RU2002651C1 - Aeromobile - Google Patents

Description

FIELD OF THE INVENTION This invention relates to motor vehicles, preferably high speed ones.

In the global development of vehicles, in connection with tougher environmental and economic sanctions, there is a tendency to improve all their parameters. In passenger cars, the issues of safer driving in the structural and operational increase in the speed characteristics of new models are primarily addressed. However, the issues of profitability and reducing the emission of toxic combustion products into the atmosphere have moved to the forefront, which today poses a real threat to curtail (or reduce) the auto industry if it does not acquire new forms of technical structures. In other words, having exhausted its resources, the global automotive industry is looking for ways to update while preserving all the achievements in this area and the prospect of further development.

It is well known that the main danger in high-speed driving is corners (bends) and objects on the road surface, even the tiniest (the higher the speed of the car, the worse its stability and the more likely it will lose control). Hence, promising passenger cars, as is known from world technical information, switch to sports-racing structures with improved running qualities, but these promising models cannot provide adequate operational reliability, because by physical assumptions, resistance should be included in the control of high-speed traffic. An extraordinary solution to the problems of a promising passenger vehicle is described in the invention of the Aeromobile, where its entire structure, deviating from accepted conventions repeating the engine-body systems, is subordinated to the most complete benefit from the laws of high-speed dynamics.

The first thing that is caused in the application by the targeted search for a homogeneous physical and mechanical complex is a limiting decrease in air resistance of the body. The second - the issue of stability and safety of superhigh-speed movement is solved by the aerodynamic method of controlling the position of the body, because body fixation with air jets is proposed. The third issue of profitability and environmental cleanliness with the simplification of mechanical-power communications has been resolved by the use of a new small-sized (high-speed) rotary-power combined-cycle gas and gas unit of the ground link. The proposed rotary-power steam-gas mechanics has the maximum heat saving, which is actually ensured by a significant reduction in all types of external and internal resistances and heat transfer to the atmosphere, the organization of an automatic scooter and a wide

regenerative recharge. In other words, an invention called the Aeromobile reveals an unusual promising approach to meeting the urgent needs of peaceful motorism in the new (in

5 spirit of the environment), a higher technical level.

The general simplified interconnection in the target search sequence allowed us to conclude the rotor power unit in

0 disks of the paired driving rear wheels and close the fairing, and the front wheels in the target simplified mechanical kinematics of folding, damping and turns managed to be made removable with

5 sides of the bottom to the body, where in the proposed five-seat variant there is no inconvenience from them. It was decided to design the body in the form of a mollusk shell with the same fundamental opening of the upper alignment, but on each side. Such a shell-like body shape, in comparison with the known ones, has the lowest coefficient of air resistance, close to 1. The location of the body with a front inclination

5 solves several targets: the convenience of a one-hundred-man landing and disembarkation of people, the creation of high-speed downforce on the rear wheels together with the horizontal elevators extending beyond the stern, and good visibility from the front and rear seats. An aeromobile can be used without a single reason, both in a city with folded aerial plumage on a par with conventional cars, as

5 and on suburban routes with control in the transition to high-speed air jets. It is these oncoming streams that take the reliable fixation of the body in a straight motion and

0 cornering. With sufficient acceleration by an aeromobile, screen forces can be used, i.e. with a large elevation of the front part of the elevator with rudders, it can be torn off from the carriageway by 2-3

5 m and plan on it through 50-60 m with support on the twin rear drive wheels. Such jumps may be undertaken in the event of a collision with road obstacles such as bypass airways. The length of the aircraft does not exceed serial cars, and the average height of its shell-like body does not reach a meter: with a significant front tilt and lift of the entire upper shell-like half, the landing and disembarkation of people is expected to be more free and comfortable than in ordinary passenger cars. A slightly oversized width is created by the front-side air bumper, which plays an extremely important role in unforeseen situations in high-speed driving modes.

In FIG. 1 schematically shows an aircraft, a side view, at the moment of raising the upper cusp half of a shell-like body (the dashed lines indicate the contours of wheel suspensions and parts of combined-cycle equipment of the power unit); in FIG. 2 - an azromobile in a high-speed position on paired rear wheels with a raised nose part of the body and retracted front wheels (arrows indicate the direction of air flow around the body); Fig. 3 is the same, top view (body assembly); in FIG. 4 - the same front view; in FIG. 5 - tr, rear view; in FIG. 6 is the same front view when the machine passes a turn (bend) in high speed mode; in FIG. 7 - the same, rear view; in FIG. 8 (a, b, c) are schematic diagrams of the contours of the fore, middle and aft transverse sections of the body, respectively, A-A, B-B, B-C in FIG. 2; in FIG. 9 - shell-shaped body with equipment; in FIG. 10- upper casement half a body; in FIG. 11 - external and internal devices of the lower keel; in FIG. 12 is a rear view (from the inside of the cavity) of the lock-loop mechanism for connecting the lower and upper body body parts; in FIG. 13 is the same side view (with the device and mounting of the spring levers of the frame target); in FIG. 14 drive lock-loop mechanism; in FIG. 15 is a side view of the six-rotor circuit of the power unit of the rear twin wheels (with a partial cutout of the side wall and in conjunction with the lever-spring suspension); in Fig. 16 - power unit assembly with suspension, front view; in FIG. 17 - the front steering wheel (the hub and the location of the wheel axle electric drive mechanism in it); in FIG. 18 - connecting part of the hub; in FIG. 19 - installation diagram 8 of the body of the rotary wheel cups; in FIG. 20 is the same top view (the dotted line indicates the wheel retracted inside the body, the hinge joint of the upper levers and the shared dimensions of the hub): in FIG. 21 - plate multi-beam spring; in FIG. 22 - spring pneumatic cylinder drive levers.

