Auxiliary tool for cleaning and assembling glass component of airplane passenger cabin
阅读说明:本技术 一种用于飞机客舱玻璃组件清洁与组装的辅助工装 (Auxiliary tool for cleaning and assembling glass component of airplane passenger cabin ) 是由 顾辉 张伟光 王德超 于 2020-07-13 设计创作,主要内容包括: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。(The utility model provides an auxiliary fixtures for aircraft cabin glass subassembly is clean and equipment, inlayer glass and outer glass clean the completion back, remove the locking of main shaft, rotate the main shaft 90, inlayer glass and outer glass all rotate to vertical state this moment, and it is fixed with the main shaft locking through main shaft locking means once more. Because the rubber skin flanging mechanism respectively outwards turns over the rubber skin of both sides around four circular arc corners of rubber seal cover in middle frame, consequently pack inlayer glass and outer glass slip into the opening of rubber seal cover, later contact rubber skin flanging mechanism is fixed with inlayer glass and outer glass parcel after the rubber skin resumes original state to the effect of rubber skin. After the fixing device is released, the installed glass assembly can be detached from the middle frame, the cleaning and installing efficiency of the aircraft cabin glass is improved, and the pollution to the glass in the installing process is effectively avoided.)
1. The utility model provides an auxiliary fixtures that is used for aircraft cabin glass subassembly to clean and assemble which characterized in that includes:
the frame comprises a left frame (1) vertically arranged at the left side end, a right frame (2) vertically arranged at the right side end and a middle support (3) connected to the left frame (1) and the right frame (2), wherein the left frame (1), the right frame (2) and the middle frame (3) form an H-shaped structure in the overlooking direction;
the guide rail I (6) is horizontally arranged in the left frame (1) along the front-back direction;
the guide rail II (7) is horizontally arranged in the right frame (2) along the front-back direction;
the rubber sealing sleeves (9) are fixed in the middle frame (3) through fixing devices, rubber skin flanging mechanisms are respectively arranged in the middle frame (3) and at the outer side ends of the four arc corners of the rubber sealing sleeves (9), and the rubber skins at the front side and the rear side of the corresponding arc corners of the rubber sealing sleeves (9) are respectively turned outwards by the rubber skin flanging mechanisms;
the two sliding blocks II (17) are internally provided with sliding holes II (18) matched with the guide rails I (6), and the two sliding blocks II (17) are respectively positioned at the front end and the rear end of the middle frame (3);
the two sliding blocks I (15) are internally provided with sliding holes I (20) matched with the guide rails II (7), and the two sliding blocks I (15) are respectively positioned at the front end and the rear end of the middle frame (3);
a main shaft (4) is arranged between the sliding block I (15) and the sliding block II (17) on the same side along the left-right direction, a plurality of rubber suckers (5) are arranged on the main shaft (4), round holes (19) matched with the outer diameter of the main shaft (4) are respectively arranged in the sliding block I (15) and the sliding block II (17), two ends of the main shaft (4) are respectively rotatably installed in the corresponding round holes (19) on the same side, the rubber sucker (5) at one end is fixedly adsorbed with inner-layer glass (8), and the rubber sucker (5) at the other end is fixedly adsorbed with outer-layer glass (32); and
and the main shaft locking device is arranged on the sliding block I (15), and locks and fixes the main shaft (4) relative to the sliding block I (15) after the main shaft (4) rotates by 90 degrees.
2. The auxiliary tool for cleaning and assembling an aircraft cabin glass assembly according to claim 1, characterized in that: the fixing device comprises a fixing rod (12) horizontally arranged at the right side end of the middle frame (3), a fixing rod (12) vertically arranged at the lower end of the middle frame (3), a movable rod (29) inserted at the upper end of the middle frame (3) in a sliding manner along the vertical direction, and a movable rod (29) inserted at the left side end of the middle frame (3) in a sliding manner along the horizontal direction, wherein a plug (31) is arranged at the inner side end of the fixing rod (12), the plug (31) is inserted into a clamping groove (27) formed in the middle part of the rubber sealing sleeve (9) along the circumferential direction, a circular boss (30) is arranged at the middle part of the movable rod (29), a spring I (14) is sleeved on the movable rod (29), the upper end of the spring I is connected with the middle frame (3), the lower end of the spring I is connected with the boss (30), the inner side end of the movable rod (29, the plugs (31) are inserted into the clamping grooves (27) arranged in the middle of the rubber sealing sleeve (9) along the circumferential direction, and the head ends of the four plugs (31) are contacted with the outer side ends of the supporting circular rings (28) clamped in the clamping grooves (27).
