DE3412008A1 - Cellular air cushion watercraft or cellular and finger-type air cushion watercraft which can be driven by all land vehicles, can be converted into an aircraft and converted back into a land vehicle/propeller-driven watercraft without lift drive - Google Patents

Abstract

The invention relates to a technical development and a supplement to the Patent Application P 3247168.8 and is characterised, as can be seen in particular from Figs. 1, 1a, 1b, 1c, in that in accordance with this development and these features L/I, L/II, 11/15, 11a/20, 20a the air cushion watercraft is only ready for use [lacuna] and in that it can be converted into a trailer 8a and 11/11a with wheels 32b and in that this wheeled trailer 8a and 11/11a is constructed in terms of its content in such a way that it can be converted not only into the cellular air cushion watercraft 20 and into the cellular and finger-type air cushion watercraft 20, 15 but also into the air cushion watercraft/aircraft with carrying-wing connecting element 6a with side walls 6b for acting on the ground, and in that this wheeled trailer 8a and 11/11a is constructed in terms of its contents in such a way that it can be converted without a large degree of expenditure from the air cushion watercraft alternately into all the flying elements 6, 6a, 9, 10, 12, 18, 6b, 21c, 41, 49, 49a, 49b, 33, 33a, 34a, associated with the prior art, in that these insertion bodies can drive the air cushion watercraft/aircraft in different ways 28, 28a, 28b, 37a, 37b, 4, 4b, and that these insertion bodies, as a motorcycle 2aa, cabin rollers 2ac, caravan 3 and the car 2, can also be released 35a, 35b, 22I, 22II from the air cushion watercraft in such a way that in this case the aforesaid bodies become independent aircraft and that, finally, in accordance with this air cushion watercraft/aircraft embodiment of this air cushion watercraft/aircraft [lacuna] into a car 2-, motorcycle 2aa and ... Original abstract incomplete. <IMAGE>

Description

Cell hovercraft or cell and finger hovercraft through 'all land vehicles drivable, to the aircraft convertible and convertible back into a "land vehicle propeller boat without lifting drive

The laid-open specifications DE 30 33 938 are used as a generic term A1, and DE. 32 47. 16.8. At benanixt .. · ■ -

Although the above disclosures by the same applicant the basis on the · propulsion area of a hovercraft reveal anew in which a motor vehicle or caravan provide the thrust and lift for this hovercraft, so it is only with the features of this further education that * This hovercraft is ready for use.

The further technical development preferably starts with the home registration · DE · 32 47.16Si A1, 'so .that with regard to the applicability of these designs according to the above Offanlegungsschrift, "in this additional application in marked Form for building through L / l and L / II stables is taken.

As a result, these statements will be made after the last disclosure document in connection with the construction lead-throughs L / l and L / lI brought the respective versions can also be used.

Due, diesu tfufbaumöglichkcitan L / L, L / Li cas hovercraft under all Fluggarät feedthroughs, einatzfähig _tt Further, the cell hovercraft / aircraft to the cell and finger hovercraft / Fluggerä ^ ferfindungsgemäö changeable. And finally, after this .aufbau implementation of this air cushion / aircraft in an automobile, Hotorrad- and bicycle propeller boat without lifting drive, preferably according to the Offenlegungs ^ documents DE 30 49 833 A1 and DE 30 29 763 A1, if z. B. these drive bodies do not have sufficient drive power for the simultaneous thrust and lifting drive> or if a propeller drive without lifting drive should be preferred.

Even when choosing the appropriate structure implementation detach the land vehicle from the hovercraft in order to self-contained land vehicle missile.

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Re. Hovercraft construction implementation L / l First, a supplementary set-up is proposed, in which the hub-propeller sheathing that is below the circular Floor plank section IIl / θ and boat floor detachable is attached, in connection with the adjustable support brackets and tension bars for the holding structure and thus for reducing the weight of the land vehicle including the driver, These adjustable support brackets and motorcycle stands also preferably ensure a certain resting pressure from the Land vehicle drive wheel or drive wheels, preferably one Roller for preferably two propellers / sheaths for the thrust, and at the same time the lay-on pressure is too preferred

a roller for the propellers / coating for the hub ν

determined, while the transmission force is preferably carried out by V-belts and loop shape is accomplished.

When operating these lift propellers, the resulting air flow pressed to the free spaces under the boat floor, so that here according to the invention by this stable clamping strips / cell delimitation a large air cushion can arise. This compressed air also gets into the already according to the invention named "clamping strips / cells" · so that in addition to the large central air cushion in a known manner, small air · cushions are created around the boat to limit the loss of this compressed air.

According to a special feature of the invention, these cells stand with the lower soann strips around the entire boat so detachably ■ in connection that these cells can also be individually exchanged, and moreover own this. '' Cell supports, tension bars and holding ropes so that there is a stable holding structure in the lower area of the boat against the air cushion pressure. Incidentally, in this construction implementation according to the invention the cells are detachably attached to the lower clamping bars so that these cells only protrude towards the interior so that they can be removed from it Air cushion space can also be conveniently supplied with compressed air can.

Due to the fact that the land vehicle and the driver about the bulges of the boat hull and floor planks occupy a high position per se, becomes with a heavy load during use be counting. In order to limit these negative properties as much as possible, the measure will preferably have to be taken to ensure that the boat has additional Uulste, which can preferably be inflated by a bellows

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around the entire boat. Da-6> se - Hlur & te stand with the hull of the boat not in connection, but are according to the invention to the Outer sides of the lower clamping bars so releasably attached by clamps that at. a collision these clamps in · their. " entire Can give in diameter, and are preferably made of elastic plastic and no internal bracing own.

The high load is also limited with this implementation, in which the upper tension rails also offer a safe and padded support structure in the driver's area.

Caused by the three power-transmission splits already mentioned, on the one hand an effective power transmission to the individual lifting propellers / sheathing and thrust propeller sheathing transmitted, but the other hand is through this Force distribution with additional force losses are to be expected, so that with these power losses, more powerful land vehicles were used PS power are to be claimed, which are also in connection with this build-up implementation through "the mentioned effective performance preferably for international racing events as an air cushion boot-Fitzer- are to be used.

Re. Air cushion construction implementation L / II. The situation is different with a further construction implementation. In this case, a far lighter and less powerful land vehicle is preferably also an all-terrain machine claimed, in which instead of the three force distributions preferably only one V-belt transmission at the same time for the Stroke and thrust in a modified form according to the disclosure document DE 3G 33 938 A1 of the applicant takes place.

In contrast to the implementation in this reference document the propeller sheathing is not preferred among the Floor planks, but preferably at the stern of the hovercraft Detachably interrupted in the suspension frame for pushing and lifting. Several air screws will be used in this build-up - Jackets for simultaneous thrust and for the hub or preferably a larger propeller casing Mounted for the thrust and lift, in which the multiple or preferred - ueisedie one propeller sheathing on preferably two Parts is divided.

The upper part of the air outlet is intended for thrust and It is not disguised, so that the air pressure in this area is unhindered accomplished the thrust-recoil.

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The lower division "- '- ^: - · -" * - - "- · .., has the effect that this air flow cannot exit directly, but reaches Dun Schürzsn / üJulstan through Werbindunijs-L'uliVCB. These aprons / Uul ;; to have erf indun-jsgemafl elastic retaining brackets, which are not legibly connected to the boat body, but preferably to the lower tensioning bars, and are exclusively supplied with compressed air by the propellers / sheathing

In contrast to the above-mentioned construction implementation L / l are at this build-up implementation L / lI the cells in the lower area of the S Then strips are detachably attached in such a way that these cells protrude to the outside to be comfortably removed from the cited aprons compressed air is supplied.

Also are preferably for each clamping bars / cell for this Air flow oval openings in the lower area of the aprons / uulste available.

According to the invention, the clamping strips / cells exist in this construction implementation from «preferably two cells, in which the outer cell is releasably and firmly attached to the clamping bars so that their Section "points to the air cushion space.

In the interior of the releasably attached. Cell is another cell housed rotatable and latchable and preferably has the same cutout as the outer cell, so that the Soann strips / -ZeHe immediately turn into one. The clamping bars / fingers can be moved if the two sections of these cells are superimposed by turning stand and snap into place.

This combination has great advantages in that these clamping bars / cells as quoted in clamping bars / fingers can be switched.

A serious feature of this invention is that, if necessary, the air flow for the central air cushion and the surrounding Air cushion field is corrected so that every second cell or every third cell can be converted into fingers according to Uunsch. If required, the central air cushion or the surrounding air cushion field can also be dispensed with entirely.

The decisive factor in this invention is the feature that the air cushion boat can achieve the best possible results through this combination of options. "Limbo" _r and "lower air intake" may .werden set.

Another feature of the invention is the fact that the inner rotatable cell is arranged so that it can be pulled out as a finger, so that due to a substantial extension of the finger

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it can even be used at sea in rough seas uird.

In this preferred construction implementation, the positive one is also It should be noted that the floor planks in the area of the supports around the boat only form a frame or this collapsible frame is completely dispensed with. This process increases the weight of the boat itself reduced.

Furthermore, "it is proposed according to DE 3G 29 763 A1, that also you in this hovercraft execution the preferably two-part exhaust of the land vehicle with preferably a drain / linkage detachable ^ rJiuriden ujijrd, This means that the exhaust gas also enters the cabin in a clad Free can get. By the way, this outer skin has a tension In the roof-rear area, this outer skin is designed to be detachable and rollable.

