Unmanned aerial vehicle model airplane heating film with multi-layer composite structure

The drone model heating film, designed with a multi-layer composite structure, solves the problem of uneven heating, achieves uniform heat distribution, and ensures stable operation and safety of the drone in low-temperature environments.

CN223772174UActive Publication Date: 2026-01-06DONGGUAN ANHUA ELECTRIC HEATING TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202520101391.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-01-16
Publication Date
2026-01-06
Estimated Expiration
2035-01-16

AI Technical Summary

Technical Problem

Existing heating films for drones and model aircraft suffer from uneven heating, leading to localized overheating or insufficient heating.

Method used

It adopts a multi-layer composite structure design, including a heating film, an insulating layer, a protective layer and an adhesive layer. Heating elements are evenly distributed on the insulating layer, and the protective layer has grooves and protrusions. Through precise circuit design, the current is evenly distributed, ensuring uniform heat transfer.

Benefits of technology

This achieves overall heating uniformity of the heating film, avoiding localized overheating or underheating, and ensuring the performance and safety of the drone in low-temperature environments.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses an unmanned aerial vehicle model airplane heating film with a multi-layer composite structure, and aims to solve the problem of uneven heating. The heating film is composed of a heating film body, an insulating layer and a protective layer, heating elements are evenly distributed on the insulating layer and correspond to grooves in the heating film body and the protective layer, and it is guaranteed that heat is evenly distributed. And bonding layers are laid on one side, deviating from the insulating layer, of the heating film and in the groove, so that the adhesion is enhanced. The heating element is made of a high-performance conductive material, the thickness of the heating element is larger than that of the insulating layer, the protective layer is a silica gel soft layer and has good flexibility and heat resistance, and water guide grooves are formed between the convex rods on the outer surface to facilitate drainage. Metal foil is arranged in the heating film, and the insulating layer is made of a polymer material, so that thermal conductivity, insulativity and durability are ensured. The heating elements are electrically connected to form uniform current distribution, so that the heating efficiency is improved. According to the design, comprehensive guarantee of heating uniformity, durability, insulativity and adhesion is provided for stable operation of the unmanned aerial vehicle or the model airplane in various environments.
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Description

Technical Field

[0001] This utility model provides a multi-layer composite structure heating film for drone model aircraft, belonging to the field of drone model aircraft technology, and particularly relates to a multi-layer composite structure heating film for drone model aircraft. Background Technology

[0002] Drone / model aircraft heating film is a flexible conductive material used on drones or model aircraft. It generates heat by passing electricity to keep the temperature of the drone's battery and key components in low-temperature environments, ensuring flight performance and equipment safety. This heating film is usually composed of conductive materials, an insulating layer, and heat-resistant materials, and can be flexibly attached to the surface of the drone to provide effective thermal protection.

[0003] Existing heating film structures for drones and model aircraft typically consist of an inner PI heating film, a middle insulation layer, and an outer waterproof layer, forming a battery insulation shell structure. This structure has a battery mounting slot in the middle and a built-in temperature acquisition module, with a control unit on one side. Both the temperature acquisition module and the PI heating film are connected to the control unit. However, the heat from this structure is concentrated in certain areas, causing localized overheating or uneven heating. Utility Model Content

[0004] In order to overcome the shortcomings of the prior art, this application provides a multi-layer composite structure heating film for drone models, which solves the problem of uneven heating in existing heating films.

[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a multi-layer composite structure heating film for unmanned aerial vehicle models, including a heating film, an insulating layer laid on the top of the heating film, and a protective layer corresponding to the other side of the insulating layer;

[0006] The insulating layer is provided with a number of uniformly distributed heating elements that penetrate through it, and the heating film and protective layer are provided with grooves corresponding to the heating elements on the side close to the insulating layer.

[0007] Preferably, an adhesive layer is laid on the side of the heating film away from the insulating layer and inside the groove.

[0008] Preferably, the heating elements are electrically connected to each other, and the thickness of the heating elements is greater than the thickness of the insulation layer.

[0009] Preferably, the outer surface of the protective layer is provided with a plurality of evenly distributed protrusions, and water guide grooves are formed between the protrusions.

[0010] Preferably, the heating film contains a metal foil, the insulating layer is a polymer material, and the protective layer is a silicone soft layer.

