Aircraft accompanying article storage cabinet

Abstract

The utility model provides an aircraft accompanying article storage cabinet which aims at solving the technical problems that in the prior art, the internal space utilization rate of a storage cabinet is low, and articles cannot be limited in the storage cabinet. The whole storage cabinet is of a long-strip-shaped structure, a plurality of storage areas are arranged in the cabinet body, a plurality of hooks are arranged at the tops of the storage areas, a door plate is arranged on the cabinet body, a plurality of connecting holes are formed in one side face of the cabinet body, and the connecting holes are matched with connecting parts on an airplane body; the plurality of bridles are arranged in the cabinet body, at least one bridle is arranged in each storage area, the position of the bridle in the cabinet body can be adjusted, the bridle is at least provided with a free end, and the free end of the bridle can be connected with the other end of the bridle; the base is arranged at the bottom of the cabinet body, and the circumferential size of the base is smaller than that of the cabinet body. According to the storage cabinet, articles placed in the storage cabinet are limited through the bridles, so that the technical problems that the utilization rate of the internal space is low and the articles cannot be limited are solved.

Description

Technical Field

[0001] The utility model relates to a storage cabinet, in particular to an airplane accompanying article storage cabinet. Background Art

[0002] Storage lockers are used to store aircraft equipment and tools, and are installed in the aircraft's rest area. These lockers meet transport aircraft standards and provide additional storage space within the limited cabin space.

[0003] Existing aircraft cockpit storage cabinets have several issues: 1. Due to their multi-layered internal structure, existing cabinets fail to fully utilize the internal space, resulting in low storage efficiency. 2. Existing cabinets lack effective internal fastening and restraints, making items easily dislodged or damaged during flight. This not only affects the safety of items but also increases flight safety risks. Utility Model Content

[0004] In response to the technical problems of low internal space utilization and inability to limit the position of items in storage cabinets in the prior art, the utility model provides an aircraft accompanying item storage cabinet. The interior of the cabinet is divided into multiple storage areas, and straps are provided in each storage area. The items placed in the storage cabinet are limited by the straps, thereby solving the technical problems of low internal space utilization and inability to limit the position of items.

[0005] The technical solution of the utility model is:

[0006] An aircraft accompanying item storage cabinet, comprising:

[0007] The cabinet body is an elongated structure with multiple storage areas inside. The top of each storage area is provided with multiple hooks. The cabinet body is provided with a door panel. One side of the cabinet body is provided with multiple connection holes, which match the connection parts on the aircraft fuselage.

[0008] A plurality of straps are provided in the cabinet, and each storage area has at least one strap, the position of the strap in the cabinet is adjustable, and the strap has at least one free end, and the free end of the strap can be connected to the other end;

[0009] The base is arranged at the bottom of the cabinet, and the circumferential dimension of the base is smaller than the circumferential dimension of the cabinet.

[0010] Optionally, each storage area corresponds to a door panel, and all the door panels are provided with a lock body.

[0011] Optionally, a plurality of reinforcing ribs are respectively provided on both side walls of the cabinet body, and the reinforcing ribs are arranged along the length direction of the cabinet body.

[0012] Optionally, the strap is movably disposed in the cabinet body and can move along the length direction of the cabinet body.

[0013] Optionally, the two ends of the strap are respectively provided with a sub-surface and a main surface of a Velcro.

[0014] Optionally, the strap is elastic.

[0015] Optionally, the strap is provided with an adsorption structure and can be adsorbed on the inner wall of the cabinet.

[0016] Optionally, a rubber pad is provided at the bottom of the base.

[0017] Optionally, a rubber strip is provided on the inner side of the door panel.

[0018] Optionally, the strap is a long sheet-like structure.

[0019] Compared with the prior art, the beneficial effects of the present invention are:

[0020] First, the cabinet is designed as a long, strip-like structure with multiple attachment holes on its sides that align with the aircraft fuselage's connection points, allowing the cabinet to be mounted on the aircraft. Multiple storage areas are then created within the cabinet, each equipped with hooks to optimize space utilization. Each storage area also features at least one restraint, which secures items within the area, preventing them from moving freely, ensuring both item safety and flight safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present application. For ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.

