Aviation part cleaning and drying box
By designing a cleaning and drying box for aviation parts, using the motor to drive the cylinder rotation and the combination of heating and cleaning liquid, the problems of low cleaning and pollution during the transfer in the existing technology are solved, and comprehensive cleaning and drying are achieved Dry, improving cleaning effect and operation convenience.
Patent Information
- Application Number
- CN202323547812.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2023-12-26
- Publication Date
- 2024-12-17
- Estimated Expiration
- 2033-12-26
AI Technical Summary
The existing aviation parts cleaning device can only clean the fixed position of the parts, and the overall cleaning level is not high enough. The cleaned parts are easily contaminated with other debris during the transfer process, affecting the cleaning effect.
A aviation component cleaning and drying box is designed, including a drying box, a washing and drying mechanism and a clamping mechanism. The cylinder is driven by a motor to rotate, combined with the conveying of heating and cleaning liquid, and achieve comprehensive cleaning and drying. Fix parts by clamping mechanism to avoid secondary contamination during the transfer process.
It improves the cleaning effect and operation convenience of aviation parts, simplifies the operation process, improves production efficiency and product quality, and avoids secondary pollution.
Smart Images

Figure CN222175079U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation component equipment, in particular to an aviation component cleaning and drying box. Background Art
[0002] Aviation refers to the flight activities of manned or unmanned aircraft in the earth's atmosphere. Aircraft refers to aircraft flying in the atmosphere, including lighter-than-air aircraft and heavier-than-air aircraft such as fixed-wing aircraft and rotorcraft. Fixed-wing aircraft are aircraft with fixed wings. According to whether they have their own driving power, they can be divided into gliders and airplanes; rotorcraft refer to aircraft that fly by generating aerodynamic force by rotating rotors, mainly helicopters and gyroplanes. In a broad sense, aviation parts are the general term for various parts and components of aircraft. According to their position and major categories in the aircraft structure, they can be divided into body parts, engine parts, avionics parts, airborne equipment and other major categories. Aviation parts need to be cleaned before installation or during maintenance to remove impurities and debris attached to them to ensure safety and extend service life.
[0003] Although the cleaning device for aviation parts processing in the prior art can effectively clean aviation parts of different specifications, this cleaning device can only clean the fixed positions of the parts, and the overall cleaning level is not high enough. The cleaned parts need to be transferred and dried. On the one hand, the operation is troublesome, and on the other hand, the transfer process may be contaminated with other debris, affecting the overall cleaning effect. Therefore, we propose an aviation parts cleaning and drying box to solve the above problems. Utility Model Content
[0004] In order to achieve the above-mentioned purpose, the utility model specifically adopts the following technical solutions:
[0005] An aviation parts cleaning and drying box, comprising:
[0006] A drying box body, wherein a take-out opening is arranged on the upper side of the front of the drying box body, and a box door is hingedly connected to one side of the take-out opening, and a drainage pipe is arranged on one side of the bottom of the drying box body, and a water valve is installed on the pipe body of the drainage pipe;
[0007] A barrel is arranged at the bottom of the drying box, and the aviation parts to be washed are placed inside the barrel. A motor is installed at the bottom of the drying box, and the output shaft of the motor passes through the bottom wall of the drying box and is connected to the bottom of the barrel. A baffle is arranged on the side wall of the barrel;
[0008] The washing and drying mechanism comprises a fixed pipe fixedly inserted on the upper side of the drying box body, the middle of the fixed pipe is connected with a connecting pipe, one end of the connecting pipe away from the fixed pipe is connected with a hollow plate, the bottom of the hollow plate is evenly distributed with through holes, the fixed pipe body is provided with a one-way valve on both sides of the connecting pipe, one end of the fixed pipe is connected with a heating conveying device, and the other end is connected with a cleaning liquid conveying device;
[0009] The clamping mechanism is arranged inside the barrel and is used for clamping and fixing aviation parts.
[0010] Furthermore, a fixed cylinder is connected to the middle of the top of the drying box body, and air holes are evenly distributed on the surface of the fixed cylinder.
[0011] Furthermore, water leakage holes are evenly distributed on the bottom of the barrel.
