Storage rack for aircraft parts

Abstract

The utility model belongs to the technical field of storage equipment, and discloses an aircraft part storage rack which comprises a bottom plate and a top plate, an inclined rod is arranged between the bottom plate and the top plate, a sleeve is arranged on the side surface of the inclined rod, and a rotating shaft is arranged in the sleeve. When the aircraft parts are taken, the storage boxes which are adjacent up and down are of a staggered stacked structure, the view angle range of the storage box on the lower layer can be expanded, and a worker can take the aircraft parts in the storage boxes conveniently, and then the storage boxes rotate around the handle under the action of the handle during taking, and then the fixed handle is rotated, so that the aircraft parts can be taken conveniently. And the fixing protrusions are attached to the rotating shaft, so that the rotating shaft is fixed through friction force between the fixing protrusions and the rotating shaft, the storage box is inclined and faces workers, and the visual angle range is further enlarged.

Description

Technical Field

[0001] The present application relates to the technical field of storage equipment, and more particularly to a storage rack for aircraft parts. Background Art

[0002] Aircraft parts are of various types and have complex and diverse structures. Most of the existing storage devices for placing aircraft parts are a box, which contains all the parts for storage. In order to improve work efficiency, people have designed storage devices.

[0003] The search application number: CN201821366066.2 discloses a storage rack for a warehouse for the production of aircraft parts, including a movable seat, a movable wheel is provided at the bottom of the movable seat, a storage box is provided on the top of the movable seat, and adjustable support guard plates are symmetrically provided on the left and right sides of the top of the storage box, a support plate is provided between the two sets of adjustable support guard plates, an air intake pipe joint is provided on the left side of the left adjustable support guard plate, and the air intake pipe joint is connected to the inner cavity of the support plate through a hose, a top plate is provided on the top of the adjustable support guard plate, an air filter device and an air pump are provided on the top of the top plate, and the exhaust end of the air filter device is connected to the air intake pipe joint through a conduit, an air nozzle is provided at the bottom of the support plate and the bottom of the top plate, and a lighting lamp is embedded in the bottom of the support plate and the bottom of the top plate. The structural design of the utility model is reasonable, easy to take and store, and reduces the possibility of dust deposition on the parts, thereby achieving the possibility of protecting them.

[0004] Due to the use of a large number of electric-controlled pneumatic push rods, although the purpose of taking and storing parts is achieved, it also greatly increases the investment cost of the storage rack, and requires maintenance personnel to regularly inspect the electric-controlled pneumatic push rods to ensure their normal use.

[0005] In order to solve the above problems, the present application provides a storage rack for aircraft parts. Utility Model Content

[0006] The present application provides a storage rack for aircraft parts that adopts the following technical solution:

[0007] A storage rack for aircraft parts includes a bottom plate and a top plate, a tilting rod is provided between the bottom plate and the top plate, a sleeve is provided on the side surface of the tilting rod, a rotating shaft is provided inside the sleeve, and the rotating shaft is fixedly connected to a frame, a storage box is provided inside the frame, and a handle is provided on the side surface of the frame, a fixed handle is provided on the side surface of the sleeve via a hinge, and a rubber protrusion is provided on the lower surface of the fixed handle, and the rubber protrusion is tightly arranged against the rotating shaft.

[0008] Through the above technical solution, due to the setting of the inclination angle of the inclined rod, the upper and lower adjacent storage boxes will be in a staggered stacked structure, which is beneficial to expanding the viewing range of the lower storage box and facilitating the staff to take the aircraft parts in the storage box. Secondly, when taking, by applying a force to the handle, the storage box rotates around, and then the fixing handle is rotated so that the fixing protrusion fits with the rotating shaft. Thus, the friction force between the fixing protrusion and the rotating shaft is used to fix the rotating shaft, making the storage box inclined and facing the staff, further increasing the viewing range.

[0009] Furthermore, a box cover is connected to the side surface of the frame through a rotating shaft, and a sealing handle is arranged on the surface of the rotating shaft.