[0022] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0023] Figure 2 It is a schematic diagram of the internal structure of the utility model. DETAILED DESCRIPTION

[0024] Hereinafter, only certain exemplary embodiments are briefly described. As will be appreciated by those skilled in the art, the described embodiments may be modified in various ways without departing from the spirit or scope of the present invention. Therefore, the drawings and description are to be regarded as illustrative in nature and not restrictive.

[0025] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, or are the orientations or positional relationships in which the products of the present invention are conventionally placed when in use, or are the orientations or positional relationships conventionally understood by those skilled in the art. They are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation to the present invention.

[0026] The disclosure below provides many different embodiments or examples for realizing different structures of the present invention. In order to simplify the disclosure of the present invention, the components and settings of specific examples are described below. Of course, they are merely examples and are not intended to limit the present invention. In addition, the present invention may repeat reference numbers and / or reference letters in different examples. Such repetition is for the purpose of simplicity and clarity and does not in itself indicate the relationship between the various embodiments and / or settings discussed. In addition, the present invention provides examples of various specific processes and materials, but a person of ordinary skill in the art will recognize the application of other processes and / or the use of other materials.

[0027] The embodiments of the present invention are described in detail below with reference to the accompanying drawings. Example

[0028] See also Figure 1 and Figure 2 This embodiment discloses an aircraft luggage storage cabinet, comprising a cabinet body 10, hooks 20, straps 30, and a base 40. The base 40 is mounted on the bottom of the cabinet body 10, the sides of which are connected to the aircraft fuselage. The hooks 20 and straps 30 are disposed within the cabinet body 10 and, when in use, are used to position items within the cabinet body 10.

[0029] Specifically, the cabinet 10 is a long strip structure, and the cabinet 10 has an open surface, and a door panel 50 is provided on the open surface, through which the cabinet 10 can be closed. Preferably, each storage area is equipped with a door panel 50, and each door panel 50 has at least one lock body.

[0030] A plurality of connection holes are provided on one side of the cabinet 10, and the connection holes are matched with the connection parts on the aircraft fuselage. Generally, the connection parts on the aircraft fuselage for mounting the cabinet 10 are a plurality of threaded holes. By matching all the threaded holes with all the connection holes and then inserting screws into the connection holes and the threaded holes, the cabinet 10 can be connected to the aircraft fuselage.

[0031] The base 40 is installed at the bottom of the cabinet 10, and the base 40 is a rectangular structure. The circumferential size of the base 40 is smaller than the circumferential size of the cabinet 10, so that after the base 40 is installed on the cabinet 10, there is a distance between the four sides of the base 40 and the four sides of the cabinet 10.

[0032] By installing the base 40 , the convex or curved fuselage structure at the bottom of the aircraft cabin can be effectively avoided, thereby making the cabinet 10 more stable.

[0033] The cabinet 10 is provided with multiple storage areas, all arranged along the length of the cabinet 10. Several hooks 20 and several straps 30 are provided in the storage areas. The hooks 20 are provided at the tops of the storage areas, while the straps 30 are movable within the storage areas, allowing their positions to be adjusted. The straps 30 have at least one free end, which can be detachably connected to the other end.

[0034] In this embodiment, the cabinet 10 is first designed as an elongated strip with multiple attachment holes on its sides that mate with the aircraft fuselage's connection points, allowing the cabinet 10 to be mounted on the aircraft. Multiple storage areas are then provided within the cabinet 10, each equipped with hooks 20 to effectively utilize the space within the locker. Each storage area is equipped with at least one tie strap 30, which secures items within the area and prevents them from moving freely, thereby ensuring both item safety and flight safety.

[0035] In one specific embodiment:

[0036] In order to reduce the overall weight of the cabinet 10, the cabinet 10 is welded with aluminum alloy plates, and in order to improve the strength of the long cabinet 10, a plurality of reinforcing ribs 60 are arranged in the cabinet 10. Specifically, a plurality of reinforcing ribs 60 are respectively provided on the two side walls of the cabinet 10, and the reinforcing ribs 60 are arranged along the length direction of the cabinet 10.