3. The auxiliary tool for cleaning and assembling an aircraft cabin glass assembly according to claim 1, characterized in that: the rubber flanging mechanism is characterized by comprising two clamping arms (11) of the rubber flanging mechanism, wherein the two clamping arms (11) are hinged through pin shafts (34) to form an X shape, the tail ends of the clamping arms (11) are connected through clamping arm springs (35), arc clamping rods (36) matched with the arc corner curvature of the rubber sealing sleeve (9) are arranged at the head ends of the clamping arms (11), supports (10) fixed on the middle frame (3) are arranged on two sides of the two clamping arms respectively, rubber blocks (37) are arranged at the inner side ends of the supports (10), sliding grooves (38) perpendicular to the corresponding arc corners are arranged in the rubber blocks (37), a plurality of insertion holes (39) matched with the outer diameters of the pin shafts (34) are formed in the sliding grooves (38) at intervals along the length direction of the sliding grooves, the pin shafts (34) on two sides of the two clamping arms (11) are inserted into the insertion holes (39) corresponding to the same side respectively, and the two arc clamping rods (36) are clamped on the The front side and the rear side are arranged, and the arc clamping rods (36) clamp the rubber sheets on the same side after the rubber sheets are outwards turned.
4. The auxiliary tool for cleaning and assembling an aircraft cabin glass assembly according to claim 1, characterized in that: the main shaft locking device comprises a locking handle (16) and a sliding rod (22), a through hole is formed in the main shaft (4) along the axial direction of the main shaft, a long hole is formed in the guide rail II (7) along the length direction of the guide rail II, an external thread I (21) is arranged at the head end of the main shaft (4), the head end of the main shaft (4) penetrates 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), a threaded section is formed in the sliding rod (22), a nut I (24) is screwed on the threaded section, a nut II (25) is screwed on the external thread I (21), a round hole is formed in the nut II (25), the head end of the sliding rod (22) penetrates through the round hole of the nut II (25) and then is connected and fixed with the locking handle (16), a spring II (23) is sleeved on the sliding rod (, the outer side end of the sliding block I (15) is provided with two clamping grooves (26) matched with the thickness of the locking handle (16), the two clamping grooves (26) are arranged in a cross shape, and after the locking handle (16) rotates by 90 degrees, the locking handle is inserted into the corresponding clamping grooves (26).
5. The auxiliary tool for cleaning and assembling an aircraft cabin glass assembly according to claim 2, characterized in that: 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).
Technical Field
The invention relates to the technical field of aircraft cabin glass maintenance, in particular to an auxiliary tool for cleaning and assembling aircraft cabin glass components.
Background
The maintenance of the glass of the airplane passenger cabin belongs to routine work of airplane regular inspection, and the work aims to inspect the damage conditions of the inner layer and the outer layer of the glass caused in the airplane operation period, avoid the damage of the glass from exceeding the limit and increase the operation risk of the airplane. When the glass is found to have too many scratches and the depth is over-limit, the glass is manually repaired or directly replaced by new glass. The components of the glass are required to be cleaned before the glass is reinstalled, firstly, the transparency of the glass is ensured, and secondly, secondary inspection is carried out in the cleaning process, so that omission is avoided. Glass unit is by inlayer glass, outer glass, the intermediate strut ring, rubber seal cover constitutes, with four parts glass water and air gun clean weather the back, assemble, need turn up the fixed rubber of the fixed cover of rubber during the installation just can make in, outer glass inserts, but this process staff needs extremely careful operation, avoid impurity in the installation, pollutant such as handprint stays including, outer glass's inboard, and then cause the secondary to do over again, this work removes to lack specialized tool again, very big extravagant staff time, work efficiency is low.
Disclosure of Invention
In order to overcome the defects of the technology, the invention provides the tool which effectively avoids secondary pollution to the inner layer glass and the outer layer glass during assembly and improves the tool efficiency.
The technical scheme adopted by the invention for overcoming the technical problems is as follows:
an auxiliary tool for cleaning and assembling a glass component of an airplane passenger cabin comprises:
the frame comprises a left frame vertically arranged at the left side end, a right frame vertically arranged at the right side end and a middle bracket connected with the left frame and the right frame, wherein the left frame, the right frame and the middle frame form an H-shaped structure in the overlooking direction;
the guide rail I is horizontally arranged in the left frame along the front-back direction;
the guide rail II is horizontally arranged in the right frame along the front-back direction;
the rubber sealing sleeves are fixed in the middle frame through fixing devices, rubber skin flanging mechanisms are respectively arranged at the outer side ends of the four arc corners of the rubber sealing sleeves in the middle frame, and the rubber skins at the front side and the rear side of the corresponding arc corners of the rubber sealing sleeves are respectively turned over outwards by the rubber skin flanging mechanisms;
the two sliding blocks II are internally provided with sliding holes II matched with the guide rails I and are respectively positioned at the front end and the rear end of the middle frame;
the two sliding blocks I are internally provided with sliding holes I matched with the guide rails II, and are respectively positioned at the front end and the rear end of the middle frame;
a main shaft is arranged between the sliding block I and the sliding block II at the same side along the left-right direction, a plurality of rubber suckers are arranged on the main shaft, round holes matched with the outer diameter of the main shaft are respectively arranged in the sliding block I and the sliding block II, two ends of the main shaft are respectively rotatably arranged in the corresponding round holes at the same side, the rubber sucker at one end adsorbs and fixes inner-layer glass, and the rubber sucker at the other end adsorbs and fixes outer-layer glass; and
and the main shaft locking device is arranged on the sliding block I, and the main shaft is locked and fixed relative to the sliding block I after the main shaft rotates for 90 degrees.
