Aerofabric processing and drying device

Abstract

The utility model provides an aviation fabric processing drying device relates to drying equipment technical field, including equipment main part, the inside of equipment main part is provided with heating case, the inner wall of heating case is provided with support structure, support structure includes support rod, the side of support rod is provided with sliding slot, the inside of sliding slot is provided with limit slot, the inner wall sliding connection of sliding slot has mobile assembly, mobile assembly includes moving rod, the bottom fixed connection of moving rod has first limit block, the top fixed connection of moving rod has first clamping plate. The utility model discloses, through setting up support rod, as the main support body, and with the inner wall fixed connection of heating case can support, through setting up moving rod and first limit block, for pulling the infrared heating tube in its inside, through setting up first clamping plate and second clamping plate, for clamping the both ends of infrared heating tube, through above -mentioned setting makes the installation and replacement infrared heating tube more convenient, need not to consume the manpower of being big.

Description

Technical Field

[0001] This utility model relates to the field of drying equipment technology, and in particular to a drying device for processing aerospace fabrics. Background Technology

[0002] In the field of aerospace fabric processing, the drying process is crucial for ensuring fabric performance and quality. Infrared heating equipment, with its high-efficiency heating performance, is widely used in aerospace fabric drying. This equipment emits infrared rays through infrared heating tubes, achieving rapid drying of the fabric through radiative heat transfer. Compared to traditional heating methods, it has advantages such as faster heating speed, higher thermal efficiency, and more precise temperature control, effectively improving the drying quality and efficiency of aerospace fabrics and meeting the stringent requirements of the aerospace industry for fabric processing.

[0003] However, due to the complex structural design of the infrared heating chamber, multiple components need to be disassembled when replacing the infrared heating tube, which is cumbersome and time-consuming. The structure inside the heating chamber where the heating tube is installed is made of metal, which may damage the heating tube during replacement. This not only increases the downtime maintenance cost of the equipment, but also easily causes wear and tear on other components due to frequent disassembly and assembly, reducing the overall operating efficiency and stability of the drying device. Utility Model Content

[0004] The purpose of this invention is to overcome the shortcomings of existing technologies and provide a drying device for processing aerospace fabrics.

[0005] To achieve the above objectives, the present invention adopts the following technical solution: an aviation fabric processing and drying device, comprising a main body of equipment, a heating box disposed inside the main body of equipment, a support structure disposed on the inner wall of the heating box, the support structure comprising a support rod, a sliding groove being provided on one side of the support rod, a limiting groove being provided inside the sliding groove, a moving component being slidably connected to the inner wall of the sliding groove, the moving component comprising a moving rod, a first limiting block being fixedly connected to the bottom of the moving rod, a first clamping plate being fixedly connected to the top of the moving rod, a second clamping plate being disposed on one side of the first clamping plate, a slider being disposed on one side of the second clamping plate, a connecting plate being fixedly connected to the outer surface of the slider, a second limiting block being fixedly connected to the outer surface of the connecting plate, and a spring being fixedly connected to the outer surface of the second limiting block.

[0006] In a preferred embodiment, the top of the support rod has a rectangular through hole, the inner wall of the rectangular through hole is fitted with a fixing plate, the top of the fixing plate is provided with a stop block, and the top of the movable rod has a fixing angle.

[0007] In a preferred embodiment, the fixing plate is movable within the inner wall of the fixing angle.

[0008] In a preferred embodiment, the top of the movable rod is provided with a connecting slot, and the interior of the connecting slot is provided with a movable groove.

[0009] In a preferred embodiment, the inner wall of the connecting slot is fitted onto the outer surface of the connecting plate, and one end of the second clamping plate is fitted into the interior of the moving slot.

[0010] In a preferred embodiment, the outer surface of the support rod is fixedly connected to the inner wall of the heating box, and the movable rod is attached to the inner wall of the sliding groove.

[0011] In a preferred embodiment, the second limiting block is fixedly connected to one end of the second clamping plate, and one end of the spring is fixedly connected to the inner wall of the moving groove.