The aeromobile body consists of four main removable and detachable parts: a shell-like frame with a wing upper half — a roof, a lower keel with an internal motor-wheel compartment, an air tail of the rear part of the body and a horseshoe-shaped wall air bumper, which simultaneously serves as a pneumatic balloon (storage).

The shell-like frame includes a mechanism for controlling the front (small) wheels and the vertical air wheel, a hinge-lock device for opening and closing the swing halves, and folding equipment for the front steering wheels. The lower keel, made in the streamlined shape of the boat, includes a suspension of the rear twin driving wheels with combined-cycle equipment of a six-cylinder motor-wheel placed between the wheels. The plumage includes the vertical rudder of the air turns, which is located behind the keel and pivotally connected with it, and two horizontal planes of the elevator, which rotate behind the air rudder.

The shell-like frame is based on a frame, which is formed by the connection of two lateral longitudinal box-shaped beams 1 having external openings 2 and end cross-members. In section, the box-shaped beams have an elongated rectangular shape. Since the frame is inclined to the front side, according to its shell-like structure and the inclination of the beam from the front edge, they are bent up, and their rear ends are bent down. To the beams between the bends on the rear side, the ends of the feed box are welded with the ends of the cross-section of a triangular cross-section, the acute angle of which is directed towards the rear ends, and the opposite side creates a rear body wall. From the side of the outer corner, a mid-semicircular recess 5 is made under the front cylindrical edge of the vertical air rudder 6. The recess has a supporting wall with an average horizontal slit, and support rollers along the edges. The rear ends of the beams do not have external openings, but have through different diameter end holes for the air drive mechanism 7. Several widened front ends of the beam are welded to the bowl-shaped body recesses 8, turned upside down, and at the same time are connected to the nose box cross member, consisting of front bracket-like plate wall 9 of the body and sickle-shaped

bonnet 10, the rigidity of the front bending of the beams is complemented by the front intermediate vertical bridge 11. From the front bracket to the stern angular cross-pieces, i.e. until the rear ends of the beams are bent, the bottom of the boat type 12 is welded from the bottom of the frame with an increase in the lower bulge 13 to the stern, as a result of which the rear ends become external. Apertures were made in the diameter of the cup-shaped niches in the bottom, and the edges of both of them were connected by welding. The shell-like frame formed by the frame and the bottom is hardened from the inside by a vertical-lamellar bar 14, welded with the ends and lower edge to the sidewalls of the frame and the bottom. This crossbar is connected to the intermediate bridge by three longitudinal vertical posts 15, which are simultaneously welded to the bottom. These struts delimited the front seats on which the reclining backs are held. Bottom holes were made in the racks for passing the transverse drive-rotary shaft for controlling the planes of the horizontal air elevator through cable assemblies passing inside the beams 1. The second vertical plate crossbar 16 gives support to the rear solid seat and the transverse plane inclined backwards 17. The crossbeam and the plane are interconnected by the shared support posts 18 and, with their help, the bottom. A wedge-shaped volume behind an inclined plane is reserved for a capacious luggage carrier 19. and for small items in the aft cross-section, niches 20 are provided. From this cross-section to the front-seat driver of the foot-steering mechanism of the front wheels and the air steering wheel 21 channel guards are laid along the bottom enclosed in their volumes by ropes. The turning mechanism consists of two wings 22 located in a row across the body. In the middle part of the wings, the upper pedals 23 are mounted. At the extreme ends of the wings, there are axial holes which are mounted on the axial protrusions of the bottom 23, and at the proximal ends there are toothed segments 25 facing each other with teeth in engagement with the gear of the shaft 26. This shaft mounted on the bottom with bearings and connected by cables with an air wheel and rotary equipment of the front wheels: switching to one or another control is done by the driver. The design principle of the switching mechanism in this case can be any.

