ES2223219B1 - MECHANISM FOR ARTICULATION, DEARTICULATION AND ASSEMBLY OF THE TECHNICAL DEVICES FOR THE RECONVERSION OF THE "AUTOCOPTER" VEHICLE OBJECT OF THE MAIN PATENT. - Google Patents

Abstract

Mechanism of assembly of the Main Rotor Axle of the "Autocópter", (object of the main patent), by lifting and lowering device, telescopic type, rising and descending by self-assembling sections with fitable and detachable pythons, mechanically by electronic excitation by Radio- control; of the Rotor-Stabilizer nestable and detachable, running by sliding to be assembled between the two tails of the vehicle, also mechanically and by electronic excitation by Radio-Control: Mechanism of folding and unfolding of the articulated Rotor Blades by sections, by means of extension cables, collectors and strength and stiffness givers, which are located on the front and back of the aforementioned blades and sliding slide for storage in the vehicle's hold; Mechanism of launching cables of the reconversion for Helicopter, composed of small launching cannons of such cables, electronically by Radio-Control; Mechanism of displacement by lanes of the Rotor Group and the Housing Bridge of the Rotor-Stabilizer to achieve the height and width necessary for the assembly of the rotors.

Description

Mechanism for articulation, disarticulation and assembly of the technical reconversion devices of the "Autocópter", vehicle object of the main patent.

First addiction to Patent ES 2151798BI (PG00023) Autocopter. (Motorized land automotive vehicle reconvertible in airmobile) Mechanisms for articulation, dismantling and assembly of the technical devices of reconversion

The present additions that are formulated by the owner of the patent in force outlined in the heading, are carried out in accordance with the rules established in the Patent and Trademark Law for invention patents; having based on the best object development of the main patent with more neat information and clearer way than it was the information provided by the inventor to achieve optimal manufacturing method at the time of execution by technicians in the matter of factories where appropriate. The additions that are formulate are fully integrated into the object of the patent principal with the same inventive unit formulated with the following descriptions:

The present additions refer more to the more generalized development of some mechanisms that come referred to some of the ingenuity systems such as the helicopter reconversion system through the performance of the Main Rotor system whose axis is self-assembled in the interior of the vehicle due to the rise and fall of its sections self-assembling telescopic type, whose sections have an embedded and disposable python, automatically by a electronic radio control procedure said Python through the aforementioned procedure fits and disengages into the recess of the section in which it is embedded.

The folding of the blades whose characteristics techniques are shown in Figure 3b) and 3c) of the main patent to get the articulation and folding of the blades and that once folded run through the pipes located next to the axis vertical of the main rotor for assembly inside the vehicle, is essentially achieved with the mechanisms and following provisions:

On the front of the sections of the articulated blades, adhere under the tube, of the section corresponding determinable in the manufacturing process the cable collector (fig. 6- 6,7,9) as well as under a tube of the same section the extension cable (fig. 6-7.5); the rigidity maintenance cable of the blades (fig. 7-8,9), extended under a tube in turn from the relevant section and in the first extendable part, at the beginning From the blade will be located a roller roller (fig. 7- 10), mounted rotatable on two sections of plate, attached in amalgam to the construction material of the blades and screwed in reinforcement with double thread in reverse thread, provided in turn with relevant magnet, so that when the cord packer arrives it winding for correct folding of the articulated sections of the shovels (fig. 7- 11). In the front and back of each of the sections of the articulated blades, in its first section they will locate a pickup roller and another magnetized steel extender available on two perforations, one on each side, so that turn easily, once you reach the extension cable that fired from the bottom of the cabin of the cabin and once the magnet has its effect of automatically receiving and winding the cable over the roller, until you get the winding effect and consequently the extension of the blade (fig. 7-10).

On the back of the blades and in its sections articulated, will be arranged under pin-type recess bolt, the devices through which the cable clamp and force donor for stiffness maintenance and solidarity of the sections of the blades, as indicated in a), b) and c) number 3 of figure 7, without the reinforcing cable is divided into sections, if not it maintains a unit of stiffness throughout its entirety, with the sole exception of a angulatura at the end under the blade of greater section than the rest of the tube, so that running in such a situation inside of the relevant tube since it was fired from the hold, by the relevant trigger mechanism located in it; trying his Once the cable is made of material with some flexibility, for example solid brass, so that it runs better (fig. 7- 5 ', 8', 9 ').

