| 摘要 |
The center of the flying vehicle / hybrid vehicle for transport on land and air is a supporting structure having a front frame section (310) and rear frame section (320) coupled to one or more cross members (330). The center of the flying vehicle has a first vertical axis (321) and a second vertical axis (322) located on the opposite ends of the section of the front frame (310).The first wing (301) is configured to rotate about a first vertical axis (321) and the second wing (302) is configured to rotate about a second vertical axis (322) in transforming the mode from air to ground mode. The center of the flying vehicle further has a first horizontal axis (314) lying in substantially parallel along the bottom section of the front frame section (310). The center of the flying vehicle is configured to pivot about a first horizontal axis (314), allowing to change the angle of inclination of flying vehicle / hybrid vehicle of transport on land and air. The center of the flying vehicle has a second horizontal rotation axis (315) lying along the bottom section of the rear frame section (320), wherein the rear frame section (320) is configured to pivot about the second horizontal axis (315) to allow engagement and disengagement of the rear frame section ( 320) of the first wing (301) and a second wing (302) during the transforming mode between the air to ground mode. The center of the flying vehicle has also a third horizontal rotation axis (316) extending along the wing trailing edge (130) enabling rotation of the little wings and the flaps and flip them on top front part of the wings and thus a reduced wing depth. |