The racks of the front seats are supported by armrests 27, and the drive transverse rotary shaft passing in their lower holes consists of an external pipe 28 and its inner hinge rod 29, on which levers 30 with manual control arms 31 are fixed. The levers are located on the sides of the driver's seat, where the branching of the shaft links takes place. In addition to this, at the branching point, the shaft pipe and its shaft have cranks pressed into them, by means of which these links are connected to telescopic pneumatic amplifiers 32 (the constructive principle of amplifiers can be any). The support of the cylinders of the pneumatic amplifiers falls on the vertical jumper 11, and the measure of their mechanical force on both links of the shaft is regulated by the button 33 on the handle of the right

0 driver leverage. The ends of the shaft are passed through holes in the inner side walls of the beams in the cavity and are connected using openings 2 in the beams with pulleys 34. These pulleys are connected by cables to similar pulleys 35 fixed to the ends of the external two-link shaft consisting of a pipe 36 and its hinge rod 37. This driven shaft is mounted on the outer ends of the beams in their extreme through holes x

0 7 and on its link x are fixed plane 39 of the air horizontal elevator. The transfer of traction force from the pulley 34 to the pulley 35 passes through the intermediate adjusting and tensioning pulleys 38 installed in the bends of the beams. The attachment points of the planes on the shaft links are closed by wedge-shaped rubber fairings 40, which reduce air-drag (Figs. 1, 3).

0 A horseshoe-shaped pneumatic bumper 41 of a trihedral cross-section is angled to the periphery of the body, and on the inward-facing face has hooks (convexity) 42 along the contour of the openings of 2 beams, which are firmly fixed to 5 on the side of the body (Fig. 11). With such a surface mount (by the entrance of the hooks and the openings of the beams), the ends of the bumper are connected by clamps 43. On top of the beams are located at a certain distance

0 from each other and the lower loops 44 of the lock-loop mechanism, which is mounted on the upper casement half of the shell-like frame, are fixed. This half-line has a parabolic base

5 a box-shaped frame for attaching a panoramic sight glass. The frame box is assembled from the lower (larger) 45 and upper (small) 46 grooved strips welded along the edges, one-sided facing up. The walls of the grooved strips are reinforced with inner ribs 47. With the flanged ends 48 extended downward, the frame is welded to the rear canopy 49, which is the roof. Gutters are welded at the junction of the frame with the roof and extend to the roof along its entire front edge. The canopy-roof has a double-walled structure: from the lower front edge of the lower wall, the canopy surrounds the groove strip that connects to the upper groove strip of the frame, which is framed by the sight glass 50 and fastened with a rubber seal 51. The side composite glasses 52 can be made to be lifted and placed between the walls 53 of the roof. On the side of the widened seats of the frame on the outer walls, windows are cut out for the drive part of the lock-loop mechanism to go outside. Since the device of the lock-loop mechanisms on each side of the frame is the same, one of them is described below. The drive part comprises a pivot plate 54 formed with a nozzle 55. This outer part of the mechanism serves as a door handle for opening (disengaging and lifting) the upper cusp half of the shell body. On the outer side of the nozzle, opposite from the plate, an equity groove extends. which is closed at the ends with pressed-in plugs 56. The plugs have wedge-shaped ends facing the inside of the groove to its periphery. For the ends of the plugs in the groove cavity, a clamping brace-like lamellar spring 57 is convex with a convexity outward. Two axial bushings58 with eccentric end flanges 59 are placed inside the nozzle, with which the bushings are fixed to the outer wall of the frame on the sides of the window using fixing holes 60. Spiral slots 61 are made from the outer ends under the tides in the walls of the bushings and their ends are connected (without slots) a central coil spring 62, which is compressed between the bends 63 of the pin hinge axles 64, extending from the bushings to the sides. The bends are made at an angle of 90 ° and have hinge rings 65 at the ends of which are installed in the spiral slots of the bushings and in the internal lobed groove 66 of the pipe wall. Through mounting holes, the tides of the bushings are bolted to inserts 67 having the shape of rectangular dies. Eccentric holes 68 were drilled in the thickness of the inserts for the passage of the rod hinge axes, and threaded holes 69 were made on the sides of the passage holes. The same inserts with paired threaded holes 69 are intended

for holding the ends of the pin hinge axes spaced apart from the drive portion. These inserts are twice as thick as the first ones and fastened through the frame wall with external decorative adjustment 70. At the level of the front and rear seats, the rod hinge axes are connected to the gear sectors 71, which mesh with similar gear sectors 72 mounted on the inside the ribs of the box-shaped frame on axles 73 and having external drive plates 74 extending into the inside of the body 74. An elastic sealing gasket 75 is mounted on the connection-separation line of the wing halves of the shell-like body 75. erhney half, which are closed all auxiliary openings necessary for mounting

0 lock-loop mechanism.

The lower keel 76 has a pointed front and smoothly raised from the rear up streamlined boat-like shape. It is welded from sheet metal with a bottom opening 77

5 under the motor-wheel and with flanges along the upper concave edges 78. The rear wall 79 kilograms is concave inward to cover the front cylindrical edge of the air wheel. In the front part of the keel, on the sidewalls reinforced with linings 80, the support axis 81 is horizontally fixed. The same axis is fixed in the same way in the rear part of the keel. Behind the rear axle 82, a steam-gas unit 83 of the instantaneous 5th conversion of water to steam is installed in the volume of a kil. The fuel gas outlet 84 of the combined cycle gas turbine unit and the exhaust gas exhaust 85 of the motor wheel are brought into the cavity of the air wheel to increase the temperature of the

