方向设置有主轴4，主轴4上设置有若干橡胶吸盘5，滑块Ⅰ 15与滑块Ⅱ 17中分别设置有与主轴4外径相匹配的圆孔19，主轴4两端分别转动安装于同侧对应的圆孔19中，一端橡胶吸盘5吸附固定有内层玻璃8，另一端的橡胶吸盘5吸附固定有外层玻璃32；以及主轴锁止装置，设置于滑块Ⅰ 15上，当主轴4转动90°后主轴锁止装置将主轴4相对滑块Ⅰ 15锁止固定。使用时，将内层玻璃8通过橡胶吸盘5吸附固定于一侧的主轴4上，将外层玻璃32通过橡胶吸盘5吸附固定于另一侧的主轴4上，之后转动主轴4使外侧玻璃32和内层玻璃8均转动至水平状态，转动到位后通过主轴锁止装置将主轴4锁止固定，此时可以方便对内层玻璃8和外层玻璃32进行清洁，清洁完成后，解除主轴4的锁止，将主轴4转动90°，此时内层玻璃8和外层玻璃32均转动至竖直状态，再次通过主轴锁止装置将主轴4锁止固定。之后向内侧移动主轴4，使主轴4通过滑块Ⅱ 17沿导轨Ⅰ 6滑动，通过滑块Ⅰ 15沿导轨Ⅱ 7滑动。由于橡胶皮翻边机构在中间框架3中将橡胶密封套9四个圆弧拐角处前后两侧的橡胶皮分别向外侧翻开，因此将内层玻璃8和外层玻璃32滑动装入橡胶密封套9的开口中，之后接触橡胶皮翻边机构对橡胶皮的作用，橡胶皮恢复原始状态后将内层玻璃8和外层玻璃32包裹固定。之后解除固定装置后即可将安装好的玻璃组件从中间框架3中拆下，提高了飞机客舱玻璃的清洁和安装的效率，有效避免了安装过程中对玻璃的污染。
固定装置可以为如下结构，其包括水平设置于中间框架3右侧端的固定杆12、竖直设置于中间框架3下端的固定杆12、沿竖直方向滑动插装于中间框架3上端的活动杆29以及沿水平方向滑动插装于中间框架3左侧端的活动杆29，固定杆12的内侧端设置有插头31，插头31插入橡胶密封套9中间部位沿圆周方向设置的卡槽27中，活动杆29中部位设置有圆环形的凸台30，弹簧Ⅰ 14套装于活动杆29上，其上端与中间框架3相连接，其下端与凸台30相连，活动杆29的内侧端设置有插头31，在弹簧Ⅰ 14的弹力下，插头31插入橡胶密封套9中间部位沿圆周方向设置的卡槽27中，四个插头31的头端与卡置于卡槽27中的支撑圆环28的外侧端相接触。装夹时，将中间框架3上方和左侧的活动杆29向外拉动从而压缩弹簧Ⅰ 14，将橡胶密封头9至于中间框架3中后使其下侧端通过中间框架3下端的固定杆12上的插头31插入卡槽27中，中间框架3右端的固定杆12上的插头31插入卡槽27中，之后松开活动杆29，从而在弹簧Ⅰ 14的弹力下，活动杆29上的插头31插入橡胶密封套中的卡槽27的上端和左侧端，实现了上下左右四个方向的夹紧固定，当将内 层玻璃8和外层玻璃32装入橡胶密封套9中后，向外拉动活动杆29使插头31从卡槽27中脱离后即可将橡胶密封套9取出，使用简单便捷。
橡胶皮翻边机构可以为如下结构，其包括两个夹臂11，两个夹臂11通过销轴34铰接形成X形，夹臂11的尾端通过夹臂弹簧35相连，夹臂11的头端设置有与橡胶密封套9的圆弧拐角曲率相匹配的圆弧夹杆36，两个夹臂的两侧分别设置有固定于中间框架3上的支架10，支架10的内侧端设置有橡胶块37，橡胶块37中设置有与对应的圆弧拐角相垂直的滑槽38，滑槽38中延其长度方向间隔设置有若干与销轴34外径相匹配的插孔39，两个夹臂11两侧的销轴34分别插装于同侧对应的插孔39中，在夹臂弹簧35的弹力下两个圆弧夹杆36分别夹紧于橡胶密封套9圆弧拐角处前后两侧，且圆弧夹杆36将同侧的橡胶皮向外翻开后夹紧。当固定装置将橡胶密封套9固定后，向内按压两个夹臂11使夹臂弹簧35压缩，使两个圆弧夹杆36张开，之后通过在滑槽38中移动整个夹臂11，由于橡胶块37为橡胶材料制成，因此移动时销轴34挤压各个插孔39变形，可以使其移动到相对应的插孔39中，实现圆弧夹杆36将卡槽27的橡胶皮处夹住，通过移动各个夹臂11从而将橡胶皮翻开。当内层玻璃8和外层玻璃32插入橡胶密封条9的左右两端的开口中后，继续向外侧移动夹臂11使销轴34沿滑槽38中滑动，直至圆弧夹杆36脱离橡胶皮，从而橡胶皮恢复到原位后将内层玻璃8和外层玻璃32包裹固定。
