CN220979251U - Mounting structure for sliding door of aircraft hangar - Google Patents
Mounting structure for sliding door of aircraft hangar Download PDFInfo
- Publication number
- CN220979251U CN220979251U CN202323017387.5U CN202323017387U CN220979251U CN 220979251 U CN220979251 U CN 220979251U CN 202323017387 U CN202323017387 U CN 202323017387U CN 220979251 U CN220979251 U CN 220979251U
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- Prior art keywords
- pulley
- hangar
- door body
- sliding
- transparent plate
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- 238000009434 installation Methods 0.000 claims description 14
- 230000007246 mechanism Effects 0.000 claims description 8
- 230000000149 penetrating effect Effects 0.000 claims description 5
- 238000012423 maintenance Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 2
- 238000004880 explosion Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
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Abstract
The utility model belongs to the technical field of hangar sliding doors, and particularly relates to an airplane hangar sliding door mounting structure which comprises a hangar wall body, wherein a lower sliding rail is arranged on one end surface of the bottom end of the hangar wall body, a pulley is connected to the inner side surface of the lower sliding rail, a connecting block is rotatably connected to the top end of the pulley, a lug is connected to the top surface of the connecting block, and one end of the lug extends into a notch. According to the utility model, the pulley and the door body are assembled, when one pulley is damaged, only the bolt is needed to be screwed out, the pulley assembly is lifted upwards in the notch to separate the pulley from the lower slide rail, so that an operator can conveniently maintain the pulley, the operator is prevented from lifting the door body to maintain the pulley, and the operator can conveniently and independently replace and maintain the transparent plate, and the operator is prevented from replacing the integral lighting window, so that the maintenance cost is saved.
Description
Technical Field
The utility model belongs to the technical field of hangar sliding doors, and particularly relates to an installation structure of an airplane hangar sliding door.
Background
The aircraft hangar is generally provided with a hangar door, and an operator generally adopts the sliding door as a gate of the aircraft hangar, so that the hangar door can be conveniently opened and closed.
When the sliding door of the aircraft hangar is used, the sliding door bottom end is provided with the pulley, the pulley is placed inside through the fixed notch, the pulley can rotate at the bottom of the sliding door through the cooperation of the bearing, the screw and the rotating shaft, when the pulley at the bottom end is damaged and needs to be replaced, an operator is required to hoist the sliding door, the pulley can be separated from the sliding rail, and then the sliding door is detached, so that the operation is complicated, inconvenience is brought to the maintenance of the pulley, the transparent plate in the lighting window on the sliding door is generally integral, and when the transparent plate of one lighting window is damaged, the whole lighting window needs to be replaced, so that the operation cost is high, and the maintenance is inconvenient.
Accordingly, the present utility model provides an aircraft hangar sliding door mounting structure to solve the above-mentioned problems.
Disclosure of utility model
The utility model aims to provide an installation structure of an aircraft hangar sliding door, which aims to solve the problems that in the prior art, a pulley arranged at the bottom of the aircraft hangar sliding door is inconvenient to maintain and a transparent plate in a lighting window on the sliding door is damaged, and the integral lighting window needs to be replaced.
In order to achieve the above purpose, the present utility model provides the following technical solutions: the utility model provides an aircraft hangar sliding door mounting structure, includes the hangar wall body, hangar wall body bottom department one end surface is provided with down the slide rail, the inboard surface connection of slide rail has the pulley down, pulley top department rotates and is connected with the connecting block, connecting block top surface connection has the lug, lug one end extends into inside the notch, the notch is seted up in the bottom department front end surface of the door body, threaded hole has been seted up to lug front end surface, threaded hole inside through connection has the bolt, the one end of bolt extends into and sets up in the fixed orifices of seting up in the door body inside, door body top department is connected with electronic slide rail, and door body top department front end surface has seted up the daylighting mouth that runs through, door body front end surface still is provided with installation mechanism.
In order to achieve convenient installation of the transparent plate, as an aircraft hangar sliding door installation structure of the present utility model, it is preferable that the installation mechanism includes: the door comprises a mounting frame, a slideway, a transparent plate, a limiting hole and a butterfly bolt, wherein the front end surface of a door body at the outer side of a lighting opening is connected with the mounting frame, the slideway is arranged on the inner side surface of the mounting frame, the transparent plate is connected with the inner side surface of the slideway, the limiting hole is arranged on the front end surface of the mounting frame, and the butterfly bolt is connected inside the limiting hole in a penetrating manner.
In order to change the position of the pulley, as a preferred installation structure of the sliding door of the aircraft hangar, the lug forms a sliding connection with the door body through a notch.
In order to fix the position of the protruding block, as an installation structure of the sliding door of the aircraft hangar, the size and the position of the threaded hole are matched with those of the fixed hole, and the bolt is in threaded connection with the fixed hole through the penetrating threaded hole.