0 its cavity and fixed at a distance from the walls of the wedge-shaped tank 86 with water (wedge-shaped is not shown). The air rudder is mounted behind the keel on the upper and lower hinges, where the lower hinge 87 is located on the lower tail support plate of the keel (Figs. 4, 5), and the upper hinge is located on the front edge of the air rudder defining its front cylindrical edge, the edge being in horizontal slit of the wall of the middle semicircular recess 5 of the rear corner frame cross member. The diagonal cut of the upper front edge of the air wheel is covered with a fairing 88, which simultaneously serves as a cover for this

5 of the opening through which a gas-vapor residue is installed and mounted, in particular a gas cylinder 89. The gas outlets, pipelines and hoses are connected to the cavity of the air rudder through an annular sleeve 90. At the junction of the air rudder with

control cables 91 are mounted at the ends of its recess 5 by control cables passing through the aft angular cross member 4. In conjunction with the lower keel and the horizontal vertical aft tail, the body appears in a final streamlined shape. The upper cusp body part, which is a fusion of the front window, doors and roof with the rear view window, has intra-body lateral spring-folding lift arms. Separately, each lateral lever consists of two U-shaped bends 92 and 93, which enter one another on the rotary axis on the pivot axis 94. The axis carries a charged coil spring 95 with the ends resting on the knees; The spring charge neutralizes the weight pressure of the upper cusp of the kitchen. The free end of the knee 93, the lever is pivotally connected to the frame, and the other free end, having a longitudinal plate loop 96 with a square hole on the side of the wall, is connected to the outer square section 97 of the drive axis passing in the cavity of the beam 1. This is the connection of the loop of the external knee of the lever with the drive axle has a slight play, softened by the rubber gaskets 99 pressed against the axle passing 98 on both sides of the hinge, and crank 101 is fitted into the middle portion of the drive axis of a smaller square section 100, with connected to the pneumatic cylinder 102 for automatically controlling the opening and closing of the upper wing half of the body, with a large 103 and a small 104 diameter, the axis is mounted in the corresponding sleeve flanges 105 and 106, where the sleeve flange 105 is riveted to the beam wall and the flange 106 is welded to the bracket 107, riveted to the beam on the opposite side of the volume. The axis is held out by a nut 108 which is screwed onto the end thread (the connection may be secured with a lock nut).

The suspension of the rear twin motor wheel (Figs. 1, 15 and 16) consists of semicircles of grooved planes 109 with a curvilinear-angled cover of the vertical walls of the front bends 110, ending in front with horizontal tubular-hinged supports 111. The semicircles of the grooved planes with elongated vertical walls are connected bolts with a crest 112 of the support strut of the rotor-power unit, containing paired chambers (cylinder) 113 with elliptical rotors 114, mounted on opposite cranks 115 of autonomous shafts, which are connected to a common th axle 116 wheels

117 by gear-gear connection 118. Submarine pipelines 119 connected to the steam generating chamber and the cavity of the air rudder are connected to the back of the support column ridge, and lower hinges 120 of a spring-damping device consisting of two diverging down on the sides of the springs 121c

0 internal air pumps 122, articulated by cylindrical links with single lower 123 and paired upper 124 connecting tips. Moreover, the suspension is connected by a tubular-hinged support in the cavity of the keel to the front axle, and a paired tip to the rear.

Since the suspensions of the front retractable steering wheels are identical, lower

0 is described alone. From the inside, the sides of the cup-shaped niches 8 of the body have additional walls 125 with protrusions 126 and flanges 127 extending around the inner circumference. The same protrusions 128 and 5 of the flange 129 and 130 have on the outside the side walls of the rotary wheel cups 131 mounted in the niches, turned upside down 132. Thanks to such a targeted constructive study, the wheels

0, the bowl is held in a body recess by means of articulated rubber damping rings 133 of circular cross section stored in a recess between opposing protrusions and flanges. In addition, 5 fluoroplastic (kapron) plate gaskets — hoops 134 under the support of rubber rings — are embedded in the outer recesses of the walls of the wheel cups. The wheel bowl is covered by a flexible pull 135 for which

An annular groove is selected on the outer lip. The lower edges of the niches 127 and bowls 130 are connected by a corrugated water and dust-proof fabric 136, and lamellar springs with

5 by several radial rays 137, turned upward by bent ends. The center of the spring is connected by a hinge 138 to the center of the inverted bottom of the wheel cup, and its ends are located in radial (centrifugal) guide plates 139 fixed along the periphery of the bottom of the body niche. The spring is connected to the bottom of the niche by a flexible stitch 140. On sickle-shaped, inverted bent mi

