发明名称 Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself
摘要 Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and reciprocal steps: Tilting the compensation cover (7) on. Expansion of both whole wings (1) from the transportation vehicle longitudinal position around two vertical axes (2) into the flying position. Expansion of rear parts of wings (1) from the top front parts of wings (1) into the spread flying position by tilting the rear of each wing (1) around a horizontal axis (3). The take-off and landing tilting of wings (1) by an angle of attack alpha=0 to 40° of the wings onset. Front wheels track (5) is reduced by axially shifting the front wheels (5) towards the fuselage. Furthermore, a corresponding hybrid transportation vehicle for ground and air is described which contains reciprocal transformation mechanisms for transformation from a sterling double or four-track automobile into a sterling aircraft for take-off and landing on the ground or water, and vice versa.
申请公布号 US9555681(B2) 申请公布日期 2017.01.31
申请号 US201214241239 申请日期 2012.08.22
申请人 AEROMOBIL, S.R.O. 发明人 Klein {hacek over (S)}tefan
分类号 B60F5/02;B64C3/56;B64C37/00;B60F5/00;B64C3/38;B64C3/54;B64C25/04;B64C25/54;B64C25/00 主分类号 B60F5/02
代理机构 Finnegan, Henderson, Farabow, Garrett & Dunner LLP. 代理人 Finnegan, Henderson, Farabow, Garrett & Dunner LLP.
主权项 1. A hybrid transportation vehicle for ground and air comprising a body, a cabin, a set of retractable wings, a chassis and a driving unit that switches a torque transfer between a propeller situated at the rear of the vehicle and a pair of driven wheels, the vehicle containing a plurality of reciprocal transformation mechanisms for transformation of the vehicle into an automobile or into an aircraft for take-off and landing on the ground or water, where two first reciprocal transformation mechanisms for retraction and expansion of the wings from or to a flying position are situated in the middle of the body; and wherein, each first reciprocal transformation mechanism contains an actuator and a vertical axis for retraction and expansion of the wing by rotating around the vertical axis between the flying position in which an axis of the wing is approximately perpendicular to a longitudinal axis of the vehicle, and a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle;two second reciprocal transformation mechanisms for changing the platform outline of the wings, each being situated separately in a wing body and each containing a horizontal axis that extends along the wing body and an actuator, for tilting a rear part of each wing onto a top front part of the wing; andthe pair of driven wheels are front wheels, and a third reciprocal transformation mechanism contains an actuator for changing a track of the front driven wheels situated in the front of the body.
地址 Bratislava SK