In order to realize the placement of the transparent plate, the installation frame structure is preferably of a C-shaped structure, and the transparent plate is in sliding connection with the installation frame through a slide way.
In order to fix the position of the transparent plate, as a preferred installation structure of the sliding door of the aircraft hangar, the position of the butterfly bolt is matched with the position of the transparent plate.
Compared with the prior art, the utility model has the beneficial effects that:
1. According to the utility model, the pulley and the door body are assembled, when one pulley is damaged, only the bolt is needed to be screwed out, the pulley assembly is lifted upwards in the notch to separate the pulley from the lower slide rail, so that an operator can conveniently maintain the pulley, and the situation that the operator needs to lift the door body to maintain the pulley is avoided.
2. According to the utility model, through the installation mechanism, an operator can conveniently and independently replace and maintain the transparent plate, and the operator is prevented from replacing the integral lighting window, so that the maintenance cost is saved.
Drawings
The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:
FIG. 1 is a schematic diagram of a front view structure of the present utility model;
FIG. 2 is a schematic view of a partial explosion structure at a pulley of the present utility model;
FIG. 3 is a schematic rear view of the present utility model;
FIG. 4 is a schematic view of a partial explosion at the mounting mechanism of the present utility model;
fig. 5 is a schematic diagram of a conventional pulley installation structure.
In the figure: 1. a wall body of the hangar; 2. a lower slide rail; 3. a pulley; 4. a connecting block; 5. a bump; 6. a notch; 7. a door body; 8. a threaded hole; 9. a bolt; 10. a fixing hole; 11. an electric slide rail; 12. a lighting opening; 13. a mounting frame; 14. a slideway; 15. a transparent plate; 16. a limiting hole; 17. butterfly bolt.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-5, the present utility model provides the following technical solutions: the utility model provides an aircraft hangar sliding door mounting structure, including hangar wall 1, hangar wall 1 bottom department one end surface is provided with down slide rail 2, down slide rail 2 inboard surface connection has pulley 3, pulley 3 top department rotates and is connected with connecting block 4, connecting block 4 top surface is connected with lug 5, lug 5 one end extends into notch 6 inside, notch 6 is seted up in the bottom department front end surface of door 7, threaded hole 8 has been seted up to lug 5 front end surface, threaded hole 8 inside through connection has bolt 9, the one end of bolt 9 extends into and sets up in the fixed orifices 10 that the inside of door 7 was seted up, door 7 top department is connected with electronic slide rail 11, and door 7 top department front end surface has seted up the daylighting mouth 12 that runs through, door 7 front end surface still is provided with mounting mechanism.
Preferably: the mounting mechanism includes: the door body 7 comprises a mounting frame 13, a slideway 14, a transparent plate 15, a limiting hole 16 and butterfly bolts 17, wherein the front end surface of the door body 7 at the outer side of a lighting opening 12 is connected with the mounting frame 13, the slideway 14 is arranged on the inner side surface of the mounting frame 13, the transparent plate 15 is connected on the inner side surface of the slideway 14, the limiting hole 16 is arranged on the front end surface of the mounting frame 13, and the butterfly bolts 17 are connected inside the limiting hole 16 in a penetrating manner.
In specific use, the transparent plate 15 is slidably placed in the mounting frame 13, and the butterfly bolt 17 is screwed into the limiting hole 16, so that one end of the butterfly bolt 17 is positioned in the slide way 14, and the butterfly bolt 17 limits the position of the transparent plate 15 to the slide way 14.
Preferably: the protruding block 5 is connected with the door body 7 in a sliding way through the notch 6.
When the pulley is particularly used, the lug 5 can slide up and down in the notch 6, so that the pulley 3 can be driven to move up and down in the sliding process of the lug 5, and the pulley 3 can be separated from the lower slide rail 2.
Preferably: the size and position of the threaded hole 8 are matched with those of the fixing hole 10, and the bolt 9 is in threaded connection with the fixing hole 10 by penetrating through the threaded hole 8.
In particular use, when the positions of the threaded hole 8 and the fixing hole 10 coincide, the door body 7 and the projection 5 can be fixed together by screwing the bolt 9 into the fixing hole 10 through the threaded hole 8.
Preferably: the mounting frame 13 is in a C-shaped structure, and the transparent plate 15 is in sliding connection with the mounting frame 13 through the slide ways 14.
In particular use, the transparent plate 15 can slide in the slide way 14, so that the transparent plate 15 can slide and pull on the mounting frame 13.
Preferably: the butterfly bolt 17 is positioned to match the position of the transparent plate 15.
In particular use, when the butterfly bolt 17 is screwed into the butterfly bolt 17, one end of the butterfly bolt 17 just constrains the position of the transparent plate 15 in the slideway 14.