The stiffening cable will be attached to a cable guide that will get rid of him once he reaches the type pins bolt (fig. 7- e, d) and once the cable had penetrated on the pins and detached the guide wire hitch, the safety pin will prevent the stiffening donor cable from being able to get out or detach (fig. 7-3, f).

The small electronic trigger cannons of the extension cables, collector and stiffness giver of the sections of the blades located in the hold of the vehicle (fig. 8- 1,2,5 ', 7), will fire their respective cables by the provision and operation of electronic and electrical systems and the cables can ascend perfectly inside the tubes; next to the small cable firing cannons will be properly placed extension cables and folding of the blades, arranged on either side of the trigger mechanisms (fig. 8-11 ', 21,13', 15 '), so that link and self-insert after the appropriate drive from the cockpit by the driver pilot, at the beginning of the channel cable outlet; they will also shoot the same way, but in its condition of stiffness unit the stiffening cables to the blades, which will be arranged in the form that appears in the (fig. 8-1,2).

Both the extension cables and the cable rigidity are cut, as well as the channels of discourse of the folded blades, at a height that does not reach where it is located the rotor whipping device, so that in its constant and very fast turn, when performing the whipping function of the blades, you will not stumble upon such devices, which in your end will have the relevant operating magnets and consecutive activation, which will be performed as a function of attraction reception of the sections of the same that remained in the end of the back of the last section of the blades articulated (fig. 7- 5 ', 4'b).

The parts of the cables, both retailers and collectors and rigidity maintenance, which will be cut to in turn so as not to impede the whipping of the rotor, they will also be equipped with the relevant magnets features, operated by radio control from the cockpit. of ingenuity, so that they are situated just at the moment of being activated, with their counterparts of the part attached to the main shaft, (fig. 7- 2,1).

The assembly in the vehicle of the whole group rotor, clutches, change and group of blades will be made in order to that adopts the necessary height and width in decrease running the whole group through two wide slides, one in the front and one in the back, on which It will run in a stabilizer rotor clamping bridge (fig. 9-3 ', (1' ', 2' ', 9' ', 12' ', 13' ').

The rotor cable clamp jumper stabilizer, it will carry two hinges that can be attached and detachable automatically for its movement towards the slide (fig. 9- 6``, 7 '').

Pickup and location of rotor blades FRE1 and PRE2 stabilizer (fig. 8-2 3), will be carried out from the position (j) of the same figure, to position (d, f), once that the blade actuator part (fig. 23-g) has disengaged automatically through the appropriate radio control order and running along the surrounding slide of the blade (B), which goes adhered to the pamper by its lower right lateral part (fig. 8-23 h).

The stabilizer rotor blades once made its slide along the slide, through its sliding device, welded to the part (fig. 8-23g ') until its place of location, in position of recollection will be subject at the bottom, by an incision made in the clamp piece of tails (fig. 8-23e), and at its outer end, held by a sturdy rotating tube descending from the tail (A) to which is attached by joining the relevant clamp (fig. 8- 23kp).

Other merely aesthetic additions and to meet social needs, to improve transportation and gain of assistance or physical travel time, They will consist of the following:

In the tails of ingenuity, and specifically in the glue (A) and duly adhered and without overweight and arranged between it and the tail (B), on top of it locate cylindrical enclosures of sufficient capacity to house, a) (fig. 8-23a) a toilet service, so that in its upper part have a hinge for actuating the ceiling at the time that ventilation is needed, and with a devices of a small slide, with a folding lid that can allow that when circulating in ingenuity as a car terrestrial, the wc room is completely hidden from view of the public.

Between the same lines, in its final part, it will have another cabin similar to a) b) (fig. 7- 23b), intended for a small operating room or a small priest's ward, when in case of autocópter destined to some service Rescue public or small store of goods or first aid kit material or small leisure room for recreational activities, if it were a private autoccopter.

