The utility model relates to a composite material UAV wing with a built-in rudder, which belongs to the field of UAV. There are left rib plate and right rib plate. The upper side and the lower side of the left rib plate and the right rib plate are fitted with upper skin and lower skin. The left rib plate, the right rib plate, the upper skin and the lower skin together constitute the wing. The lower skin is processed with a rudder box hole. The rudder box hole is equipped with a rudder box. The rudder box is fixed in the rudder box. The port of the rudder box is equipped with a rudder box cover, and the outer surface of the rudder box cover is equipped with a rudder box cover. The curvature of the outer surface of the lower skin is the same. The inner side of the wing is machined with long aileron groove. The aileron groove is equipped with aileron. The aileron and the wing are hinged together by narrow band of aramid fabric. The steering box installed in the aileron is hinged with the telescopic rod of the rudder. The inner side of the wing is transversely fixed with the main girder tube of the wing. The inner side of the wing girder tube is inserted with the main girder of the fuselage, and the inner side of the wing is There is a steering wheel thread through pipe, and the servo line is connected with the steering gear box. The right rib plate is fixed with a locating pin, and the inner cavity of the wing between the lower skin and the upper skin is filled with foam core material.
【技术实现步骤摘要】
内置舵机式复合材料无人机机翼
本技术属于无人机领域,具体地说是一种内置舵机式复合材料无人机机翼。
技术介绍
目前,随着无人机飞控航电系统的发展,无人机正处在飞速发展的阶段,应用领域也越来越广泛。电动无人机具有操作简单、环保节能的特点深受市场青睐,但是由于短时间内无法对电池的能量密度有革命性的突破,那么增加启动效率优化机体结构对提高续航时间来说就显得尤为重要。目前小型固定翼无人机的副翼舵机多采用拉杆式结构,势必会在机翼上留出一块凸起的拉杆控制结构,不但影响外观还严重影响气动效率,造成不必要的能量消耗。
技术实现思路
为了克服现有技术的不足,本技术提供一种内置舵机式复合材料无人机机翼,可以有效提高机翼的气动效率,增加续航时间。本技术解决其技术问题所采用的技术方案是:一种内置舵机式复合材料无人机机翼,设有左肋板及右肋板,其特征在于,左肋板与右肋板的上侧面及下侧面贴合有上蒙皮及下蒙皮,左肋板、右肋板、上蒙皮及下蒙皮共同组成了机翼,下蒙皮上加工有舵机盒孔,舵机盒孔内安装有舵机盒,舵机盒内固定有舵机,舵机盒的端口安装有舵机盒盖,舵机盒盖的外表面与下蒙皮的外表面曲率一致,机翼内侧加工有长条式副翼槽,副翼槽内安装有副翼,副翼与机翼之间经芳纶织物窄带铰连在一起,副翼内安装的转向盒与舵机的伸缩杆相铰连,机翼内部横向固定有机翼主梁管,机翼主梁管内插装有机身连接主梁,机翼内部横向还安装有舵机穿线管,舵机穿线管与舵机盒相连通,右肋板上固定有定位销,下蒙皮与上蒙皮之间的机翼内腔中填充有泡沫芯材。本技术具的有益效果是,整套的舵机控制结构内置在机翼内部,机翼表面光滑平整无任何凹凸机构,可以有 ...
【技术保护点】
1.一种内置舵机式复合材料无人机机翼,设有左肋板及右肋板,其特征在于,左肋板与右肋板的上侧面及下侧面贴合有上蒙皮及下蒙皮,左肋板、右肋板、上蒙皮及下蒙皮共同组成了机翼,下蒙皮上加工有舵机盒孔,舵机盒孔内安装有舵机盒,舵机盒内固定有舵机,舵机盒的端口安装有舵机盒盖,舵机盒盖的外表面与下蒙皮的外表面曲率一致,机翼内侧加工有长条式副翼槽,副翼槽内安装有副翼,副翼与机翼之间经芳纶织物窄带铰连在一起,副翼内安装的转向盒与舵机的伸缩杆相铰连,机翼内部横向固定有机翼主梁管,机翼主梁管内插装有机身连接主梁,机翼内部横向还安装有舵机穿线管,舵机穿线管与舵机盒相连通,右肋板上固定有定位销,下蒙皮与上蒙皮之间的机翼内腔中填充有泡沫芯材。
【技术特征摘要】
1.一种内置舵机式复合材料无人机机翼,设有左肋板及右肋板,其特征在于,左肋板与右肋板的上侧面及下侧面贴合有上蒙皮及下蒙皮,左肋板、右肋板、上蒙皮及下蒙皮共同组成了机翼,下蒙皮上加工有舵机盒孔,舵机盒孔内安装有舵机盒,舵机盒内固定有舵机,舵机盒的端口安装有舵机盒盖,舵机盒盖的外表面与下蒙皮的外表面曲率一致,机翼...
【专利技术属性】
技术研发人员:朱有欣,王玉琳,杨帅,邱新旺,
申请(专利权)人:山东光威碳纤维产业技术研究院有限公司,
类型:新型
国别省市:山东,37
还没有人留言评论。发表了对其他浏览者有用的留言会获得科技券。