[0012] Furthermore, a bull's eye universal wheel is installed in a circular array at the corners of the bottom surface of the barrel, and the bull's eye universal wheel is slidably connected to the inner bottom wall of the drying box body.
[0013] Furthermore, the clamping mechanism includes a limit plate fixed on one side of the interior of the barrel, a mounting cylinder is fixed on the side of the interior of the barrel away from the limit plate, a sliding plug is slidably inserted into the interior of the mounting cylinder, a spring is connected between the sliding plug and the inner wall of the mounting cylinder, a sliding rod is connected to the end of the sliding plug away from the spring, and an extrusion block is connected to the end of the sliding rod away from the sliding plug that slides through the top wall of the mounting cylinder.
[0014] Furthermore, the limiting plate is V-shaped, and a rubber sleeve is provided on the surface of the extrusion block.
[0015] The beneficial effects of the utility model are as follows:
[0016] The utility model can comprehensively clean and dry aviation parts through the combined design of the drying box, the washing and drying mechanism and the clamping mechanism, thus avoiding secondary contamination during the transfer process, improving the overall cleaning effect and operating convenience, simplifying the operating process, improving production efficiency and product quality, and has high practicality and is worthy of widespread application and promotion. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] Figure 1 It is a three-dimensional structural schematic diagram of the utility model;
[0018] Figure 2 It is a top view schematic diagram of the utility model;
[0019] Figure 3 This utility model Figure 2 Schematic cross-sectional view in the AA direction;
[0020] Figure 4It is a schematic diagram of the barrel structure of the utility model.
[0021] Figure numerals: 1. drying box; 101. taking port; 102. box door; 103. drain pipe; 2. barrel; 201. baffle; 202. water leakage hole; 3. motor; 4. washing and drying mechanism; 401. fixing pipe; 402. connecting pipe; 403. hollow plate; 4031. through hole; 404. one-way valve; 5. clamping mechanism; 501. limit plate; 502. mounting barrel; 503. sliding plug; 504. spring; 505. sliding rod; 506. extrusion block; 6. fixing barrel; 7. bull's eye universal wheel. DETAILED DESCRIPTION
[0022] In order to make the purpose, technical solution and advantages of the embodiments of the present utility model clearer, the technical solution in the embodiments of the present utility model will be clearly and completely described below in conjunction with the drawings in the embodiments of the present utility model.
[0023] The present application provides an aviation parts cleaning and drying box, which is mainly used to solve the problem that the existing technology can only clean the fixed position of the parts, the overall cleaning degree is not high enough, and the cleaned parts need to be transferred and dried, which is troublesome to operate on the one hand, and on the other hand, other debris may be contaminated during the transfer process, affecting the overall cleaning effect, and provides the following technical solutions, which will be combined with Figure 1-Figure 4 Make a detailed description:
[0024] An aviation parts cleaning and drying box, comprising:
[0025] A drying box 1 is provided with a take-out opening 101 on the upper front side of the drying box 1, and a box door 102 is hingedly connected to one side of the take-out opening 101, and a drain pipe 103 is provided on one side of the bottom of the drying box 1, and a water valve is installed on the body of the drain pipe 103;
[0026] The barrel 2 is arranged at the bottom of the drying box 1, and the aviation parts to be washed are placed inside the barrel 2. A motor 3 is installed at the bottom of the drying box 1. The output shaft of the motor 3 passes through the bottom wall of the drying box 1 and is connected to the bottom of the barrel 2. The side wall of the barrel 2 is provided with a baffle 201;
[0027] The washing and drying mechanism 4 includes a fixed pipe 401 fixedly inserted on the upper side of the drying box 1, the middle of the fixed pipe 401 is connected with a connecting pipe 402, one end of the connecting pipe 402 away from the fixed pipe 401 is connected with a hollow disk 403, and the bottom of the hollow disk 403 is evenly distributed with through holes 4031. The fixed pipe 401 is located on both sides of the connecting pipe 402 and is provided with a one-way valve 404. One end of the fixed pipe 401 is connected to the heating conveying device, and the other end is connected to the cleaning liquid conveying device;
[0028] The clamping mechanism 5 is arranged inside the barrel 2 and is used to clamp and fix aviation parts. The clamping mechanism 5 includes a limit plate 501 fixed on one side of the barrel 2, a mounting cylinder 502 is fixed on the side of the barrel 2 away from the limit plate 501, a sliding plug 503 is slidably inserted inside the mounting cylinder 502, a spring 504 is connected between the sliding plug 503 and the inner wall of the mounting cylinder 502, a sliding rod 505 is connected to the end of the sliding plug 503 away from the spring 504, and the end of the sliding rod 505 away from the sliding plug 503 slides through the top wall of the mounting cylinder 502 and is connected to an extrusion block 506.