According to a final feature - of the two mentioned construction throughputs - in these two cases, the elastic seal is not on the blowable / Uulsten or aprons / Uulstsn _# . but _t releasably secured to the inside of the mold clamping bars and that is detachably attached under the boat bottom, a holding Kiel, on the one hand has the task to keep retired heavy se land vehicle via the air cushion space, and on the other hand upright when using also the retaining structure relative to the air cushion to obtain.

Should a trip as a propeller boat without a lifting drive take place, then · is to choose the construction implementation L / L, in which the drive wheels or drive wheel on, preferably a push-roller, releasable is attached.

The following design content is more influenced by the aircraft, in which the hovercraft preferably has the task as a Undercarriage of a so-called soft landing takes over, and taking into account the torque of the rotary wing the boat the ' Accomplishes compensation, and that with the hydrofoil as a hovercraft / Aircraft wing ΙΓ can be used for ground impact. According to the invention drives in this proposed implementation - the Kfz./FIo tor wheel to Uahl the hovercraft as a speedster or the converted hovercraft as a missile.

According to the state of the art, the following statements exist today -of aircraft: »Drachenflügler», Tragflügler », TragflüglerlI",

= - no - * - "- ^{1 sw}

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"Rotary wing aircraft", and rotary wing aircraft include: "Gyrocopter", ■ "Flugicopter" and "Helicopter / Helikoptsr".

And according to the invention, the Flitzer air cushion system can be converted into these aircraft designs. "; The following features;. Pertaining to the rotor wing aircraft I & II, ailerons and Drachenflügler Tiragschrauber, ^are technically 'uerainfachtsn features uorzugw for Lu-ftkissaahao.ts-HU.fh.au bushing according L / li in claim. to take.

The boom structure is preferred. constructed so that on this Linkage structure of a flying sail or a hydrofoil, or a support ■ · Wing connector, bzu, hydrofoil / hydrofoil connector with Seitenuärtden 'is housed and releasably fastened, and that with this design the .. Hydrofoil / hydrofoil Is tut zen / S ei te nuände, ailerons preserved, urrri that the hydrofoil / Tragflügslstutzen rigid and detachable firmly attached to the boom assembly by pulling the rotor head ropes through "- the rotor head axle eyelets slide and the rotor head is not inclined participate. By this fact, according to the invention, the inclination on the wobble structures produced by the footplates has been achieved is passed so that the rotor ropes this inclination uon. received the tumble louvers, and through the bores of the wing / wing connector and rotor head axle eyelets, so that on the other hand in the wing / wing liner Coupling rods of the ailerons housed in bearings, the rotor cable ends are attached to these coupling rods so that this inclination is passed on to the ailerons in the form of a rotation transmission. And also in the lower area of the The wing / wing connector will be at the same angle of inclination starting with the tumbling scales, carried along in the one also in the lower one Area the rotor ropes uon. the wobble balance to the coupling rods the ailerons also transmit the inclination in the form of a rotation transmission.

And as the 'further development of this application will show, hydrofoil parts are attached to port and starboard on the wing connector, so that the preferred. two-part wing pieces connected by hinges without the preferred and two-part also by preferential Hinges connected • hydrofoil parts according to the invention for the hang glider or flight screwdriver and with the hydrofoil parts, can be converted into a hydrofoil for the hydrofoil.
In this regard, this embodiment is in a special embodiment

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to see the feature, such as the above-mentioned extension the invention already indicates that both sides in the area The hinges of the wing support, the so-called coupling rods are housed in their bearings separated by the hinges, and with the separate right and left rotor cables rotatable with the right bzu. left wing socket aileron stay in contact.

The solution is also to be seen in this feature that the wing parts, which preferably snap into place on both sides, likewise preferred a coupling process between the two-part hydrofoil connector coupling rods and the two-part hydrofoil part coupling rods takes place -. so that the inclination of the rotor ropes not only to the wing / wing support • sn ailerons on both sides, but also to the wing parts ailerons on both sides is transmitted rotatably, so that when you press the right footplate without wing parts, only that right wing socket aileron, bzu. when the lin -

ken base plate with wing parts, the left wing nozzle and wing parts - aileron deflect bzu. vice versa. And that the tensioning cables used in this embodiment are supported by tensioning devices, directly from the linkage attachment points to the wing / wing connector, to the side ' walls or clamping walls with the support of the same Soann devices, also be effectively braced. It should also be pointed out that the footplates on both sides have a counter-voltage so that you can perform the described task correctly, and only for both parties Ailerons are hydrofoil / hydrofoil connector as aileron control can be used.

The two wobble relays are on the one hand with the footplates, and on the other hand with the ailerons in connection, so that the upper wobble balance fingers with the footplates on the one hand, and the lower wobble balance fingers on the other hand, with the counter-tension are also connected on both sides.

"This also represents * jf ^cn JL ^{s he} k tasks as height control can fulfill, in this version only determined the upright and vertically swiveling fingers for the elevator. The uorzugsw. Two-piece Höhensteuerse'il is rotationally transferable attached to the elevator rotating rod. The slide without rotor ropes for the rotor, but equipped with elevator ropes,

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should preferably be used for the wing / wing connector. · ■ ■ · In contrast, the slide is with rotor cables for the rotor and equipped with elevator ropes for the rotary wing aircraft to use.

According to the invention, preference is given to the hang-glider. the hydrofoil connector suggested with ailerons, and that in this version the rudder ropes for the hang glider need an extension. ^ By the way, by performing the above., The task the navigation can be done so that the hovercraft turns into a hang glider and. Hydrofoil bzu. Hydrofoil II convertible is. Hydrofoil II with ground impact.

According to the invention, the hovercraft is preferred in a further embodiment. converted into a rotary wing and driven by the motor vehicle / motorcycle / cabin scooter and accelerated against the air flow until this air flow moves the rotor. This process is favored by this measure, in which the vehicle. _} that should speak in the course of this application for all of the mentioned insert bodies, vorzugsw. two propellers / jackets for the 'forward motion drives to get through this ro-. tor the appropriate buoyancy, so that the converted hovercraft preferentially. from a hang glider or hydrofoil to a gyroplane.

For the "l to use a flight screwdriver / helicopter, Sodenolanken-bike trailer and linkage assembly 22/1, 22 / are 1I concern preferably the Luftkissenboats Construction performing L / the following features. In part, these characteristics have been technically verainfacht.

The car. can operate the hovercraft / aircraft in several ways drive. One of these drive options is that a motor vehicle '.- drive wheel or drive wheels ^ the on bzu. in the collapsible Drive floor plank-mounted sliding claws, and these Rotational movement of the preferably under the joinable floor planks attached "bzu. attached generator received and pass on the generated energy to the power engines / propellers for the lift, thrust and to the rotor, so that the Hovercraft / aircraft from the gyroplane into a helicopter

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about bzu. Can be moved around the helicopter.

The change mentioned has become possible with this version, because the rotor had received a drive.

According to a preferred feature of the invention is the fact that vorzugs'u. a car. , the leaves change from the prior art zugehörenda _n aircraft on the type of caravan cars or even ain Caravan by airboat in an aircraft in accordance with those versions. Except for hang-gliders. Another feature of the invention is that especially in this embodiment with the. Caravan automobiles also prefer the drive features with the power generator. are to be used. Preferential should be a bzu. Several power generators in the automobile caravan are directly connected to the drive elements, and the generated energy is supplied to the power drives / propellers for lift, thrust and for the rotor, so that in this version too the hydrofoil can be converted into a gyroplane . To be able to move helicopters. In this regard, the invention should make use of the feature that said drive process occurs when the drive wheels of the motor vehicle are stationary. is carried out because the drive motor of this body drives the power generator in idle mode and this power generator also supplies all power drives / propellers, including the rotor, with energy.

According to an essential feature of the invention are on the other hand in the execution with the. Caravan use correspondingly strong additional drive motor ^ in use. These additional Drive motors are directly connected to the propellers / Jackets in connection. This also applies to the rotor, so that this version also changes from the air cushion traot into a of the flight types mentioned can be changed.

Furthermore, according to the further development of the invention, it is preferred. a Floor plank wheel hanger proposed in the assembled Condition of the vehicle. taken in tow. In this embodiment, the floor planks can be joined together Named floor plank trailer. The reason for this measure is that the floor plank wheel trailer will soon be ^ -ster Time in a container for the hovercraft bzu. Hovercraft / aircraft can be joined together, and in front of this container

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'Zugsu. zuei rubber wheels are releasably attached. The side panels exist uorzugu. from the two-part screws / sheathing, whose. Protective grille come to lie on the outside. The bottom of the boat is also drawn into this container. According to the invention is preferred for this version. the advantage to see that all operational parts mounted on the floor planks, even during assembly to the container, not to be dismantled. And that it is preferable to attach them to these floor planks Roller for thrust, transmission to the stern, uorzugu. from V-belt, single-track bzu. '·' Zueispurig be used, and that for the rotary transmission of. the caster via the transmission means to the lifting propellers and on the other hand uorzugu for the rotation transmission from transmission means at the stern to the thrust propellers. a loop shape in use taken.