5 counter to levers 141 extending along the edges of the volume of the wheel cup and mounted by proximate sleeve-articulated ends 142 on the lateral support axis 143, and on the upper tensile levers 144 mounted in the center of the volume on the axis 145 of the hinge-joint with bottom, wheel hub 146 is suspended. The wheel edge leading out of the wheel is in the form of a square flange 147 with axially pressed axles 148 of the hinge joint with the ends of the levers 141 and axle 149 of the hinge joint with the ends of the levers 144. At the end of the square flange there is a circular recess 150, on whose side an eccentric recess for the installation of an electric motor 151 (generator), In the vertical cut 152 of the lower part of the flange, a hook-shaped rod 154 is mounted on the axis 153, connected to the end cover 155 of the flange covering the circular recess, and between the axis 156 and the loop of the rod Pneumatic cylinder 157 brake system. The front part of the eccentric hub has a cavity with a figure-eight cross section, where the inner hinge link 159 of the electric motor shaft passes in the upper cylindrical volume in the support bearing 158 and the wheel axis 161 is installed in the lower cylindrical volume on the tapered bearings 160. Moreover, the outer surface is well polished. the wheel connecting flange 162 is enclosed by a grooved ring seal 163 inserted into the front circumferential edge 164 of the hub. A sleeve spacer 165 is laid between the tapered bearings and connected to the hub wall by bolts 166. The internal hinge link of the electric motor shaft has a small end helical gear 167 that is engaged with a large helical gear 166 of the wheel axle. The tubular shaft link on the reverse side of the electric motor carries a friction disk 169, and the shaft carries a pressure metal disk 170 extending in front of the friction disk and bordering the pressure end cap of the outer flange of the hub. At this point, a similar friction clutch 171 is deepened into the cover with an adhesive joint. For cooling the electric motor, the lower wall of the hub below it has through cuts 172. The rim 173 and the front wheel disk 174 175 are made by simplified shredding and welding. Since the supporting axis of the crescent arms inside the wheel cup extends adjacent to the wall (in a bulge 128). then the wheel in the raised position retracted in the underbody position 176 occupies a somewhat eccentric position with the disc down. The sleeve-hinged ends of these levers sitting on the axis are interconnected by end protrusions, and the axis is secured from extensions by screw fixing secret pins 177. The upper levers are pressed onto the ends of the axis, which, with the middle eyes 178, come out of the hinge loop riveted to the bottom 132. In connection with the hub flange, these levers have hooks 179 for fixing with latches 180, pivotally mounted on the inverted bottom of the wheel cup with the wheel fully retracted into it. The eyelets of the levers are pivotally connected to a pneumatic cylinder 181, which has an internal return spring 182 (Fig. 20) and which connects its external 183 and internal 184 cups from the inside by screw clamps located at the ends. The clamps are bolts with boss flanges 185, in which lateral holes were drilled for the ends of the spring, and their outer nut halves in the form of washers 186 with lateral thickenings 187 and threaded holes 188 are screwed onto the threaded ends leading outward. With one end washer, the pneumatic cylinder is mounted on an axis in the eyes of the axis of the upper levers, the other end of the washer is connected by an axis with a hinge bracket riveted to the wall; air is supplied to the cylinder through the nozzle 189. The release buttons 190 of the drive part of the lock-loop mechanism are located under the locking springs 57 and are fixed to the beams 1. The location of the exhaust window 191 on the air steering wheel is chosen experimentally.

The device operates as follows.

Before boarding the aircraft, the driver (passenger) grabs the pivot plate 54 of the pipe 55 of the drive part of the hinge-lock mechanism of the upper wing half of the body and presses it upward with a slight muscular effort (Fig. 13). At the same time, the nozzle rotates on the axial bushings 58 and moves the bends 63 with the rod loop axes 64 to each other along the spiral slot 61 of the bushings to the axial bushings 66. These target rotary-axial movements of the rod loop axes compresses located between them in the bushings the return coil spring 62, and when the plate is turned up a quarter, the ends of these axes completely exit from the holes of the hinges 44 of the lower casement half of the body - separation occurs on this side of the loop connection, by pressing on the rotary plate 54 simultaneously, the rotary plates 74 are raised from the inside. Since the lateral surfaces of the petelboard

lock-loop mechanisms tightly in contact with inserts 69 - holders in

the cavity of the rim of the upper casement half of the body of the ends of the pivot axles, the raising of this upper body part with this disconnected side on a sufficiently extended rod-loop connection on the other hand will be free, backlashless. Conversely, when boarding / disembarking people from another side disconnected by the described method, this side of the upper casement half will be in a loop-free loop connection. The lifting of the upper casement half from one side of the body or another is carried out both manually and mechanically (automatically).

In the manual mode, the driver (passenger), after pressing the rotary plate and turning it a quarter, continues to send a slight force upward, releasing a part of the energy compressed under the weight of the lateral top of the upper leaf half of the return spring 95. Under the action of this part of the released kinetic energy, the spring spreads a lateral folding lift arm that opens up a shell-like body for landing and disembarking people. At the moment of lifting of the upper casement half, the spring 57 of the outer equity groove of the nozzle 55, having freed itself from the release button 190, enters the opening 192 of the lower wall of the frame, fixing in the upper position the rotary plates 54 and 74 of the locking mechanism. Manual body closure is also easy and free. The driver (passenger) grasps the body plate 74, which is connected to the pipe via the gear sectors 71 and 72 and the pin axles 64, and with a light pressure lowers the top of the body, additionally loading the return spring 62 of the folding side lever. When the body halves are tightly closed, the nozzle spring 57 is squeezed out of the lower frame wall (from the groove 192) by the release button 190 and the nozzle freed from blocking by the action of the internal coil spring 62 will turn a quarter of a turn in the opposite direction with the rotary plates 54 and 74 lowering on both sides of the mandrel . The ends of the pivot axes at this moment will fit tightly into the holes of the hinges 44 of the lower wing half of the body. The input of the axes into the holes is surrounded by rotations of the rods, which, when opened by the spring, are rolled by hinged bends 63 into the spiral slots x 61 of the bushings 56 of the drive part of the lock-loop mechanism. The mechanical method only automates the process of lifting the upper wing half of the body after

