Dust collector for aircraft cockpit
By using silicone suction heads in the aircraft cockpit vacuum cleaner and quickly replacing the suction heads, the problem that existing vacuum cleaners cannot adapt to the aircraft cockpit environment is solved, and the dust cleaning speed and equipment protection effect is improved.
Patent Information
- Application Number
- CN202421932909.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-12
- Publication Date
- 2025-05-27
- Estimated Expiration
- 2034-08-12
AI Technical Summary
The existing vacuum cleaner heads cannot adapt to the internal environment of the aircraft cockpit and cannot accurately dust the cockpit internal equipment, resulting in the inability to vacuum the many places.
A vacuum cleaner for aircraft cockpit is designed, using silicone suction heads and the connection mechanism realizes rapid replacement of suction heads to meet the needs of different environments.
The use of silicone suction heads can avoid wear on the equipment, and at the same time, it can quickly replace suction heads suitable for different environments, which improves the dust cleaning speed and solves the problem that existing vacuum cleaners cannot adapt to the cockpit environment.
Smart Images
Figure CN222899010U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of vacuum cleaners, in particular to a vacuum cleaner for an aircraft cockpit. Background Art
[0002] A vacuum cleaner is a device that uses a gas pump to create partial vacuum, generate suction and suck up dust and debris on the floor or other locations. Inside the aircraft cockpit, in order to facilitate dust removal inside the aircraft cockpit, special cleaning cloths, cleaning agents and vacuuming equipment are usually equipped.
[0003] The suction heads in existing vacuum cleaners are usually in a fixed state. However, the environment inside the aircraft cockpit is relatively complex, and the existing vacuum cleaner heads cannot adapt to the internal environment of the cockpit, and cannot accurately remove dust from the internal equipment of the cockpit, resulting in the inability to vacuum many places.
[0004] Therefore, it is very necessary to invent a vacuum cleaner for an aircraft cockpit to solve the above problems. Summary of the Utility Model
[0005] The purpose of the utility model is to provide a vacuum cleaner for an aircraft cockpit to solve the problem that the existing vacuum cleaner heads in the technology cannot adapt to the internal environment of the cockpit, cannot accurately remove dust from the internal equipment of the cockpit, and result in the inability to vacuum many places.
[0006] To achieve the above purpose, the utility model provides the following technical solution: A vacuum cleaner for an aircraft cockpit includes a dust collection box. The right side of the dust collection box is fixedly connected with a transmission pipeline. The right end of the transmission pipeline is fixedly connected with a handle. A suction pipeline is arranged on the right side of the handle. The right end of the suction pipeline is fixedly connected with a silicone suction head. A connection mechanism is arranged between the suction pipeline and the handle. The connection mechanism includes a first connection cylinder, a plug-in slot, a rubber cushion block and a second connection cylinder.
[0007] By adopting the above technical solution, the silicone suction head protects the surface of the equipment during use, avoids abrasion of the equipment, and at the same time, corresponding suction heads can be customized for different environments, and different suction heads can be quickly replaced through the connection mechanism.
[0008] Optionally, the left end of the first connection cylinder is fixedly connected with the right end of the handle, and the right end of the second connection cylinder is fixedly connected with the left end of the suction pipeline.
[0009] By adopting the above technical solution, the handle is used to adjust the position of the suction pipeline.
[0010] Optionally, a plug-in slot is opened inside the first connection cylinder, and a rubber cushion block is fixedly connected to the left end of the plug-in slot.
[0011] By adopting the above technical solution, the second connecting cylinder is inserted into the inside of the insertion slot, and the rubber cushion block seals the connection part.
[0012] Optionally, a positioning groove is formed on the surface of the first connecting cylinder, a clamping groove is formed on the side wall of the positioning groove, the positioning groove is communicated with the clamping groove, and a positioning rod is slidably connected inside the positioning groove.
[0013] By adopting the above technical solution, the positioning rod slides inside the positioning groove.
[0014] Optionally, a limiting groove is formed on the surface of the second connecting cylinder, and a supporting groove is formed at the bottom of the limiting groove.
[0015] Optionally, a limiting block is slidably connected inside the limiting groove, a supporting spring is fixedly connected to the bottom of the supporting groove, and one end of the supporting spring located outside the supporting groove is fixedly connected to the limiting block.
