DE10251280A1 - Aerostatic flying device comprises balloon-like hollow component filled with several gas bags forming outer skin and especially constructed as supporting gas envelope connected to platform by support framework - Google Patents

Abstract

The aerostatic flying device (I) comprises a balloon-like hollow component filled with several gas bags which form the outer skin (4) and especially constructed as a supporting gas envelope (1). A support framework connects the supporting gas envelopes to a walkable platform (2) and encompasses all the gas envelopes protecting them against damage. The flying device is remotely controlled from a station such as a lorry (3) on the ground or can be manoeuvred in air space from the flying device itself.

Description

The present invention relates to an aerostatic aircraft, from which work operations or transports of various kinds Way executable are.

From the prior art are for the execution of Work and transport work on buildings such as Cable cars, oil derricks, church towers, mountain slopes, narrow Mountain gorges, avalanche slopes, Explorations, measurements, rescue of avalanche victims, observations the air, on radio / transmission towers, television towers etc. from or from Airspace known from a number of technical means, e.g. Helicopters, hot air balloons, semi-rigid / rigid airships also known as blimps, or on Jib booms at working height promoted Cabins, pulpits, etc. when the attack on September 11, 2001 on the World-Tradecenter the world and the emergency services

Disadvantages of these known transport u. Aircraft are their Possible uses and applications limited by a number of different criteria and thus also severely restricted are. These criteria include the working height, with a crane max. approximately 100 meters. With a helicopter, it is the high operating u. Flight costs, difficult Positioning by the pilot, the risk of falling, even in the event of overload, Risk of collision, the terrain profile, or the work-related dangerous Near the rotor blades to tall buildings, trees Rocks, mountain gorges too narrow, balloons and airships is the big one Case diameter and the tall Length that Space problem. There is a risk of tight terrain conditions that the Outer shell injured, the gas cell / s is leaking and also causing balloons to crash as well the blimps (i.e. semi-rigid airships) can lead; is also a large airship, that for Loads of over 100 tons is designed, with loads well below a hundred tons not Can be used profitably, i.e. not adaptable to the load. Because of the closed Outer shell can no devices either or scaffolding additionally screw onto the internal supporting structure. For space reasons is also the normal airship in rock and house canyons because of the length for construction work or rescue operations suitable. The long cigar shaped Airship also cannot simply be turned vertically i.e. vertical be set up if it would be necessary for reasons of space, since the internal supporting structure does this not allow because it is firmly connected to the cabin. Other criteria are how e.g. Control, suspensions, horizontally mounted drive motors, which are the possible uses limit the aforementioned means or airships.

The boundaries became particularly clear the previous technical possibilities shown when the attack on September 11, 2001 on the World Tradecenter the betting and rescue services passed out watching how at a height of approx. 400 meters people shouted for help and died in the fire because with none of the known rescue devices was to help them. Because of the high altitude, no ladder and because of the strong outside no helicopter could be used to strike the flames, because he would be through the flames because unprotected, caught fire and crashed

The object of the present invention consists in the proposal of an aerostatic aircraft in the simplest and very robust construction and, if necessary, modular construction, that it in the load capacity, the external dimensions, as well in the compilation of the carrier gas casings and the supporting frame the respective Work deployment, the environment (e.g. in the mountains, canyons, avalanche slopes, mountain gorges, towers, Buildings of all kinds), those to be lifted or transported Modular load adjustment is, in contrast to known airships with their inner Falsework, So inside the closed outer skin, but with that in the Aircraft described invention the supporting structure Outside around the gas envelope (s) is built. This makes the support structure easier to construct, can be enlarged at any time or can be adapted to the task and the load to be lifted or transported, but still inexpensive manufactured by modular construction and assembled by means of modules can be. Thus, with the external scaffolding an all-round impact protection for the gas envelope (s) is automatically formed and at the same time the aircraft the dimensional stability given. On this outside shoring in contrast to the normal airship with the inside Shoring, all kinds of devices and components can be installed without using the outer shell the very sensitive carrier gas cells for the assembly located in it holed by elements to have to. Also, the aerostatic aircraft should pass through the outside modular shoring concept without great Preliminary planning, in every shape, size, arrangement of the gas casings and adaptation to the often still unknown load, as well as terrain environment quickly on site according to the requirements, operating conditions using universal and different shoring elements can be assembled which is important for disaster relief.

By means of the aircraft according to the invention, it will be possible to provide an aerostatic flight carrying and / or lifting device which is advantageously used and used where the possible uses of known means are scarcely or not possible. In particular, due to the aircraft according to the invention, it will also be possible to use it on buildings and skyscrapers over 100 meters high in the event of a fire, such as the fire on 11 Sep. 2001 in the World Tradecenter, even at such heights extinguish the fire and save those in need.

The object is achieved in that the aircraft (I) consists of more than one with possibly several gas cells ( 1.1 ) filled balloon-like in the further as a carrier gas envelope ( 1 ) designated hollow body ( 1 ), at least one stage-like accessible platform ( 2 ), the carrier gas envelope ( 1 ) with the platform ( 2 ) connecting the carrier gas envelope ( 1 ) all-round supporting frame protecting against mechanical damage ( 2.1 ) is formed.

Further explanations are provided by means of the in the protection claims 1 to 45 specified characteristics explained.

Embodiments of the specified Invention will be explained in more detail with reference to the following drawings.

1 shows the entire aerostatic aircraft (I) with crane in front view

2 shows the entire aerostatic aircraft (I) with crane in side view

2a shows as the longitudinal section 2a the aerostatic aircraft with crane in side view, which indicates the waves with the rope pulleys for the synchronization control of the two separately running trolleys (lower one for receiving the rotating roller for the crane rope and upper one for the load balancing balloon).

2 B shows the crane cross-section AA 2c of the aerostatic aircraft

2c shows the crane in top view 2a , especially the synchronous system ( 4 Rope pulleys with the all-around tow rope, which in turn is attached to the cross struts at the back and front ( 9.1 , 3 ) the trolley on eyelets ( 9.1 , 4 ) is connected) for the two trolleys

3 shows the entire aerostatic aircraft in section 3a eg as a floating scaffolding with a carrier gas envelope in an annular design, other shapes of the carrier gas envelopes are also conceivable.

3a shows the entire aerostatic aircraft 3 in plan view with indicated distance or holding elements for the carrier gas envelope.

4 shows the entire aerostatic aircraft as a floating scaffolding, for example around a round water tower with a variant of vertical hanging cyl. or cigar-shaped carrier gas casings

4a shows the entire aerostatic aircraft 4 in the top view.

5 shows the entire aerostatic aircraft also as a floating scaffolding for, for example, a fire brigade deployment around a stand-alone high-rise building with a variant of horizontally hanging (vertical is also possible here) carrying gas casings.

6 shows side view of the entire aerostatic aircraft in flight, with load crane, load taken in, but also with complete wind-slip covering of the carrier gas casings including the supporting structure.

6a shows a front view of the entire aerostatic aircraft in flight, with load crane, lifted load, but also with complete wind-slip covering of the carrier gas casings.

7 shows enlarged detail X as a side view (front view analogous elements) of the scaffolding elements in the z. Example as any grid frame, with the connecting flanges, for any length design and connection of the supporting frame or supporting frame parts in all directions.

7a shows the top view of 7 (Detail X) with the indicated cylindrical carrier gas casings.

description of the details

1 shows the aerostatic aircraft I in the front view with two cigar-shaped carrier gas casings 1 , a centrally located load balancing envelope / balloon 8th which on the upper trolley 9.0 , 1 , This runs in the trolley rail 9.2 of the overhead crane 9 and is on the upper eyelet 8.1 tied up and drives with the lower and upper trolleys 9 , 0 / 9.0.1 With.