主轴锁止装置可以为如下结构，其包括锁定手柄16以及滑杆22，主轴4内沿其轴向设置有通孔，导轨Ⅱ 7中延其长度方向设置有长孔，主轴4的头端设置有外螺纹Ⅰ 21，主轴4的头端穿过长孔，滑杆22沿主轴4的轴向插装于主轴4的通孔中，滑杆22上设置有螺纹段，螺母Ⅰ 24旋合于螺纹段上，螺母Ⅱ 25旋合于外螺纹Ⅰ 21上，螺母Ⅱ 25中设置有圆孔，滑杆22的头端穿过螺母Ⅱ 25的圆孔后与锁定手柄16连接固定，弹簧Ⅱ 23套装于滑杆22，其一端与螺母Ⅱ 25相接触，其另一端与螺母Ⅰ 24相接触，滑块Ⅰ 15的外侧端设置有两个与锁定手柄16厚度相匹配的卡槽26，两个卡槽26相互呈十字形设置，当锁定手柄16旋转90度后，其插装于对应的卡槽26中。初始状态下锁定手柄16插入水平状态的卡槽26中，此时主轴4转动至其通过橡胶吸盘5吸附固定的内层玻璃8和外层玻璃32处于水平状态，此时可以方便对玻璃进行清洁工作，清洁后，向外拉出锁定手柄16，驱动滑杆22沿主轴4中的通孔向外滑动，由于主轴4的头端固定有螺母Ⅱ 25，因此滑杆22向外滑动的时候移动的螺母Ⅰ 24挤压弹簧Ⅱ 23，实现锁定手柄16从水平状态的卡槽26中脱离，之后通过旋转锁定手柄16使主轴4旋转90°，从而实现驱动内层玻璃8和外层玻璃32由水平装置转动至竖直状态，当转动到位后松开锁定手柄16，在弹簧Ⅱ 23的弹力下，锁定 手柄16插入竖直状态的卡槽26中，实现主轴4旋转到位的锁定，确保处于竖直状态的内层玻璃8和外层玻璃32处于竖直状态。
优选的，活动杆29的头端设置有外螺纹Ⅱ 33，外螺纹Ⅱ 33上旋合有六角螺母13。通过六角螺母13可以方便拉动活动杆29，从而使插头31从卡槽27中脱离，提高了操作的便利性。

Claims (5)

  1. 一种用于飞机客舱玻璃组件清洁与组装的辅助工装，其特征在于，包括：
    机架，其由竖直设置于左侧端的左框架(1)、竖直设置于右侧端的右框架(2)以及连接于左框架(1)与右框架(2)的中间支架(3)构成，左框架(1)、右框架(2)与中间框架(3)在俯视方向上形成H形结构；
    导轨Ⅰ(6)，沿前后方向水平设置于左框架(1)中；
    导轨Ⅱ(7)，沿前后方向水平设置于右框架(2)中；
    橡胶密封套(9)，通过固定装置固定于中间框架(3)中，所述中间框架(3)中且位于橡胶密封套(9)的四个圆弧拐角处的外侧端分别设置有橡胶皮翻边机构，橡胶皮翻边机构将对应的橡胶密封套(9)的圆弧拐角处前后两侧的橡胶皮分别向外侧翻开；
    两个滑块Ⅱ(17)，其内部设置有与导轨Ⅰ(6)相匹配的滑孔Ⅱ(18)，两个滑块Ⅱ(17)分别位于中间框架(3)的前后两端；
    两个滑块Ⅰ(15)，其内部设置有与导轨Ⅱ(7)相匹配的滑孔Ⅰ(20)，两个滑块Ⅰ(15)分别位于中间框架(3)的前后两端；
    同侧的滑块Ⅰ(15)与滑块Ⅱ(17)之间沿左右方向设置有主轴(4)，所述主轴(4)上设置有若干橡胶吸盘(5)，所述滑块Ⅰ(15)与滑块Ⅱ(17)中分别设置有与主轴(4)外径相匹配的圆孔(19)，主轴(4)两端分别转动安装于同侧对应的圆孔(19)中，一端橡胶吸盘(5)吸附固定有内层玻璃(8)，另一端的橡胶吸盘(5)吸附固定有外层玻璃(32)；以及