Turn on the tail (A) (fig. 8-23c) and on its First section, there will be a cabin equipped with a door descending and provided with the relevant way of producing light and transparency. Intended to accommodate the stretchers for transfer of injured and / or sick, in the case of an autocopter intended for public service or rescue, or an alcove of the dimensions where appropriate, if it were the autoccopter version of private property

In the cellar, in turn the mill will be established the laser system for optical signals in connection with the acoustics on request to be left by other vehicles 35 meters for landing of the autocopter, a message that will project its words in orange and green, in rays projected aliquotically by the central ventral part in the form and arrangement that appears in (fig. 8-17) and (fig. 6-8). In connection with the system reviewed of emission of the laser-central, in the windshield of the front glass of the vehicle, and on the rear will go located two systems of emission of laser rays of the same characteristics for take-off (fig. 6-13,14).

Technical sector to which the additions belong

Additions to the main patent that are propose in the same inventive unit, technical characteristics and functions belong, like that, to the technical sectors of  mechanical engineering of land automotive (automobiles) and of aeronautical mechanical engineering

Background of the additions

There are many blades for rotors of helicopters of different materials and construction structure, but all of them have as common denominator their stiffness, which for use only in the air environment does not present any problem, not so in the case of the invention of the autocopter in which having the possibility to access the cables and parking lots of the cities through its reconvertibility in airplanes, supposed a problem insoluble until the invention of autocópter, by to the installation of a system of folding of the blades through its articulation as described in the description of these additions, which solve it radically.

Descriptions of additions

When ingenuity is reconverted, so that the vehicle work as a land car or automobile and avoid problematic that would involve circulating between the streets of the cities and access urban parking with shovels fully extended and rigid; the blades of the autocopter are already established in the main patent that they would be articulated by folding sections; to achieve said articulation and folding without problematic some, and so that its assembly inside of ingenuity, it is established that you have to essentially get with the devices outlined in Figure 7, and which are the following:

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10) montado, discurrible en rotación sobre dos secciones de pretina adheridos en amalgama al material de construcción de las palas y atornillados en refuerzo con doble rosca, en rosca inversa, provisto a su vez del pertinente imán a fin de que cuando le llegue el cable extendedor lo enrolle para el extendido correcto de las secciones articuladas de cada pala ( fig. 7-10).On the back of the sections of the articulated blades, they adhere under a tube of the corresponding section that can be determined in the manufacturing process of the pick-up cable (fig. 7-5b), as well as under the tube of the same section, the extension cable ( Fig. 7- 5 ', 8', 9 ') and the blade stiffening maintenance cable (fig. 7-9') extended under a tube along with the relevant section and in the first part extensible at the beginning of the shovel will be located a roller roller

 \ hbox {(fig. 7-} 

10) mounted, rotatable on two sections of waistband attached in amalgam to the construction material of the blades and screwed in reinforcement with double thread, in reverse thread, provided in turn with the relevant magnet so that when the cable arrives extender extends it for the correct extension of the articulated sections of each blade (fig. 7-10).

On the front of the first section of the blade articulated will be located in turn, another roller roller (fig. 7- 11) of the same characteristics as the former extender cited for the collection of the blades by winding the collector cable as shown in (fig. 7-11).

Also on the back of the blades through all articulated sections will be provided to each section under recess type bolt pin devices through which will penetrate the force-giving cable for the stiffness and solidity of the blade sections, as indicated in sections a), b) and c) of number 3 of the fig. 7, without said reinforcing cable being divided into sections, but it maintains a unit of rigidity in all the extension that covers the different sections of articulated blades presenting in its final part duly welded a clamp and release clamp (fig.7- 3d) guide wire, cable that will detach from the cable (donor of rigidity to the blades) automatically, once this penetrates in all the holes of the corresponding type pins cerojillo (fig. 7- e) d)); the last section of The extendable blades of a cross-pin fastener stiffening giver cable immobilizer to ensure that once the conductor cable removed and the stiffening cable penetrated to the sections of the blades said cable will not drain or come out (fig. 7- 3 f)), this cross pin fastener of the donor cable of rigidity to the sections of the blades, it will run and enter operation immediately after the cable has penetrated in all the holes of cerrojillo and has separated automatically the guide wire (fig. 7- 3 e) d) and f)).