the fourth turn of the plates 54 and 74 upward, and its descent is automated by pressing a button displayed in the side panel of the body at each seat. In order to automate the process, pressure is applied to the lifting mechanisms when the valve is opened along the pneumatic line. The button for actuating the pneumatic extension of the cylinder 102 interacts with the eccentric part of the nozzle and ensures the passage of pneumatic pressure into the cylinder when the plates 54 and 74 are completely turned upward by the muscular effort of the driver (passengers). Crank 101 associated with the cylinder through faceted sections 100 and 97

5 axes and the square hole of the plate loop 96 rotates the outer link 92 of the folding lever, which, leaning on the frame, increases the angular distance between the ends to straighten the knees on the axis 94. B

In the automated lowering of the upper casement half of the body, another button for the pneumatic compression drive of the cylinder 102, brought out, and the body buttons indicated inside are involved. At

5 closing the body halves, the operation of the lock-loop mechanism is similar to that described above.

Landing in an aircraft takes place through the corner space

0 or another edge of the upper casement half of the body and the low-haired side of the front of its lower half (Fig. T); if necessary, the front part can be lowered onto the road. The driver takes

5 the left (Fig. 3) front seat, puts the legs on the pedals 23 of the wings 22 of the foot control mechanism of turns and special drives heats the chamber of the steam-gas unit 83 (Figs. 1 and 9), creating pressure in the pneumatic drives by injecting into it some water. In urban vehicle driving modes (Fig. 1), tail tail air control is not applied. The horizontal levers 39 of the elevators are in the front position (retracted on the sides of the driver's seat), and the planes are turned forward and are adjacent to the upper edge of the rear corner cross member

0 4. The wedge-shaped rubber fairings 40 of the plane are turned back and act in this case as rear bumpers. The foot control mechanism of the machine has been shifted to the front wheels 175.

5 Since the intermediate shaft 26 with the gear is mounted in bearings on the underbody, the wings 22, which are engaged by means of gear sectors 25 with the gear of this shaft, can purposefully perform only the opposite

horizontally swinging on the axis x 24 movements. Cable winded pulleys sitting on the shaft can be connected individually with a special device, as one pulley is connected by a cable to the sides of the vertical air steering wheel b, the other to the wheel cups, and the cable 135 passes in the outer annular grooves of the side walls of the latter through the slots of the rubber inserts of the vertical ones. slotted in the sidewalls of body niches 8. Spring damping of the front wheels (Fig. 19) occurs when the outer sides of the wheel cups are rolled on rubber rings 133 along the inner sidewalls of the body niches, and the sliding properties of the wheel cups in the hoops 134 are indicated by the sliding properties of the fluoroplastic (kapron) materials. At the same time, rubber rings well seal the volumes between the bottoms of body niches and wheel cups, reliably centered by 137 springs. The compression of air in these volumes, as well as the compression in the cylinders of the rear suspension air pumps 122, feed the steam-gas chamber during the oscillation of the wheels, from which the compressed air in the heated expanded volume is added as a working medium to the cylinders of the rotor motor wheel. With the pressure being applied to all 6 cylinders of the motor wheel (Fig. 15) and the electromotor drive of the front wheels 175 turned on, the start of the movement of the aircrafts is characterized by extremely fast dynamic acceleration. Since the shaft of the electric motor (Fig. 17) is tubular, and its internal pin link 159 is articulated, at the initial moment of starting the electric motor the pipe link engages the internal pin with the gear 167 fixed to its end behind the support bearing 158, which is shifted by the bevel gear Mi oblique teeth m gear 168 to the axis 161, creates an axial connection of its disk 170 with the friction of the tubular shaft of the electric motor, th. When the power is turned off (capacitors may be sources) when the wheels of the accelerated aircraft roll, as a result of a change in the power flow from the wheels to the electric motor, the gear wheel 168 starts to rotate the gear 167 of the shaft 159 and shift the bar link in the opposite direction under the influence of the bevels of the teeth. This force displacement separates the disc 170 with the friction clutch 169 and the shaft shaft link with the disc in the tubular link of the electric motor rotates idle. With a gear ratio of 1: 2, idle rotation of the disk is most advantageously used in the simplest braking mechanism. By applying pressure to the brake cylinder 157, the cover 155 of the flange 147 of the wheel hub 175 moves into the recess 150 and squeezes the disk 170 between the friction clutch 169 and 171; reducing the speed of the disk by frictional friction reduces the speed of the shaft 159. The displacement of the shaft 159 in the tubular link is insignificant, but sufficient for the joint-disconnections of the disk and frictions.