If you intend to convert from gyrocopter to airplane and helicopter, you should first think of a motor drive that can also drive the rotor, so that it is assumed that the airplane has a rotor driven by a fiotor, a tail rotor ... and a traction or pusher propeller. In order that this process can be transferred according to the invention to this proposed embodiment, it is necessary that preferred. a roller circuit is to be mounted on the floor planks. Through this implementation, in a Schaltuorgang the of the Kf z, drive wheels bzu. Drive wheel driven hub sliding roller, tapped. Through this

■ Measure uorzug.su the turning movement. about a mirror that is known per se Transfer means conveyed to the rotor head. This rotor head approach stands with the. upper rotatable retaining cross rotor head part inseparable. The flexible transmission means, known per se, can preferably be detached from the rotor head attachment attached. This solution found drives the motor of the motor vehicle according to the invention. the propellers as a hub, the propellers as a thrust and by the Schaltuorgang the rotor. By this switching process is uorzugu in this version. the prerequisite was created to first transfer the gyroplane into an airplane helicopter. with hydrofoil connection to convert. Incidentally, the rudder controls are also used in this version in this way ensures that when operated

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movement of the Kfζ.-handlebar, this inclination angle made about the front wheel, the pivot plates, and control cables to the preferential rudder attached on both sides uird.

It is known that the main rotor of the rotary wing aircraft is used for lift

. generation and the tail rotor for torque compensation from the engine driven uird. To the hovercraft according to a special one To convert the feature of the invention into a rotary wing aircraft is vorzugsu. to remember that the rotor blades, rotating in the predetermined direction, the hull of the hovercraft into the try to turn away in the opposite direction. This response is called torque.

In order to eliminate this reaction in the proposed design, an example of torque compensation in the coaxial rotor system is cited. In the case of the coaxial rotor system, it is known that two rotors, one above the other, rotate in opposite directions. If both rotors have the same blade diameter, they need the same torque so that the fuselage remains in its original position.
So that the hull of the hovercraft is in its original position

. · Can also pause, the rotor rotates on the boom assembly in the opposite direction to those under the floor planks also rotating lifting propellers. The difference is there in the large rotor blades, which offer greater performance than the lifting propellers. According to the invention can this difference is compensated, if preferred. several propeller blades on top of each other in a casing or several original propeller jackets underneath the bodan planks can be used. In addition, differences can also be compensated if the sliding rollers are connected to the transmission means have corresponding speed differences. Differences can also This is compensated by the use of wing nozzles and rotor blades that are shorter in length, since these are Hydrofoil connection with respect to the lift, the rotor blades accordingly relieve. . *

The rotor head attachment is designed so that it connects to the upper part of the retaining cross is inseparably attached and preferential. to the untar remaining rotor head parts acts as an axis. It should be mentioned in this regard that the swivel rope _ Lower part on both sides swivel axes for the boom assembly

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Has snap-in eyelets. The frame assembly snap-in eyelets are like this formed that sis although the corresponding inclination in the longitudinal direction allow, but a loosening by the rotor stroke impossible do.

Furthermore, it is pointed out according to the invention that in the angle of inclination alongside on both sides of the rotor ropes, on the one hand on the lower part of the Schusnk rope and on the other hand on the swivel rope are releasably attached, so that the downward movement of the footplates with the support of these rotor cables, ofie rotor blades also get the corresponding angle of inclination.

In a special further development of the invention, it is pointed out that that the boom structure is preferred. of two parts 221, 2211 is put together in which the / upper linkage structure as Extension rod structure called uird and vorzugsw. for a Vehicle or caravan as a hydrofoil, rotary wing aircraft also without a hovercraft is to be used in which the separation takes place in the middle area * of the boom structure. And that with a motorcycle uorzugsw. with sidecar or cabin scooter the two rod parts remain joined and the separation in the upper Area of the supports of the hovercraft is carried out, so that the non-positive fastening even without the hovercraft is held upright with the upper clamping bars and with these missile versions, after which the team or a cabin scooter also switch to a hang glider can.

The characteristic that the Carav / an or the Carauan-Automcbil can be used without a hovercraft when using an extension rod assembly 221 is also to be assessed of serious importance. is used as a hydrofoil. In addition, it should be added with reference to the hydrofoil that the hydrofoil uorzugsw. composed of three two-part unfolded plastic parts, while the middle two-part unfolded and preferred. part connected by hinges, which is the wing connector. And in this middle part port and starboard are preferred. by insertable bolt snap-in locks, the two-part also by vorzugsw. Hinges of connected wing parts are effectively detachable.
In a further embodiment of the invention, it should be taken into account that

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that according to the exchange possibilities of the drive in the area of this Registration preferred bBi this version with the add-on linkage structure ein.Stromergenerator with the drive organs the vehicle. connected, so that it can be detached from the attachment rod structure attached Stromtriobusrke can drive, and the rudder cables that to. the rudders are attached., no longer on the Schuenkplatten, but on the steering organs of the vehicle. solvable attached. Should a conversion to a helicopter be intended for the version without an airboat Another tail rotor engine also on the stabilizing fin holder releasably attached and conductive with the correspondingly powerful power generator in the vehicle. tied together. And that is preferable. with motorcycle + sidecar bzu. Cabin scooter, at the version 22I + II without hovercraft, the relocation of the tumbling floors takes place, and also .dar '· slider for Use comes.

The following features the dan drive in conjunction with the so-called "solar cells" are preferred for accomplishing to use both hovercraft construction bushings L / l and L / lI.

Missiles and boat bodies with solar cell propulsion are known per se. On the other hand, should be preferred here. In addition to the old procedure, new procedures are used, which in principle the have the same effect as these solar solar cells. With this method They are not known per se plate-shaped solar cells, but a prepared'Masse on the hydrofoil / hydrofoil connector Rotor blades, flying sails and other surfaces of the hovercraft / Aircraft applied bzu. sprayed on in liquid form. What advantages are to be expected in this regard is shown in vorzugsu. the application in the kite wing. When kite hemp 1-ugly remains, even after the preferential The sprayed-on layer of this flying sail is elastically foldable. The procedure.as marked under "applied" treats a US case known in 1982 became. According to the invention is vorzugsw. in this context to see the feature that this "applied" bzu. "sprayed on" Alternating layers bzu. with the support of. Kfz. bzu. of the caravan drive.

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And now the advantageous effect of the invention should be described in relation to the prior art usrden.

The applicant had already given his disclosure documents in the preamble, in which he had referred to the new drive farm in the area of the air cushion batteries with regard to the drive bodies mentioned. If this important invention should also come to a breakthrough, it is preferably also for this reason that the same applicant with this further development enables this usability of this invention in the first place. And to the. Vortex.-lea of this procedure would only indicate that the familiar speedster hovercraft are preferred. need three expensive drive motors. A lifting and a thrust rotor. And on the basis of this invention, these three ffiotore can be dispensed with if a high-performance vehicle is needed . _f the anyway z. B. a. Sports motorcycle rider “owns, is used as a drive and steering unit. 'And in this circumstance is preferred. the reason why this airboat sport is so well and unknown to us. For our youth it is still closed due to the aforementioned drive motors as an acquisition. dew. There is also an important note, namely that on our inland waterways the use of outboard motors is as good as forbidden. At the moment only that fleer is available without restriction. In contrast, a hovercraft or a reversed propeller boat by bicycle or motor vehicle is. or other named drive bodies driven according to the proposed designs ENVIRONMENTALLY FRIENDLY, since they cannot cause any contamination in the water.

It should also be borne in mind that the air cushion boat is an enormous one Oxygen enrichment for uasar oxygen-poor sensory waters would bring.

The training shows the above-mentioned hovercraft as Air cushion boat / flying device with the hydrofoil nozzles with side walls, with soil impact,

These aerodynamic hovercraft are known to float on a dynamic cushion of air between them and the surface beneath them forms. These aerofoil boats fly low on a "ground effack" air cushion,

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According to the invention, this embodiment is used here with those mentioned Brought drive bodies in connection. In contrast, non-collapsible missiles obns' these drive bodies u. with lift propellers under the. This type of aircraft is known.

A rotor which is designed to be pivotable at an angle of inclination for the rotor blades has been known per se for a long time. In contrast, an uncomplicated rope rotor is presented here, which achieves the cited angle of inclination for these rotor blades only in connection with a motorcycle / cabin scooter, caravan or automobile. In addition, this Sailen rotor can also be used in conjunction with the wobble and rotor ropes for the flying sail. There are no "gyroplanes', '' flight screwdriver helicopter" propellers known in the aircraft floor, which are driven by the cited drive body Further, the upgraded to hovercraft / aircraft hovercraft _f is particularly inexpensive to manufacture "u." -. Which, moreover, even in can change all the known to the state of the art flight-body. and that that statement must be bediensn in the simplest Usise to Uasser, on land and in the i_ _u ftt ^ and that this hovercraft / aircraft on the one hand to selb. ".- permanent missile without an air cushion bed or in a propeller boat without a lift drive.

Furthermore, it has become apparent from the description that preferably two construction leadthroughs disclosed in this supplementary application who preferably ensure that alia versions It. the Gffenlegungsschriften DE 32 42 960 A1 and DE 32 47 158 £ 1 in technically simplified form, become operational. In addition, t> t; i in these construction bushings L / l and L / II Features have also been disclosed which show particularly clearly that For example, the L / II assembly bushing can be manufactured very cheaply there will be only one power transmission for simultaneous Thrust and stroke through preferably an air screw / casing takes place and floor planks are no longer required.

In this regard, the dead weight is significantly reduced, so that land vehicles are much weaker in terms of power for the drive are needed, and that z. B. the hovercraft through this combination the possibility of changing cells to the best results with regard to "suspension" and "less air supply" ωετdan can.