The small electronic trigger cannons of the pickup extension cables, and stiffness giver sections of shovels located in the hold of the vehicle (fig. 8- 1,2,5 ', 6') they will fire their respective cables using the provision and operation of electronic and electrical systems; next to the small trigger cannons cable launchers extension cables will be properly wound and folding of the blades arranged on each side of the cannons (fig. 8-9.11 ', 13', 15 '), so that they link and autoinserten prior the appropriate operation from the cabin of the pilot-driver; at the beginning of the output channel of cables, they will also be arranged in the same way but in their stiffness unit condition the power donor cables and shovel stiffness will be arranged in the manner shown in the numbers 3 and 4 of figure 8.

Both cable conduit tubes Extenders, pickers and stiffness givers to the sections of the articulated blades are cut just like those ascend from the warehouse of the vehicle at level, above and by under the swinging ventral swing of the main rotor in order to avoid any obstacle to the circular rotation of said whipping (fig. 7- 5 ', 2') being endowed in its extreme end part of the timely operation and consecutive attraction magnets that perform the corresponding attraction based on the attraction of reception for crimping the sections, which will also remain suspended at the last ends of the articulated parts of the blades on its front and back, given that the parties of the conductive tubes of the extension cables, stiffness pickers and maintainers of the sections of the extendable shovels, in turn will be suspended in the sections internal ends of the articulated blades, will be equipped with them  fitting and crimping purposes of all sections and both some like others are infallibly facing each other and can perform the discourse function through the channelers of the appropriate cables perfectly, accurately and chronologically (fig. 7- 5 ', 2', 4b, 1).

The laser system will also be located in the warehouse for issuing optical messages on demand that others vehicles leave space of 35 meters for landing autocópter, messages in luminosity of orange and green rays flashers thrown through the appropriate exits to that effect from the ventral part of the vehicle (fig. 6-8) and (fig. 8-17).

In connection with the laser reviewed system, ventral emission for landing and with transmitter transmission Central, located in the cellar, will exist both on the windshield, front glass, as in the rear glass other devices lifts and descents for emission of the same signals optics in the same color shades of rays, to sue vehicles that circulate both in front and behind, leaving distance of 35 meters for the take-off of the autocopter (fig. 6- 13.14).

Brief description of the drawings

Figure 6: Perspective view of the autoccopter's cellar with its electronic cannon trigger devices or throwers of extension cables, pick-ups and strength and rigidity girders to the sections of the folded blades (fig. 6- 6,8) extension cable, coiled next to the small cannon (fig. 6-7), stiffening cables to the sections of articulated blades arranged in parallel direction in front of the mouth of the launching cannon device
(fig. 6- 8) section of sliding slide of folded blades with head device of one of the folded blade sections, sliding through the slide (fig. 6- 5,11,12); conductive tubes of extension cables, collectors and stiffness givers to the blades articulated by sections (fig. 8- 3,4,5 ', 8'). Ventral laser device for landing and front and rear windows emitting optical messages for take off (fig. 6-8,13 and 14), section of the central rotor shaft with telescopic lifting and lowering (fig. 8-18).

Figure 7: front and back of blades by articulated sections, properly hinged with tubes cable conductors extender, collector and stiffness giver at  articulated sections of the blades (fig 8-9 ') rollers winders (fig. 8-10.11), detail of the main rotor shaft, arranged in ascending and descending sections with system telescopic and sliding section of sliding section of blades folding (fig. 7- 4a, 4b). Detail of the type pins bolt with the stiffening cable to the sections of the articulated blades with details of the guide wire attached to the stiffness giver by means of fit and release devices automatic prior electronic order and of radio-control and pin donor cable clamp of rigidity in guarantee of avoiding that such cable is loose or drain (fig. 7- 3 f) d) e)); detail of the roller roller Extender and collector cables with circular movement on their fasteners and equipped with the corresponding magnet (fig. 7-6); detail of hinge for main rotor articulated blade sections, screwed to double thread, reverse thread, of main rotor (fig. 7-7).

