The invention relates to the field of aircrafts, and firstly provides a flapping wing mechanism with a suspension type gliding function. The flapping wing mechanism comprises a whole parasol wing, a front operation plane and a rear operation plane which are in bilateral symmetry, and the parasol wing comprises a front spar, a rear spar, a plurality of ribs and a wing film; the upper ends of the front operation plane and the rear operation plane are rotationally connected with the parasol wing at the front wing beam and the rear wing beam respectively; and the upper end of the front operation plane is rotationally connected with the parasol wing and then continues to extend upwards by a part. In the flying process, loads are hung below the parasol wing through the front operation plane andthe rear operation plane respectively. According to the flapping wing mechanism, the energy utilization efficiency in the flapping wing process can be further improved, and flapping wing flight with higher efficiency is realized; when the flapping wing mechanism is used as a suspension type gliding mechanism, the flapping wing mechanism has the advantages of being safer than a paraglider and lighter than a delta wing. The invention further provides a manual flapping wing aircraft applying the flapping wing mechanism. The manual flapping wing aircraft has all the advantages of the flapping wingmechanism.
本公开涉及飞行器领域,首先提供了一种具有悬挂式滑翔功能的扑翼机构,包括左右对称的一整只伞翼、前操作平面、后操作平面,伞翼包括前翼梁、后翼梁、数根翼肋和翼膜;前、后操作平面的上端分别与伞翼在前、后翼梁处转动连接,并且,前操作平面的上端与伞翼转动连接之后还继续往上延伸一部分;在飞行的过程中,载荷分别通过前、后操作平面悬挂于伞翼的下方。该扑翼机构能够进一步提高扑翼过程中的能量利用效率,实现更高效率的扑翼飞行;该扑翼机构作为悬挂式滑翔机构时具有比滑翔伞更安全、比三角翼更轻的优点。本公开还提供了一种应用该扑翼机构的人力扑翼机,其具有该扑翼机构的所有优点。
Flapping wing mechanism with suspension type gliding function and manual flapping wing aircraft
一种具有悬挂式滑翔功能的扑翼机构及人力扑翼机
2020-07-03
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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