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Fig. 1a Fig. 1b Fig. 1c Fig. 1d

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The drawing shows the example of the invention, Show it:

Fig. 1 is a rear view in section after the construction implementation L / l with Spannlsibtün / Zellün and inflatable Uulsten releasably attached to the clamping bars,

a side view with three Kraf t-r-transmission-in,

a rear view in section 'after the construction implementation l / ii,

a Seityn view with a power transmission,

a rear view in section with Luftflu3 from Hub and Thrust propellers / sheathing over Vsrbindungslüulste, Apron-Uulstan to the cells and fingers,

Fig. 2 shows a side view of a closed elastic cabin and use of a flying sail and Hydrofoil / hydrofoil connector υοη a motorcycle over the push and lift caster driven,

fig. 3 is a side view when a rotor is used , Rotor blades, rotor circuitry, power generator and Stromtriebuerke / Luftschrauban in a Luffckissenboot / rotary wing aircraft, '.

Fig. 4 is a side view with an automobile parauan-An -, '■ / drive unit for the air cushion boat / aircraft,

5 shows a side view with a taravan as an air cushion boat / aircraft drive body,

Fig. 6 is a side view of the Bodenpla-nken-Radanhangsr overturned hovercraft / aircraft, '

Fig. 7 is a plan view of the smoothly assembled Floor planks with their drive transmission options,

Fig. 8. a rear view of the linkage structure for eiqen flying sail, rotor and Tcag wing / hydrofoil connector developed too. for one. JTlugkörpsE with or without a hovercraft, ■.

Fig. 8a is a side view of the Seilan rotor with its individual parts,

9 and a hedge view in the representation of the air cushion 9a boats and the possibility of changing from the inflatable Uulsten air cushion boat for Schiaufsn-Schürzen-Luftkissanb-oat, with baseplates and wobble relays,

Fig. 10 "is a rear view with the wing connector and Seitenuändsn for the bodana effect ^ dis also with ailerons " are equipped

Figure 11 is a rear and side view of the upper linkage bauSI, the one for all closed motor vehicles and Carauans is to be used,

FIG. 12 shows a rear view of the footplate marked with Wobble conditions for the hydrofoil / hydrofoil nozzle aileron, '.. "· ■■

13 '"shows a side view of the wobble balance in connection

with the Fuflnlattan, for Traof lüqler / Traof lijoler «, tqtrea

G. 13a - - --v a side view of the slide without Kotorseilsn '^ the Ro $ no, for hydrofoil / hydrofoil connector,

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• The foundation concerns a t ^ chri ^ before · parental satisfaction and a complement to the. Disclosure reference DE 32 47-158 A1

and is characterized by uie

^ z from Fig. 1 to 3a can be seen after this Ueiter-O education and through the features of the construction implementation ™ L / I, L / II, 113 / 15,19,118 / 20,20,20a, 2013,200,373,3713,43,1Ic, ^ 13a, the following statements of this published application CO

be feasible, so that the air cushion dot is not only convertible to the Zellsn air cushion boat or to the cell and finger air cushion boat, but also to the air cushion boat aircraft with hydrofoil connector 6a, with cross winds 6 b for 3o deneinuirkung, and this R a dan hanger- · 8a or. 1i / i1a and its contents are constructed in such a way that from the hovercraft it alternates between all of the prior art missiles 6, 6a *. 9, 10,12,18 _v 6b, 21c, 41,49,49a, 49b, 33,33a, 34a, in which these insert bodies have different heise 28,28a, 28b, 37a _t 37b, 4,4b propel the hovercraft / aircraft, b.ru. that these insert bodies, as "motorcycle 2aa, cabin scooter 2a'e, caravan 3 and the automobile 2 can also detach themselves from the hovercraft 35a, 35b, 22Γ, 2211, so that in this case the named bodies become independent flying devices, and that after this air cushion boat / aircraft version this air cushion boat / aircraft can be converted back into an automobile 2, motorcycle 2aa and bicycle 1 propeller boat without lifting drive 37 + 37a bzu . ■ · ·

The abbreviated process cited becomes the individual Features uie follows completely:

The Luftkissenbuot implementation L / l show in Fig. 1 and 1a initially a supplementary embodiment according to the Cffanlegungsschrift '' -,. . DE 32 "7 163 A1 _; in which the Hub-Luftschraubcn-U.-nmantellung 4, 7, di & under the circular, shaped floor panel section III / 8 and boat floor is detachably attached, in connection with the adjustable 16a, 17a holding supports 16, 17 and clamping bars 11, 11a'für the support structure and thus for the Aboau the Geuichtakraft of Landfahrzsuges einschlisSllch. driver care, care also preferably these adjustable 17a Haltestützcn "17 and f'iotorrad / stand 19 for Einan certain Hufliege- ^Pressure!" v ° ^{n dßil} land vehicle drive wheel 32 bzu. Drive

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wheels 32,32 to be preferably "piRaf;Gl3.itcül; ^ie: 3 o for vqrzugs-OQ, two propellers / sheaths 4b, Ac for the thrust ° while the lay-on pressure is preferably to a S sliding roller 37a? the propeller / sheathing 4.7 for the * "" stroke is determined, while the transmission force is preferably brought about by CO V-belt 42 and loop shape 46.

When operating these lift propellers. 4 becomes the resulting one Air flow to the free spaces under the boat floor 3ff printed, so that here by this stable soann strips / Zallen-demarcation 11a / 20 a large air cushion is created. This compressed air also gets into the already named Clamping strips / cells 11a / 20, so that they approach the central large-area Air cushions small air cushions around the entire boat are generated so that the loss of this compressed air is restricted will.

Likewise, it can be seen quite clearly from Fig. 1 and 1a, that these cells 20 as the name of these clamping bars / cells 11a / 20 indicates, with the lower Soännträger 11a around the entire these clamping strips / cell 11a / 2Q supports 16, Soannlefeten 11a and holding ropes 38 to the holding keel 38a, thus a stable holding structure is present in the lower part of the boat.

Incidentally, in this construction process, the cells 20 are on the lower Soannleistan 11a is detachably attached in such a way that these cells only protrude towards the interior so that they can be removed from it Air cushion space also conveniently with. Comorinated air can be supplied. This implementation can be seen in FIG.

Due to the fact that the land vehicle and the driver over the Uulsten 13 of the hull and floor planks 8 a occupy a high position, which Fig. 1a shows, will be expected to be heavy during use. To "these negative To restrict properties as much as possible, the measure to be taken will preferably be that the boat additional preferably by a bellows inflatable Uulste 13a u.t the entire Boat gets around. This Uulstc 13a, according to FIG. 1 are not connected to the hull 13, but are on the cracks on the lower clamping strips. 11a by means of a clamp 11b so releasably attached that in the event of a collision the clamping bracket 11b can yield in the entire diameter, and

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are preferably made of elastic * "plastic and have no interior lining.

The high quality with diaser implementation is also limited, in which the upper clamping strips 11 also offer a secure and padded support structure in the driver's area. This construction process can also be seen from FIG. 1a.

Due to the previously mentioned three power transmission partitions 4,7, 4b, 4c as shown in FIG showing * 1a, on the one hand Uird a while effective force transmission to the individual lifting propellers / Ummantellung 4.7 and thrust propellers / sheaths & b , 7, 4c, 7 transmitted, but on the other hand, this Kraftauftsi development with additional power consumption must be expected, so that with these power losses, stronger land vehicles with respect to horsepower are to be claimed, which are also in connection with This build-up implementation through the mentioned effective service are preferably to be used for international racing events as air-cushioned snooters.

It is different with a further construction implementation L / 11 according to Figures 1b and 1c.

In this case, a far lighter and less powerful land vehicle, preferably also an all-terrain machine, is used in which, instead of the three power distributions, preferably only one X-belt transmission 42/45 at the same time for lifting and thrust in a different farm according to the disclosure DE 3Ü 33 938 A1 of the applicant takes place. In contrast to the implementation in this document, which is shown in Fig. 1a, the propeller / sheathing 7 is not preferably placed under the floor planks 8, but preferably at the stern of the hovercraft in the suspension frame 14 for pushing and lifting. In this construction implementation, several propellers / jackets 4,4b, 7, 4a, 4c, 7 for. the simultaneous thrust and stroke or preferably the larger stroke air screws / sheathing according to the assembly lead-through L / l for the air screws / casing 4, 4b, 7 _{s of} this assembly lead-through L / 11 for the thrust and stroke, in the dia several 4,4b, 7, 4a, 4c, 7 or preferably die'eine propeller / casing 4,4b, 7 is divided into preferably two parts.

The upper part of the air outlet, which can also be found in Fig. 1c is intended for thrust and is not disguised, so that the air pressure in this area unhindered the thrust-return force accomplished. The lower split-7bb causes this —S? T3

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· - ": V i '' ■ - :: l 3412008 Air flow not direct" aiistr-aten- k '& rin, s-ond-ern reaches the aprons / Julsten 43 through connecting ljulBte 4 * 3a.

This construction implementation is also particularly clear in Fig.

1d to be seen.

This apron / Uulste 43 have elastic retaining clips Hcydis not with the hull 13 / but preferably with the lower clamping strips 11a are releasably connected, and uerdsn exclusively by the Luftschraub.en / sheathing 4,4b, 7 supplied with compressed air. This process is shown in Fig. 1b.