This is also the carrier gas envelope 1 as a protective frame surrounding the supporting structure 2.1 , as well as the platform 2 shown with a railing on which the assembly personnel can walk and work. For the adaptation of the load capacity to the load to be taken up min. an additional load balancing balloon 8th' and min. two more carrier gas casings 1' indicated, which can be quickly unloaded from the truck, inflated with lifting gas and additionally attached, so that the lifting capacity can be increased on site without knowing it beforehand. It also shows the tethers 6.1 with pegs hammered into the ground / rock, as well as adjustable, inclined or straight telescopic for any terrain, also hydraulically adjustable supports 11 ' with which the aircraft I at any working distance from the ground 12 can be held and fixed. A supply vehicle is indicated below 3 with the control units, with the lines 5 / 5.1 for the operating media, for example 1 Helium gas, compressed air and for the power supply. This supply vehicle (s) is constructed in such a way that the disassembled aircraft I can be transported, set up, supplied with the media required for operation via lines and can be remotely controlled for use in work.

2 shows the aircraft I in a longitudinal view. This shows the outer skin in particular 4 that the carrier gas casings 1 with their individual gas cells 1.1 encloses. Above that are the additional ones Supporting gas envelopes 1' and load balancing balloon 8th' with the surrounding supporting structure 2.1 , which also serves as a protective frame, with the platform 2 drawn with symbolic. Personal / operator 3.1 , Trolley crane 9 trolleys 9.0 / 9.0.1 , Trolley rail 9.2 , indicated as a line. cables 5 / 5.1 , Supply car 3 , Crane hook 9.1 , Crane hook rope 9.1 , 1 , Crane hook rope pulley 9.1 , 2 , with attached load 10 , Ropes indicated 6.1 , telescopic supports 11 , Seat belts 1.2 , Safety nets / string nets 1.3 or as tarpaulin cover. for holding the carrier gas casings 1 , Pipe clamp with eyelet 1.4 for attaching the lines and ropes, lower support frame 6 to which all crane parts and safety ropes are attached, the pluggable quick connection elements 7 for quickly connecting the scaffolding parts 6 / 2.1 which are of course secured against slipping out.

2a shows the aircraft I in its longitudinal view as a sectional view 2c , where the following is shown in detail. It is mainly shown the synchronous system of the two trolleys 9 , 0 / 9.0.1 , Trolley crane 9 , Crane hook rope 9.1 , 1 , Crane hook 9.1 , Crane hook rope pulley 9.1 , 2 to hold the crane hook rope 9.1 , 1 , Trolley rail 9.2 to accommodate the two trolleys, trolley rollers 9.3 to carry the trolleys 9 , 0 / 9.0.1 , Deflecting rope 9.4 for the synchronization of the upper and lower trolley 9 , 0 / 9.0.1 , eight pulley pulleys 9.5 for guiding and deflecting the deflecting rope 9.4 , four waves 9.6 the the upper and lower pulley pulleys 9.5 Connect non-positively with each other, so that a precise synchronization of the balloon for load balancing and the lower trolley, on which the crane hook with the attached load is rotatably fastened. The two trolleys with synchronous control are required because there is a stable connection in the middle of the trolley rail to the left and right by means of supporting bolts to the lower supporting structures, through which the entire crane system hangs on the supporting structure. These support bolts 6.2 can only be avoided by the aforementioned system of two separately suspended trolleys with the synchronism shown here as a rope deflection without the load balancing balloon slipping away, which serves to prevent the normally horizontally suspended aircraft from tipping over when the load is off-center.

2 B shows the trolleys 9 , 0 / 9.0.1 above and below with the rope pulleys required for synchronization 9.5 as section A – A 2a , where the following is shown in detail.

The lower frame is on average 6 , shown here in the example as a tubular construction, on which the support bolts are used 6.2 the trolley rail to the left and right 9.2 is attached to the neutral fiber in the middle of the trolley rail. At the top is the suspension point here as a holding eye 8.1 Designed for the connection of the load balancing balloon, the deflection roller system from the front view, consisting of deflection rope, is also clearly shown here 9.4 , Pulley pulleys 9.5 , four waves 9.6 the the upper and lower pulley pulleys 9.5 Connect non-positively to each other.

The synchronous system can of course also out other drive elements, e.g. through a toothed belt drive be formed.

2e shows as a cut 2a the top view with the lower support structure 6 , the trolley rail 9.2 with the trolleys 9 , 0 / 9.0.1 , the synchronization device in the form of deflecting ropes 9.4 , Pulleys 9.5 , Cross struts 9.1 , 3 the trolley, eyelets 9.1 , 4 for fastening the deflecting ropes 9.4 for the synchronism of the two trolley cars. In the top view, the arrangement of the cable pulleys in the lower support frame is also clearly visible, which is what makes this synchronizing device so special, around the support bolts 6.2 without too much effort.

In the case of a very long trolley rail with the trolleys moving back and forth and the load attached to it, would be without the connection by the support bolts 6.2 and with the lower inner scaffold profile, no rigid scaffold structure is possible, but would be very unstable and the trolley rail support would bend excessively.

However, due to the intimately connected construction of the trolley rail 9.2 with the supporting frame profiles closely arranged on the left and right 6 and stiff with the support bolts 6.2 connected, there is also good statics for the supporting structure, which also affects the weight and thus the helium gas consumption as a lightweight construction.

3 represents a variant in which here a one-piece annular carrier gas envelope 1.5 and as an example around a water tower 1.6 built around hovers, a support frame, here as a pipe ring 1.8 with working platform 2.1.2 which at the same time via spacers inside 1.8 , 1 at a distance x the carrier gas envelope 1.5 from friction with the water tower 1.6 on the outer wall A should prevent. This is achieved by min. three soft or springy spacers 1.8 , 1 reached. Via vertical scaffolding poles going down 2.1 , 1 becomes the all-round working platform 2.1 , 2 by means of connecting elements 2.1 , 3 with the upper ring-shaped pipe ring 1.8 connected. Several, but min. three holding ropes that are flexibly adjustable in height 6.1 provided that can be adjusted by means of winches attached to the floor.

The above example shows one Construction as used in many places of work, e.g. on all types from very high towers, vertical grain stores and all silo types for repair and construction work, which with the usual Turntable ladders are no longer accessible, but analogously as one for the staff safe working platform in large Heights used can be.

Is also through some standardization the parts a fairly inexpensive work platform that can also be produced at still more undisclosed locations than the helper in the Emergency where it can not be done with helicopters can.

Thanks to the quick components and trained technicians, the system is relatively quick in an emergency assembled and operational. The operating costs should also be significantly lower as a result than in helicopter operations.

3a shows the top view of 3

The top view shows the special ring shape of the carrier gas envelope 1.5 clearly, that by means of indicated straps 1.2 , Safety nets 1.3 and pipe clamps 1.4 , on the ring 1.8 is attached or hung. To avoid damaging the round carrier gas envelope on the building, there are at least three resilient spacers 1.8 , 1 on the round support frame 1.8 appropriate. Other protective cover designs for the carrier gas cover 1.5 are indicated in the form of a spiral 1.5 , 1 around the round carrier gas envelope, or as a resilient grid surrounding the carrier gas envelope 1.5 , 2 , which can consist of all materials and their combination.