[0016] By adopting the above technical solution, the supporting spring pushes the limiting block outwards. After the second connecting cylinder is inserted into the inside of the insertion slot, the limiting block is stuck in the clamping groove to fix the second connecting cylinder.
[0017] Optionally, a dust suction pipeline is formed inside the second connecting cylinder.
[0018] Optionally, a hand-held rod is fixedly connected to the surface of the dust collection box.
[0019] In the above technical solution, the technical effects and advantages provided by the present utility model are as follows:
[0020] During the use of the silica gel suction head of the present utility model, the surface of the device is protected to avoid abrasion of the device. At the same time, suction heads corresponding to different environments can be customized, and different suction heads can be quickly replaced through the connection mechanism, so that the device can quickly suck the dust inside the cockpit, improve the dust cleaning speed, and avoid damage to the device, solving the problem that the existing vacuum cleaner head cannot adapt to the internal environment of the cockpit and cannot accurately remove dust from the internal devices of the cockpit, resulting in the inability to perform vacuuming on many places. BRIEF DESCRIPTION OF THE DRAWINGS
[0021] Figure 1 is a schematic diagram of the overall structure of the present utility model;
[0022] Figure 2 is a schematic diagram of the handle structure of the present utility model;
[0023] Figure 3 is a schematic diagram of the transverse sectional structure of the connection mechanism of the present utility model;
[0024] Figure 4 Schematic longitudinal sectional structure diagram of the connection mechanism of the present utility model;
[0025] Figure 5 For the present utility model Figure 3 Schematic diagram of Structure A;
[0026] Figure 6 For the present utility model Figure 3 Schematic diagram of Structure B.
[0027] Explanation of reference numerals:
[0028] 1, dust collection box; 11, carrying handle; 12, transmission pipeline; 2, handle; 21, first connecting cylinder; 22, insertion slot; 23, rubber cushion block; 24, positioning slot; 25, clamping slot; 26, positioning rod; 3, second connecting cylinder; 31, dust suction pipeline; 32, limiting slot; 33, support slot; 34, limiting block; 35, support spring; 36, suction pipeline; 37, silicone suction head. Detailed implementation manners
[0029] In order to enable those skilled in the art to better understand the technical solutions of the present utility model, the present utility model will be further introduced in detail below in conjunction with the accompanying drawings.
[0030] The present utility model provides a vacuum cleaner for an aircraft cockpit as shown in Figures 1 to 4 , which includes a dust collection box 1. A carrying handle 11 is fixedly connected to the surface of the dust collection box 1. A transmission pipeline 12 is fixedly connected to the right side of the dust collection box 1. The right end of the transmission pipeline 12 is fixedly connected to a handle 2. A suction pipeline 36 is arranged on the right side of the handle 2. The right end of the suction pipeline 36 is fixedly connected to a silicone suction head 37. A connection mechanism is arranged between the suction pipeline 36 and the handle 2. The connection mechanism includes a first connecting cylinder 21, an insertion slot 22, a rubber cushion block 23 and a second connecting cylinder 3. The left end of the first connecting cylinder 21 is fixedly connected to the right end of the handle 2. The right end of the second connecting cylinder 3 is fixedly connected to the left end of the suction pipeline 36. A dust suction pipeline 31 is arranged inside the second connecting cylinder 3.
[0031] Among them, suction heads corresponding to the environments of different equipment surfaces in the cockpit are customized, so that the suction heads can accurately suck dust for this environment, and at the same time avoid abrasion of the equipment surfaces. During the process of replacing the suction heads, the original second connecting cylinder 3 is pulled out of the first connecting cylinder 21, and the second connecting cylinder 3 in the new suction head is rinsed and inserted into the inside of the first connecting cylinder 21. During the suction process, the sucked dust enters the inside of the suction pipeline 36 through the silicone suction head 37, and then sequentially enters the inside of the dust collection box 1 through the handle 2 and the transmission pipeline 12.
[0032] Refer to Figures 3 to 6, an insertion slot 22 is provided inside the first connecting cylinder 21. A rubber cushion block 23 is fixedly connected to the left end of the insertion slot 22. A positioning slot 24 is provided on the surface of the first connecting cylinder 21. A clamping slot 25 is provided on the side wall of the positioning slot 24. The positioning slot 24 communicates with the clamping slot 25. A positioning rod 26 is slidably connected inside the positioning slot 24. A limiting slot 32 is provided on the surface of the second connecting cylinder 3. A supporting slot 33 is provided at the bottom of the limiting slot 32. A limiting block 34 is slidably connected inside the limiting slot 32. A supporting spring 35 is fixedly connected to the bottom of the supporting slot 33. One end of the supporting spring 35 located outside the supporting slot 33 is fixedly connected to the limiting block 34.