Figure 8: Section view of the mechanisms of electronic firing or launching of extension cables, collectors and stiffness givers to the articulated blades of the Rotor (fig. 8- 1,2,5 ', 6', 9 ', 10', 12 ', 19', 20 '), small cannons triggers or cable launchers by electronic system and radio control (fig. 8-1,2,5 ', 6'); electronic transmission controls of orders radio control for launching or firing cables (fig. 8-10 ', 20'); transmission devices of launch orders received from vehicle cab and transmitted by the transmission controls (fig. 8-12 ', 19); guide wire winding of the stiffening cables to the paddles articulated in sections (fig. 8-9.11 ', 13', 15 '); system central laser emitting optical messages so that others vehicles leave 35 meters of space to land the autocopter (fig. 8-17); Tail A, new compartment with sliding door and windows to be used for location of stretchers, two small rooms for the operating room and WC (fig. 8-23 a b).

Fig 9: Rail travel mechanism (3 ') of the main rotor group (2', 13 ') and of the main shaft (8') to achieve reduction of height and width in the assembly in housing, by means of fitting and disengagement of the group and bridge of stabilizer rotor housing (5``, 6 '', 7.8``, 9 '' and 10 '').

Description of a preferred embodiment

In view of the drawings described above it can be seen that the preferred embodiment of the Additions formulated for the main patent is as follows:

Figure 6: The system for the embodiment preferential and perfect functioning of the articulation and dismantled sections of the main rotor blades, will be two cables under tube, one extender of the blade sections and another collector of all sections also under tube, (fig. 6- 2,3) (fig. 7- 5 ', 5b, 8', 9 '); shooting or releasable cables from its storage in the cellar of the vehicle by mechanisms electronic, of small firing cannons through the timely order message by radio control (fig. 6- 6.7); stiffness giver cable to the articulated sections of the shovels under tube (fig. 6- 7,8); Main Rotor shaft section with self-assembly device with telescopic system (fig. 8- 4 '), section of the slide intended for the blade sections of the main rotor, to place them in the place of location in the vehicle that corresponds to them (fig. 6-5); Pallas folded and sliding device detail by the slides (fig. 6- 11,12); a laser control system for optical emission  launching messages to other vehicles on request for space to land or take off (fig. 6-13,14).

Figure 7: The conductive tubes of both extension cables such as collectors, as well as from the giver of stiffness to the sections of the rotor's articulated blades main will be cut as well as the sliding section paddle slider already folded to the height of the device ventral whip (fig. 7-5,4b); to avoid obstacles to rotary-rotating function of said device; These sections run through the right place at the time of unemployment of the baton lengthening to join the sections cut to its once below the batting head (fig. 7- 1 ', 2) and when going one and the other endowed with the appropriate magnets at their ends can be activated and deactivated, it will be accurate, fair and chronometrically the crimping of both for the perfect inside of the corresponding cables; the articulated sections of the poles will also carry, for the purpose of perfect confrontation and circulation inside the tubes, of the relevant cables in turn at their ends the corresponding activatable and deactivatable magnets; on the front of the sections of the articulated blades will be located the tubes conductors of the extension cable (fig. 7-8 ', 9') semi-mated with The construction material of the flanged blade consistent and in turn in the last outer section of the blade is place a roller roller attached on two strong plates with  central hole to receive the roller shaft and that it can perform your winding circulatory movement when said in turn equipped with the corresponding magnet (fig. 7-10).

The clamping of the blade sections by the reverse once extended and giving them enough strength and maintaining its rigidity when the blade cuts the air, in its strong and very fast rotating movement, will be achieved by the placement in the pin-type shovel sections bolt amalgamated with the construction material of the blades and double threaded and reverse thread threaders (fig. 7- 3a) b) c) g)), the stiffening cable penetrates into said bolts, the one who has once penetrated all the pins guided in his path through the conductive tube through the guide wire, automatically, the guide wire clamp opens detaching from the stiffening cable and immediately the insurer pin will seal the rigidity donor cable for the purpose to ensure that it will not slip or detach (fig. 7-3 d) e) f)).

To prevent the conductive tubes of the extension cables, pick-up and stiffness giver to the sections articulated blades, as well as the slide through which folded blades will be moved to the places of location, inside the vehicle, could hinder rotation of the ventral beater of the rotor head, so they will be cut immediately above said head (fig. 7-5,4b)) and equipped of the pertinent. activatable and deactivatable magnets, in turn the rest of the sections of the mentioned tubes until the mechanism launch of the winery and the slide to the places of location of folded blades will also be cut immediately below the ventral batte head of rotor (fig. 7- 12) for purposes not to obstruct the rotation and timely, this sections will also be equipped in their ends of the corresponding connectable magnets and disconnectable so when the batter head is in the proper position and the radio control is received launch order of the cables for reconversion in aircraft and previous consecutive connection of the action of the magnets, the sections cut, with the appropriate extension devices can be embedded just, accurately and mathematically to perform the conversion and conversion function, as well as the driving of folded rotor blades (fig. 7- 4b, 5 ', 1', 2 ').