4 shows a modified variant of the 3 / 3a , in which instead of a one-piece annular carrier gas envelope 1.5 , cigar-shaped or cyl. Carrying gas sheath / n 1'' in a vertical position around the water tower 1.6 built hovers, also a horizontal all-round support frame made of standardized pipes or profile elements, which are laid crosswise and by means of connecting elements 7.1 as well as clamps 7.1 , 1 be held together with a work platform 2.1 , 2 , which simultaneously holds the carrier gas envelope 1'' from friction with the water tower 1.6 should prevent. This is also achieved by min. three soft or springy spacers 1.8 .2 and or with min. three horizontally adjustable rubber / plastic rollers 1.8.3 reached. Via vertical scaffolding poles that go down or up 2.1 .1 will be the three working platforms around the tower 2 by means of connecting elements 2.1 , 3 connected. However, several are min. For the required working height. three holding ropes that are flexibly adjustable in height 6.1 provided that can be adjusted by winches attached to the floor.

The above example shows one Construction as used in many places of work, e.g. on all types from very high towers, vertical grain stores and all silo types for repair and construction work, which with the usual Turntable ladders are no longer accessible by analogy and as one for the staff safe working platform in large Heights used can be.

Is also through some standardization the parts a fairly inexpensive work platform that can also be produced at still more undisclosed locations than the helper in the Emergency where it can not be done with helicopters can.

Thanks to the quick components and The system is also integrated in the event of an emergency Assembled relatively quickly and operational, especially since one for rescue firefighting operations many assemblies as possible and situation in the pre-assembled state. This should also help the dangers and operating costs are significantly lower than at Helicopter operations.

4a shows the top view of 4 In plan view, the ring-shaped or polygonal space-saving arrangement is shown here by a total of eight vertically hanging cigar-shaped or cyl. Carrying gas sheath / n 1'' 1.5 clearly, the also with (not shown here) straps, safety nets and pipe clamps, with the scaffold 1.7 are attached.

5 shows a variant in the form of a rescue airship in use on a burning high-rise or skyscraper, on which, for example, a horizontal and two perpendicular to the plane of the drawing gas casings arranged around the building 1'' stand at the very top near the burning floor, a quick-erect scaffolding specially designed for fire use 2.1 that with vertically mobile work platforms 2 as rescue baskets 2 ' is equipped on the left and right to extinguish the fire from there, and to be able to save people and goods in the baskets by means of a fall bridge. The baskets can be cooled with water and hung on winches to serve as a rescue elevator at a safe distance. The carrier gas casings 1'' are here additionally with one or multi-layer protective shields 2.1 .4 protected from the flames.

The entire floating system is held at the respective height by winches on the indicated fire engines 3 attached, or standing on the floor. Of course, the fire extinguishing medium (water; foam) is routed from the fire engines up through hoses, whereby all types of water spray or fire extinguishers can be used at the top of the fire.

The fire protection shields are on the left and right 2.1 , 4 indicated which should keep the heat from the gas carrier sleeves. Protective shields are of course installed wherever fire or radiant heat goes (but not shown here).

The supporting structure is according to the house lengths in various quick components (from all conceivable materials) statically calculated in advance with secure connection nodes and mechanically designed so that each Length off different lengths of scaffolding elements is practical and quick to assemble. Likewise, the size is that Number or length of the gas casings adaptable to the load to be lifted. But if there is a fire at row houses breaks out, the modular scaffolding with the attached Supporting gas envelopes can also be used appropriately converted here.

But then on the wall of the house in one To stay a certain distance, a bracket or wheels with suction cups, magnets, grappling hooks or other mech. Claws that cling to the wall are operated. The great advantage of this floating extinguishing system is that the height of the building is irrelevant, so it can be used universally on any tall building, including skyscrapers or mountain walls, as a work, fire extinguishing and rescue system. Long training is also not necessary, since the assemblies are simple, very modular and self-explanatory.

6 and 6a shows another variant of the aircraft in a simplified longitudinal and front view, where the carrier gas casings 1'' to reduce the air resistance all around or optionally only at the front, with stable, light but tear-resistant film cladding 13 made of plastic, sheet metal or other covering against the wind pointed and thus aerodynamic ie aerodynamically to all sides and inside by means of supports 13.1 can be stiffly clad. The longitudinal view also shows 6 two indicated motorized cables 14 on which ropes 14.1 hanging down on a traverse 15 are attached. It depends on the risers 16 weight 17 , This also shows the front view in 6a , with the pulley installed in the middle 14 , the ropes 14.1 , the traverse 15 , the risers 16 and the load attached to it 17 , The number and position of the pulley blocks, as well as the size of the traverse, can be variable, that is, they can be economically adapted to the cargo or the application.

The decision to disguise the aircraft because of the air resistance can also be decided at the construction site by the likewise modular cladding technology and then assembled when it is finally certain how long or how high, depending on the arrangement of the carrier gas casings, the aerostatic airship will be, and then get dressed up quickly. By the way, absolutely gap-free cladding for wind repellency is not necessary here, since it is not necessary at flight speeds of generally less than approx. 30 km / h. But against the fluttering in the wind, the panels should be supported from the inside according to the invention 13.1 be supported. So with this module system you have all possibilities to adapt to the tasks on site. In the event that the airship is to fly self-piloted or remotely controlled to the unloading location with the load, the engine can be assembled quickly 22 with propeller 23 (also known as a propeller), as well as the elevator required for the direction of flight 24 , Rudder 25 including the other control, fuel, and fuel tank systems required for flight operations as ready-to-fly modules. These drive assemblies can be attached to the support frame at predefined screwing surfaces, with dowel pin holes and threads, using screws, dowel pins, guide bolts or other connecting means, as well as on existing lines (for electricity, fuel, compressed air, exhaust gases, etc.) relatively quickly using trained mechanics what makes this air transport system also very flexible and economical to use.

All of the aforementioned assemblies can also always at hand on the trolley (from case to case Case also requires several vehicles due to the number of components} carried along and thus also in unknown or unpredictable situations (such as e.g. erasable u. Rescue operation on skyscrapers, rescue in the event of avalanches or ship accidents) can be used immediately. In practice it will be e.g. the fire department in america Major cities due the skyscraper is a larger kit on carrier gas casings and scaffolding parts, carry must as the fire department in Munich. Likewise, e.g. the city of Oberndorf in the Algäu each have a special part or Assembly for Mining, avalanche or mountain rescue operations in the Workshops on trailers have it ready, then quickly and, above all, rationally to the respective To be able to react. At sea rescue is natural again a special compilation is required. Due to the very flexible modular design the versatile support frame- rods- connecting elements- different sizes Lifting gas shells as well as the automatic query sensors at the connection points, which the assembled parts to the central monitoring station as OK. or report as an error, the respective can for almost every application Assortment to be stored in advance. The same goes also with individual surveillance cameras mounted on the frame, which quickly using a computer and a parts / assembly status program created the actual-target comparison so that the monitoring person is not overloaded too much becomes. Moreover is a certain process security possible during assembly. It is through this surveillance the faults are also recognized more quickly and can thus be fixed more quickly, saving time become. After a certain routine, it also emerges where the assembly needs to be improved or optimized. The advantage of the camera is that you can doesn't have to install as many sensors. You can also choose the right one Current state including all screws, cables, fasteners, assemblies in the program similar to the Program robot programming. This happens through recurring Recordings of the individually assembled parts, or elements, which be recorded and saved each time as the assembly progresses. this will work later on Insert no attached element lost the camera eye. The scope this total surveillance will determined according to security requirements or regulations.

