Adjustable fixing device for airplane water storage tank

Abstract

The utility model belongs to the technical field of aviation equipment, and discloses an adjustable fixing device for an airplane water storage tank, which comprises a bandage, a support and a nut assembly, wherein the number of the supports is two, the two supports are longitudinally installed on the same horizontal plane of the inner wall face of an airplane decorative plate or a life equipment cabinet wall plate through nut assemblies respectively, long holes are formed in the two supports at the same horizontal height, the binding belt penetrates through the two long holes and binds the water bucket, and a folding and unfolding and locking structure is arranged on the binding belt. According to the utility model, installation and fixation are realized on an airplane only through the screws and the bracket, different water tank placement requirements are met through the adjustment of the binding band after installation is completed, a large amount of manpower and time are saved for disassembly and assembly, and the water tank can be completely folded when not in use, so that the internal space of a cabin is greatly saved.

Description

Technical Field

[0001] The utility model belongs to the technical field of aviation equipment, relates to an optimization design technology for a living facility system, and specifically relates to an adjustable fixing device for an aircraft water storage tank. Background Art

[0002] At present, military transport aircraft, special aircraft, etc. will decorate and arrange living equipment in the aircraft cabin to meet the daily mission needs. In the case of long-distance flights and a large number of crew members, the water storage capacity of an electric water heater can no longer meet the crew's drinking water needs, and a separate water tank is required to meet the crew's drinking water needs.

[0003] The existing water tank placement mechanisms are all set on the floor, connected to the aircraft body, and cannot be disassembled, occupying a certain space, and the form of placing the water tank is fixed, which cannot meet the use requirements of different forms of water tanks. According to the requirements of different combat missions and flight durations, a device that can fix water tanks is needed. This device can meet the fixing requirements of water tanks of different sizes and shapes, and can be folded up when not in use, without taking up space. Utility Model Content

[0004] In order to solve the above problems, the utility model provides an adjustable fixing device for aircraft water tanks, which can quickly place the water tank and provide fixing devices for different water bucket installations.

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

[0006] An adjustable fixing device for an aircraft water tank comprises a strap, a support and a nut assembly; wherein there are two supports, which are longitudinally mounted on the same horizontal plane of the inner wall surface of an aircraft decorative panel or a wall panel of a living equipment cabinet through the nut assembly, respectively, and long holes are respectively provided at the same horizontal height of the two supports, and the strap passes through the two long holes and is used to bind a water bucket, and the strap is provided with a retractable and locking structure.

[0007] Furthermore, there are two straps, and a support is provided with two long holes at a high and a low level, and the two straps are respectively tied at the upper and lower sides of the bucket at a high and low level.

[0008] Furthermore, the interval between the two supports is no greater than the width of the bucket.

[0009] Furthermore, a shock absorbing strip is pasted between two supports on the aircraft decorative panel or the wall panel of the living equipment cabinet.

[0010] Furthermore, there are at least three shock-absorbing strips, which are respectively arranged at the upper, middle and lower positions of the corresponding bucket.

[0011] Furthermore, the bucket is provided with a handle, the handle of the bucket faces outward, and at least one strap passes through the handle of the bucket.

[0012] The beneficial effects of the utility model are as follows:

[0013] The utility model can be installed and fixed on the aircraft only by screws and brackets, and can be adjusted by straps after installation to meet different water tank placement requirements, saving a lot of manpower and time for disassembly and assembly, and can be completely folded up when not in use, greatly saving the internal space of the cabin. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] In order to more clearly illustrate the technical solution of the implementation method of the utility model patent, the following is a brief introduction to the drawings required for use in the implementation method. It should be understood that the following drawings only show certain embodiments of the utility model patent and should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without paying creative work.

[0015] Figure 1 This is a rendering of a fixed water tank device of the utility model;

[0016] Figure 2 It is the installation diagram of the fixing device of the utility model;

[0017] Figure 3 It is a schematic diagram of the utility model being quickly folded up when not in use;

[0018] Among them, 10 is a strap, 20 is a support, 30 is a nut assembly, 40 is a shock-absorbing strip, 11 is a nylon strap, 12 is a leather cover, 13 is a mesh buckle, 31 is a screw, 32 is a gasket, and 33 is a self-locking nut. DETAILED DESCRIPTION

[0019] This section is an embodiment of the utility model, which is used to explain and illustrate the technical solution of the utility model. In the absence of conflict, the embodiments of the utility model and the features in the embodiments can be combined with each other.

