The invention discloses an aircraft and a cross-domain method thereof. The vehicle includes a vehicle body, a first hover system, and a second hover system. The vehicle body is provided with a first shell and a second shell, the first shell comprises a first section and a second section which are arranged in the first direction, and the first direction is parallel to the axial direction of the vehicle body; the second shell is arranged on one side of the first section in the second direction, and the second direction is parallel to the radial direction of the aircraft body. The first hovering system is provided with a first folding and unfolding mechanism and a first flexible bag, and the first folding and unfolding mechanism is configured to drive the first flexible bag to contract and/or be attached and unfolded along the outer bottom wall, deviating from the first shell, of the second shell. The second hovering system is arranged on the second shell and provided with a second folding and unfolding mechanism and at least two second flexible bags arranged at intervals in the first direction, and the second folding and unfolding mechanism is configured to drive the at least two second flexible bags to retract and/or unfold towards the two ends, in the first direction, of the exterior of the second shell.
本申请公开了一种航行器及其跨域方法。航行器包括航行器主体、第一垫升系统和第二垫升系统。航行器主体具有第一壳体和第二壳体,第一壳体包括沿第一方向布置的第一区段和第二区段,第一方向平行于航行器主体的轴向;第二壳体设于第一区段在第二方向上的一侧,第二方向平行于航行器主体的径向。第一垫升系统具有第一收展机构和第一柔性囊,第一收展机构被配置为驱动第一柔性囊收缩和/或沿第二壳体背离第一壳体的外底壁贴合展开。第二垫升系统设于第二壳体,且具有第二收展机构和沿第一方向间隔布置的至少两个第二柔性囊,第二收展机构被配置为驱动至少两个第二柔性囊收缩和/或分别向第二壳体外部沿第一方向的两端展开。
Aircraft and cross-domain method thereof
航行器及其跨域方法
2024-02-13
Patent
Electronic Resource
Chinese
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