[0029] It should be noted that one port of the fixed pipe 401 is connected to the heating delivery equipment, and the other port is connected to the cleaning liquid delivery equipment. The heating delivery equipment is generally a heater. When the heater is working, the warm air can be delivered to the fixed pipe 401 through the delivery pipe. The cleaning liquid delivery equipment is generally a water pump. When the water pump is working, the cleaning liquid can be delivered to the fixed pipe 401. The setting of the one-way valve 404 can ensure that the operation of the heating delivery equipment and the cleaning liquid delivery equipment does not affect each other.
[0030] The specific implementation steps and principle description of the aviation parts cleaning and drying box:
[0031] The first step is to open the box door 102, put the aviation parts to be washed into the barrel 2, and fix them with the clamping mechanism 5. The clamping mechanism 5 is used in the following way: the aviation parts to be washed are placed on one side of the limit plate 501, and under the action of the spring 504, the slide plug 503 slides outward, and the extrusion block 506 at the end of the slide rod 505 is pressed against the aviation parts, and the aviation parts to be washed can be fixed in cooperation with the limit plate 501;
[0032] The second step is to close the box door 102, start the motor 3, make the barrel 2 start to rotate, connect one end of the fixed pipe 401 with the cleaning liquid conveying device, and the cleaning liquid passes through the fixed pipe 401 and the connecting pipe 402 and finally flows from the through hole 4031 at the bottom of the hollow disk 403 to the washed aviation parts, thereby cleaning the washed aviation parts. At the same time, during the cleaning process, the cleaning liquid is discharged through the drain pipe 103;
[0033] The third step is to turn on the heating conveying device after the cleaning is completed, and send hot air into the fixed pipe 401, the connecting pipe 402 and the hollow plate 403. The warm air flows to the aviation parts through the through hole 4031 at the bottom of the hollow plate 403 to achieve the drying effect. During this process, the motor 3 drives the barrel 2 to rotate. Under the action of centrifugal force, the water loss on the surface of the aviation parts can be accelerated, thereby improving the drying efficiency.
[0034] Step 4: After the drying is completed, open the box door 102 and take out the aviation parts, thus completing the entire washing and drying process.
[0035] The aviation parts cleaning and drying box can comprehensively clean and dry aviation parts through the combined design of the drying box body 1, the washing and drying mechanism 4 and the clamping mechanism 5, avoiding secondary contamination during the transfer process, improving the overall cleaning effect and operating convenience, simplifying the operating process, and improving production efficiency and product quality.
[0036] like Figure 3 As shown, in some embodiments, the top middle of the drying box 1 is connected to a fixed cylinder 6, and the surface of the fixed cylinder 6 is evenly distributed with air holes. More specifically, firstly, the air holes can play the role of exhausting air to ensure air circulation in the box. Secondly, the air holes can effectively remove moisture and odor accumulated in the column, keep the box column dry and fresh, and in addition, the air holes can reduce the pressure in the box column and improve its stability.
[0037] like Figure 4 As shown, in some embodiments, leakage holes 202 are evenly distributed on the bottom of the barrel 2. More specifically, the leakage holes 202 can discharge the cleaning liquid inside the barrel 2, ensuring that it flows out quickly and smoothly, avoiding stains from remaining, and improving cleaning efficiency.
[0038] like Figure 4 As shown, in some embodiments, a bull's eye universal wheel 7 is installed in a circular array at the corners of the bottom surface of the barrel 2, and the bull's eye universal wheel 7 is slidably connected to the inner bottom wall of the drying box 1. More specifically, the use of the bull's eye universal wheel 7 can reduce the friction between the barrel 2 and the inner bottom wall of the drying box 1, thereby reducing the energy loss during rotation and allowing the barrel 2 to move more smoothly. At the same time, the setting of the circular array can also ensure that the bull's eye universal wheel 7 is always in a good position, avoiding problems caused by the misalignment or falling off of the bull's eye universal wheel 7. In this way, the barrel 2 can complete the cleaning and drying tasks more efficiently, thereby improving production efficiency and product quality.