[0011] One or more technical solutions provided in the embodiments of this application have at least the following technical effects or advantages:

[0012] This invention features an insulating layer laid on top of a heating film, with a protective layer on the opposite side of the insulating layer. Several heating elements are evenly distributed throughout the insulating layer, ensuring uniform heat transfer across the entire heating film. Additionally, grooves corresponding to the heating elements are provided on the side of the heating film and protective layer closest to the insulating layer. These grooves facilitate even heat distribution and conduction, improving the overall heating uniformity of the heating film. This structural design allows the heating film to more effectively transfer heat to all parts of the drone model during operation, avoiding localized overheating or underheating, and ensuring the performance and safety of the drone model in low-temperature environments.

[0013] Other advantages, objectives and features of this invention will be set forth in part in the description which follows, and in part will be apparent to those skilled in the art from the following examination or study, or may be taught from the practice of this invention. Attached Figure Description

[0014] Figure 1 This is a three-dimensional schematic diagram of a multi-layer composite heating film for unmanned aerial vehicle (UAV) models according to the present invention.

[0015] Figure 2 This is a three-dimensional schematic diagram from another perspective of the multi-layer composite structure heating film for UAV model aircraft according to this utility model;

[0016] Figure 3 This is an exploded view of a multi-layer composite heating film for UAV model aircraft according to the present invention.

[0017] Figure 4 This is a three-dimensional schematic diagram of the insulating layer of a multi-layer composite heating film for unmanned aerial vehicle (UAV) models according to this utility model.

[0018] As shown in the figure:

[0019] 1. Heating film; 2. Insulating layer; 3. Protective layer; 4. Heating element; 5. Groove; 6. Adhesive layer; 7. Protruding rod. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] It should be noted that the terms "vertical," "horizontal," "up," "down," "left," "right," and similar expressions used in this article are for illustrative purposes only and do not represent the only possible implementation.

[0022] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains; the terminology used herein in the description of this invention is for the purpose of describing particular embodiments only and is not intended to limit the invention; the term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0023] like Figure 1 and Figure 2 As shown, a multi-layer composite heating film for drones or model aircraft includes a heating film 1, an insulating layer 2 on top of the heating film 1, and a protective layer 3 on the other side of the insulating layer 2. The insulating layer 2 has several evenly distributed heating elements 4 that penetrate it. Grooves 5 corresponding to the heating elements 4 are provided on the side of the heating film 1 and the protective layer 3 closest to the insulating layer 2. Furthermore, an adhesive layer 6 is laid on the side of the heating film 1 away from the insulating layer 2 and inside the grooves 5 to enhance the adhesion of the heating film to the surface of the drone or model aircraft.

[0024] In this embodiment, the heating element 4 is made of high-performance conductive material, ensuring heating efficiency and stability. Simultaneously, the thickness of the heating element 4 is carefully designed to be greater than the thickness of the insulation layer 2, thus guaranteeing not only the mechanical strength of the heating element 4 but also contributing to the overall durability of the heating film 1. The protective layer 3 is made of a soft silicone layer, a material with good flexibility and heat resistance, capable of protecting the heating element 4 from damage in various environments. Furthermore, the outer surface of the protective layer 3 has several evenly distributed protrusions 7, forming water-guiding grooves between these protrusions 7, facilitating rapid drainage in humid environments and further protecting the heating film 1 from moisture erosion. To further improve the heating uniformity of the heating film 1, the heating elements 4 are electrically connected to form a uniform current distribution, ensuring consistent heating performance across the entire heating film 1. The adhesive layer 6 is selected considering the different materials of the drone or model aircraft surface, ensuring that the heating film 1 can firmly adhere to various surfaces, maintaining stability during high-speed flight or complex maneuvers.

[0025] like Figure 3 and Figure 4As shown, the heating elements 4 are electrically connected, and the thickness of the heating elements 4 is greater than the thickness of the insulating layer 2 to ensure heating effect. Several evenly distributed protrusions 7 are provided on the outer surface of the protective layer 3, forming water-guiding grooves between the protrusions 7, which facilitates drainage and protects the heating film. The heating film 1 contains a metal foil, the insulating layer 2 is made of polymer material, and the protective layer 3 is a soft silicone layer. These materials are chosen to provide good thermal conductivity, insulation, and durability.

