DE10206306A1 - Rescue cabin for aircraft accident, separates from remaining body of aircraft and carries passengers safely to ground using parachutes - Google Patents

Abstract

The passenger cabin can be rapidly separated from the remaining heavy body of the aircraft, and is then able to land safely on the ground using sufficiently large parachutes. The passengers remain in their seats within the independent, airtight enclosure.

Description

The invention relates to a rescue device for aircraft of all kinds, in which the passengers take place crash fatally by plane, can be saved by means of the rescue cabin. This happens in the form of a modified removable passenger cabin, which is used as a rescue cabin constructed with parachutes and other anti-impact devices attached the rescue cabin is fitted properly.

In an emergency, the flight occupants (passengers and staff) should go first with this rescue cabin be separated from the rest of the aircraft, i.e. the heavy part, and then by means of Large parachutes and the devices already mentioned sink relatively gently to the ground thereby saving life again and getting away without major injuries if possible.

Current status with the disadvantages is that if a passenger plane, no matter what type and the latest technology, crashes due to engine damage, inevitably also the occupants crash and usually die. The damage from it is human and Substantially gigantic, as well as an enormous loss for the insurance companies and now almost only still an unprofitable business. The insurance premiums make the flight costs so expensive that soon only a few people / cargo can fly because of the high costs.

So far, only different types of parachutes are known for rescuing people Military, test pilots and glider pilots. The currently only known device for rescuing a Aircraft occupants are the ejection seat, but this is only due to physical / psychological reasons specially trained pilots with jumpers / pilot suits is possible. But this is not possible with normal or older passengers in day clothes, and also not with several occupants is feasible. In addition, an ejection seat is not for the inexperienced occupant.

Furthermore, only heavy-duty parachutes for dropping devices or boxes are known.

Conclusion: So usually come with an airplane crash despite modern flight technology almost always all inmates to death. Another disadvantage is that the insurance companies hardly cover the To be able to raise billions in insurance losses. The same applies even more to that airlines in bankruptcy, which are becoming more and more.

The economy and especially taxpayers suffer because of the frequent ones Airplane disasters very much below. In the long run, flying is no longer affordable, especially since everyone Claims on American courts lead to infinite amounts of compensation. This Ultimately, costs lead to a reduction in aircraft safety because of the personnel is saved. As an example, reduction in service personnel and, consequently, the necessary technical checks of the aircraft parts and engines.

• - Die Passagiere bei einem Flugzeugbsturz zu retten.
• - Dadurch die sehr hohen Versicherungsschäden und die Schadensansprüchen zu senken.
• - Möglichst viel vom teuren Flugzeug zu retten.
• - Z. B. die Triebwerke, die Fahrgestelle, die Pilotenkanzel einschließlich der Steuerungselektronik und falls machbar, den Gepäckraum mit dem teurem Gepäck usw.
• - Die Treibstofftanks bei Absturz des Flugzeuges über einen automatischen Alarm/Tankablaßhahn zu öffnen und in der Luft fast ganz zu entleeren,.
• - so, daß der mögliche Brandschaden auf dem Boden in normalen aber sicheren Schadensgrenzen bleibt.
• - Durch das schon in der Luft in Hauptteile zerlegte Flugzeug und dann an einzelnen Fallschirmen hängenden und dadurch relativ sanft landenten Flugzeugteile, den Schaden an der Absturzstelle durch Warnung/Alarm und somit gleichzeitiges Evakuieren der Bewohner am Boden zu minimieren.
• - Dadurch bedingt (über Sirenen, Radio, TV, Polizeialarm usw.) können die Bewohner sich dann noch rechtzeitig durch das Wegrennen (in der Regel fast alle) in Sicherheit bringen.

The object of the invention is now:

• - Rescue passengers in the event of a plane crash.
• - Thereby reducing the very high insurance losses and claims.
• - To save as much as possible from the expensive aircraft.
• - Eg the engines, the chassis, the pilot's cockpit including the control electronics and, if feasible, the luggage compartment with the expensive luggage, etc.
• - Open the fuel tanks in the event of a plane crash via an automatic alarm / tank drain valve and empty them almost completely in the air.
• - So that the possible fire damage on the floor remains within normal but safe damage limits.
• - By the aircraft already broken down into main parts in the air and then hanging on individual parachutes and therefore relatively gently landed aircraft parts, the damage to the crash site by warning / alarm and thus simultaneous evacuation of the residents on the ground is minimized.
• - Due to this (via sirens, radio, TV, police alarm, etc.), the residents can still get to safety by running away (usually almost all of them).

The invention described below is intended to be the one that usually results in the death of an aircraft Rescue injured passengers from fatal crashes in an emergency.

This is done according to the invention by means of the detachable passenger cabin, which is attached to Large parachutes (which in an emergency are thrown out of the roof) hanging down sinks.

Detailed description of the invention. (see also the sketches Fig. 1 to Fig. 8)

The construction of the collapsible aircraft looks like the cabin is as long as it is Has passenger seats. In front of the first seat and the last seat there is a relatively stable one Provide cabin end wall with a sliding or swinging door that can be used in an emergency impending crash can be quickly sealed airtight by the flight crew. The front and rear wall doors have small pressure-resistant round windows for later pilot orientation during the rescue flight of the cabin. This can also happen when the rescue cabin sinks necessary air does not escape, which from an air or oxygen bottle battery, the z. B. in the cabin ceiling is intended for the emergency landing.

Like every airplane, the cabin has a window at every seat, as well as the usual doors. For weight reasons, the cabin is made of the most modern materials that have been tried and tested for aircraft built, e.g. B. aircraft aluminum (duralumin) and or steel, and where necessary high quality fiber plastic, wood-plastic composite and other materials, which the cabin sitting on the plane and or in the event of disconnection / descent even without the rest of the Aircraft fuselage remains stable.