[0010] Through the above technical solution, the box cover is driven by the sealing handle to seal the storage box.

[0011] Furthermore, an observation window is inlaid on the surface of the box cover.

[0012] Through the above technical solution, the storage situation of the aircraft parts inside the storage box can be directly observed.

[0013] Furthermore, a buckle groove is formed on the side surface of the storage box.

[0014] Through the above technical solution, it is convenient to take out the storage box from the frame.

[0015] Furthermore, a reinforcing rib is arranged between adjacent inclined rods.

[0016] Through the above technical solution, it is used to reinforce the inclined rod.

[0017] Furthermore, moving wheels are arranged on the lower surface of the bottom plate, and the moving wheels are equipped with a self-locking structure.

[0018] Through the above technical solution, it is convenient to move the storage rack.

[0019] In summary, the present application includes the following beneficial technical effects:

[0020] Due to the setting of the inclination angle of the inclined rod, the upper and lower adjacent storage boxes will be in a staggered stacked structure, which is beneficial to expanding the viewing range of the lower storage box and facilitating the staff to take the aircraft parts in the storage box. Secondly, when taking, by applying a force to the handle, the storage box rotates around, and then the fixing handle is rotated so that the fixing protrusion fits with the rotating shaft. Thus, the friction force between the fixing protrusion and the rotating shaft is used to fix the rotating shaft, making the storage box inclined and facing the staff, further increasing the viewing range. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a schematic diagram of the overall structure of the present application;

[0022] Figure 2 This is a schematic diagram of the overall structure of the framework of this application;

[0023] Figure 3 This is a schematic diagram of the structure at location A of this application.

[0024] Explanation of the reference numerals in the figure:

[0025] 1. Bottom plate; 2. Top plate; 3. Inclined rod; 4. Framework; 5. Storage box; 6. Box cover; 7. Reinforcing rib; 8. Movable wheel; 9. Fixed handle; 10. Rubber protrusion; 11. Buckle groove; 12. Sealing handle; 13. Observation window; 14. Sleeve; 15. Handle. Detailed implementation manners

[0026] Next, the technical solutions in the embodiments of this application will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of this application; obviously, the described embodiments are only a part of the embodiments of this application, rather than all the embodiments. Based on the embodiments in this application, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of this application.

[0027] In the description of this application, it should be noted that the orientation or positional relationship indicated by the terms "upper", "lower", "inner", "outer", "top / bottom end", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing this application and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation to this application. In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0028] In the description of this application, it should be noted that unless otherwise clearly specified and limited, the terms "installed", "provided with", "sheathed / connected", "connected", etc. should be understood in a broad sense. For example, "connected" can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific situations.

[0029] Embodiment:

[0030] The embodiment of this application discloses a storage rack for aircraft parts. Please refer to Figure 1 and Figure 3, including a bottom plate 1 and a top plate 2. An inclined rod 3 is arranged between the bottom plate 1 and the top plate 2. A sleeve 14 is arranged on the side surface of the inclined rod 3. A rotating shaft is arranged inside the sleeve 14, and the rotating shaft is fixedly connected to a frame 4. A storage box 5 is arranged inside the frame 4, and a handle is arranged on the side surface of the frame 4. A fixed handle 9 is arranged on the side surface of the sleeve 14 through a hinge, and a rubber protrusion 10 is arranged on the lower surface of the fixed handle 9. The rubber protrusion 10 is in close contact with the rotating shaft. Due to the inclined angle setting of the inclined rod 3, the upper and lower adjacent storage boxes 5 are in a staggered stacked structure, which is beneficial to expanding the viewing range of the lower storage box 5 and facilitating the staff to take the aircraft parts in the storage box 5. Secondly, when taking, by applying a force to the handle, the storage box 5 rotates around it. Then, the fixed handle 9 is rotated so that the fixed protrusion fits with the rotating shaft. Thus, the rotating shaft is fixed by using the friction force between the fixed protrusion and the rotating shaft, and the storage box 5 is inclined and faces the staff, further increasing the viewing range.