[0026] In this embodiment, the electrical connection of the heating element 4 is achieved through precise circuit design, ensuring that current flows evenly through each heating element, thereby generating a uniform heat distribution across the entire heating film 1. This design avoids heat concentration in certain areas, reducing the risk of localized overheating and improving heating efficiency. The protruding rod 7 not only aids in drainage but also increases the mechanical strength of the protective layer 3 to a certain extent, making it more resistant to wear and impact. The water channel design allows moisture to drain quickly from the surface of the heating film in rainy or humid environments, reducing the impact of moisture on the performance of the heating film. The metal foil placed inside the heating film 1 provides an efficient heat conduction path, further enhancing the heating performance of the heating film. The insulating layer 2, made of polymer material, not only has good insulation properties but also sufficient flexibility to adapt to the surfaces of drones or model aircraft of different shapes. The silicone soft layer, as the protective layer 3, provides physical protection and also has good temperature and weather resistance, ensuring stable performance even under extreme temperature changes. Furthermore, the addition of adhesive layer 6 ensures that the heating film 1 can firmly adhere to the surface of the drone or model aircraft, maintaining stability even during high-speed flight or violent maneuvers, without displacement or detachment. This multi-layered composite structure design comprehensively considers the heating uniformity, durability, insulation, and adhesion of the heating film, providing strong support for the stable operation of drones or model aircraft in various environments.

[0027] In use, the heating film 1 serves as the core heating element. The insulating layer 2 above it not only provides necessary electrical isolation but also acts as a carrier for the heating elements 4, ensuring their uniform distribution. These heating elements 4 are made of high-performance conductive materials and are thicker than the insulating layer 2 to enhance mechanical strength and improve durability. The electrical connections between the heating elements 4 are achieved through a precise circuit design, ensuring uniform current distribution and generating uniform heat across the entire heating film 1, avoiding localized overheating and improving heating efficiency. The protective layer 3 is composed of a soft silicone layer with good flexibility and heat resistance, protecting the heating elements 4 from physical damage. The protruding rods 7 and water-guiding grooves on its outer surface facilitate rapid drainage in humid environments, reducing the impact of moisture on the heating film's performance. The metal foil within the heating film 1 provides an efficient heat conduction path, further enhancing heating performance. The insulating layer 2 is made of polymer materials with excellent insulation properties and flexibility, adapting to the surfaces of drones or model aircraft of different shapes. The adhesive layer 6 ensures that the heating film 1 adheres firmly to the surface of the drone or model aircraft, maintaining stability even during high-speed flight or complex maneuvers.

[0028] This multi-layered composite structure design comprehensively considers the heating uniformity, durability, insulation, and adhesion of the heating film, providing strong support for the stable operation of drones or model aircraft in various environments. It ensures the temperature of the battery and key components in low-temperature environments, thereby guaranteeing flight performance and equipment safety.

[0029] Although the present invention has been disclosed above with reference to preferred embodiments, it is not intended to limit the present invention. Any person skilled in the art can make various modifications and alterations without departing from the spirit and scope of the present invention. Therefore, the scope of protection of the present invention should be determined by the claims.

Claims

1. A multi-layer composite structure of a drone model aircraft heating film, comprising a heating film (1), characterized in that: The heating film (1) is laid with a corresponding insulation layer (2) on the top, and the other side of the insulation layer (2) is provided with a protective layer (3) correspondingly; A plurality of heating elements (4) are arranged on the insulation layer (2) and are uniformly distributed and penetrate the insulation layer (2), and the heating film (1) and the protective layer (3) are provided with grooves (5) corresponding to the heating elements (4) on the side close to the insulation layer (2).

2. The multi-layer composite drone hobbyist heating film of claim 1, wherein: The side of the heating film (1) away from the insulation layer (2) and the inside of the groove (5) are laid with an adhesive layer (6).

3. The multi-layer composite drone hobbyist heating film of claim 1, wherein: The heating elements (4) are electrically connected, and the thickness of the heating element (4) is greater than the thickness of the insulation layer (2).

4. The multi-layer composite drone hobbyist heating film of claim 1, wherein: The outer surface of the protective layer (3) is provided with a plurality of uniformly distributed convex rods (7), and the convex rods (7) form a water guide groove.

5. The multi-layer composite drone hobbyist heating film of claim 1, wherein: The heating film (1) is provided with a metal foil, the insulation layer (2) is a polymer material, and the protective layer (3) is a soft silicone layer.