Controlling the front wheels with the help of the legs through the pedal-link mechanism is unusual, but reliable. In the operational movement of an aeromobile

The 5 hands of the driver are occupied by air control and the selection of the most optimal driving modes with targeted environmental and economic benefits. For example, as the aircraft accelerates, it is envisaged to turn off the paired cylinder-rotor groups one by one, with their transition to neutral functioning. The same groups are included in the process of generating compressed air, and this provides the aero5 mobile with effective braking without blocking.

The transition of the aeromobile to high-speed movement is carried out as follows. The shaft 26 of the foot control of turns is engaged with a pulley connected by a cable to the vertical air wheel 6. The levers 30 for turning the planes 39 of the horizontal elevator are brought out from the sides of the seat with the planes turning backwards (Fig. 2). When turning to the right, the driver’s right leg and arm move forward, when turning to the left, the left leg and arm (Fig. 5), respectively, the vertical air rudder rotates right to raise the right plane of the horizontal elevator or vice versa. Speed and braking control are displayed on the handle of the left lever 30 in the form of a pressure pin, followed by half

5 or by full pressing of which there is an increase in production and pressure in a combined cycle gas turbine unit, and from half pressing to full tempering, the motor-wheel is decelerated by compression in its cylinder-air volumes.

Upon reaching a high speed of movement, the raising of the front part of the body while maintaining a negative angle of attack to one degree or another occurs due to

5 of the upper rotation of the planes 39 of the horizontal elevator with the help of pneumatic amplifiers 32, controlled by the button 33 of the handle 31 of the right lever 30. The raising of the front part of the body is necessary for constant tight grip of the rear twin air wheels 117 with the road surface and this is integral to high-speed quality is achieved by the balance of the car on the driving wheels of the shell-like body part and the planes of the horizontal air steering wheel in the differentiation of their negative angles of attack relative to one or another movement speed. The aeromobile does not create turbulence in a well streamlined body (FIG. 2, arrows) and is designed for speeds of the order of 400-500 km / h. Its front wheels are retracted inside the body and rotated by discs to the bottom level.

Claims (2)