Figure 8: Systems for realization most important practice of the object of the patent that is now add, fold and articulate the main rotor poles and the execution mechanisms are determined by the existence of the conductive tubes of the extension and collection cables of the blades, as well as the stiffness giver to them once extended (fig. 8- 3,4,7,8), the cables that after being collected, rolled extenders and pickers, stagnant in the winery, disposed its end tackled next to the electronic cannon trigger or launcher (fig. 8-9 ', 13', 15 ', 21), driven by the electronic radio-control order through its conductive tubes until reaching the winding roller that tense or disconnect by distending them, where appropriate for the conversion or conversion of land vehicle to air vehicle; the stiffening cables to the blades will be in turn arranged in parallel in their rigid condition quasi vertically to the firing cannon to be launched according to the timely order of radio-control and gifted in their ends of the adhesion device and the guide wire, whose all will also be rolled up next to the cables paddle stiffness givers (fig. 8- 3,4 ', 7,13,16,21).

The shooting cannons launchers ready with the corresponding dedicated cables will be activated and placed in operation through the appropriate orders of radio-control ordered in the cabin of the vehicle by the pilot driver and transmitted through the two exchanges electronic stations and their corresponding transmitting stations secondary (fig. 8-10 ', 12', 19.20).

The laser system for launching messages optical together with the consecutive acoustics at the request that other vehicles leave a space of 35 meters, to take off and landing of the autocopter, composing each emitter tube in color orange and green the words of the message just like the vehicle front and rear glass device for take-off messages that will work in extension of the central laser station, located in the cellar (fig. 8- 17) and (fig. 6-13,14).

In the first section of the tail A of the mill in addition to the watertight compartments that were described in the main patent for luggage compartments and for fuel, the ingenuity of another compartment will be provided for dedication to contain stretchers for the reception of injured or injured in the event that the autocopter is dedicated to public rescue and lifeguard or ultra ambulance service fast (fig. 8-23c).

Between queues A and B of the mill, they will be located two circular cabinets with sufficient dimensions to install, respectively, in a) a toilet, with a hinged roof to provide ventilation and light, equipped with a curtain horizontally movable, so that when the vehicle runs as land car, the toilet is not visible from the outside (fig. 8-23a), in turn, in queue B, another passenger compartment, the b), to provide the vehicle with a small operating room or a small priests room, for urgent medical care, when try salvage public service autocopter and Lifeguards or ultra-fast ambulances and in case of autocópteros private the cabin will be destined to a small living room or of recreational recreation or first aid kit.

Claims (11)