[0031] Please refer to Figure 1 and Figure 2 , a box cover 6 is connected to the side surface of the frame 4 through a rotating shaft, and a sealing handle 12 is arranged on the surface of the rotating shaft. When the box cover 6 is opened to take out the parts, the sealing handle 12 can be directly held and a downward force can be applied, so that the sealing handle 12 rotates around the rotating shaft, and then the box cover 6 rotates around the rotating shaft and covers the storage box 5 to seal the storage box 5 and prevent dust from adhering to the aircraft parts and corroding the aircraft parts. The setting of the sealing handle 12 enables the staff not to reach into the back of the storage box 5, greatly improving the use convenience of the device.

[0032] Please refer to Figure 2 , an observation window 13 is inlaid on the surface of the box cover 6. The staff can directly observe the storage situation inside the storage box 5 through the observation window 13.

[0033] Please refer to Figure 2 , a buckle groove 11 is opened on the side surface of the storage box 5. After the box cover 6 is opened, by pressing the finger at the buckle groove 11 and applying an upward force, the storage box 5 can be taken out from the frame 4 so that the staff can clean the inside of the storage box 5.

[0034] Please refer to Figure 1 , a reinforcing rib 7 is arranged between adjacent inclined rods 3, making the adjacent inclined rods 3 more stable and preventing the overall structure from being easily loose.

[0035] Please refer to Figure 1 , a moving wheel 8 is arranged on the lower surface of the bottom plate 1, and the moving wheel 8 has its own locking structure. The staff can push the storage rack and use the moving wheel 8 to roll on the ground, thus achieving the purpose of convenient movement.

[0036] The implementation principle of this embodiment is as follows: During use, due to the set inclination angle of the inclined rod 3, the upper and lower adjacent storage boxes 5 will form a staggered stacked structure, which is beneficial to expanding the viewing angle range of the lower storage box 5 and facilitating the staff to take the aircraft parts in the storage box 5. Secondly, when taking, by applying a force to the handle, the storage box 5 is rotated around, and then the fixed handle 9 is rotated so that the fixed protrusion fits with the rotating shaft. Thus, the rotating shaft is fixed by using the friction force between the fixed protrusion and the rotating shaft, making the storage box 5 inclined and facing the staff, further increasing the viewing angle range.

[0037] The above are all the preferred embodiments of this application. The protection scope of this application is not limited thereby. Therefore, all equivalent changes made according to the structure, shape, and principle of this application shall be covered within the protection scope of this application.

Claims

1. A storage rack for aircraft parts, comprising a bottom plate (1) and a top plate (2), characterized in that: An inclined rod (3) is arranged between the bottom plate (1) and the top plate (2). A sleeve (14) is arranged on the side surface of the inclined rod (3). A rotating shaft is arranged inside the sleeve (14), and the rotating shaft is fixedly connected to the frame (4). A storage box (5) is arranged inside the frame (4), and a handle (15) is arranged on the side surface of the frame (4). A fixed handle (9) is arranged on the side surface of the sleeve (14) through a hinge, and a rubber protrusion (10) is arranged on the lower surface of the fixed handle (9). The rubber protrusion (10) is in close contact with the rotating shaft.

2. The storage rack for aircraft parts according to claim 1, characterized in that: A box cover (6) is connected to the side surface of the frame (4) through a rotating shaft, and a sealing handle (12) is arranged on the surface of the rotating shaft.

3. The storage rack for aircraft parts according to claim 2, wherein: An observation window (13) is inlaid on the surface of the box cover (6).

4. The storage rack for aircraft parts according to claim 1, wherein: A buckle groove (11) is formed on the side surface of the storage box (5).

5. The storage rack for aircraft parts according to claim 1, characterized in that: Reinforcing ribs (7) are arranged between adjacent inclined rods (3).

6. The storage rack for aircraft parts according to claim 1, characterized in that: Moving wheels (8) are arranged on the lower surface of the bottom plate (1), and the moving wheels (8) are provided with a self-locking structure.

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