All airship types can of course meet the requirements built accordingly from the individual modules u. for the faster Use filled with gas carrying cases to be provided. This means e.g., as a pure transport airship, the rescue teams, firefighters or staff in the mountains, at sea, on avalanche slopes, in narrow gorges, narrow forests, or in cities fly to work on any buildings.

7 and 7a shows X as detail 6 another variant of the design of the supporting structure 2.1 as a side view and a top view, a lattice frame construction made of metal or plastic in different lengths being possible as an example. In the example, such a support structure consists of a long supporting frame part 18 , short supporting frame part 18.1 , Struts 18.2 for stiffening the beams, screw-on flanges 19 , Screw holes 19.1 and as a fastener in the example, correspondingly strong screws 20 with safety nuts 21 were chosen. Due to the concept of the different lengths of scaffolding parts, e.g. as a lattice-tube folding sheet or other supporting scaffolding parts permitted for flying bones and built from appropriate materials, the entire supporting scaffold can be used whether side, front strut or for scaffolding / platform parts Parts from the combination of different lengths of scaffolding parts in a logical construction sequence, also with or without plans put together by the operating team, screwed or otherwise securely connected. The assembly is easy to assemble due to the elements and prefabricated assemblies after thorough training and some practice, since the system is similar to scaffolding.

Of course, before taking off everything can still be checked according to a checklist.

8th and 8a shows a connection angle as an example 26 made of light metal or plastic with appropriate screw holes 19.1 , Dowel pin holes for precise fixing of the scaffolding parts.

18 u. 18.1 , The design of the corner connections or other necessary scaffolding part connections can of course also be carried out in any other form or as a purchased part. Nevertheless, everything should fit into the modular structure of the supporting structure so that any assembly (depending on the design of the respective airship type) of the prefabricated supporting structure parts is possible at the place of use without machining. Above all, this can be achieved in accordance with all airship types 1 to 7 , all assembly and add-on parts on the screw-on surfaces for each screw type and direction are sensibly distributed, and through holes and threads are available for several screw sizes and dowel pins.

Also, the connection of the support frame parts by means of hinges, which are molded onto the flange ends are. It looks like that Connecting flanges are designed as hinges at the ends and are always connected with a hinge pin. Thereby The Z-shaped support frame can be used for space-saving transport the hinge connections on the connecting flanges save space folded and transported on the truck. So it doesn't have to totally disassembled. When rebuilding the folded support frame after pulling apart the support frame, attention is now paid to that the Flanges lie parallel one on top of the other so that one is on top of the other offset side of the hinges, also through a hinge pin which can now slide through the two hinge openings. Subsequently a safety ring against slipping out through the hole inserted at the end of the inserted hinge pin. By this hinge system saves you a lot of assembly time, what with a pure screwed flange connection goes longer. This hinge connection is ideal for Rescue equipment, where every minute counts when it comes to use. All connections will be after assembling over electr. Sensors or contact switches on complete and correct assembly checked, what is monitored on a display on the control panel. Show everyone Sensors on the contact, everything is correctly assembled, if not, so immediately the fault location which over the indicator lights are visible.

General information about the aerostatic Airship, including its function and uses.

Through the sketchy in the 1 to 8th illustrated examples and the description of the details, it becomes clear how relatively uncomplicated and universal the airship for the respective application, the respective load, the location, the height, the terrain structure and or the respective assembly or transport task is assembled and assembled from standardized kit parts can be. In terms of load-bearing capacity, length, or ability to fly, it can always be adapted in economic terms from the aforementioned prefabricated components in a variety of ways for the required load-lifting-assembly-observation-fire-fighting or flight / transport task and assembled on site by trained technicians.

The whole airship system with all its infinite designs can be packed with the still empty ones Lifting gas shells Reserve lifting gas shells Reserve load balancing balloons, drive / control units, components, Trolley crane system, work platforms of all kinds, wind panels, various scaffolding parts, Gas bottles or tanks, energy supply devices, field workshop etc. with Tractor-trucks brought to the site and only then, depending on the task, by means of little or more components are installed.

That has the invaluable advantage over the known rigid / semi-rigid airships that unnecessary aviation to the site with the very expensive helium gas, which is also consumed in the process, be avoided.

So gas is only passed through directly at the place of use the filling the covers with helium gas and during of the work involved. At the end of the work, the gas can again by means of the built-in gas bubbles (so-called trim bubbles), vacuum pumps with a gas separation device and pumped back into the gas pressure container through filters to be around for the next Order available again to stand. Also all bulky shoring parts according to a pre-designed assembly plan, only dismantled to the extent that everything again on the transport vehicle (s) in containers, trays and the like. packaging devices fits. The carrier gas casings with the inner ones become particularly special sensitive gas cells packed against damage. After every filling is using gas directional sensors, pressure monitoring devices with Gas-filled wrap searched for leaks. Only then will they be hooked into the scaffolding. Of course you can the aircraft also a few days with gas filling be parked until a new order arrives. How it is handled can always depend on the customer order, situation and required assembly work short-term and cost-dependent be decided. This makes you opposed to the expensive rigid airships in the decision more freely whether it is parked ready for operation, ie filled with gas is, or should it be better parked without gas due to unclear order situation become. The scaffold remains until the order is received, but the expensive helium gas then becomes provisional pumped out and the relatively expensive gas carrier sleeves stowed in protective containers. This will keep the operator from being under the cost pressure of the very expensive helium gases, as is the case with a rigid / semi-rigid airship because of this missing, but still quick and very flexible assembly / disassembly option of the aerostatic airship described in the invention is possible. Because the usual Airships are normal due to the internal scaffolding cannot be dismantled and therefore only for built the continuous use, but what between long periods of use the orders because of an everlasting Gas permeability the gas cells / casings too expensive gas refills leads, because otherwise the gas cells on the inside of the scaffold will relax impaled over time or could hurt. Also, with these known airships, the gas casings cannot be used easily get out of the scaffolding around them, but what with that airship according to the invention just the big one This is an advantage, since according to the invention the gas casings do not constitute the supporting structure inside, but outside mostly around and easily accessible to have. So you can them in one piece relatively unimpeded from the supporting structure built around them can be removed quickly, i.e. easy to assemble. Likewise, through the possibilities mentioned in the invention of hanging one above the other or one behind the other Gas bearing shells the load capacity can be quickly adapted to any load, which is not unnecessary Gas costs. It is also possible according to the invention, if possible exact adjustment of the required load capacity, different sizes from Gastraghüllen zu use, which also reduces gas costs. Because with the usual Airships are always the same gas filling with the associated ones high gas costs necessary. So they are unnecessarily high Operating costs connected, no matter whether a small or large load must be transported.

This is the big cost advantage across from the normal rigid airships, because the aerostatic according to the invention Airship is only that big and extensively equipped, such as the load to be lifted or the expectorant Task requires. Moreover offers the modular system from the above Invention infinite more uses, than they are ever possible with normal airships.

Again the outstanding features and Advantages over a normal, i.e. not permanently convertible, large airship.