1. Mechanisms assembled axis of the main rotor of the Autocópter by telescopic type lifting and lowering device by self-assembling sections by nestable and detachable pythons; and of the stabilizer, nestable and detachable by sliding to assemble between the tails of the vehicle. Folding and unfolding of articulated blades by means of extension cables, collectors and stiffness givers, located on the front and back of the blades. Cable release by small electronically excitable cannons by radio control. Provision and adaptation in the tails of a small operating room and a WC, with necessary hygiene and aseptic systems and concealment of external vision when the vehicle is running in an automotive version
land. 2. Self-assembling mechanism of the main Rotor shaft, according to the first claim and according to the present claim, characterized by a telescopic type lifting and lowering device operated for both positions by means of radio-control orders issued electronically from the control cabin, each section of the shaft having a python fitted in the relevant recess of the section in which it is assembled, withdrawing in turn in the same way (fig. 8-4). 3. Mechanism of extension and folding of the sections of the articulated blades of the main rotor of Autocópter, according to the first claim and characterized according to the present claim by the provision in the part of the obverse of the sections of the blades, of the corresponding hinges adhered with semi-thinning with the construction materials of the blades screwed with double nut of reverse screwing, alternated by the reverse side, every two sections with the same adhesion characteristics (fig. 7-7). 4. Extension and folding mechanism of the sections of the articulated blades of the main rotor according to the first claim and characterized according to the present claim by the provision on the back of the sections of the blades, of the main rotor of a bolt-type pin in each section, also adhered by amalgam with the material of manufacture of the blade and reinforced with plates welded and amalgamated with the same material, screwed with double screwed in reverse (fig. 7-3 abc). The bolt-type pins shall be properly calibrated so that the cable holding stiffness and strength giver, crosses them without play but also without any impeding obstacles (fig. 7-
3 abc), both in the extension as in the removal of the cable, once said force and rigidity donor cable is penetrated and the guide wire detached, a pin will fall to close this cable (Fig. 7-3 fde). 5. Folding mechanism of the sections of the articulated blades of the main rotor according to the first claim and according to the present claim characterized by presenting on the back of each blade the appropriate conductive tube sections of the pick-up cable (fig. 7- 8 ', 9'), recessed semiamalgamated with the material of the sections of the blades adhered in half a channel, reinforced the grip with pins, keeping each tube section a perfect confrontation, millimetrically exact in its confrontation, so that it runs through inside the collection cable without any difficulty or obstacle; also it will appear in the last part of each section of the tube and will present at its final end a groove properly cut to be able to bend by bending and folding on the blade (fig. 7-8 ', 9'), since this last section does not it will be amalgamated, but fixed with pins; however, if these pins will be amalgamated in support for the tube, this section of the tube will present at the end of the corresponding part of the magnet tube to facilitate in its moment the confrontation of these tube sections with the section attached to the axis of the main Rotor which at the same time, it will be cut at the level of the ventral bevel of the main rotor (fig. 7-5 ') whose section at the same time will be equipped with the relevant magnet for the purpose of perfect confrontation with the tube section of the last section of the blades and that the pick-up cable in its day, when fired from the firing mechanisms, the guide wire can circulate under tube without any difficulty or lock, also the last section of the blade will have attached in the same way and In this way, the guide tube of the rigidity maintaining cable of the blades is also cut and provided with the corresponding magnet for the purpose of perfect confrontation with the guide tube part of the stiffness maintenance cable that ends in the first section of articulated blade just at the mouth of the first bolt type bolt in which the maintenance wire will penetrate, will have the same power of small rotation to stick and bend over the section of the articulated blade, ( fig. 7- 5bc) and will also carry, at its end, a terminal clamp the relevant magnet can be activated and deactivated. The conductive tube of the rigidity-giving cable to the blades will be cut in turn at the height of the beginning of the ventral beating so as not to hinder the rotational function of such a beat and will be provided therewith. instead of the corresponding magnet and an envelope tube to lengthen, to turn to face the section of the same tube that in turn will have been centered below the ventral beat, both sections attracted to each other by the force of the magnets to disengage a Once the force of attraction of the magnetic fields ceases, disconnecting the magnets for the appropriate collection of articulated blades, as evidenced by all of them in (fig. 7- 5 ', 8', 9 '). 6. Extension mechanism of the articulated sections of the blades of the main rotor according to the first claim and according to the present claim characterized by presenting on the back of the sections of the articulated blades the corresponding sections of the conductive tube of the maintenance cable of rigidity in small semi-heated pipeline with the construction material of the blades reinforced with the pertinent double threaded fasteners in screw arrangement in the provision of counter-threads, these tube sections will in turn be equipped with the relevant magnets. In the last articulated section of the blade, a rolling device with a rotating roller, embedded on both sides, will be located in two strong semi-flattened plates with the construction material of the blade, screwed in the same way and arrangement as the conductive tubes. The winding roller will in turn be equipped with the relevant magnet for attraction depending on the winding of the extension cable, once it is driven after it is fired from the hold of the vehicle by the appropriate trigger mechanism and reaches its contact with the winding roller ( Fig. 7- 10.11). 