    主轴锁止装置，设置于滑块Ⅰ(15)上，当主轴(4)转动90°后主轴锁止装置将主轴(4)相对滑块Ⅰ(15)锁止固定。
  2. 根据权利要求1所述的用于飞机客舱玻璃组件清洁与组装的辅助工装，其特征在于：所述固定装置包括水平设置于中间框架(3)右侧端的固定杆(12)、竖直设置于中间框架(3)下端的固定杆(12)、沿竖直方向滑动插装于中间框架(3)上端的活动杆(29)以及沿水平方向滑动插装于中间框架(3)左侧端的活动杆(29)，所述固定杆(12)的内侧端设置有插头(31)，所述插头(31)插入橡胶密封套(9)中间部位沿圆周方向设置的卡槽(27)中，所述活动杆(29)中部位设置有圆环形的凸台(30)，弹簧Ⅰ(14)套装于活动杆(29)上，其上端与中间框架(3)相连接，其下端与凸台(30)相连，所述活动杆(29)的内侧端设置有插头(31)，在弹簧Ⅰ(14)的弹力下，插头(31)插入橡胶密封套(9)中间部位沿圆周方向设置的卡槽(27)中，四个插头(31)的头端与卡置于卡槽(27)中的支撑圆环(28)的外侧端相接触。
  3. 根据权利要求1所述的用于飞机客舱玻璃组件清洁与组装的辅助工装，其特征在于：所述橡胶皮翻边机构两个夹臂(11)，两个夹臂(11)通过销轴(34)铰接形成X形，夹臂(11)的尾端通过夹臂弹簧(35)相连，所述夹臂(11)的头端设置有与橡胶密封套(9)的圆弧拐角曲率相匹配的圆弧夹杆(36)，两个夹臂的两侧分别设置有固定于中间框架(3)上的支架(10)，所述支架(10)的内侧端设置有橡胶块(37)，所述橡胶块(37)中设置有与对应的圆弧拐角相垂直的滑槽(38)，所述滑槽(38)中延其长度方向间隔设置有若干与销轴(34)外径相匹配的插孔(39)，两个夹臂(11)两侧的销轴(34)分别插装于同侧对应的插孔(39)中，在夹臂弹簧(35)的弹力下两个圆弧夹杆(36)分别夹紧于橡胶密封套(9)圆弧拐角处前后两侧，且圆弧夹杆(36)将同侧的橡胶皮向外翻开后夹紧。
  4. 根据权利要求1所述的用于飞机客舱玻璃组件清洁与组装的辅助工装，其特征在于：所述主轴锁止装置包括锁定手柄(16)以及滑杆(22)，所述主轴(4)内沿其轴向设置有通孔，所述导轨Ⅱ(7)中延其长度方向设置有长孔，主轴(4)的头端设置有外螺纹Ⅰ(21)，主轴(4)的头端穿过长孔，滑杆(22)沿主轴(4)的轴向插装于主轴(4)的通孔中，滑杆(22)上设置有螺纹段，螺母Ⅰ(24)旋合于螺纹段上，螺母Ⅱ(25)旋合于外螺纹Ⅰ(21)上，螺母Ⅱ(25)中设置有圆孔，滑杆(22)的头端穿过螺母Ⅱ(25)的圆孔后与锁定手柄(16)连接固定，弹簧Ⅱ(23)套装于滑杆(22)，其一端与螺母Ⅱ(25)相接触，其另一端与螺母Ⅰ(24)相接触，所述滑块Ⅰ(15)的外侧端设置有两个与锁定手柄(16)厚度相匹配的卡槽(26)，两个卡槽(26)相互呈十字形设置，当锁定手柄(16)旋转90度后，其插装于对应的卡槽(26)中。
  5. 根据权利要求2所述的用于飞机客舱玻璃组件清洁与组装的辅助工装，其特征在于：活动杆(29)的头端设置有外螺纹Ⅱ(33)，所述外螺纹Ⅱ(33)上旋合有六角螺母(13)。
PCT/CN2020/101750 2020-07-13 2020-07-14 一种用于飞机客舱玻璃组件清洁与组装的辅助工装 WO2022011522A1 (zh)

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