• - Man does not always need to know the exact load in tons, but the airship is on site by the number of carrier gas casings adapted to the load, So small load means little gas envelopes, big load correspondingly more gas envelopes. Very accurate cost-conscious The load capacity can be designed using different sized gas carrying sleeves.
• - Becomes it as scaffolding on a water tower or building construction, so only for those here existing total load attached correspondingly to a lot or a few carrier gas casings. Here e.g. it is the sum of the scaffolding, working platform, concrete bucket, crane parts, cables, Safety railings, Connecting parts, building materials, steel cables, straps or nets for anchoring the carrier gas casings, Personnel weight, other small parts plus a percentage security surcharge.
• - Becomes it by the fire department as a rescue device and extinguishing device on a tower, building construction or Skyscrapers are also used, so the aircraft is e.g. as above assembled, but additional for the Rescue and extinguishing of the fire in e.g. upper floors with fire fighting equipment, water u. Air hoses, Power lines, emergency lifts, Fire protection plates on the carrier gas casings additionally equipped. Retrofit of new fire extinguishers on the free outside shoring immediately possible.
• - Specifically for the fire brigade, it would of course be better in the interest of the firefighters if they were given an aerostatic aircraft that had been specially parked for you as a kit with the parts and devices for the extinguishing / rescue operation at great heights with the adapted parts and devices so far pre-assembled on the supporting frame, that they could be deployed more quickly in an emergency, so not everything else Fire fighting equipment must then only be installed. This is easier to handle on normal construction sites.
• - Becomes it in urban Building yard for recurring work e.g. on the same square or round Buildings used, so the gas envelope from gas cost reasons one piece, but still for security with multiple internal gas cells as well in special forms such as can be made round or square. The scaffolding elements can, however in turn be taken from the modular system, what the matter simple and inexpensive.
• - Becomes it only needs to lift a load e.g. on church towers, then only the assemblies and parts (e.g. supporting structure, gas envelopes, can be walked on Work platform, pulley, lighting, etc.) assembled, which for this use is needed. This also applies to the covers the expensive helium gas. So here, too, only those necessarily arise force Assembly costs. because unnecessary Components are not used and therefore not in the gas costs act. which is not feasible with a closed airship would.
• - If it is only required to lift a long bulky load and to transport it for a relatively short distance (e.g. from the power plant to the nearby port), the Aer. Airship can be assembled here very spartan. So just the normal airship 1 , possibly also with the telescopically extendable supports, the anchor ropes with the pegs hammered into the ground, which is towed by a towing vehicle along with the load for unloading onto a ship after lifting the load.

Now comes the way problem, so that Towing vehicle under a bridge or would have to drive through the tunnel, so that's not a reason to give up because of the technical problem. Then it can also be towed by helicopter. going not that either, so you have to Go self-propelled. Because now we have because of the assembly method the possibility, instead of the towing vehicle at the rear of the support frame in the already existing holes the engine with propeller u. Grow tank. Only for this 2-way distance plus safety required fuel is refueled. If it is a short flight distance, the elaborate long-distance flight equipment will not grown, which is additional Need gas would. So the whole structure flies to the port and unloads the load directly into the ship's belly.

However, if incorrect information turns out, for example that the goods cannot be transported by ship due to a lack of waterway or obstacles, this does not make any difference except for a little extra work, because the inventive design also ensures this. In a manner analogous to that described above, the long and windy flight path means that the simple airship is now being retrofitted with the necessary remote equipment from the transporter. According to the checklist, everything that is now required for independent long-haul flights, like that 6 and 6a demonstrate. Important components are added here as follows: The wind-repellent all-round cladding, drive in the form of aircraft engines with propellers, the fuel tank system, the heights and the like. Rudder, the self-steering pot with integrated heated cabin u. Control units for the airship pilot, warning lights, possibly radar, radio system, because of the safety a little more gas casings in the event that a cover would leak and u. should fail that there will be no sinking. Then water ballast tank, counter-compressed air bubble system for trimming in height and later lowering with the load on site. Various cables for control and power supply, all with special couplings or plugs, landing ropes, etc.

For standardized loads, a yoke that hangs on two winches as in 6 shown, can be used as a central load holder over risers. After the quick assembly, all vital assemblies, control units, safety devices are controlled by an electr. Cable system with contact switches on the retrofitted modules u. Items reported to a computer as OK or not connected thus checking the completion. So if a contact switch is not pressed, the element is incorrectly installed and must be remedied. then the error must first be looked for. If everything is depressed and thus reported as OK, the engine can be started and by draining ballast water, or by means of the trim bubbles, which let the air filling out by opening the valve and thus allow the displaced carrier gas to flow back into the gas cells. which means that the buoyancy is now slowly taking effect. Now the airship slowly takes off. The skipper begins to control the airship and drives to the destination. Here, air is filled into the trim bladders again, which compresses the lifting gas and causes the airship to sink. The load can then be unloaded. Now the L-ship can practically fly back again or be brought back disassembled by truck.

For all types where the airship as in the example after 2a to 2c Shown when a huge trolley crane suspended in the air is used, a round load balancing balloon becomes normal on the upper trolley or a cylindrical load balancing balloon, which is much smaller in diameter than the round load balancing balloon, but flat because of the required gas volume longer is attached. In order to achieve a safe load balance, this is always carried along by means of a synchronization control, which consists of 4 rope pulleys that are non-positively connected via 4 shafts. with 2 deflecting ropes, or also as a chain toothed belt drive or other synchronous device, carried simultaneously with the lower crane trolley. Because of the very long trolley rail, the max. can also extend over the entire length of the ship, this rail must u. the rigidity at regular intervals by means of supporting bolts on the lower supporting frames, shown here as pipes, to be suspended rigidly. When used on large construction sites, for example where a trolley crane with several hundred meters of running track is absolutely necessary, almost any crane length can be assembled from the modular components using the modular system and the external support frame. This is a great advantage over all previously known flight transport devices for use in inaccessible areas.

This can also for static and stability reasons whole frame and airship additionally by means of telescopic u. thus adjustable supports on even uneven terrain for the duration supported the work safely become. this results in further uses for the aerost. Airship, where you have never been able to get by helicopter.

The system also offers rescue or building assignments on fonts and derricks.

For cost reasons, the gas filling can also be combined in such a way that a relatively thin fire-retardant helium gas envelope is around the outside and inside is a large inner envelope consisting of several gas cells with the lighter and also cheaper hydrogen filling. This helium / hydrogen combination is particularly interesting for pure construction work, where not many people are involved, for reasons of cost and the better load-bearing capacity. If the whole thing is needed as a high-flying airship, the outer cleavage that splits the wind becomes the same as with 6 u. 6a , shown, grown. This fairing in turn brings a great technical advantage in that it is not round, but is designed as a sharp wedge, as is practiced with jet fighters, and thus significantly reduces the wind resistance of this aircraft, compared to previously known zeppelins / blimps / airships / balloons, etc.

Features and elements that are forgotten were mentioned in the description, but cited in the claims are ultimately also considered to belong to the description.

I

aircraft

1

balloon-like hollow body = ( 4 ) Outer skin

1.1

battery from lifting gas cells

1.2

Safety belts

1.3

nets or tension nets

1.4

pipe clamp with eyelet for fastening / receiving the safety lines / ropes

1.5

Ring-shaped carrier gas envelope Adjusted building object

1.5.1

Spiral wire as a protective covering for the annular, (also for straight Lifting gas envelope)

1.5.2

Latticed wire as a protective covering for the annular, (or straight) carrier gas envelope

1.6

water tower or similar Tower building, too Skyscrapers, round, polygonal, square, or other shape

1.7

horizontal scaffolding poles all kinds u. lengths at the tower or building site

1.7.1

vertical scaffolding poles

1.8

circulating Pipe as protective rod / ram protection against chafing of the outer shell on the building, object etc.