Furthermore, the fixing device comprises a fixed rod horizontally arranged at the right side end of the middle frame, a fixed rod vertically arranged at the lower end of the middle frame, a movable rod inserted at the upper end of the middle frame in a sliding way along the vertical direction, and a movable rod inserted at the left side end of the middle frame in a sliding way along the horizontal direction, the inner side end of the fixed rod is provided with a plug which is inserted into a clamping groove arranged in the middle of the rubber sealing sleeve along the circumferential direction, the middle part of the movable rod is provided with a circular boss, the spring I is sleeved on the movable rod, the upper end of the movable rod is connected with the middle frame, the lower end of the movable rod is connected with the lug boss, the inner side end of the movable rod is provided with a plug, under the elasticity of the spring I, the plugs are inserted into clamping grooves formed in the middle of the rubber sealing sleeve along the circumferential direction, and the head ends of the four plugs are in contact with the outer side ends of supporting rings clamped in the clamping grooves.
Furthermore, the two clamping arms of the rubber sheet flanging mechanism are hinged through a pin shaft to form an X shape, the tail ends of the clamping arms are connected through a clamping arm spring, arc clamping rods matched with the arc corner curvature of the rubber sealing sleeve are arranged at the head ends of the clamping arms, supports fixed on the middle frame are arranged on two sides of the two clamping arms respectively, a rubber block is arranged at the inner side end of each support, a sliding groove perpendicular to the corresponding arc corner is formed in each rubber block, a plurality of inserting holes matched with the outer diameter of the pin shaft are formed in each sliding groove at intervals along the length direction of each sliding groove, the pin shafts on two sides of the two clamping arms are inserted into the inserting holes corresponding to the same side respectively, the two arc clamping rods are clamped on the front side and the rear side of the arc corner of the rubber sealing sleeve respectively under the elasticity of the clamping arm spring.
Furthermore, the main shaft locking device comprises a locking handle and a sliding rod, a through hole is arranged in the main shaft along the axial direction of the main shaft, a long hole is arranged in the guide rail II along the length direction of the guide rail II, an external thread I is arranged at the head end of the main shaft, the head end of the main shaft penetrates through the long hole, a slide rod is inserted into the through hole of the main shaft along the axial direction of the main shaft, a threaded section is arranged on the slide bar, a nut I is screwed on the threaded section, a nut II is screwed on the external thread I, a round hole is arranged in the nut II, the head end of the slide bar passes through the round hole of the nut II and then is connected and fixed with the locking handle, a spring II is sleeved on the slide bar, its one end contacts with nut II, and its other end contacts with nut I, the outside end of slider I is provided with two and locking handle thickness assorted draw-in grooves, and two draw-in grooves are the cross setting each other, and after locking handle rotation 90 degrees, its cartridge is in the draw-in groove that corresponds.
In order to operate conveniently, 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 invention has the beneficial effects that: on being fixed in the main shaft of one side with inlayer glass through the rubber suction cup absorption, on being fixed in the main shaft of opposite side with outer glass through the rubber suction cup absorption, later rotate the main shaft and make outside glass and inlayer glass all rotate to the horizontality, it is fixed with the main shaft locking through main shaft locking means to rotate after targetting in place, can conveniently clean inlayer glass and outer glass this moment, after the cleanness is accomplished, remove the locking of main shaft, rotate the main shaft 90, inlayer glass and outer glass all rotate to vertical state this moment, it is fixed with the main shaft locking through main shaft locking means once more. And then the main shaft is moved inwards, so that the main shaft slides along the guide rail I through the sliding block II and slides along the guide rail II through the sliding block I. Because the rubber skin flanging mechanism respectively outwards turns over the rubber skin of both sides around four circular arc corners of rubber seal cover in middle frame, consequently pack inlayer glass and outer glass slip into the opening of rubber seal cover, later contact rubber skin flanging mechanism is fixed with inlayer glass and outer glass parcel after the rubber skin resumes original state to the effect of rubber skin. After the fixing device is released, the installed glass assembly can be detached from the middle frame, the cleaning and installing efficiency of the aircraft cabin glass is improved, and the pollution to the glass in the installing process is effectively avoided.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic perspective view of a spindle portion according to the present invention;
FIG. 3 is a schematic perspective view of the rubber boot seal portion of the present invention;
FIG. 4 is a schematic perspective view of the active lever portion of the present invention;
FIG. 5 is a schematic perspective view of a clamping arm portion of the present invention;
in the drawing, 1, a left frame 2, a
Detailed Description
The invention will be further explained with reference to fig. 1 and 2.
An auxiliary tool for cleaning and assembling a glass component of an airplane passenger cabin comprises: the frame comprises a
The fixing device may be a structure including a
The rubber sheet flanging mechanism can be of a structure comprising two clamping
The main shaft locking device can be of a structure comprising a locking handle 16 and a sliding rod 22, a through hole is formed in the
Preferably, the head end of the
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