Working implementation principle: when the aircraft hangar sliding door mounting structure is used, an operator is connected with the electric sliding rail 11 at the top end of the door body 7 by hoisting the door body 7, at the moment, the lug 5 is placed in the notch 6, the lug 5 is positioned at the upper end of the notch 6, when the lug 5 moves downwards in the notch 6, the pulley 3 can be driven to move into the lower sliding rail 2, at the moment, the position of the threaded hole 8 and the position of the fixing hole 10 are overlapped, the door body 7 and the lug 5 can be connected together by screwing the bolt 9 into the fixing hole 10 through the threaded hole 8, so that the integral sliding door can be mounted between the lower sliding rail 2 and the electric sliding rail 11, when one pulley 3 is damaged, the bolt 9 is screwed, one end of the bolt 9 is separated from the fixing hole 10, at the moment, the lug 5 can move upwards and downwards in the notch 6, the pulley 3 can be driven to be separated from the lower slide rail 2, the damaged pulley 3 can be separated, an operator can maintain and replace the pulley 3, the door body 7 and other pulleys 3 are supported because only the damaged pulley 3 is replaced, the door body 7 cannot topple over, when the pulleys 3 on two sides are damaged, the operator can assist to support the door body 7 through a hydraulic tool, the operation is not required to lift the door body 7 to replace the pulley 3, the maintenance of the pulley 3 is more convenient, secondly, the butterfly 15 is slidingly placed in the mounting frame 13, at the moment, the butterfly 17 is screwed into the limiting hole 16, one end of the butterfly 17 is positioned in the slide way 14, the butterfly 17 can limit the position of the transparent plate 15 in the slide way 14, when the transparent plate 15 is damaged and needs to be replaced, the butterfly 17 is screwed out, the damaged transparent plate 15 can be separated, the operator can replace the new transparent plate 15 for use, so that the operator is prevented from replacing the integral lighting window, and the maintenance cost is saved.
Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and the present utility model is not limited thereto, but it is to be understood that modifications and equivalents of some of the technical features described in the foregoing embodiments may be made by those skilled in the art, although the present utility model has been described in detail with reference to the foregoing embodiments. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.
Claims (6)
1. The utility model provides an aircraft hangar sliding door mounting structure, includes hangar wall body (1), its characterized in that: the surface of one end at the bottom end of the machine library wall body (1) is provided with a lower sliding rail (2), the inner side surface of the lower sliding rail (2) is connected with a pulley (3), the top end of the pulley (3) is rotationally connected with a connecting block (4), the top surface of the connecting block (4) is connected with a bump (5), one end of the bump (5) extends into a notch (6), the notch (6) is arranged on the front end surface at the bottom end of a door body (7), threaded hole (8) have been seted up on lug (5) front end surface, threaded hole (8) inside through connection has bolt (9), in fixed orifices (10) of seting up in the inside of the door body (7) are seted up in the one end extension of bolt (9), door body (7) top department is connected with electronic slide rail (11), and door body (7) top department front end surface has seted up daylighting mouth (12) of running through, door body (7) front end surface still is provided with installation mechanism.
2. An aircraft hangar sliding door mounting structure according to claim 1, wherein: the mounting mechanism includes: mounting frame (13), slide (14), transparent plate (15), spacing hole (16) and butterfly bolt (17), door body (7) front end surface in daylighting mouth (12) outside is connected with mounting frame (13), slide (14) have been seted up to mounting frame (13) inboard surface, slide (14) inboard surface is connected with transparent plate (15), spacing hole (16) have been seted up to mounting frame (13) front end surface, spacing hole (16) inside through connection has butterfly bolt (17).
3. An aircraft hangar sliding door mounting structure according to claim 1, wherein: the protruding blocks (5) are connected with the door body (7) in a sliding way through the notch (6).
4. An aircraft hangar sliding door mounting structure according to claim 1, wherein: the size and the position of the threaded hole (8) are matched with those of the fixing hole (10), and the bolt (9) is in threaded connection with the fixing hole (10) by penetrating through the threaded hole (8).
5. An aircraft hangar sliding door mounting structure according to claim 2, wherein: the mounting frame (13) is of a C-shaped structure, and the transparent plate (15) is in sliding connection with the mounting frame (13) through a slide way (14).
6. An aircraft hangar sliding door mounting structure according to claim 2, wherein: the butterfly bolt (17) is matched with the transparent plate (15) in position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323017387.5U CN220979251U (en) | 2023-11-09 | 2023-11-09 | Mounting structure for sliding door of aircraft hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323017387.5U CN220979251U (en) | 2023-11-09 | 2023-11-09 | Mounting structure for sliding door of aircraft hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220979251U true CN220979251U (en) | 2024-05-17 |
Family
ID=91065911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323017387.5U Active CN220979251U (en) | 2023-11-09 | 2023-11-09 | Mounting structure for sliding door of aircraft hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220979251U (en) |
-
2023
- 2023-11-09 CN CN202323017387.5U patent/CN220979251U/en active Active
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