The invention relates to a cluster launching wide-speed-domain variant aircraft, belongs to the technical field of wide-speed-domain aircrafts, and solves the problem that the wide-speed-domain flight capability and the cluster loading capability cannot be considered at the same time in the prior art. The invention relates to a cluster launching wide-speed-range variant aircraft, which comprises a fuselage with a structure meeting cluster loading constraint; the rotary telescopic wing is of a long structure, is operably connected to the fuselage and can be switched between a rotary folding state in which the rotary telescopic wing is rotationally folded on the fuselage and a rotary unfolding state in which the rotary telescopic wing is rotationally unfolded from the fuselage; the rotary telescopic mechanism is connected to the rotary telescopic wing and acts on the rotary telescopic wing to enable the rotary telescopic wing to be switched between a rotary folded state and a rotary unfolded state, and the aircraft can be switched between the folded state and the first unfolded state.
本发明涉及一种集群发射宽速域变体飞行器,属于宽速域飞行器技术领域,解决了现有技术中宽速域飞行能力与集群装载能力无法兼顾的问题。本发明的一种集群发射宽速域变体飞行器,包括:机身,该机身具有满足集群装载约束的结构;旋转伸缩翼,该旋转伸缩翼为长形结构,且可操作地连接至所述机身,可在旋转收拢于所述机身的旋转收拢状态与从所述机身旋转伸展开的旋转展开状态之间转换;和旋转伸缩机构,其连接至所述旋转伸缩翼且作用于所述旋转伸缩翼使其在旋转收拢状态与旋转展开状态之间的转换,其中,所述飞行器可在收起状态和第一展开状态之间转换。
Cluster launching wide-speed-range variant aircraft
一种集群发射宽速域变体飞行器
2024-08-16
Patent
Electronic Resource
Chinese
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