1.8.1

spacer

1.8.2

Rammschutz e.g. in the form of a foam sleeve, or inflated rubber / plastic film body, or also other resilient soft parts / pillows

1.8.3

adjustable Spacers or other adjustable spacers, e.g. also horizontal / inclined adjustable rubber roller

1'

additional Carrying gas sheath / n for more Load capacity (for flexible Load increase)

1''

cylindrical Lifting gas envelope

2

stage similar platform

2 '

rescue baskets

2.1

Supporting frame construction = short scaffolding

2.1.1

vertical scaffolding poles for scaffolding

2.1.2

Work scaffolding ( 2.1.1 ) vertical scaffolding poles

2.1.3

fasteners for scaffolding poles

2.1.4

Fire fender, also from different materials and combinations

2 '

Walkin Platform with a railing as a catwalk for the artisans

3

station

3.1

staff = Operator

4

shell

5

lifting gas

5.1

other media

6

lower shoring

6.1

Take-up measures = Tensioning ropes for fixing the aerostatic airship to the ground or in the field by means of anchors, fish, ring anchors, concrete weights, also mobile anchor weights, etc.

6.2

support bolts

7

Quick fasteners (Pluggable)

7.1

Quick fasteners also for the supporting structure (Pluggable)

7.1.1

Clamping bracket for Holding the bars of the scaffolding together

8th

balloon for load balancing

8.1

suspension point the load balancing balloon on the upper trolley

9

Overhead crane

9.0

lower trolley

9.0.1

upper trolley

9.1

crane hook

9.1.1

Crane hook rope

9.1.2

Crane hook pulley

9.1.3

crossbars the trolley

9.1.4

Eyelets for attaching the synchronous or deflecting ropes ( 9.4 )

9.2

Trolley track

9.3

Trolleys rolls

9.4

Deflection rope for synchronous control of the lower and upper trolley ( 9.0 / 9.0.1 )

9.5

Deflection rope pulley for synchronous control of the lower / upper trolley ( 9.0 / 9.0.1 )

9.6

wave the upper and lower pulley pulleys for synchronous control

10

Bucket, container, building material, or also rescue worker, or other object

11

supports telescopically adjustable, also hydraulically adjustable for the airship

11 '

supports telescopically adjustable, but adaptable to the terrain at an angle

12

Terrain, mountains, uneven floor, or building contour, or (with marine rescue operations also attachment to the hulls of all Art.

13

wind slippery, current budget Covering of the carrier gas casings including Shoring tear-resistant Plastic film, carbon fiber, other organic materials

13.1

inner supports of the cladding ( 13 )

14

Cable drive Crane winch, block and tackle gear, cable winch or other lifting devices

14.1

Crane cable, Load chain, also possible as steel or fabric belt

15

yoke for lifting with two or more ropes tied to it

16

Last risers or other holding devices for lifting the load

17

Load, Transport goods, etc. indicated as a block

18

long Shoring part as an an example

18.1

short Shoring part as an an example

18.2

struts welded, screwed to the side members, riveted, laminated, or glued, or punched, injection molded, as well as other production method of a stable but light lattice construction made of St./Alu/carbon fiber

19

Verschraubungsflansche with corresponding holes to accommodate the connecting screws, quick-assembly bolts, clamps, or other connection

19.1

Screw holes in the connecting flanges

19.2

drilling for dowel pins

20

screw implied

21

mother implied

22

drive motor for propellers or propeller

23

propeller or propeller

24

elevator

25

rudder

26

connecting brackets for the shoring as an example, also cube Three-six-octagonal shape etc. possible

Claims (45)