In contrast to the above-mentioned construction leadthrough L / 1, in this construction leadthrough L / II the cells 20 are detachably attached in the lower area of the tensioning strips 11a in such a way that these cells 20 protrude outwards so that they can be comfortably removed from the cited aprons / ridges 43 can uertfen supplied with compressed air, and that preferably present at jeaer SDsnnleisten / Zel Is 11a / 2D oval for this air flight openings 44 in the lower region of the Schürzan / Uulste 43 ^s i ⁿ -d ··

Likewise, it can be seen from Fig. Ib that this setup is carried out L / II the SpannlGisten / Zc-llen 11a / 23 consist of preferably ζωε-i cells 20 and 20a, in the above cell 2G is detachably attached to the sounn strips in such a way that their Cutout 20b to the air cushion space ucist.

In the interior of the detachably attached cell 20, this is the outer surface Cell 2Qa can be rotated and re-installed and has preferential features If the same section 2Cb and the outer cell, so that'3 the clamping strips / cell egg 11a / 2ü immediately into a clamping strip finger I1a / 15 can be changed over, if the two cutouts are rotated 20b, 20c of these -Zirlien 2Ü, 20a stand on top of each other and snap into place.

Another feature of this construction implementation is shown in Fig. "Tb it can be seen that the inner rotatable cell 20a acts as a finger 15 extractable, "q that due to a-e'uesen t-

LighB extension of the finger 15 even the use in the army in a high sea state is possible. It can also be seen in FIG. 1b that the floor planks 3 in the area of the supports 16 around the boat only have a frame 8/16, or this collapsible frame S / 16 is completely dispensed with. ij _n j r \ n _a likewise ^De i-carrying this Aufbou oil-γ worzügsuniss zuei- • piece nusouff 9/2 of Landfahrzeugas with preferably one Abf.luß / Gtestcinga g / 22 lünbar varbundtjn Uird so :: uch bsi a skinned Cabin, through the tensioning frame / Au-3snh? Ut 11/1 din

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Exhaust gases can get into the open. Incidentally, this outer skin is in the roof-rear area of this tensioning strips / outer skin 11/1 designed detachable and rollable l / l.

Make a final feature of the two mentioned structural leadthroughs L / I and L / II according to FIG. 1 and according to FIG. 1b, in both cases, the elastic seal 13b is not on the inflatable / luulsten 13a or aprons / uulsten 43 _; but releasably attached to the inside of the clamping strip 11a. And that under the boat floor 33 a retaining pad 38a is detachably attached, which on the one hand has the task of holding the land vehicle, which is actually heavy, over the air cushion space in retirement, and on the other hand also of holding the retaining structure upright with respect to the air cushion during use.

If one drive carried out as LuftpraoalLerboot without lifting drive, as is, according to Fig. 1a, the structure-carrying L / l to uählan in which the drive wheels 32 or drive wheel 32 ^ 32 preferably has a push-sliding roller 37a hefestigt releasably i ₃ t.

It can also be seen from Fig. 2 'that v.orzugu. three sliding rollers 37, 37a, 37b lying one behind the other are placed on the floor planks 8. Idle caster '37, push caster 37a. and lift caster 37b. If an air cushion ride is intended, the drive wheels have bzu. Drive wheel 32 rotatably in contact with the lifting and pushing roller 37a + 37h. If, on the other hand, only a bicycle-Prcpellerfahrt is provided without a lift drive, then the drive wheels have bzu. the drive wheel 32 rotationally transferable contact with the thrust bzu. Lear.-Lauf-Gleitrolla 37 _.; 37a. The young ones. Shifts to the bow "lifting and pushing roller", to the stern "pushing to, idling roller" allow the suspension systems, in which the new location 37a + 37b bzu.'37 _y -37a the insert body: 2.2aa , 2ac bzu. 1 rigid and their drive wheels bzu. Keep drive wheel 32 elastically releasable attached. The shift is preferred. carried out so that the drive wheel 32 bzu. 32, 32 only has contact with a push-roller 37a, if a push-and-lift air cushion travel is dispensed with

From Fig. 2 it can be seen that the elastic envelope of the Forrnspannleistsn 1b, 11, 11a in this embodiment called "3chlauf err outer skin 1b", in the mixing area of the clamping strip 11.11a should be trained on one side

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Loop outer skin 1b made so that it is in the immediate Area of the tensioning strips 11, 11a, loops 1b for these tensioning strips and with the elastic cabin 1b, la, 1c connected '. The loop skin 1b in the Bow cabin area 1c. get a cut te so that the two-sided elastic cabin walls 1a of the Bow part 1c preferably with plastic zippers 1ae connect bzu. solve, let. The boom construction. 22, on the other hand, is constructed in this embodiment so that on this rod structure 22 a flying sail 1S bzu. a 'hydrofoil 6 bzu. an unfolded hydrofoil connector 6a with side walls 6b for floor effects and housed

is releasably attached, and by using • preferably, four R ο to rs ei lan. 23, 23, 24, 24, preferably u. zuei rudders 7a _t rudder parts 36a, Höhensteuerseilen4Q, tailplane 33, Fu3platten -21, aileron 49a, 49b, 21c slide 6 ß, ^s can be done the Au.fg.ahe the navigation implementation. By using this, the hovercraft is in a Drachenflüglsr 18, hydrofoil 6 bzu. has been converted into a hydrofoil with hydrofoil connection 6a with side walls 6b for floor penetration.

It can also be seen from FIG. 2 that the flying sail of the kite winged wing 18 and the wing of the wing 6 bzu. 6a + 6b a layer on the surfaces facing upwards 28a, 28b received.

According to FIG. 3, in this construction, the air cushion boat preferred converted into a rotary wing aircraft and from the Kfz.2 Motorbike 2aa, cabin scooter 2ac driven and so long against accelerates the air flow until it also drives the rotor 25 in question. This process is carried out by this measure favors, in which * z. B. the motorcycle 2aa vorzugsu. two propeller sheaths 4b, 7, 4c, 7 for the Uor-ortsbewegung drives to through this rotor to get the appropriate buoyancy so that the converted Hovercraft from the hang glider 18 or hydrofoil 6 or 6a, 6b can be transformed into a gyroplane 9. These named drive bodies' 2,283,28C can, the hovercraft / aircraft propel in different ways. One of these drive options is that vorzugcw. a motorcycle-

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Drive wheel 32, -the on bzu. in the hinge floor planks 8 built-in sliding rollers 37, 37a, 37b .drives and this rotary movement, of the preferential 28 bzu attached under the floor planks 8. attached 28.28 -generator received. the Energy generated in this way is via rubberized transmission lines to the Stromtriebuerke 41,4äII, 4bLII, 4cIV, the directly with the. Propellers 4,4a, 4b, 4c in connection stand, forwarded. And when using varzuqsu.

27 /

a rotor circuit'bzu. a power drive 25V, the hovercraft / aircraft, from the gyroplane 9 into a flight helicopter 10 bzu. Helicopter 12 changed over, and that the rotor blades 26a, elevator 33 + 41 + 21 to stabilization fl. 34a and the other upwardly moving surfaces of the hovercraft / aircraft a layer 28a, 2Bb of the type Solar solar cells ^ obtained.

From Fig. 4 it can be seen that uorzugu. a car. 2 according to Art the caravan automobiles or even according to FIG. 5 a caravan 3 from the propeller boat 37,37a bzu. Hovercraft 37a, 37b in an aircraft 6,9,10,12 bzu. 6, Sa, 6b can be changed. Another Feature preferred for this version with the Caravan Atrtomabil is that the drive features with the power generator 28 vorzug.su. are to be used should be a bzu. several power generators. 28 in this version in the automobile caravan 2 with the drive units. 2b immediately stay in contact. To the hydrofoil also in this version 6 or 6a + 6b bzu. Gyrocopter 9 into a flight helicopter 10 + 5a bzu. To be able to move the helicopter 12, uird Rotor circuit 27 housed in motor vehicle 2. With this execution ■ tion is preferred. to take advantage of the feature that the called driving process with stationary drive wheels 32 of the Vehicle 2 is carried out while the drive motor. 2 B. of the vehicle 2 in idle 2bl drives the generator 2G. In this measure, u is the collected energy from the. Generators 28 on the Stromtriebuerke 41,4aII, 4bIII, 4cIV, 25V supplied, and these u in turn transform the energy into rotary motion, so that this Rotational movement directly from the said 5tronrtriebuerkan to the propellers 4,4ε, 4b, 4c and the rotor 25 will.

On the other hand, according to FIG. 5, correspondingly strong additional drive motors 5b, 5c are each loaded with the caravan version 3. ^:

aft

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standing or »newly developed manufacturing and auCtr of fuel to use. These additional drive motors 5b, 5c stand directly with the Luftschraubsn 4,4a, 4b, 4c in connection. This also applies to the rotor 25.29, so that the execution of the hovercraft in a d3r named. Aircraft executor gen. 6,9,10 + 6a, 12 switch Iä3t. The changeover is to be taken into account in the case of Use of preferential u. an additional drive motor 5b, the warzug.su. also only one power generator 28 drives and the energy gained to the 3tromtriebuerke 4I, 4aII, 4cIII, 4cIU, 25V usiter gives.

