KT-1无人机用低空螺旋桨三维模型（2020）

该模型为KT-1临近空间太阳能无人机用低空螺旋桨几何外形，针对无人机的低空爬升状态进行设计，同时兼顾其在不同高度的巡航性能。该螺旋桨为拉力桨，每架飞机配备两付拉力桨，且螺旋桨采用正反桨的设计方式，从无人机的机尾向机头看，左侧桨顺时针转动，右侧桨逆时针转动。螺旋桨桨径2.0米， 5km高度爬升状态拉力174.2N。（协议共享）

This model corresponds to the geometric profile of the low-altitude propeller for the KT-1 near-space solar-powered unmanned aerial vehicle (UAV). It is optimized for the low-altitude climb phase of the UAV, while also balancing its cruise performance across different altitudes. This propeller is a thrust propeller, and each aircraft is equipped with two such propellers adopting a counter-rotating configuration. When viewed from the tail towards the nose of the UAV, the left propeller rotates clockwise while the right one rotates counterclockwise. The propeller has a diameter of 2.0 meters, and its thrust reaches 174.2 N during the climb phase at an altitude of 5 km. (Shared under agreement)

搜集汇总

背景与挑战

背景概述

该数据集包含KT-1太阳能无人机低空螺旋桨的三维几何模型，专为无人机低空爬升状态设计，兼顾不同高度巡航性能。螺旋桨采用张力设计，每架飞机配备两对，直径2.0米，5公里高度爬升力为174.2N。