A heat preservation device for drone flight remote controllers in high-altitude and cold regions

Abstract

This utility model discloses a heat preservation device for a drone flight remote controller in cold regions, relating to the field of drone flight technology. The utility model includes a protective cotton cover with a transparent cover installed at the upper center. Insertion components are installed on both sides of one end of the outer wall of the protective cotton cover. When using the flight remote controller in cold regions, the operator can directly place the remote controller into the inner cavity of the protective cotton cover through the insertion slot. By attaching the female Velcro to one side of the female Velcro, the sealing cover blocks the insertion slot. The operator inserts their hand through the inner cavity of the insertion components. An anti-fog sheet is placed in the inner cavity of the mesh bag beforehand. The use of the anti-fog sheet allows the operator to still operate the remote controller through the transparent cover even when the temperature inside the protective cotton cover rises. The protective cotton cover effectively warms the operator's hands while allowing the operator to directly operate the remote controller without affecting operational flexibility.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) flight technology, specifically, to a heat preservation device for a UAV flight remote controller in cold regions. Background Technology

[0002] Unmanned aerial vehicles (UAVs), also known as drones, are unmanned aircraft controlled by radio remote control equipment and their own program control devices. Radio remote control refers to the non-contact remote control of the controlled target. Currently, UAVs are controlled by flight remote controllers.

[0003] Currently, when using drones in winter or in cold regions, operators need to hold a remote control to control the drone's flight. Due to the low temperatures in cold regions during winter, winter gloves are usually thick to keep warm, which makes it difficult for operators to operate the remote control while wearing gloves.

[0004] Therefore, we propose a heat preservation device for drone flight remote controllers in high-altitude and cold regions to solve the problems mentioned above. Utility Model Content

[0005] The purpose of this utility model is to provide a heat preservation device for a drone flight remote controller in cold regions, in order to solve the problem mentioned in the background art that when using a drone in winter or in cold regions, the operator needs to hold the flight remote controller to control the drone's flight. Because the temperature is low in cold regions in winter, winter gloves are usually thick for warmth, which leads to poor flexibility for the operator when using the remote controller while wearing gloves.

[0006] To solve the above problems, the present invention adopts the following technical means: A heat preservation device for a drone flight remote controller in cold regions includes a protective cotton cover. A transparent cover is installed at the middle of the upper end of the protective cotton cover. Slip-on components are installed on both sides of one end of the outer wall of the protective cotton cover. The slip-on components are designed to be fitted and fixed at the wrist position. Suspension components are installed on both sides of the outer wall of the protective cotton cover. The suspension components are designed to be hung around the neck when the protective cotton cover is not in use.

[0007] An inlet groove is provided at the middle of one end of the outer wall of the protective cotton cover, and a sealing cover is fixedly installed at the lower end of the inlet groove.

[0008] The inner wall of the protective cotton cover has square pockets on both sides in the middle, and the inner wall of the cover is sewn with a female Velcro closure. The upper end of the groove opening is sewn with a female Velcro closure.

[0009] The inner wall of the protective cotton cover has grooves on both sides of the middle of one end, and mesh bags are installed on both sides of the middle of the upper end of the inner wall of the protective cotton cover.

[0010] The fitting assembly includes a cotton ring tube and connecting grooves on both sides of the upper end of the outer wall of the cotton ring tube, with a binding strap inserted into the inner cavity of the connecting groove.

[0011] The suspension assembly includes a long rope and hooks fixedly installed at both ends of the long rope.

[0012] This utility model has the following beneficial effects during use: When using the flight remote controller in high-altitude and cold regions, the operator can directly place the remote controller into the inner cavity of the protective cotton cover through the inlet slot. By attaching the female Velcro to one side of the female Velcro, the sealing cover blocks the inlet slot. The operator then inserts their hand through the inner cavity of the fitting assembly. An anti-fog pad is placed in the inner cavity of the mesh bag beforehand. The use of the anti-fog pad ensures that even when the temperature inside the protective cotton cover rises, the operator can still operate the remote controller through the transparent cover. The protective cotton cover keeps the operator's hands warm, while allowing the operator to operate the remote controller directly with their hands without affecting operational flexibility.