Furthermore, after the training according to FIG. a Floor plank wheel trailer 8a proposed in the assembled Condition of the vehicle. 2 is towed. The Bodsnplanken 8 are in this version as xusammsn available Go-r denplanken bike trailer 8a named. The 'reason for this measure is that the floor plank wheel trailer 8a is in no time in a container for the hovercraft or hovercraft / Can assemble aircraft, and preferably to this container 8a two rubber wheels 8b are detachably attached./Per floor plank wheel trailer '8a is preferred of five parts. Four parts 118,1113, IV8, 'J8 form the Seitenuänds, and the fifth part' 13 and is folded onto the wall 118 in the opposite way. Dissa Wall 118 is preferred. represented by the unfolded boat bathing. The walls VI8 and UIIB are preferably made the two-part air screws / casing 4b, 7, 4c, 7, their Protective grid 45 to come to lie outside.

Fig. 7 shows the rudder control system 7.a. This rudder control In both cases it is used as rudder control for the air cushion b, oot or aircraft of the versions mentioned from Fig. 1 to Fig. 5, and in this way it is accomplished da3 when the motorcycle / cabin scooter handlebar is operated 2d.d, 2ad, this inclination angle made over the front one Wheel 32a, the Hchuenkplatte'n 36 and rudder cable 36a to the preferred rudder 7a attached on both sides uird. It should also be mentioned that between the rudders 7a, the horizontal stabilizer 33-elevator 33a-St.-Flos.-Sen 34a, bracket 34 aa dan supports 14 can be pulled out or in the length is adjustable and detachable. by the way, the mentioned swivel plate 36 on the front wheel 32a of a mo-

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Torrades 2aa is detachably fastened not in the front but in the rear area. It can also be seen from FIG. 7 that preferably from the sliding roller 37a to the transmission means 42 at the stern, preferably two-lane V-belts 42, come to the gear set, and that for the wire transfer from the sliding roller 37b via the transmission means 42a the lifting Propellers 4 and on the other hand for the rotation of transmission means 42 at the stern. To the thrust propellers 4b, 4c, preferably V-belts 42a, which have a thrust 46 and a stroke 46 point ^Ir or are used in three 46 places. From cig. 7- it can be seen that the height control cable 40 can be rotated on the elevator linkage 33b, and the paddles "7/8" are attached to the floor planks 8 the preferably toei rudder 7a attached to these side fins 7b so that they can be swiveled and detached and covered by the casings -7 which can also drive the rotor 25, so that it is assumed that the flight wrench 10 uses a motor-driven rotor 25, a tail rotor and a push or pull propeller That it is preferable to mount a sliding roller circuit 27 on the corresponding floor plank 8, Ls = W-- Through this implementation, as also shown in FIG. 7, during a switching process 27a of the motor vehicle ..- drive wheels bzu. Motorcycle drive wheel 32, driven caster 37b, tapped. With this measure, the turning movement is preferred. conveyed via a flexible transmission means 29 known per se to the rotor head attachment 30.

This rotor head extension 30, as shown in FIGS. 8 and 8a, stands with inextricably linked to the upper rotatable holding collar upper part 25a. The flexible transmission means 29 is preferred. to the Rotor head attachment 30 releasably attached. Through this solution found the sliding claw circuit 27, drives the motor 2b, 2bb, 2ae from the car / motorcycle 2,2aa bzu. from the cabin scooter -2ac dia propellers as stroke 4,4a, the propellers as thrust 4b, 4c, and eJurct den Switching operation 27a the rotor 25 on. The switching process 27a is preferred in this embodiment. the presupposition

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been creating the. First to convert gyrocopter 9 into a flight helicopter 10. In the case of the coaxial rotor system, it is known that two rotors lying one above the other rotate in opposite directions. Uenn. Both rotors have the same blade diameter, they need the same torque so that the fuselage remains in its original position. So that the trunk of the air cushion cot also remains in its original position, the rotor 25 rotates, according to Figure B, on the frame structure 22 in the opposite direction to the lifting air screws 4, which are also rotating under the bathing planks B, according to FIG. 9 The difference consists in the large-area rotor blades 26a, to compensate for this difference _f several propeller blades 4, 4 are to be used one above the other in a casing 7 or several propeller casings 4, 7, 4a, 7 under the bathing planks a. Differences can also be compensated if the sliding roller 37b to the transmission means 39c corresponding speed differences are on ws. Fig. 7 shows this process quite clearly. 3 also shows that the rotor head extension 30 is designed in such a way that it is inseparably attached to the retaining cross upper part 25a and functions as an axis to the lower remaining rotor head parts 25b, 25c. In this regard, it should also be mentioned that tfp.s swivel cable lower part 25c has swivel axes 25ca on both sides for the linkage structure-locking eyelets 47. The gesture structure-locking eyelets 47 are designed in such a way that, although they allow the corresponding inclination in the longitudinal direction, they make it impossible to detach them through the rotor stroke.

Furthermore, it can be seen from Fig. 8,9,9a that in the angle of inclination alongside on both sides of the rotor cables 23, 24, on the one hand on the Schuenkseil lower part 25c and on the other hand on the wobble balance 41 are releasably attached, so that when the foot plates move downwards 21 with the support of these rotor cables 23,24, the rotor blades 26a receive the corresponding angle of inclination. If necessary This same angle of inclination can also be applied to the elevator 33a of the Hchenleitwfjrks 33 by the upright Finger 41 of the foot plates..21 transmitted, if on a stabilizing fin 34a is dispensed with. In Fig. 9a, the hand control cable 40 can also be seen in relation to this. As a supplement, attention should be drawn to the feature that the osseous footplate 21 is preferred. on the nut wheel foot

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support 21a, have swivel eyes 21b and vorzucsw in this version. from these base plates 21 to the wobble balance fingers 41 rigid Qsenführungsgestängeteile 21/41 to claim taken, and that also when these footplates are bent upwards 21, this angle of inclination is transmitted in the opposite sense to the rotor blades 26a and elevator 33a. Fig. 9a shows the foot plates 21 with the tumble scales 41 at the same time operate the rotor 25 and elevator 33a. This version does not require an additional slide 21c. Should the Foot plates 21 can only be used as ailerons 49a, 49b, 6b, the wing / hydrofoil connector 6, 6a, 6b needs an additional one Slide 21c. To be seen in Fig. 10 and Fig. 13a. From Fig. 8 and Fig. 9 it can be seen at the same time that the linkage structure 22, 22a, 22b, 22c, 22d, 22e, 22f, 22g, 22h + 16,11,11a vcrzugu. is composed of two parts 221 and 2211, in which the upper rod structure is used as an extension rod structure .221 denotes uirdund vorzugsw. for a car. 2 or Caravan 3 as hydrofoil 6, rotary wing 9,10,12 also without an airboat is to be used, in which the separation in the central area 35a of the linkage structure 22 takes place. Should be one of the above Separation take place, so is a hydrofoil support:. '6a: with . 6b for soil impact · no longer possible. And preferably with a motorcycle 2aa. with sidecar 2ab or cabin scooter 2ac, the two rod parts 22I + 22II joined together remain, and the separation in the upper area 35b of the ': Supports 16 of the inflatable boat carried out uird, so that also Without an air cushion boJt, the force-fit fastening with the obersn clamping strips 11 and with the missile execution 5, 9,10,12 is held upright, after which the team 2aa + 2ab bzu. a cabin scooter 2ac can also be converted into a Dra- :. chenflügler 18 can switch.

It must also be taken into account that, according to the drive replacement options, vorzugsw. in this embodiment with the attachment linkage structure 221, a power generator 28 with the drive members 2b of the motor vehicle. 2 is connected so that it can drive the power drives 4b Hl ₉ AcIM , which are detachably attached to the attachment linkage structure 221, and the side rudder ropes 36a, which are attached to the rudders 7a, no longer on the swivel plates 35, but on the Lsnkorganen of the vehicle . 2 can be attached detachably. Should be when running without a hovercraft

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A ₃ conversion "to the helicopter 12 is intended, a further tail rotor engine 25V - likewise detachably attached to the stabilizing fin holder 34, and conductively connected to the correspondingly powerful power generator 28 in the vehicle.

The hydrofoil designs are preferably from Fig. 10, 11 and 12 can be found. These designs have on the wings 6, wing connector 6a, or the side walls 6b, Ailerons 49a and 49b. The wing / wing connector 6, 6a are rigidly and releasably firmly attached to the rod structure 22, by the rotor cables 23,24 through the rotor head axle eyelets 25cd slide and do not incline the rotor head 25. · By this fact has been achieved that the inclination generated by the foot plates 21 is passed on to the wobble balance 41 is so that the rotor cables 23, 24 receive this inclination from the wobble balance 41, and through the bores 23a, 24a the wing / wing connector

6,6a urtd rotor head axle eyelets 25cd, so that finally on the other hand in the wing / Tragflgslstutzren 6,6a _y in bearings housed coupling rods 6aa, the ailerons 49a, 49b, the rotor cable ends 23b, 24b are attached to these coupling rods 6aa, so that this inclination in Forir, is further transmitted by a rotary transmission to the ailerons 49a, 49b. And also. in the. lower area, represent. hydrofoil / hyd. lügelstutzsn 6,6a the same'MeigungsuinkRl v / .jn dsn "Taumsluacgen 41 is carried along, in the lower area of the rotor cables 23,24 from the wobble balance 41 to the Kopoel linkage 6aa, Saa + 23b, 24b of the ailerons. 49a, 49b also transmit the inclination in the form of a rotary transmission. The above process can be seen preferably in FIGS It is stated that port and starboard, an.dem hydrofoils Istutzaπ 6a, hydrofoil silc 6T and 6II were attached so that the hydrofoil connector 6a, which is preferably connected in two parts by hinges 49, without preferably two-part hydrofoil parts 61,611 for the dragon wing parts 61, 611, which are also connected by hinges 49 . Aircraft 1C and share with the wing 61,611, in a wing 61,53,611 for the TragflÜglür 6 convertible

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is. In this regard, this embodiment is in a special embodiment the feature in Fig. 10 'can be seen, uie the above Redesign of the implementation already indicated that both sides in the area of the hinges 49 of the Tra-jf wing connector 6a, the so-called Kappel linkage 6aa separated by their bearings the hinges 49 are housed, and with the separate right bzu. left rotor iron 23 bzu. 24 rotatable portable 23b,

• 24b with the right bzu. left wing port ailerons 49b 'bzu. 49a related.

