一种耐高温抗振动的无人机动力线束组件

Abstract

本专利公开了一种耐高温抗振动的无人机动力线束组件，包括线束本体，线束本体的线体上左右两侧均设有螺旋部，线束本体的左右两端均固定安装有安装件，本专利通过在线束本体的强振动源连接部位设置5cm‑8cm的螺旋部缓冲段，利用螺旋结构的伸缩回弹特性(类似电话连接线的缓冲设计)，通过线束自然弯曲吸收振动能量，避免振动导致的刚性拉扯，有效解决了振动环境下线束易损坏的问题，镀镍层提升耐高温性(耐温达300℃以上)，解决高温氧化问题；无氧铜确保高导电性(导电率≥98％IACS)，满足动力传输需求；同时采用7股 / 19股绞合设计，增强导体柔韧性，提升抗振动疲劳能力(单股线径0.3mm‑0.8mm适配载流量)，全面解决了传统导体的性能缺陷。

Claims

1. A high-temperature-resistant and anti-vibration power wire harness assembly for a drone, characterized by: Includes a wire harness body (1), wherein the wire harness body (1) has a spiral part (2) on both the left and right sides of the wire body, and mounting parts (3) are fixedly installed at both the left and right ends of the wire harness body (1). The wire harness body (1) includes an oxygen-free copper core (4), a nickel plating layer (5) is fixedly installed on the outside of the oxygen-free copper core (4), a silicone rubber insulation layer (6) is fixedly installed on the outside of the nickel plating layer (5), and a protective reinforcement layer (7) is fixedly installed on the outside of the silicone rubber insulation layer (6). The protective reinforcement layer (7) includes an aramid braided layer (8) and a glass fiber tape layer (9). The aramid braided layer (8) is fixedly installed on the outer side wall of the silicone rubber insulation layer (6), and the glass fiber tape layer (9) is fixedly installed on the outer side wall of the aramid braided layer (8).

2. The high-temperature resistant and anti-vibration power wire harness assembly of claim 1, wherein: The mounting component (3) includes a fixed base (10) and a conductive ring (12). A threaded post (11) is integrally formed in the middle of the left side of the fixed base (10). The right side of the conductive ring (12) is attached to the left side of the fixed base (10). A pressure ring (14) is attached to the left side of the conductive ring (12). A nut (13) is screwed to the left end of the threaded post (11). The right side of the nut (13) is tightly attached to the left side of the pressure ring (14). Limiting components are provided at both the upper and lower ends of the inner sidewall of the pressure ring (14).

3. The high-temperature resistant and anti-vibration power wire harness assembly of claim 2, wherein: The limiting component includes a slider (15), which is integrally formed on the inner side wall of the pressure ring (14). The left side wall of the threaded column (11) is provided with grooves (16) on both the upper and lower sides. The slider (15) is slidably installed in the grooves (16).

4. The high-temperature resistant and anti-vibration power wire harness assembly of claim 2, wherein: The inner wall of the pressure ring (14) does not make thread contact with the side wall of the threaded column (11).

5. The high-temperature resistant and anti-vibration power wire harness assembly of claim 2, wherein: The outer side wall of the pressure ring (14) is provided with an annular groove (17), and an annular ring (18) is rotatably installed in the annular groove (17). A connecting ring (19) is fixedly installed on the outer side wall of the annular ring (18), and the left side of the inner side wall of the connecting ring (19) is fixedly installed on the outer side wall of the nut (13).

6. The high-temperature resistant and anti-vibration power wire harness assembly of claim 5, wherein: The ring (18) includes a first half-ring (20) and a second half-ring (21), the two ends of the first half-ring (20) and the second half-ring (21) are fixed together, and the outer sidewalls of the first half-ring (20) and the second half-ring (21) are fixed to the inner sidewall of the connecting ring (19).

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