[0013] When the operator puts their hand through the cotton ring tube, they can tighten and knot the straps to improve the stability of the cotton ring tube and protective cotton cover on their hand. The operator can also hang the hook on the loop-shaped straps on both sides of the outer wall of the protective cotton cover and then hang the long rope around their neck to place the remote control when their hand is not operating it.

[0014] This new invention patent can improve the safety of drone operation in high-altitude and cold regions, reduce operator errors in low-temperature conditions that could lead to aircraft malfunctions and other problems, and effectively improve the safety of drone operation. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the overall three-dimensional structure of this utility model.

[0016] Figure 2 For the present utility model Figure 1 Enlarged view of point A.

[0017] Figure 3 This is a three-dimensional structural diagram of the fitting component of this utility model.

[0018] Figure 4 For the present utility model Figure 3 Enlarged view of point B.

[0019] Among them, 1-protective cotton cover, 11-entry groove, 12-sealing cover, 15-square pocket, 13-female hook and loop fastener, 14-female hook and loop fastener, 16-thread groove, 17-mesh bag, 2-transparent cover, 3-insertion assembly, 31-cotton ring tube, 32-connecting groove, 33-strap, 4-suspension assembly, 41-long rope, 42-hook. Detailed Implementation

[0020] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can typically be arranged and designed in various different configurations.

[0021] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.

[0022] It should be noted that, where there is no conflict, the embodiments and features in the embodiments of this utility model can be combined with each other.

[0023] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0024] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product of this utility model is in use, or the orientation or positional relationship commonly understood by those skilled in the art. They are only used for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first," "second," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0025] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0026] Please refer to Figures 1 to 4 As shown, a heat preservation device for a drone flight remote controller in cold regions includes a protective cotton cover 1, a transparent cover 2 installed at the upper middle part of the protective cotton cover 1, and two fitting components 3 installed on both sides of one end of the outer wall of the protective cotton cover 1. The fitting components 3 are designed to fit and fix the wrist position. Two suspension components 4 are fitted on both sides of the outer wall of the protective cotton cover 1. The suspension components 4 are designed to hang on the neck when the protective cotton cover 1 is not in use.

[0027] The outer wall of the protective cotton cover 1 has an inlet groove 11 in the middle of one end. A sealing cover 12 is fixedly installed at the lower end of the groove opening of the inlet groove 11. A male Velcro 13 is sewn on one side of the inner wall of the sealing cover 12. A female Velcro 14 is sewn on the upper end of the groove opening of the inlet groove 11. The sealing cover 12 blocks the inlet groove 11 by connecting the male Velcro 13 and the female Velcro 14.

[0028] The inner wall of the protective cotton cover 1 has square pockets 15 on both sides of the middle section. The square pockets 15 are designed to hold hand warmers to increase the internal temperature of the protective cotton cover 1. The hand warmers can be purchased from the market.

[0029] The inner wall of the protective cotton cover 1 has wire grooves 16 on both sides of the middle of one end. The upper middle of the inner wall of the protective cotton cover 1 has mesh bags 17 on both sides. The wire grooves 16 are designed to allow the antenna of the flight remote controller to pass through. The mesh bags 17 are set on both sides of the lower end of the transparent cover 2. By placing anti-fog sheets in the inner cavity of the mesh bags 17, the transparent cover 2 is prevented from fogging. The anti-fog sheets can be purchased and used directly from the market.

[0030] In this embodiment: When the operator uses the flight remote controller in a cold region, the remote controller can be directly placed into the inner cavity of the protective cotton cover 1 through the slot 11. By attaching the female Velcro 13 to one side of the female Velcro 14, the sealing cover 12 can block the slot 11. The operator inserts their hand through the inner cavity of the fitting component 3. An anti-fog sheet is placed in the inner cavity of the mesh bag 17 in advance. The use of the anti-fog sheet allows the operator to still operate the remote controller through the transparent cover 2 even when the temperature inside the inner cavity of the protective cotton cover 1 rises. The protective cotton cover 1 keeps the operator's hands warm, and the operator can directly operate the remote controller with their hands without affecting the flexibility of operation.