10 also shows that instead of the ailerons 6a + 49b, ailerons 6b + 49b on the trailing edges of the wing / wing connector 6, 6a in the area of the side walls 6b are installed rotatably. And that the side walls 6b for the Dodeneinuirkung so with the coupling rods 6aa in connection stand that the ailerons 6a * 49b and the ailerons 6b + 49b can be used at the same time. These processes mentioned also relate to the aileron 49a.

Furthermore, from Fiq. 10 that a slide 21c is also used as an elevator 33a on the motorcycle 2dd, which adjusts the setting of the elevator 33a by means of its elevator control cables 40, 40a.
Lt. The solution can also be seen in this feature in FIG. 11

that with both sides uorzugu. snap-in hydrofoil parts 61 and 611 also preferred. a coupling unit 50a, between the wing connector coupling rods 6a, 6aa + 50a and the associated wing parts 61,611,6aa, + 50a

• 'according to Fig. 12 ajl /
takes place, so that the inclination of the rotor rope is transmitted not only to the two-sided hydrofoil nozzles 6a, 49a, 49b, but also to the hydrofoil parts 6r, 6II, 49a, 49b rotatably 23b, 24b and separately 21, 21, see above that bsi the actuation of the right foot plate 21 without wing parts 61,611, only the right wing connector Qüsrrudsr 6a, 49b, bzu. on actuation of the left footplate 21, with wing parts 61, 6TI, the left wing connector U'uerrucisr 6a, 49a-. and Tragriüg Gltsilen ailerons 6'I, 6II, 49a deflect bzu. vice versa. This implementation, uird. supported with clamping devices 48. ^{In a} summary of Figs. 10, 11, 12 and 13 is

13 clearly shows the process "that the two Taumeluaagen 41a, 41a siners & its with the footplates 21, and on the other hand with the hydrofoil / hydrofoil connector-Quarrudeir, b, 6a 6b,

EPOGOPY

49a, 49b are connected, and that the same pivotable upright pointing wobble finger finger 41a with the footplates 21 through rigid eyelet guide rod parts 21/41 the setting angle qjnne. ^ clamping. enable üartraghap.

Fig. 13a shows in this wing / wing socket embodiment 6.6a.6b, that preferred, only the upright 41aa and vertical 41bb • Pivoting fingers for the elevator cable 40,40a used is, so that without 41,23,24.this slide 21c for hydrofoil / Traqflügelstutzen 6,6a, 6b and with 41,23,24 the same slide 21c for rotary wing aircraft 9,10.12 is used .. These versions 6, 9, 10 and 12 can be an independent one Have fin 7b, on which the higher rudsr 33a can be released is appropriate. This can be seen in FIGS. 3 and 4. Finally, it can be seen from Fig. 2 that the Qrachanflügldr 18 has wing connector 6a and ailerons 49a, 49b, and that It. Fi, g. 5 the support rod 14 is formed so that the RaJträger ^ 8a can also be transported as a container 8a.

Instead of * floor planks 0, these floor planks 3 according to l / II üpannbaren 11,11a and boat bathing. 38 for dsn bike trailers 1 1/1 1. & in. Claim, taken wetcsn »

The mentioned versions of δ, 6a + 6b, 9, 10, 12 usrdsn preferably with the following airboat implementation L / I, L / II ' suggested:

! \ iach L / I

Floor plank trailer 3a ",
Flugschraubsr 10, resp.
Helicopter 12

Awake L / II

Clamping strip wheel trailer 11/11 a

Hydrofoil 6,

Hydrofoil / rotary wing aircraft with hydrofoil connection 5a and side walls 6b,

- Gyroplane 9.

y The imprint of the drive wheel 32 is preferably iibar the Plotorrad / ii tänduT 19 for. Lifting device 32b accomplished.

EPO - copy

style

Claims (1)