[0039] like Figure 4 As shown, in some embodiments, the limit plate 501 is V-shaped, and the surface of the extrusion block 506 is provided with a rubber sleeve. More specifically, the purpose of the V-shaped design of the limit plate 501 is to better adapt to parts of different shapes and provide a better clamping effect. The V-shaped limit plate 501 can better wrap the parts, provide a larger contact area during the clamping process, and increase the clamping force. The design of the rubber sleeve on the surface of the extrusion block 506 is to increase the friction and stability of the clamping mechanism 5 on the parts. The rubber sleeve has good friction characteristics, can provide a firmer clamping force, and prevent the parts from sliding or loosening during the clamping process. Through the V-shaped design of the limit plate 501 and the use of the rubber sleeve, the clamping mechanism 5 can better clamp the parts, ensure their stability and safety, and avoid the parts from falling off or shifting during the cleaning and drying process, thereby improving the cleaning and drying effect and quality.
[0040] The above description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention will not be limited to the embodiments shown herein, but will conform to the widest scope consistent with the principles and novel features disclosed herein.
Claims
1. An aviation parts cleaning and drying box, It is characterized in that include: A drying box (1), wherein a take-out opening (101) is provided on the upper front side of the drying box (1), and a box door (102) is hingedly connected to one side of the take-out opening (101); a drainage pipe (103) is provided on one side of the bottom of the drying box (1), and a water valve is installed on the pipe body of the drainage pipe (103); A barrel (2) is arranged at the bottom side of the drying box (1), and the aviation parts to be washed are placed inside the barrel (2). A motor (3) is installed at the bottom of the drying box (1), and the output shaft of the motor (3) passes through the bottom wall of the drying box (1) and is connected to the bottom of the barrel (2). A retaining net (201) is arranged on the side wall of the barrel (2); The washing and drying mechanism (4) comprises a fixed pipe (401) fixedly inserted into the upper side of the drying box (1), the middle of the fixed pipe (401) is connected to a connecting pipe (402), one end of the connecting pipe (402) away from the fixed pipe (401) is connected to a hollow disk (403), the bottom of the hollow disk (403) is evenly distributed with through holes, the fixed pipe (401) is provided with a one-way valve (404) on both sides of the connecting pipe (402), one end of the fixed pipe (401) is connected to a heating conveying device, and the other end is connected to a cleaning liquid conveying device; The clamping mechanism (5) is arranged inside the barrel (2) and is used to clamp and fix aviation parts.
2. An aviation parts cleaning and drying box according to claim 1, It is characterized in that The middle of the top of the drying box (1) is connected to a fixed cylinder (6), and the surface of the fixed cylinder (6) is evenly distributed with air holes.
3. The aviation parts cleaning and drying box according to claim 1, It is characterized in that The bottom of the barrel (2) is evenly distributed with water leakage holes (202).
4. The aviation parts cleaning and drying box according to claim 1, It is characterized in that Bull's eye universal wheels (7) are installed in a circular array at the corners of the bottom surface of the barrel (2), and the bull's eye universal wheels (7) are slidably connected to the inner bottom wall of the drying box body (1).
5. The aviation parts cleaning and drying box according to claim 1, It is characterized in that The clamping mechanism (5) comprises a limit plate (501) fixedly arranged on one side of the interior of the barrel (2); a mounting tube (502) is fixedly arranged on the side of the interior of the barrel (2) away from the limit plate (501); a sliding plug (503) is slidably inserted into the interior of the mounting tube (502); a spring (504) is connected between the sliding plug (503) and the inner wall of the mounting tube (502); a sliding rod (505) is connected to one end of the sliding plug (503) away from the spring (504); and an extrusion block (506) is connected to one end of the sliding rod (505) away from the sliding plug (503) that slides through the top wall of the mounting tube (502).
6. An aviation parts cleaning and drying box according to claim 5, It is characterized in that The limiting plate (501) is V-shaped, and a rubber sleeve is sleeved on the surface of the extrusion block (506).