[0031] For further details, please refer to Figure 3 The fitting component 3 includes a cotton loop tube 31 and a connecting groove 32 opened on both sides of the upper end of the outer wall of the cotton loop tube 31. A strap 33 is inserted into the inner cavity of the connecting groove 32. The strap 33 is designed to bind the cuff of the cotton loop tube 31 to improve the stability of wearing the cotton loop tube 31.

[0032] The suspension assembly 4 includes a long rope 41 and hooks 42 that are respectively fixedly installed at both ends of the long rope 41.

[0033] In this embodiment: when the operator puts his hand through the cotton ring tube 31, he can tighten and knot the strap 33 to improve the stability of the operator's hand wearing the cotton ring tube 31 and the protective cotton cover 1. He can hang the hook 42 on the loop-shaped hanging strap in the middle of the outer wall of the protective cotton cover 1, and then hang the long rope 41 around his neck. This allows the remote control to be placed when the hands are not operating the remote control.

[0034] Working principle: When using the flight remote controller in cold regions, the operator can directly place the remote controller into the inner cavity of the protective cotton cover 1 through the slot 11. By attaching the female Velcro 13 to one side of the female Velcro 14, the sealing cover 12 blocks the slot 11. The operator inserts their hand through the inner cavity of the fitting component 3. By tightening and knotting the strap 33, the stability of the operator's hand wearing the cotton ring tube 31 and the protective cotton cover 1 can be improved. The hook 42 can be hung on the loop straps on both sides of the outer wall of the protective cotton cover 1, and the long rope 41 can be hung around the neck. This allows the remote controller to be placed even when the hands are not operating it. An anti-fog film is placed in the inner cavity of the mesh bag 17 in advance. The use of the anti-fog film allows the operator to still operate the remote controller through the transparent cover 2 even when the temperature inside the protective cotton cover 1 rises. The protective cotton cover 1 keeps the operator's hands warm and allows the operator to directly operate the remote controller.

[0035] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.

Claims

1. A high-cold-region unmanned aerial vehicle flight remote controller heat preservation device, comprising a protective cotton cover (1), characterized in that: A transparent cover (2) is installed at the middle of the upper end of the protective cotton cover (1). A fitting component (3) is installed on both sides of one end of the outer wall of the protective cotton cover (1). The fitting component (3) is designed to fit and fix the wrist position. A suspension component (4) is fitted on both sides of the outer wall of the protective cotton cover (1). ​ 2. The high-cold region unmanned aerial vehicle flight remote controller heat preservation device according to claim 1, characterized in that: The outer wall of the protective cotton cover (1) has an entry groove (11) at the middle of one end, and a sealing cover (12) is fixedly installed at the lower end of the groove opening of the entry groove (11).

3. The high-cold region unmanned aerial vehicle flight remote controller heat preservation device according to claim 2, characterized in that: The inner wall of the protective cotton cover (1) is provided with square pockets (15) on both sides of the middle section, and the inner wall of the cover (12) is sewn with a female Velcro (13) and the upper end of the groove opening of the groove (11) is sewn with a female Velcro (14).

4. The high-cold region unmanned aerial vehicle flight remote controller heat preservation device according to claim 3, characterized in that: The inner wall of the protective cotton cover (1) has a thread groove (16) on both sides of the middle part of one end, and a mesh bag (17) is installed on both sides of the middle part of the upper end of the inner wall of the protective cotton cover (1).

5. The heat preservation device for a UAV flight remote controller in cold regions according to claim 4, characterized in that: The fitting assembly (3) includes a cotton ring tube (31) and a connecting groove (32) on both sides of the upper end of the outer wall of the cotton ring tube (31). A binding strap (33) is inserted into the inner cavity of the connecting groove (32).

6. The high-cold region unmanned aerial vehicle flight remote controller heat preservation device according to claim 5, characterized in that: The suspension assembly (4) includes a long rope (41) and hooks (42) fixedly installed at both ends of the long rope (41).

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