/ ft According to the Offenlegungsschrift DE '32 47 168 A1 main application, collapsible, seaworthy automobile propeller boat according to the Offenlegungsschrift DE 3049833 A1 preferably discloses a new type of air propeller drive for thrust in connection with a propelling automobile, Collapsible, seaworthy automobile jet planing boat according to laid-open specification DE 3029763 A1 preferably discloses a new electric air propeller, electric water screw drive type, and a water jet nozzle drive type for thrust in connection with a propelling automobile, collapsible, seaworthy automobile air cushion boat or »Carauan hovercraft according to the laid-open specification DE 3033938 A1 refers not only to the thrust drive, as the above-mentioned main and additional application, but to a new type of drive in the field of hovercraft, in which the automobile, or motorcycle, or Caravan provide the thrust and lift, and this. Patent application is an additional application to the above-mentioned main application, dadur,, c 'hg' e ^ ke η η rich η et that after this Ueitar formation (L / I., L / II, .Ha / 15.11a / 20.11.bi ^ 3a, 19,208 ^ 43,43a, 11cl,: ·) the hovercraft is only operational, and that it can turn into a trailer (8a or 1 T / 11a) with wheels (32b) ', and that this wheel trailer (8a bzu. 1i / i1a) with content is designed so that it. not only to the cell air cushion boat (20) flia / 20) bzu. zumZellen and. Finger, air cushion boat (15.2G.)> But also to the air cushion boat aircraft with hydrofoil connection (6a) with Seitenuändan (6b) for ground impact ^ - _, and that this wheel trailer (8a or 11 / 11a) with The content is constructed in such a way that it can alternately move from the airboat into all the state-of-the-art missiles (6,6a, 6b, 9,10,12,18 + 21c, 41,49,49a, 49b, 33, 33a, 34a), in which this Einsatzk ^ r-pel- in different ways (28, 28a, 28b, 37a, 37jD _> 4 _J + jibf - 'tfas hovercraft / aircraft ard ^^ M ^ & n-k ^ m & x ^ y ^ ifzu ^ that these insert bodies can be identified as Ματ _, --- ~~ t ^: orrad (2aa), cabin scooter (2ac), caravan (~ 3) - ~ ^ ufijd_the automobile (2) also from the air cushion boat can solve (35a, 35b ^ Tf ^ L ^^ 22II), so that in this case the mentioned insert bodies become independent missiles, and that finally after this hovercraft / aircraft version this hovercraft / EPO - COPY 'Aircraft in a' automobile (2), motorcycle (2aa) and bicycle (1) propeller boat without lifting drive. (37a + 37b) or according to DE 3049833.0 A.1 and DE 3029763 A1 and to the air jet boat according to DE 33938 A1, and that the above and the remaining features (.2a, 2b, 2bl, 2ad, 4a, 4c, 4I, 4aII, J1, 4bIII, 4cIV, 13b., 13c, 13d, 9 / 22,38a, 14,16,16a, 11b £ 1,21a, 21b, 38 j _1c , 21c, 22,22a, 22b , 22c22d, 23.23a, 23b, 25.25a, 25b, 26.26a, 27a, 31.1b, 34.34a, 36.36a, 40.41a, 43.44.44a, 45.46.47 £ 9y32k50 , 18,113,1II, 32b, .8,11 / 8, V8, 'JIS ₁ Bc ₁ Bd, 20c, ITb.Iä) ¹ ' within 'this application - are interchangeable. ~ .. ■ 2. Hovercraft / aircraft according to claim 1 or one of the following, characterized in that.-During the operation of these lifting propellers (4) tthe resulting Air flow to the free spaces under the Baotsboden (38) pressed {see above that here according to the invention by this inherently stable clamping strips / cells - Delimitation of a large air cushion can arise in which this compressed air is already in this erf indyngsgema'ß named "clamping strips / cells" (11a / 2Q) arrives, so that small air pebbles next to the large central air cushion are generated around the entire boat, and that 'these Cells (20) with. the lower clamping strips (11a) so detachably connected stand that these cells (20) can also be replaced individually, and that these cells (20) on the lower clamping strips (11a) are detachably attached so that these cells (20) only to the interior protrude, and that also on the outside of the tensioning strips for the inflatable Uulste (i3a), tensioning bracket (11b) are detachably attached, and preferably constructed according to L / l will. 3. Hovercraft / aircraft according to claim 1 or one of the following, characterized in that instead of three force distributions according to L / l, preferably only one V-belt transmission simultaneously for lift and thrust in a modified form according to DE 30 33 938 A1 takes place in which the propellers / sheathing is not preferred under the floor planks (B), but preferably at the stern of the hovercraft in the suspension frame (14) for this Push and stroke is detachably housed, and vorzugsw. according to L / lI is being built. ■ EPO-COPY Air cushion / missile according to patent claim 1, 3 or one of the following, characterized in that in this construction implementation L / II several propellers / jackets (4, 4b, 7), (4a, 4c, 7) or preferably a larger propeller / Sheathing for the simultaneous thrust and stroke mounted /, in which the several or preferential as one propeller / sheathing (4,4b, 7) on preferably zuei parts (7b.b _/ ) is divided so that the air flow in the upper part for provides the thrust and in the lower. Part of this air flow cannot exit directly, but through Uerbindungs-Uulste (43a) to the aprons / bulges (43) and to the clamping strip cells (I1a / 20) or rearranged clamping strips / fingers, and is preferably built up according to L / II . Hovercraft / missile according to claim 1, 3, 4 or one the following, characterized in that these aprons / 'Julste (43) have elastic -Haltesparnbügel (11c), which do not cirt the hull (13) _} but vorzugsw. are releasably connected to the lower tensioning strips (11a), and that, in contrast to the above-mentioned assembly lead-through L / I, in this assembly-lead-through L / II the Zslleh (20) is detachably attached in the lower area of the tensioning bars (11a) are that these clamping strips / cells (11a / 20) protrude `` to the outside '' so that they can be comfortably supplied with compressed air from the cited aprons / bulges (43), and that the aprons / bulges (43) have oval openings (44) to the cells (20) or fingers (15) for the air flow. Hovercraft / aircraft according to claim 1, 3, 4, 5 or one of the following, characterized in that the clamping bars / cell (I1a / 2O) preferably consist of two cells (20, 20a) exist in which the outer cell (20) is releasably fixed to the clamping strips (11a) so that their cutout (20b) points to the air cushion room, and that another cell (20a) rotatably and .exnrqstbar housed in die.ser outer cell (20) is, so that this rotatable cell (20a) vorzugsw. has the same section (20c) as the outer cell (20), so that the Clamping strips / cell (.113 / 20) immediately into a clamping strip finger (11d / i5) can be switched, if necessary by turning the two Section «(20b, 2Cc) of these cells (20, 20a) one above the other stand and lock and preferably. is built up according to L / II. EPO - COPY 7. air cushion boat / aircraft according to claim 1, 2 or one of the following, characterized in that the roller system. (37) preferably consists of three rollers (37,37a, 37b), and in that these rollers are successively placed on the floor planks {8) is thus a displacement _t of the insert body from the hovercraft-B'etrieb to the air propeller boot 8etrieb easily convertible xst _r the respective shifts to the bow "lifting and pushing roller ", to the stern "pushing üz.u. idling roller" ·, JL 3S S θ Π the hanging systems in which the new location (37-'ä + 37b) or. (37 _; 37a) the tin.satzkkörei (2,2aa, 2ac or 1) rigid and their drive wheels bzu. Hold the drive wheel (32) in an elastically releasable manner (17a), and that the V-belt (42a) at two points (4.46) + (4b, 46) or preferably during the rotary transmission. three digits (4,46) + (4u, 46, 4c, 46) a loop shape (46) .geigen, .and is preferably built according to L / I. . Air cushion boat / aircraft according to claim 1 or one of the following claims, characterized in that when using a linkage structure (22), rotor (25), Flugseqel (18), wing (6,6b) wing connector (6a, 6b \ footplates (~ 21), wobble balance (41,41a, 41 b, 40, 4Oa), slider (21 c, 41, 41aa, 41bb, 40,40a), rudder E4 propellers / jackets (7a, 4b, 7.4c, 36 / 36a + 2a, 2dd), horizontal stabilizer (33) and ailerons f49a, 49b, 6b] the hovercraft the prerequisite is preserved in a dra- ' small wing (i8), hydrofoil (6,6a, 6b) or rotary wing (9 | 10, 12) ^ to convert and - while the drive from the vehicle / motorcycle / cabin scooter (2:, 2äa, 2ac. :) in different ways (32 + 37, 37a, 42, 42a, 4,4a, 4b, 4c, 25 + 27, 32 + 28,41,4aII, 4bIII, 4cIV, 2bI, 25V, 29) takes place, and is built up according to L / l or L / II. . Air cushion boat / aircraft according to claim 1 or one of the following, characterized in that the foot plates (21) and the slider (21c) in connection with the tumbler (41,. 41b) + (21,21 / 41,23,24,25,40,33a), (41, . 41a,. ) + (21, ^ 21 / 41,23,24,49a, 49b, 6b, 6,6a, 6b), (41aaa, 41bb) + (21c, 41aa, 41bb, 40,40a, 33a), (21c, 4'1,41aa, 41bb) + (21c, 41aa, 41bb, 40,40a, 33a + 41,23,24,49a, 49b, 6b, 6,6a, 6b) or ' (41,41aa, 41bb) + (21c, 41aa, 41bb, 40,40a, 33a + 41,23,24,25), and for all missiles belonging to the state of the art (6,6a, 6b, 9, 10, 12) im - «äU EPO - COPY Connection with a motor vehicle. (2), motorcycle (2aa), caravan (3) bzu. Cabin roller (2ac) can be claimed, and that in the case of the wing / hydrofoil connector versions (6,6a, 6b) vorzugsu. only the right (41aa) and vertical (41bb) pivotable fingers for the elevator cable (40, 40a) in "Claim, so that without (41,23,24) y this slide (21cj for hydrofoil / hydrofoil- ' .stubs (6,6a, 6b) and with (41,23,24). the same slide 21c for rotary wing aircraft (9,10,12) is to be used, and the steering rod (2dd) bzu. Steering wheel (2a) in connection with the rudder / Luftschraubsn / sheaths (7a, 4b, 7, 4c, 36 / 36a + 2a, 2dd) and " that instead of the aileron (6,6a + 49a, 49tj εη this wing / Wing connector (6,6a), ailerons (6b + 49a, 49b) at the end edges the wing / hydrofoil connector (6,6a) in the area of the side walls (6b) are installed so that they can be rotated, and that the side walls (6b) for the floor impact with the Koncelgsstängen (5aa) are connected to the fact that the ailerons (6a + 49a, 49b) and the ailerons (, 6b + 49.a »49b) are at the same time for the. mission commarr, and built according to L / l or L / II uirdo 10 .. Hovercraft / aircraft according to claim 1 or one the following, characterized in that with additional drive motors (5b, 5b) bzu. at a Drive motor (5b), power generator (2B) and propeller propulsion engines (4I, 4aII, 4bIII, 4cIU, 25V), this drive is also carried out by Carauan (3), and the structure of the rods: (22,1,1 + 11,22a, 22b, 22c, 22d, 22a, 22f, 22g, 22h, 47 h to 221,35a) and the rotor (25,25a, 25b, 25c, 23,24,26,26a, ' 26aa, 26bb, 25ca, 25cb) so. are such that the vehicle. (2) bzu. the Carauan (3) with bzu. without friction in the hovercraft housed (16,11), alternately in a hydrofoil (6,11b) bzu. Rotary wing aircraft (9,10 + 6a, 12) um-: is adjustable, also a cabin scooter (2ac) bzu. Motorcycle with attachments 2ab) can be converted into the aircraft versions (6,9,10, 18) move without a hovercraft, and preferably after L / l built up. . Hovercraft / aircraft according to claim 1, d a d u r ch characterized that when applying an applied (28a) bzu. sprayed layer (28b) on the wing / wing connector (6,6a) the rotor blades (26a) to the plug sail (1B), the energy received from this layer (23a, • 2Bb) alternately bzu. with the support of the motorcycle (2aa) _-, EPO - copy Caravan (3), cabin scooter (2ac), motor vehicle (2) motor drive (2bb, 5b, 2ae, 2b) or via the hovercraft to the power units (4 I, 4aII, 4bIII, AcIM _t 25U), and is preferably built according to L / I or L / II. 12. Air cushion boat / aircraft according to claim 1 or one of the following, i.e. characterized by that the inner rotatable cell (2Qa) is arranged as a finger (15) so that it can be pulled out, so that due to a substantial extension dss Fingers (15) can even be used at sea in rough seas, and is preferably set up according to L / II, 13. Air cushion boat / aircraft according to patent application 1 or one of the following, characterized in that the mentioned versions of 6, 6a + 6b, 9, 10, 12 are preferred suggested with the following airboat bushings L / I, L / II be, according to L / l, - floor plank wheel trailer (Ba), flight wrench (10), b'zu. Helicopter (12), on the other hand ^ to L / lI, Tension bar wheel trailer (H / I1a), hydrofoil "(6), hydrofoil rotary wing with wing connector (6a) and side walls (6b), and gyroplane (9). 14. Air cushion boat / aircraft according to patent application 1 or one of the following, characterized in that da3 according to a feature of the two mentioned structural leadthroughs L / l and L / II in both cases, the elastic seal (13b) not on the inflatable / uulsten (13a) or apron / uulste (43) / but on ^ the inside of the clamping strips (11a) releasably attached is
attached, and that under the Boo'tsboden (38) a holding keel (38a) is also detachably attached, which on the one hand has the task of holding the actually heavy land vehicle over the air cushion space in retirement, and on the other hand also the holding structure against the air cushion when in use to be maintained by holding ropes (38b). 15. Air cushion boat / aircraft According to patent application 1 or one of the inferring, characterized in that according to the letter Dl3o297.63 1 (folding boat) preferably also for these superstructure bushings L / l and L / II as a hovercraft Oie embodiment is claimed that the preferably two-part exhaust of the Landfahrzeuges'mit vorzugsw. one -GoS-HbflüQ-T ^ stanga (9/22) is detachably connected. 5 ^ 3 "' EPO - COPY