[0012] Compared with the prior art, the advantages and positive effects of this utility model are as follows:

[0013] This invention utilizes a support rod as the main support, which is fixedly connected to the inner wall of the heating box for support. A movable rod and a first limiting block are used to pull the infrared heating tube inside. A first clamping plate and a second clamping plate are used to clamp the two ends of the infrared heating tube, with the first and second clamping plates symmetrically positioned at both ends of the movable rod. A slider, a connecting plate, and a second limiting block facilitate the movement of the second clamping plate from the slider, allowing it to be released and the infrared heating tube removed. A spring, a connecting slot, and a movable slot allow the second clamping plate to move within the top of the movable rod. When the spring is released, the second clamping plate can be clamped, thus fixing the two ends of the infrared heating tube. This design makes installing and replacing the infrared heating tube more convenient, requiring less manpower, and eliminating concerns about damaging the heating tube during movement. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the structure of an aviation fabric processing and drying device provided by this utility model.

[0015] Figure 2 This is a schematic diagram of the internal structure of the heating box of an aviation fabric processing and drying device provided by this utility model.

[0016] Figure 3 This is a schematic diagram of the supporting structure of an aviation fabric processing and drying device provided by this utility model.

[0017] Figure 4 This is a schematic diagram of the moving component of an aerospace fabric processing and drying device provided by this utility model.

[0018] Legend:

[0019] 1. Equipment body; 2. Heating box; 3. Support structure; 31. Support rod; 32. Sliding groove; 33. Limiting groove; 34. Fixing plate; 35. Stop block; 4. Moving component; 41. Moving rod; 42. First limiting block; 43. First clamping plate; 44. Second clamping plate; 45. Sliding block; 46. Connecting plate; 47. Second limiting block; 48. Spring; 49. Connecting slot; 410. Moving groove; 411. Fixing angle. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] Example 1

[0022] like Figures 1-4 As shown, this utility model provides a technical solution: an aviation fabric processing and drying device, including a main body 1, a heating box 2 inside the main body 1, a support structure 3 on the inner wall of the heating box 2, the support structure 3 including a support rod 31, a sliding groove 32 on one side of the support rod 31, a limiting groove 33 inside the sliding groove 32, a moving component 4 slidably connected to the inner wall of the sliding groove 32, the moving component 4 including a moving rod 41, a first limiting block 42 fixedly connected to the bottom of the moving rod 41, a first clamping plate 43 fixedly connected to the top of the moving rod 41, a second clamping plate 44 on one side of the first clamping plate 43, and a slider 45 on one side of the second clamping plate 44. A connecting plate 46 is fixedly connected to the outer surface of the slider 45. A second limiting block 47 is fixedly connected to the outer surface of the connecting plate 46. A spring 48 is fixedly connected to the outer surface of the second limiting block 47. A connecting slot 49 is opened at the top of the moving rod 41. A moving groove 410 is opened inside the connecting slot 49. The inner wall of the connecting slot 49 is sleeved on the outer surface of the connecting plate 46. One end of the second clamping plate 44 is sleeved inside the moving groove 410. The outer surface of the support rod 31 is fixedly connected to the inner wall of the heating box 2. The moving rod 41 is attached to the inner wall of the sliding groove 32. The second limiting block 47 is fixedly connected to one end of the second clamping plate 44. One end of the spring 48 is fixedly connected to the inner wall of the moving groove 410.

[0023] In this embodiment, a support structure 3 is provided to support the movement of the movable component 4 inside the heating box 2. The movable component 4 makes the installation and replacement of the infrared heating tube more convenient and requires less manpower. Specifically, a support rod 31 is provided as the main support, and it is fixedly connected to the inner wall of the heating box 2 for support. A sliding groove 32 is provided, forming a long sliding groove 32 between the support rod 31 and the heating box 2, serving as the space for the movable rod 41 to move. A limiting groove 33 is provided, allowing the first limiting block 42 to slide inside, preventing the movable rod 41 from detaching from the support rod 31 during movement. The movable rod 41 and the first limiting block 42 are used to pull the infrared heating tube inside. A first clamping plate 43 and a second clamping plate 44 are provided to clamp both ends of the infrared heating tube, with the first clamping plate 43 and the second clamping plate 44 symmetrically arranged at both ends of the movable rod 41. A slider 45, a connecting plate 46, and a second limiting block 47 are provided to facilitate movement from the slider 45... The second clamping plate 44 is moved to relax it, thereby removing the infrared heating tube. By setting the spring 48, connecting slot 49 and moving slot 410, the second clamping plate 44 can move inside the top of the moving rod 41. When the spring 48 is relaxed, the second clamping plate 44 can be clamped, thereby fixing the two ends of the infrared heating tube. The size of the inner side of the moving slot 410 can be set to fit against the second limiting block 47 to restrict the movement of the second clamping plate 44.