[0020] In the description of the present utility model, it is necessary to understand that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicating directions or positional relationships are based on the orientations or positional relationships of the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or case referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model. In addition, the terms "first", "second", etc. are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implying the number of technical features indicated. Thus, features defined as "first", "second", etc. may explicitly or implicitly include more of the features. In the description of the present utility model, unless otherwise specified, "multiple" means two or more.

[0021] In the description of the present utility model, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be interpreted in a broad sense, for example, it can be a fixed connection, a detachable connection or an integrated connection; it can be a mechanical connection or a point connection; it can be a direct connection or an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present utility model can be understood by specific circumstances.

[0022] Embodiment 1:

[0023] An adjustable fixing device for an aircraft water tank comprises a strap 10, a support 20 and a nut assembly 30; wherein, there are two supports 20, which are longitudinally mounted on the same horizontal plane of the inner wall surface of an aircraft decorative panel or a wall panel of a living equipment cabinet through the nut assembly 30, respectively, and long holes are respectively provided at the same horizontal height of the two supports 20, and the strap 10 passes through the two long holes and binds the water bucket, and the strap 10 is provided with a retractable and locking structure.

[0024] There are two straps 30, and one support 20 is provided with two long holes at a high and a low level, and the two straps are respectively tied at the upper and lower sides of the bucket at a high and low level.

[0025] The interval between the two supports 20 is no greater than the width of the bucket.

[0026] A shock absorbing strip 40 is pasted between two supports 20 of the aircraft decorative panel or the wall panel of the living equipment cabinet.

[0027] There are at least three shock-absorbing strips 40, which are respectively arranged at the upper, middle and lower positions of the corresponding bucket.

[0028] The bucket is provided with a handle, the handle of the bucket faces outwards, and at least one strap 30 passes through the handle of the bucket.

[0029] Embodiment 2:

[0030] Combination Figure 1 , install the support 20 on the side wall of the living equipment cabinet or the decorative panel through the screw and nut assembly 30; wrap the strap 10 around the front through the support 20, and stick the shock-absorbing strip 40 on the decorative panel or the wall panel of the living equipment cabinet.

[0031] Combination Figure 2 The support 20 is installed on the side wall of the living equipment cabinet or the decorative panel through screws 31, washers 32, and self-locking nuts 33.

[0032] Combination Figure 3 , Figure 3 It is a schematic diagram of the fixing device when the water tank is not folded up. After the nylon belt 11 is tightened by the mesh buckle 13, the excess belt can be stored through the leather cover 12.

[0033] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, but the protection scope of the utility model is not limited thereto. Any technician familiar with the field can easily think of various equivalent modifications or substitutions within the technical scope disclosed in the utility model, and these modifications or substitutions should be included in the protection scope of the utility model.

Claims

1. An adjustable fixing device for an aircraft water tank, characterized in that , comprising a strap (10), a support (20) and a nut assembly (30); wherein there are two supports (20), which are longitudinally mounted on the same horizontal plane of the inner wall surface of the aircraft decorative panel or the wall panel of the living equipment cabinet through the nut assembly (30), and the two supports (20) are respectively provided with long holes at the same horizontal height, and the strap (10) passes through the two long holes and is used to tie the bucket, and the strap (10) is provided with a retractable and locking structure.

2. The adjustable fixing device for an aircraft water tank according to claim 1, characterized in that There are two straps (10), and a support (20) is provided with two long holes at different heights, and the two straps are respectively tied at different heights on the upper and lower sides of the bucket.

3. The adjustable fixing device for an aircraft water tank according to claim 1, characterized in that , the interval between the two supports (20) is no greater than the width of the bucket.

4. The adjustable fixing device for an aircraft water tank according to claim 1, characterized in that A shock absorbing strip (40) is pasted between two supports (20) on an aircraft decorative panel or a wall panel of a living equipment cabinet.

5. The adjustable fixing device for an aircraft water tank according to claim 4, characterized in that There are at least three shock-absorbing strips (40), which are respectively arranged at the upper, middle and lower positions of the corresponding bucket.

6. The adjustable fixing device for an aircraft water tank according to claim 1, characterized in that The bucket is provided with a handle, the handle of the bucket faces outward, and at least one strap (10) passes through the handle of the bucket.

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