[0037] In another specific embodiment:

[0038] The strap 30 is movably arranged in the cabinet body 10 and can move along the length direction of the cabinet body 10. Generally speaking, the middle part of the strap 30 is slidably arranged on the cabinet body 10, and a slider is generally provided on the strap 30, and the slider is slidably arranged in the cabinet body 10. For example, the structure of the reinforcement rib 60 is groove-shaped, and the slider is slidably arranged on the reinforcement rib 60.

[0039] By movably arranging the strap 30 in the cabinet 10 , the strap 30 can limit the position of different items.

[0040] In another specific embodiment:

[0041] The two ends of the strap 30 have a quick connection and disassembly structure, for example, a Velcro sub-surface and a Velcro main surface are respectively provided at the two ends of the strap 30. Through this design, items can be quickly fixed in the cabinet 10 and quickly taken out of the cabinet 10.

[0042] In another specific embodiment:

[0043] The strap 30 is elastic. Through this design, the strap 30 has the effect of tightening and tensioning the items in the cabinet 10, thereby preventing the items from shaking slightly.

[0044] In another specific embodiment:

[0045] In this solution, the strap 30 is provided with an adsorption structure and can be adsorbed on the inner wall of the cabinet 10, wherein the inner wall of the cabinet 10 is a relatively smooth surface. Generally speaking, the adsorption structure is a suction cup, and the suction cup is installed in the middle of the strap 30, so that the strap 30 can limit the object at any position in the cabinet 10.

[0046] In another specific embodiment:

[0047] A rubber pad is provided at the bottom of the base 40. By providing the rubber pad, the base 40 and the bottom surface of the aircraft cabin have a soft buffer structure, thereby avoiding noise caused by the shaking of the aircraft and damage to the cabinet 10.

[0048] Similarly, a rubber strip is provided on the inner side of the door panel 50 .

[0049] In another specific embodiment:

[0050] In order to prevent the strap 30 from damaging the items it restricts, the strap 30 is designed as a long sheet structure, thereby increasing the contact area between the strap 30 and the items, thereby reducing the pressure between the strap 30 and the items, and achieving the purpose of protecting the items.

[0051] The above-described embodiments merely represent specific implementations of the present invention. While the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the present invention. It should be noted that a person skilled in the art would be able to make numerous variations and improvements without departing from the scope of the present invention, all of which fall within the scope of protection of the present invention.

Claims

1. An aircraft accompanying item storage cabinet, characterized in that: include: The cabinet body is an elongated structure with multiple storage areas inside. The top of each storage area is provided with multiple hooks. The cabinet body is provided with a door panel. One side of the cabinet body is provided with multiple connection holes, which match the connection parts on the aircraft fuselage. A plurality of straps are provided in the cabinet, and each storage area has at least one strap, the position of the strap in the cabinet is adjustable, and the strap has at least one free end, and the free end of the strap can be connected to the other end; The base is arranged at the bottom of the cabinet, and the circumferential dimension of the base is smaller than the circumferential dimension of the cabinet.

2. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: Each storage area corresponds to one door panel, and all the door panels are provided with a lock body.

3. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: A plurality of reinforcing ribs are respectively provided on the two side walls inside the cabinet body, and the reinforcing ribs are arranged along the length direction of the cabinet body.

4. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: The strap is movably arranged in the cabinet body and can move along the length direction of the cabinet body.

5. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: The two ends of the strap are respectively provided with a sub-surface and a main surface of a Velcro.

6. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: The strap is elastic.

7. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: The strap is provided with an adsorption structure and can be adsorbed on the inner wall of the cabinet.

8. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: A rubber pad is provided at the bottom of the base.

9. The aircraft accompanying item storage cabinet according to claim 1, characterized in that: A rubber strip is provided on the inner side of the door panel.

10. The aircraft accompanying item storage cabinet according to any one of claims 1 to 9, characterized in that: The strap is a long sheet structure.

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