Transformation method of hybrid transportation vehicle for ground and air, and hybrid transportation vehicle itself

A hybrid transportation vehicle for ground and air comprising a body, cabin, retractable wings, chassis and driving unit with switching of the torque transfer between a propeller situated at the rear of the vehicle and driven wheels, the vehicle containing reciprocal transformation mechanisms for transformation into a sterling double or four-track automobile or into a sterling aircraft for take-off and landing on the ground or water,

• where one or two first reciprocal transformation mechanisms for wings retraction and expansion of the wings (1) from or to a flying position are situated in the middle of the body (4);
• and wherein,
• each first reciprocal transformation mechanism contains a first actuator and a vertical axis (2) for refraction and expansion of the wing (1) by tilting around the vertical axis between a flying position in which the axis of the wing is approximately perpendicular to the 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 (1) and each containing a horizontal axis (3) of the wing and a second actuator, for tilting the rear part of each wing (1) onto the top front part of the wing (1);
• and
• the driven wheels are front wheels, and a third reciprocal transformation mechanism containing a third actuator for changing the track of the front wheels is situated in the front of the body (4).

A method of transforming a hybrid vehicle, comprising:

• transformation of a sterling double or four-track automobile into a sterling aircraft for take-off and landing on the ground or water includes:
• expansion of both whole wings (1) from a retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle to a flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle around the two vertical axes using the first reciprocal transformation mechanism;
• expansion of rear parts of wings (1) using the second reciprocal transformation mechanisms from the top front parts of the wings (1) into the spread flying position;
• and
• reducing the track of the front wheels using the third reciprocal transformation mechanism;
• and reciprocal transformation of a sterling aircraft into a sterling double or four-track automobile includes:
• expansion of the track of the front wheels track using the third reciprocal transformation mechanism;
• retraction of the rear parts of the wings (1) from the spread flying position onto the top front parts of wings (1) using the second reciprocal transformation mechanism;
• and
• retraction of both wings (1) from the flying position in which the axis of the wing is approximately perpendicular to the longitudinal axis of the vehicle into the retracted position in which the wing axis is approximately parallel to the longitudinal axis of the vehicle around two vertical axes using the first reciprocal transformation mechanism.