[0024] Example 2

[0025] like Figure 4 As shown, a rectangular through hole is provided at the top of the support rod 31, and a fixing plate 34 is attached to the inner wall of the rectangular through hole. A stop block 35 is provided at the top of the fixing plate 34, and a fixing angle 411 is provided at the top of the moving rod 41. The fixing plate 34 is movable within the inner wall of the fixing angle 411.

[0026] In this embodiment, since the movable rod 41 can slide, a structure is set to restrict its movement to prevent the movable rod 41 from moving with the infrared heating tube during use and affecting the machine operation. Specifically, a rectangular through hole is set at the top of the support rod 31 so that the fixing plate 34 can move inside it. In addition, a small slot matching the stop block 35 is opened on the upper side of the outer end of the rectangular through hole to prevent the fixing plate 34 from detaching from the support rod 31. At the same time, when the stop block 35 moves to this position, it will not obstruct the movable rod 41 from pulling outward. Pushing the fixing plate 34 to lock at the fixing corner 411 can block the movable rod 41 from moving outward.

[0027] Working principle:

[0028] like Figures 1-4As shown, when replacing the infrared heating tube, first pull the fixing plate 34 away from the fixing angle 411 from the top side of the support rod 31. The stop block 35 is stuck in the small slot. After removing the wire ends of the infrared heating tube, pull the moving rod 41 outward to move it in the sliding groove 32. At the same time, the first limiting block 42 moves in the limiting groove 33, thereby bringing the infrared heating tube out. Then push the slider 45 to the right, causing the connecting plate 46 to move at the connecting slot 49. The second limiting block 47 moves inside the moving groove 410. At the same time, the second clamping plate 44 retracts into the moving groove 410, and the spring 48 retracts at the same time, so that the first clamping plate 43 and the second clamping plate 44 are relaxed, thereby removing the infrared heating tube for replacement.

[0029] The above description is merely a preferred embodiment of the present utility model and is not intended to limit the present utility model in any other way. Any person skilled in the art may make changes or modifications to the above-disclosed technical content to create equivalent embodiments for application in other fields. However, any simple modifications, equivalent changes, and modifications made to the above embodiments based on the technical essence of the present utility model without departing from the technical solution of the present utility model shall still fall within the protection scope of the technical solution of the present utility model.

Claims

1. An aerospace fabric processing and drying device, comprising a main body (1), characterized in that: The main body (1) of the equipment is provided with a heating box (2) inside. The inner wall of the heating box (2) is provided with a support structure (3). The support structure (3) includes a support rod (31). A sliding groove (32) is provided on one side of the support rod (31). A limit groove (33) is provided inside the sliding groove (32). A moving component (4) is slidably connected to the inner wall of the sliding groove (32). The moving component (4) includes a moving rod (41). A first limit block (42) is fixedly connected to the bottom of the moving rod (41). A first clamping plate (43) is fixedly connected to the top of the moving rod (41). A second clamping plate (44) is provided on one side of the first clamping plate (43). A slider (45) is provided on one side of the second clamping plate (44). A connecting plate (46) is fixedly connected to the outer surface of the slider (45). A second limit block (47) is fixedly connected to the outer surface of the connecting plate (46). A spring (48) is fixedly connected to the outer surface of the second limit block (47).

2. The aerospace fabric processing and drying device according to claim 1, characterized in that: The top of the support rod (31) has a rectangular through hole, and the inner wall of the rectangular through hole is fitted with a fixing plate (34). The top of the fixing plate (34) is provided with a stop block (35), and the top of the moving rod (41) has a fixing angle (411).

3. The aerospace fabric processing and drying device according to claim 2, characterized in that: The fixing plate (34) is movable on the inner wall of the fixing angle (411).

4. The aerospace fabric processing and drying device according to claim 1, characterized in that: The top of the movable rod (41) is provided with a connecting slot (49), and the inside of the connecting slot (49) is provided with a movable slot (410).

5. The aerospace fabric processing and drying device according to claim 4, characterized in that: The inner wall of the connecting slot (49) is fitted onto the outer surface of the connecting plate (46), and the inside of the moving slot (410) is fitted onto one end of the second clamping plate (44).

6. The aerospace fabric processing and drying device according to claim 1, characterized in that: The outer surface of the support rod (31) is fixedly connected to the inner wall of the heating box (2), and the moving rod (41) is attached to the inner wall of the sliding groove (32).

7. The aerospace fabric processing and drying device according to claim 1, characterized in that: The second limiting block (47) is fixedly connected to one end of the second clamping plate (44), and one end of the spring (48) is fixedly connected to the inner wall of the moving groove (410).

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