CZ201547A3 - Hybrid means of conveyance automobile - aircraft with foldable wing of the parasol type - Google Patents

Abstract

Hybrid Vehicle Vehicle - A parasol-type folding wing aircraft consists of the body body (1), the centroplane (2) of the folding wing, the right and left (3) folding wings that open and close on the right and left (4) folding wings. wings that are located on the right and left beams (5) that rotate on the right and left support joints (6). The support joints (6) are located in the right and left beds in the body of the body (1) of the hybrid vehicle. For the flight phase, the beams (5) rotate from horizontal to vertical position to move the centroplane (2) from the vertical position at the rear of the device to the horizontal position on the quarter-circle path. The right and left folding wing portions (3) open in the right and left hinges (4) of the folding wing in an upright position, continuous and straight with their centroplanes (2). For road travel, the beams (5) rotate from vertical to horizontal to move the centroplane (2) from a horizontal position over the device to a vertical position at the rear of the device along a quarter-circle path. The right and left folding wing portions (3) in the right and left folding wings (4) fold into a compact position along the right and left sides of the body (1). The right and left tips (3) of the folding wing abut the front of the body (1) and face forward.

Description

Hybrid Vehicle Vehicle - Plane with Folding Wing Type Parasol Technique

Combined Honor and Air Transport; individual and collective transport of passengers by land and air, freight transport by land and air.

Background Art

The current automobile-plane hybrid vehicles use for their flight phase mainly the design of the low-wing, high-wing, gyroplane or helicopter. The disadvantages of these solutions are: in the low wing and high wing aircraft, the center of gravity of the machine is very close to the wing axis, resulting in more difficult aircraft stability; gyroplanes and helicopters have the disadvantage of relatively short range and high fuel consumption. All these types of machines place high demands on the expertise and experience of pilots. All of these design solutions also use different types of folding mechanisms for wings, turbines and propeller blades to enable road traffic. However, these mechanisms lack the compactness, aerodynamics, and aesthetics that are needed and desirable for ground-based travel.

SUMMARY OF THE INVENTION

The aforementioned operational and structural deficiencies eliminate the hybrid vehicle automobile - a parasol-type folding wing consisting of a body body, a folding wing centroplane, a right and left folding wing, a right and left folding wing joint, a right and left folding wing swivel, a right and left support joint for rotating the folding wing beams, the right and left beds of the nose joints in the body of the hybrid vehicle body. The essence of the invention is that the parasol-type folding wing opens, closes and rotates on the beams in such a way as to provide the hybrid vehicle with optimum flight and driving characteristics. For the flight phase, the invention is characterized in that the open wing of the parasol type is lifted high above the body of the hybrid vehicle and thus moves the mass center of gravity of the whole machine deep under the wing axis, thus ensuring flight stability and very easy handling of the device. The machine is very compliant and tolerant to its pilot's faults, flying is simple and intuitive, suitable for less experienced pilots The invention is characterized by the fact that the parasol-type folding wing folds along the perimeter of the hybrid for road use. the vehicle, encircles it on the principle of beetle bushes and ensures compactness and the necessary aerodynamic properties. List of drawings in the drawing

Figure 1 shows a front view (left), a top view (center) and a side view (right) of a hybrid vehicle with the parasol folding wing closed for road use as a conventional automobile

Figure 2 illustrates the opening and closing of a parasol-type folding wing; a side view (left) shows the rotation of the wing beams to a vertical open position and a horizontal closed position; the plan view (right) shows the rotation of the wing sides to the open and closed positions

Figure 3 shows a front view (left), a top view (center) and a side view (right) of a parasol-type, open-wing, hybrid, take-off, flight and landing phase hybrid vehicle. An example of the invention

Hybrid Vehicle Vehicle - A parasol-type folding wing aircraft consists of a body body 1 in which the right and left nostrils of the nasal joints Z are located. The right and left support joints 6 for rotating the right and left pivoting beams 5 of the folding wings are located therein. The two rotating beams 5 carry the centroplane 2 to which the right and left portions of the folding wing 3 are attached by the right and left joints of the folding wing 4. The mechanism of the folding wing of the parasol type thus constructed permits a smooth transition between flight and phase by rotating, opening and closing its individual parts. on the road, either in idle mode or in slow motion before or after landing.

For flying, the pivoting beams 5 are rotated 90 ° from their horizontal position to the upright vertical position in the support joints 6. They thus lift the centroplane 2 together with the two parts of the folding wing 3 above the body of the body 1, while at the same time the parts of the folding wing 3 open in the joints of the wing 4 into a straight position with the centroplane and thereby form a whole continuous wing of the parasol type. For road travel, the rotating beams 5 are rotated 90 ° from the upright vertical position to the horizontal position in the bearing joints 6, placing the centroplan 2 vertically behind the body 1, while at the same time closing the folding wing portions 3 in the wing joints 4 to a position along the sides of the body 1 to form a compact ground vehicle.

The opening of the wing parts 3 and the rotation of the beams 5 is standardly hydraulic, emergency mechanical. The process of opening and closing this parasol-type wing can be carried out separately in phases - opening of the wing portions 3 and subsequent lifting of the centroplane 2 by the rotating beams 5 for flying and closing the wings 3 and subsequently lowering the centroplane with 2 rotating beams 5 for driving or synchronized opening of the portions the wings 3 and simultaneously lifting the centroplane 2 by the rotating beams 5 for flying and closing the wing portion 3 and simultaneously releasing the centroplane 2 with the rotatable support beams 5.

This type of parasol folding wing is suitable for its function, layout and construction for the combined means of transport, where the individual functions of the device are fully fledged (car and aircraft). The car can have a classic four-wheel or three-wheel arrangement, the aircraft can be classic or seaplane. This invention is also suitable for unmanned flying machines, so-called drones. Types of propulsion are: propeller propulsion, blower, combustion turbine, an alternative for road use can be a conventional internal combustion engine, electric motor, hybrid engine and the like.

List of reference numbers 1 body of hybrid vehicle 2 centroplan of folding wing 3 right and left of folding wing 4 right and left joint of folding wing 5 right and left swivel support of folding wing 6 right and left support joint for folding wing support Z right and left a bed of nose joints in the body of a hybrid vehicle

Claims (2)

PATENT CLAIMS 1. Hybrid vehicle vehicle - a parasol-type folding wing, characterized in that it is a body body (1), a centroplane, a folding wing, and a right and left folding wing (3) that open and close to the right and left the hinge of the folding wing (4), wherein the folding wing is located on the right and left beams (5), the beams rotate on the right and left support joints (6) and the support joints (6) are located in the right and left beds in the body of the body ( 1) of the hybrid vehicle, for the flight phase, the beams (5) rotate from horizontal to vertical position, thereby displacing the centroplane (2) from the vertical position at the rear of the device to the horizontal position over the device on the quarter-circle path, the right and left portions of the folding wing ( 3) in the right and left joints of the folding wing (4) open up in an upright position in their surfaces with a centroplane (2), for road travel, the beams (5) rotate from vertical to horizontal, thereby displacing the centroplane (2) from a horizontal position over the device to a vertical position at the rear of the device along a quarter-circle path, right and right the left wing of the folding wing (3) is in a compact position along the right and left sides of the body (1) in the right and left joints of the folding wing (4), the tips of the right and left of the folding wing (3) abut the front of the body ( 1) and facing forward.