The mechanism for cleaning and releasing the wheels operates as follows. With pneumatic pressure applied to the cylinder cavity (Fig. 20, arrows), the cup 184 extends, stretching the internal return coil spring 182, and presses on the eyes 178 of the axis 145, lifting its upper upper arms 144 and pressing them to the bottom with the entrance of the end hooks 179 ( Fig. 17) beyond the edge of the latch 180. In this case, the lower crescent arms 141 are mounted closely below the upper ones when the wheels 175 are laterally turned. Two, three cylinders mounted in a row (FIG. 19, dashed line) may be applicable to increase force moments. You Claims 1. AEROMOBILE, comprising an indoor body with a motor compartment and a trunk, two front swivel and two rear twin drive wheels and their suspensions, characterized in that the body is mounted on a frame formed by box-shaped beams and made in the shape of a shell, consisting consisting of two halves, the upper of which is made of a wing, and the lower is equipped with lock-and-fly mechanisms for connecting the poloins between themselves and is made in the aft part with a boat-shaped keel, inside of which a power unit with a lever-spring suspension is placed steam and gas-gas unit, with an external hatch for the exit of the twin wheel and a rear wall concave inward, horizontal elevators mounted on a tubular and rod link, a transverse driven shaft installed in the side holes of the rear ends of the frame beams and the associated cable, passed through cavities of beams, with a leading hall installed on the body, made of tubular and connecting links, a vertical air rudder located between the mountains 5 th 15 20 25 thirty 35 0 5 0 5 the wheel is thrown out of the bowl by the controlled release of the latch and the force of the return spring of the pneumatic cylinder (pneumatic cylinders). The levers during rotation in the hinges occupy the initial positions with the wheel in the longitudinal-vertical position for rolling motion. The turns of the aircrafts at high-speed driving modes occur with the corresponding lateral inclinations of the body, where the difference in the negative angles of attack on the planes 39 of the horizontal elevator is created by the muscular efforts of the driver in pressing the levers 30 away. To raise the car over the roadway, the driver using pneumatic amplifiers (pressing the button 33 on the handle of the right lever 30 to failure), when sufficient speed is reached, sharply increases the negative angle of attack on horizontal planes x 39, disrupting the reference balance of the machine. In the subsequent on-screen planning and landing, the azromobile is controlled only by the air plumage in the presence of a flat, shell-like body shape that is stable in flight. (56) Application EP No. 03918646.cl. B 62 D 36/00, 1980. with height elevators and pivotally connected to the aforementioned rear wall of the body, moreover, control links for raising and lowering the planes of the horizontal rudders are mounted on the links of the drive shaft, and on the axial vertical protrusions of the bottom of the body there are lateral pedal levers for controlling the rotation of the vertical air steering wheel and front wheels, equipped with gear sectors at ends facing each other, mounted on the bottom by a support shaft with coupling pulleys connected by cables to the sidewalls of the wheels of bowls and a vertical rudder and an intermediate gear interacting with said gear sectors, while the body is equipped with a horseshoe-shaped bumper. 2. The aircraft according to claim 1, characterized in that the box-shaped beams of the frame of the body are in cross section in the shape of an upward-extending rectangle and are provided with concave front and bent rear ends, the body is made with cup-shaped niches facing upwards, the sides of which are rigidly connected to the ends of the frame beams with the formation of the front cross member, consisting of VIA vertical21200265122 a jumper located between the double wires. The aircraft according to claim 1, characterized in niches, a front bracket-shaped plate, so that the body is equipped with a folding bead wall and sickle-shaped hood, and your levers raise its upper half-angled cross-beam with a semicircular bend placed inside the body along the edge from the side of an external acute angle, co,. walls of the frame, and driven pneumatically connected rigidly with the rear ends of the double acting cylinders connected by beams, with the ends of the levers by means of a crank.3. The aircraft according to claim 1, characterized in that the pneumatic cylinders are cranked with T8m, which has a rigidly connected underbody They are installed in the cavities of the beams with a frame and lamellar crossbars; by means of supporting axes made between the cross members and made with faceted connecting sections, neno with a bulge increasing in cd. An azromobile according to claim 1, characterized in stern and passing at the junction in that the suspension of the rear twin bottom with an angular cross member in the horizontal driving wheel comprises grooved underfloor section, wherein in places of the connection there are 15 onions with lever branches in the form of a vertical the front and rear rungs from teak walls of curvilinear shape, longitudinal vertical vertical struts equipped with horizontal tubular rigidly fixed to the body, three front supports connected to the wheel ridge with inclined backs Th engine, and coil springs, ball seats. and nirno connected with semicircles, at 4. The aircraft according to claim 1, characterized in that the front is installed in the keel cavity in that the upper casement half of the horizontal axis, on which the callas are mounted, contains a parabolic box-like supports and a rear horizontal frame for the front windshield, .. ,, - on an axis connected to spiral bays connected to a rear canopy-roof. with zins. while the lateral outer and lower. The aircraft according to claim 1, characterized in the frames of the frame are made with windows, in which the hub of the front wheel of the suppliers is equipped with the outer parts of the lock with a tetrahedral flange with upper and loop mechanisms mounted on the lower side axial protrusions in the cavity of the walls. .Aeromobile according to claim 1, characterized by a forest bowl, and upper driving and lower ones, such that the locking-loop mechanism includes guided crescent-shaped levers, includes axial bushings with spiral ends connected at the same ends, with said cuts e, to which are fitted with a 35th flange, and with the other ends a hinge-pipe with an external lobed groove, in which a staple spring, cups are stocked with a torus, the cups, while on the outside of the wheels it is made with an external bulge, and other cups and the lateral surface of the body is an internal lobed groove of the intermediate tires, a counter annular return spring and 40 rod protrusions are made for connecting the cups and tires between the axle with the bent ends, opposite to each other by means of rubber wheels circular and existing from the logo of the cross section, inserted between the mentioned lobar groove, spiral bowls and niches. mi slot mi and return spring. The aircraft according to claim 1, characterized in 6. The car according to claim 1, characterized in that the wheel cups are connected to the inside, that the outer ends of the spherical axial surface of the spherical body are mounted in the cavities of the side wall tires using plate-like frames with loop brackets, multi-beam springs with concave upward adjacent to the loops of the lower half of the rh ends, while the centers of the springs of the hinge-cousin are connected to the centers of the bottoms of the bowls, and 7. The car according to claim 1. The distinguished bottoms of the niches are made with radial bearings, in that the lock-loop mechanism is provided with masonry blocks in which the radial is located by turning plates, the placed spring beams. different inside the body at the level of the front and 55 12. An aircraft according to claim 1, characterized by a rear seat and equipped with teeth, in which the front wheel hub has stoic sectors, while the pivot axles of the flange are made with a recess, also equipped with gear sectors, which is placed the pressure cap interacting with the gears of the secto-brake device with the internal frictors of the intra-body rotary plates. eccentric disc, and eccentric 23 mom in which the electric motor, when 200265124 the housing is located between the mentioned friction disks, and on the other end there is a pinion gear, moreover, the wheel axis is also equipped with a helical gear, a friction disk is attached, a metal disk, a romotor, is fixed to one rod connecting the shaft with the gear of the shaft. . installed this last .. is made with a tubular shaft with an inner shaft, on the shaft from the side of the cover for , ",., / / Y /, / VinU 24 8 30 11 ft H 1W & Fiyo.Z 3 W FIG. 6 At 31 59 L 8 Aa FIG. 7 FIG. 8 S $$ and h V fe WITH "about I I AM 4/ W U1 sh uy hell t is t t $ / g; j 69 6f 59 33 K 57 & & Ft.% ff7 2002651 / Off I / 7 17E Wo epЈse t7 / / 7. 76 / /.57 / Ј # / Ј q & ts & .fS 181 fig AS 138 180 / j; shshk tmy t79W L No. U I9 W Vs a u®sh -175 FIG. nineteen Editor F # -AND. 22 Compiled by A. V tkmn Tehred M. Morgenthal Corrector E- Papp G W t b1 w No. 178 # R w