[0033] Specifically, during the installation process, first, the two limiting blocks 34 are pressed into the inside of the limiting slot 32. Then, the second connecting cylinder 3 is inserted into the inside of the positioning slot 24. When it is inserted to the bottom, the second connecting cylinder 3 is rotated, so that the limiting blocks 34 are clamped into the inside of the clamping slot 25, locking and fixing the second connecting cylinder 3 and the first connecting cylinder 21.
[0034] In addition, when replacing the suction head, the two positioning rods 26 are pressed. At this time, the positioning rods 26 slide inside the positioning slot 24, thereby squeezing the limiting blocks 34, so that the limiting blocks 34 are retracted into the inside of the limiting slot 32. At this time, the second connecting cylinder 3 is pulled outwards, and the corresponding suction head can be replaced.
[0035] The working principle of the present utility model: During use, the surface of the device is protected by the silicone suction head 37 to avoid abrasion of the device. At the same time, corresponding suction heads are customized for different environments, so that the suction head can better adapt to different device environments. Different suction heads are quickly replaced through the connecting mechanism, so that the suction head can quickly suck the dust inside the cockpit, improving the dust cleaning speed.
[0036] The above shows and describes the basic principle, main features and advantages of the present utility model. Those skilled in the art should understand that the present utility model is not limited by the above embodiments. The above embodiments and the descriptions in the specification are only preferred examples of the present utility model and are not used to limit the present utility model. Without departing from the spirit and scope of the present utility model, the present utility model will have various changes and improvements, and these changes and improvements all fall within the scope of the present utility model claimed.
Claims
1. A vacuum cleaner for an aircraft cockpit, comprising a dust collecting box (1), characterized in that: The right side of the dust collecting box (1) is fixedly connected to a transmission pipe (12), the right end of the transmission pipe (12) is fixedly connected to a handle (2), a suction pipe (36) is provided on the right side of the handle (2), the right end of the suction pipe (36) is fixedly connected to a silicone suction head (37), and a connecting mechanism is provided between the suction pipe (36) and the handle (2), the connecting mechanism comprising a first connecting tube (21), a plug-in slot (22), a rubber pad (23) and a second connecting tube (3).
2. A vacuum cleaner for an aircraft cockpit according to claim 1, characterized in that: The left end of the first connecting tube (21) is fixedly connected to the right end of the handle (2), and the right end of the second connecting tube (3) is fixedly connected to the left end of the suction pipe (36).
3. A vacuum cleaner for an aircraft cockpit according to claim 1, characterized in that: The first connecting tube (21) is provided with an inserting groove (22) inside, and a rubber pad (23) is fixedly connected to the left end of the inserting groove (22).
4. A vacuum cleaner for an aircraft cockpit according to claim 3, characterized in that: A positioning groove (24) is provided on the surface of the first connecting tube (21), a clamping groove (25) is provided on the side wall of the positioning groove (24), the positioning groove (24) and the clamping groove (25) are connected to each other, and a positioning rod (26) is slidably connected inside the positioning groove (24).
5. A vacuum cleaner for an aircraft cockpit according to claim 4, characterized in that: A limiting groove (32) is provided on the surface of the second connecting tube (3), and a supporting groove (33) is provided at the bottom of the limiting groove (32).
6. A vacuum cleaner for an aircraft cockpit according to claim 5, characterized in that: The limiting groove (32) is internally slidably connected to a limiting block (34), the bottom of the supporting groove (33) is fixedly connected to a supporting spring (35), and one end of the supporting spring (35) located outside the supporting groove (33) is fixedly connected to the limiting block (34).
7. A vacuum cleaner for an aircraft cockpit according to claim 1, characterized in that: A dust suction pipe (31) is provided inside the second connecting tube (3).
8. A vacuum cleaner for an aircraft cockpit according to claim 1, characterized in that: A carrying rod (11) is fixedly connected to the surface of the dust collecting box (1).