7. Self-assembling mechanism in the motor vehicle of the folded articulated blades of the main rotor, according to the first claim and according to the present claim characterized by slides located on the back of the last part of the articulated blades and cut after a curvature to the height of the ventral and with another piece of sliding adhered for elongation (fig. 7-4b) and that continues after saving such a mixture until each of the four places destined in the corresponding interiors of the motor vehicle, destined to house the blades folded Each part of the slides has a central canalization with two wide tabs whose sliding and sliding embedded in the tabs of that runs the device that for this purpose on its front, carries the last articulated section of the collected blades whose sliding is done by the relevant order issued for this purpose or by radio-control from the vehicle cabin (fig. 7- 1 ', 4b) and (fig. 6- 5', 12) and with the corresponding elongation (fig. 7- 4b). 8. Mechanism for the extension and collection of articulated blades of the main rotor according to claim first and in accordance with the present claim made through of the relevant cables conducted, through the corresponding tubes and the rigidity donor cable to the blades extended and its tube, all done from the cellar of vehicle the relevant small type cannons, of the used for launching torpedoes and missiles in submarines and aircraft electronically operated by means of relevant orders issued for that purpose by radio control (fig. 8- 3,5 ', 7,16). The cables Extenders and pickers will remain properly wound with the starting end just to the mouth of the small canyon that when fired would lead to the conductive tubes once the firing order is issued through radio control (fig. 8-9.11 ', 12', 15 '). The cables rigidity maintainers of extended blades will remain embedded, perpendicularly and placed in parallel. The section of the tube in the extension that in the mouth they require these cables will be the right one so that properly adjusted they can be shot but in the section corresponding to the small angle below the corresponding first sections of the paddles in the slightly angled entry maneuver the section of the conductive tube will be hooked in the section you choose the perfect cable maneuver, anyway this cable is will ensure that, despite the role it has to play in giver of rigidity to the blades, be made of a material that without losing its base hardness, however, has some small chance of slight flexibility, for example of solid brass and in that way its arrival to the type pins is totally satisfactory lock in which it has to be embedded. These wires they will represent in turn, at its final base a fitting device and disconnect from your cable guide subsidiary the one who himself it will remain wound next to said maintenance cables of rigidity for its provision of guidance function and at the time of collection, for when the vehicle is converted into a car terrestrial, always coming into operation, prior to activation by the relevant order issued by radio control from the cockpit (fig. 8- 21,22) and that electronically fired both the main cable paddle rigidity maintainer as the guide subsidiary they will lead to the respective conductive tubes (fig. 8- 13 ', 14', 21.22). All firing and driving orders of cables, transmitted from the cabin of the vehicle, will be in turn retransmitted through the corresponding exchanges electronic devices (fig. 8-10 ', 20). 9. Mechanism for collecting stabilizer rotor blades according to the first claim and characterized according to the present claim for discarding the container part of said blades electronically and mechanically from its axis, in order of radio-control and prior sliding by sliding arranged in the glue (B) in its lower right part will be housed between the tails (A) and (B) held on its inner side by the relevant slot of necessary width and calibration made in the tail clamp piece and on the outside by a fastener swivel plate lowered from the tail (A) attached to the tail reinforcing beam and also reinforced by the corresponding clamp (fig. 8-23 PR1, PR2,
kf) Q. 10. Provision on the tail A of the vehicle of a passenger compartment according to the first claim and according to this claim characterized by having on the floor part sliding doors with clamping mechanisms for securing stretchers, with a sliding and sliding ramp for access and evacuation of the stretchers, retractable, which in its back will present a door for access to the interior corridor that communicates said passenger compartment with other services and departments of the vehicle and in the front part that faces the exterior will present a sliding side door that can be fitted with sliding doors that will have windows in turn, on its upper part, a sliding glass cover to provide ventilation and light and a curtain of sliding canvas material on the roof to avoid its visibility from the outside when driving in a vehicle as a land car (fig. 8-
23 c). 11. Provision between tails A and B of two circular cabinets according to claim one and the present claim, one characterized by having an optional technical installation for surgery, a small operating room, a cure room and small aids with sufficient and relevant enclaves for securing the operating table and cures, and the cabinets of surgical material and with a lamp of necessary illuminative power, which in its back will present access door and communication with other rooms and dependencies of the vehicle; and another destined to the installation of a WC with sanitary devices of properly fitted and anchored and with provision of aquifer supply and provision of crushing and eliminating mechanism by means of the relevant chemical substances of the detritus; having on its upper part a covered sliding cover to provide ventilation and light and that its interior is not visible when traveling as a land car by means of a sliding canvas curtain
(fig. 23- b).