Aerostatic aircraft which can be operated via an internal and or external control, characterized in that the aircraft (I) according to l from more than one with several gas cells ( 1.1 ) filled balloon-like hollow body that covers the outer skin ( 4 ) forms u. here in particular as a carrier gas envelope ( 1 ) referred to, at least one stage-like accessible platform ( 2 ) the carrier gas casings ( 1 ) with the platform ( 2 ) connecting the carrier gas casings ( 1 ) all around, at the same time protecting against mechanical damage, around all carrier gas casings ( 1 ) All-round closed scaffolding construction, briefly referred to as the scaffolding ( 2.1 ) is formed, wherein this aircraft (I) from a station, for example truck ( 3 ) on the ground ( 12 ) remotely controllable, and or from the aircraft (I) itself, maneuverable in airspace. Aerostatic aircraft according to claim 1, characterized in that the station ( 3 ) stationary or mobile on water and on land and at the same time can be designed as a means of transport / vehicle, as a gas tank, electricity / air station and for controlling the aircraft (I). ( 1 ) Aerostatic aircraft according to claims 1 and 2, characterized in that the carrier gas casings ( 1 ), each consisting of at least two or more modular gas cells that can be filled with carrier gas independently of one another ( 1.1 ) assembled into a battery with a certain length and load capacity in the carrier gas envelope ( 1 ) stored, as well as with straps ( 1.2 ) and safety nets ( 1.3 ), which with the supporting structure ( 2.1 . 6 ) are connected, and form the main part of the aircraft. ( 2 ) Aerostatic aircraft according to claims 1 to 3, characterized in that the supporting structure ( 2.1 . 6 ) a modular convertible, by means of detachable, plug-screwable connecting elements ( 7 . 7.1 ) formed construction, which is the platform ( 2 ) and the balloon-like hollow bodies ( 1 ) connects to the aircraft (I). ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized; that on the aircraft ( 1 ), to ensure the equilibrium position and position, mechanical arrangements for load balancing are provided, preferably for those on the crane ( 9 ) hanging load ( 10 ), in the form of at least one balloon ( 8th ), or as a cylindrical or cigar-shaped carrier gas envelope ( 1 ), which can be refueled and defueled with lifting gas and the buoyancy of built-in displacer bubbles operated with compressed air, which presses on the inner gas cells and can be trimmed controlled by a computer, or the lowering for landing can also be done by sucking up water or sand Ballast or by min. 2 winches arranged on the ends of the supporting frame, ropes with anchors or grappling hooks, which are embedded in large mech. The steel brackets that can be opened hang easily when they are slid over them, after which the winches immediately begin to roll up the ropes and pull the airship evenly to the landing site. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I) on the lower supporting structure ( 6 ) arranged mechanical arrangements, in the form of tension cables ( 6.1 ), which is infinitely variable, adaptable to the surrounding profile of the landscape or the silhouette of the building at the site, anchored and thus making the airship lockable. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I) is preferably operated with helium as the carrier gas, that the platform ( 2 ) can be equipped with various devices and work equipment such as optical precautions such as lamps, measuring devices and similar devices and that the external supporting structure ( 6 ) without hindrance with a trolley-like crane ( 9 ), Crane hook ( 9.1 ), Crane running track ( 9.2 ) Excavator, bucket-like container ( 10 ) or rescue equipment can be equipped. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the arrangement of the balloon-cylindrical or cigar-shaped and similar carrier gas envelope ( 1 . 1'' . 8th . 8th' ) in the network, one after the other and, for reasons of space, the longitudinal axis also vertically one above the other, can be adapted on site to the tasks, load and operating conditions. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I), by means of several, but at least 3, on the supporting frame ( 2.1 ) attached telescopic, vertically extendable, correspondingly stable supports ( 11 ), with each individual support ( 11 ), the different terrain ( 12 ) can extend adapted, and is therefore supported against falling. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft ( 1 ), also by means of several on the supporting structure ( 2.1 ) attached but now preferably telescopic extensions in every direction ( 11 ' ), each individual support of the different terrain in height or width ( 12 ) can be adjusted, e.g. vertically, horizontally or diagonally fixable, is supported against undesired slipping of the aerostatic aircraft (I) on all sides, and serves as a fixed spacer to the mountain, house, etc. ( 1 - 2 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I), in the middle on the lower support frame ( 6 ) between the support frame profiles, shown here as a tube, by means of several rigid support bolts ( 6.2 ) a double crane runner ( 9.2 ) simply a double T-profile, which at the same time strengthens the statics for the entire support frame, is attached in order to use a trolley crane ( 9 ), consisting of a lower and upper trolley ( 9.0 . 9.1 , 0 ), with trolley rollers ( 9.3 ) around the support bolts ( 6.2 ) to be able to bypass, almost over the entire length of the aircraft ( 1 ) from the floor ( 12 ) from a load ( 10 ) on the crane hook ( 9.1 ) with the crane hook rope ( 9.1.1 ) can be hoisted in order to unload them again, for example, over a construction site, the length of the trolley rails ( 9.2 ) here like a usual trolley crane ( 9 ) weight ( 10 ) can be transported from point A to B preferably in difficult-to-access terrain or height. ( 2a . 2 B and 2c ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I), on the lower trolley ( 9.0 ) the overhead crane ( 9 ) and on the upper trolley ( 9.0 , 1 ), on the eyelet ( 8.1 ) the load balancing balloon ( 8th ) that the two trolleys ( 9.0 . 9.0 , 1 ) positively guided by means of a cable synchronization device, consisting of 4 pairs of pulleys, where 2 pulleys each ( 9.5 ) again via a wave ( 9.6 ) are non-rotatably connected, as well as in the 4 upper and 4 lower rollers ( 9.5 ) for the synchronism of the two trolleys ( 9.0 . 9.0 , 1 ) one pull rope each ( 9.4 ) is guided and deflected horizontally, which in turn is attached to the respective trolley at the rear and at the front on the cross strut ( 9.1 , 3 ) and here at the eyelet ( 9.1 , 4 ) is attached so that when the crane trolley ( 9.0 ), the other trolley is moved automatically via the synchronization device ( 9.0 , 1 ) is moved in parallel with the load balancing balloon so that the aircraft is off-center Load lifting with the help of min. a load balancing balloon, which is electr. calculated in advance in terms of size, the number of gas cells, balloons and thus the load-bearing capacity, but is always kept in the horizontal position, a toothed belt drive can also be used for the synchronizing device instead of a cable pull. ( 2a . 2 B and 2c ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the carrier gas envelope also as a closed ring ( 1.5 ) or in all other polygonal versions of the respective building, e.g. water tower ( 1.6 ) are ideally adjustable and close to the body, as well as on the inside of the ring of the carrier gas envelope ( 1.5 ) and if necessary also the outside of the ring with correspondingly ring-shaped tubes ( 1.8 ) are surrounded as ram protection, which are preferably made of light metal but also of other suitable material made of plastic, carbon fiber, wood or metal or from their combination as a lattice construction ( 1.5 , 2 ), as a spiral ( 1.5 , 1 ), which, for example, surrounds the ring-shaped carrier gas protective or can exist as other lightweight designs, e.g. as a spacer ( 1.8 , 1 ) made of soft plastic at a safe distance (X) from the building object ( 1.6 ) on the outer wall A the ring carrier gas body filled with lifting gas ( 1.5 ) in the event of a storm, etc., before the working platform is destroyed or dangerous 2.1 , 2 ) or scaffold ( 1.8 . 2.1.1 . 2.1.3 ) to protect, furthermore the airship is on the support ring ( 1.8 ) using tensioning nets ( 1.3 ) and straps attached, as well as for height limitation with ropes ( 6.1 ) anchored to the ground. ( 3 and 3a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the floating all-round support structure ( 2.1 ), consisting of horizontal and vertical scaffolding poles ( 1.7 . 1.7 , 1 ), Connecting elements ( 7.1 ), Fasteners ( 2.1 , 3 ) designed as a clampable pipe section with eyelet for vertical cyl. Carrying gas envelope ( 1'' ), the work platforms ( 2 '' ) in the example due to lack of space from min. 3 or more cylindrical or cigar-shaped carrier gas casings ( 1'' ), which is around a building object ( 1.6 ) with the longitudinal axis here, preferably vertically, but also horizontally, obliquely, or else in a combined manner, and the supporting structure ( 2.1 ) at usual, the carrier gas envelope ( 1'' ), support cables spanning nets made of any material, or netting on the connecting elements ( 2.1 , 3 ) is suspended, as well as to protect against stripping or boxing the supporting frame or the vertically hanging carrying gas casings on the object min. 3 horizontally adjustable rubber support rollers ( 1.8 , 3 ) are provided. ( 4 and 4a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the floating all-round support structure ( 2.1 ), and the horizontal arrangement of the cylindrical or cigar-shaped carrier gas envelope in the example ( 1'' ), which are connected around a high-rise building ( 1.6 , 1 ), Skyscrapers, or tower-like buildings with all-round walkable work scaffolding ( 2.1 ), can be designed for extinguishing rescue operations, whereby the cylindrical, spherical or cigar-shaped carrier gas casings ( 1 '') because of the balance of min. 3 pieces must exist, these for height adjustment, as well as for quick setup using winches on fire engines ( 3 ). are attached. ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the carrier gas casings ( 1 '') with single or multi-layer fire protection shields ( 2.1 , 4 ) also possible with vertically hanging balloons, all-round or at least 180 °, as a protection against flames, which could flare upward from the building windows, mainly flickering obliquely upwards. ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that, due to the modular construction, it is modified accordingly, and can be used as an elevator-like rescue and extinguishing device with refractory cabins on high-rise buildings / buildings. ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that in the rescue and extinguishing device similar to an elevator, the carrier gas casings ( 1 '') depending on requirements, for stand-alone or in-line skyscrapers / buildings ( 1.6.1 ) Can also be adapted to the shape of the house wall on one side and designed as a rolling rubber roller with mainly horizontally adjustable spacers. It can be fixed to the wall at a safe distance. ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the spacing means in a size and material corresponding to fire safety are designed as a spacing device from the house wall and as wheels, rollers, caterpillars and the like rolling on the wall, or as running vertically on the wall Pneumatic / hydraulic cylinder operated robot feet, which are all equipped with vacuum suction cups, or vacuum suction cups moved with other movement mechanisms are designed for continuous holding on the house wall so that when lifting and lowering the aforementioned elevator-like rescue and extinguishing device via vacuum, magnetic, adhesive or other mechanical claws can be securely attached to the house wall as a holding force even in strong winds ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft is designed in its assemblies as a quick-assembly structure, ie, connections and node pieces as plug-in elements with automatically locking safety bolts, barbs and also as a folding structure, for example as an emergency elevator ( 10 ) on the wall of the skyscraper ( 1.6 , 1 ) if the fire breaks out quickly enough by the fire brigade / techn. Aid organization etc. can be brought to the rescue operation ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the carrier gas casings ( 1 '') also over long special ropes ( 6.1 ) and winches, which are attached to the fire engine ( 3 ) is attached and attached to the support frame, is held high enough at a safe distance from the fire. ( 5 ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the shape of the outer skin ( 4 ) is designed so that it is horizontal or in the direction of flight, all carrier gas casings ( 1 ) roofed and as a lightly cutting through the air, preferably as a sharp-edged, slippery lens shape, or pointed cone shape, wedge shape, arrow shape, disc shape, shell shape or other all around aerodynamic contour in flight / direction of travel or as a covering ( 13 ) formed, with the cladding ( 13 ) can be made from all suitable, stable, against UV rays, water, ozone, as well as from tear-resistant woven, also as grid fabric materials, also foils or also from biologically or synthetically manufactured substances or fabrics. ( 6 and 6a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft can also be quickly and easily upgraded for long flights by means of the modular assembly system, which is made possible by mounting surfaces with threads, dowel holes provided on the support frame, and by swiveling drive motors which can be mounted quickly ( 22 ), Propellers ( 23 ), Elevator ( 24 ), Rudder ( 25 ), Control platform with electron. Control unit, fuel supply system, radar, radio, lighting system, made airworthy, in addition, after assembly of all the necessary assemblies and parts via control lamps and. Monitoring sensors at the connection points of the elements, displayed as OK or not OK in the control cabin. ( 6 and 6a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the circumferential carrier designed to protect the hollow body filled with carrier gas ( 2.1 ) as a lightweight lattice construction made of solid or drawn hollow profiles ( 18 . 18.1 . 18.2 ) with connecting flanges ( 19 ), Screw holes ( 19.1 ), by screws ( 20 ), Nuts ( 2l ) and further threads / holes on the support elements for a universal assembly possibility of all types of prefabricated assemblies, elements, is constructed, the elements of which can be designed in any other bracing form, in any suitable, preferably lightweight material or also as a sheet-wood lightweight construction ( 7 and 7a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the connection angle ( 26 ) for the assembly of the supporting frame parts ( 2.1 . 6 ) are provided, which holes ( 19.1 ) for screws and Dowel pins ( 19.2 ), deviating from the angle, other shapes and sizes of the connecting means are also possible, e.g. as a square, cube, arch, triangular or ball, each with a thread or holes ( 19.2 . 19.1 ) in the screw-on surfaces. ( 8th and 8a ) Aerostatic aircraft according to at least one of the preceding claims, characterized in that the overall outer skin ( 4 ) can be designed from two types of carrier gas shells, that inside a carrier gas envelope made of antistatic foil material is provided filled with hydrogen gas cells and for protection reasons (fire, damage, etc.) this in turn as a second skin with antistatic and thus fire-preventing with helium gas cells ( 1.1 ) filled tubular film is adapted to the respective outer shape, whereby the load capacity with the same material consumption and external dimensions is significantly increased by the hydrogen gas. Aerostatic aircraft according to at least one of the preceding claims, characterized in that the carrier gas casings ( 1 . 1' ) for trimming (e.g. for horizontal posture in the air, inclined direction of ascent, lowering, leveling, etc.) of the aircraft inside with inflatable / inflatable air bubble covers made of elastic or other flexible material, meaningfully distributed, equipped, which serve to to reduce the helium carrier gas cells, then downforce, or let them grow again, then lift, so that they can steer the aircraft in any required direction, which is possible directly from the pilot in the aircraft (I), as well as from the ground station. Aerostatic aircraft according to at least one of the preceding claims, characterized in that the aircraft (I) can be controlled in all directions and in the same way as an airship by means of a pilot, crew, etc., but also from the ground by transmitter / radio control over all distances normal airship is steerable. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the aircraft (I) from an aircraft, helicopter, airship or similar transportierbar- and can be activated, i.e. can be moved or dragged in any direction is. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the aircraft (I) can be dismantled into easily assembled components, by truck can be brought to the site and then quickly reassembled, and that the gas envelopes quickly over several gas connections are inflatable so that the aircraft can be used for emergencies in just a few minutes. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that each The number and size of the carrier gas casings can be varied depending on the load to be absorbed are to save gas costs. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that by the modular design, of the support frame, platform, drive motors with control, gas casings and last but not least, the overall outer shell tear-resistant Foils, rudder / elevator, can be assembled so that the entire aircraft is seen from the outside, like a streamlined one self-propelled airship appears, but modular to save costs The external dimensions vary depending on the load to be transported will be what the expensive helium gas consumption due to the adjusted load capacity significantly reduced. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that suction or pressure pumps are provided over which gas shells are not required to be taught can, to keep the lifting gas consumption within economic limits. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the shoring instead of a overhead crane with a simply constructed, in variable in size Passenger cabin for Team transports in inaccessible Sites, construction sites, mountains, jungles, canyons is what is particularly ideal in size for rescue operations customized can be. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the aircraft due to its modular design also as a simple team and Material handling equipment, as well as a burden, as well as for the assembly team in preferably inaccessible Unloading points (e.g. gorges, mountains, narrow valleys, high-rise gorges can be used is, the aircraft with pilot on board, self-controlled or by someone driving on the ground Car can be controlled remotely. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the aircraft after use, if necessary, with relatively simple steps Pumping out the lifting gas into a tank car, then rolled up the empty casings and the scaffolding can be quickly disassembled so that everything can be safely stored on trucks and easy to bring back to your home town. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that the aircraft so modular with different types of cables, rescue baskets, rope hooks, Extinguishers etc. convertible is that it also used for Ship disasters, oil rigs, wind turbine construction etc., lifting, securing, Rescue of crew and goods, or also in large construction Lifting ships can be used. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that it is also modularly designed so that long bridges over rivers, straits, gorges, Valleys, Housing estates corresponding to the load. with few, many or accordingly huge, or long carrier gas casings are verifiable. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that it is also designed in a modular way to provide emergency bridges in the event of flooding or long bridges over rivers, straits, Gorges, valleys, housing estates etc. as a temporary bridge, or to be worn from above for a certain period of time, to be too strong flow , or at a great distance, if pillars are missing between the support points as a bridge replacement because of for the statics required supports, To serve tension ropes. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that it is also modularly designed to be used as an observation tower, weather station at great heights , Solar power generator about the clouds through solar cells and power cables down to the ground or as a satellite for radio or transmission waves serve, the aircraft is secured against the wind by anchor ropes on the ground and thus fixed. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that it to increase the load capacity too is modularly designed so that shoring as an arbitrarily extendable Lightweight construction is designed and that at the junctions flanges with through holes for receiving connecting screws, or also for Quick connection bolt with safety spring wire against falling apart are provided. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that for a quick Assembly of the scaffolding tongue and groove connections are also provided at the connection points instead of screw flanges are that with cross bolts and locking ring against slipping out the cross bolt can be secured. Aerostatic aircraft according to at least one of the aforementioned claims, thereby characterized that for a quick Assembly of the scaffolding At the individual connection points, instead of screw flanges, hinge connections are also provided are, always opposite the hinge also two hinge parts on the hinge flange provided and by means of a 2 hinge pin and locking ring to prevent the 2 hinge pin from slipping out. are secured, so that through alternately attaching the hinges to the flanges the support frame parts in Z-shape very space-saving for the transport can be folded up and vice versa simply quick in case of use as far apart until all hinge flanges again are parallel to each other and the second hinge pin in the now congruent 2 hinge part holes are inserted. can. Aerostatic aircraft according to at least one of the characterized above and particularly the 43 th claim, that by the connection by means of hinges both very large everything enclosing , as well as small ones in certain lengths and widths depending on size and number the required gas jackets, Very quickly standardized and in special sizes aircraft of all kinds, both for rescue operations of all Art can be assembled very flexibly. Aerostatic aircraft according to at least one of the aforementioned claims, characterized in that by different rows, laterally, one behind the other or one above the other several aircraft a big Roof is created, e.g. For Sports facilities, large construction sites, or as a huge life raft / platform in the event of natural disasters, for ship rescue (prevent sinking. delay) or for the transport of e.g. welded and therefore very long oil-gas water pipes, overseas lines and similar can be used.