The cabin is tapered at a certain angle at the ends and into the Rounded corners so that when they are separated from the rest of the aircraft they slide out and open immediately no case is stuck so as not to be dragged into the deep. There is also the critical points additional separation aids in the form of gas pressure pistons, steel springs, Detonators or other ejectors, similar to injection molds.

The cabin is normally equipped with several that can be unlocked or detached at the same time Fixing bolts, explosive rivets or special screws connected to the fuselage.

The cabin is also equipped with a breathing air tank to ventilate passengers during the flight Equipped for descent.

There is also a cell phone, rescue missiles, life jackets, bandages etc. The cabin has also been fixed in the roof section, folded to save space and stored the necessary items Large parachutes for the cabin.

The parachutes are arranged so that they are not pulled out of the roof can get caught. Auxiliary parachutes and other deployment aids are also the most modern Art provided.

The parachutes drop out the moment the release button is pressed to immediately after unlocking the fixing or retaining bolts the cabin from the rest of the fuselage by means of Parachutes is torn out.

In the rest of the fuselage, as before in the aircraft, the luggage is in the lower part of the Fuselage housed, but also lost in the event of a crash, which is the smaller in an emergency Is evil.

The cabin is waterproof and therefore built to float.

In addition, on the side of the cabin in chambers, which are molded into the cabin wall and are normally invisibly closed with detachable lids, additionally Floating bodies that can be inflated using propellant gas are stowed away or attached in some other way his. They are used to be able to land on the water. Also for a longer time Time to swim on the water until the occupants are rescued.

The floats can also serve as impact absorbers when landing on the ground. Furthermore, can be folded out on the bottom side of the cabin, also several meters long and downward-hanging telescopic resilient collecting rods to reduce the impact to be appropriate. In order not to carry unnecessary weight in the normal case, which is the Increased fuel consumption, the rods are integrated into the fuselage and by means of clips anchored that they also increase trunk stability.

An auxiliary motor can, if it is possible by weight, for maneuvering the Rescue cabin can be installed extendable.

In order not to have any problems after a water landing with the large umbrellas the parachutes from the inside of the cabin by means of a waterproof quick coupling detachably constructed. This process does not apply when landing on firm ground.

For a makeshift control of the cabin in descent are at the required places Solid rockets arranged.

Also, the cabin shell can be designed for weight reasons that all cover caps in Emergencies are automatically blasted off due to the weight of the actual rescue cabin to keep the size of the parachutes as small as possible.

As a sinking aid, the roof space of the cabin can also be folded and with helium inflatable balloons.

For everything in terms of additional weight and the resulting additional costs caused by this Compensating the rescue cabin concept can also be a little less comfortable and thus lighter seats can be accessed. From experience, these seats are due to a possible Emergency landing very stable and heavy. This, previous emergency landing would now according to the invention no longer take place on the ground but in the air. So now that Seat weight, due to the firmness of the seats, practically not so for safety unlike in the past, the seat weight and therefore the seat stability is very important. So a lot of the seat weight can be slimmed down, without endangering security. Because according to the invention is the previous type of crash landing no longer possible with the new construction or a crash is therefore predictable and safer for individual life.

Another variant of the invention is that as described the rescue of the cabin, the expensive aircraft parts such. B. the engines, the aircraft control / computer / pilot's cockpit, Chassis and if possible also the luggage containers from the aircraft fuselage delayed by automatic separation or detonators are separated and analogous to the Passenger cabin then hanging these important parts on parachutes, safely and without large Damage will sink to the ground, causing damage to the destroyed aircraft Insurance or airline can be kept smaller.

Summary

The invention offers the possibility of using an airtight separable from the aircraft Rescue cabin, in an emergency on parachutes and maybe also on helium balloons hanging gently and therefore fall-proof, the passengers who are belted in the seats are relative brings you comfortably to earth, which was previously not possible in the event of an airplane crash.

Due to the aforementioned floating bodies and impact damping, both on land and can also be landed relatively softly on the water without destroying the cabin.

Another significant improvement due to the invention is that with this before described technology now also hang important aircraft and luggage parts on parachutes, can be saved from crashes and destruction. This aspect will be for future aircraft be important.

Due to the solid rockets installed in the important places, the cabin can in time by the flight personnel in the direction of the flight which is important for the rescue to be controlled. Another advantage is that many guests fly through this additional security only becomes interesting again because the fear of flying is reduced.

The total cost of the flight is also reduced by fewer deaths Insurance costs etc. decrease again. The additional construction costs are reduced Death / damage claims quickly settled.

The emergence of new paying passengers increases and increases with this fall protection the claims for damages decrease.

The image of the airlines is brought back to the old high.

The debt decreases.

The crash-proof cabin is easy and convincing for anyone interested in flying, since all elements of this fall protection mostly function in the normal people are known.

Another significant improvement due to the invention is that with this before described technology now also hang important aircraft and luggage parts on parachutes, can be saved from destruction and thereby material damage for all can be reduced.

The possibility of saving people, luggage and also saving expensive parts increased additionally trust in flying, which in turn leads to economic success.

Declaration of drawings for the patent drawings of the rescue cabin

It shows

Fig. 1 whole aircraft I outlined
shown with window 1
shown with doors 2 ,
with the occupant cabin 3 used below in the fuselage also called the rescue cabin 3
Parachute balloon room 4
Detachable roof cover 5 in the area of the parachute room / balloon room
with the sloping ends 6 , 6.1 at the two cabin ends 7 (visible as a sloping line)
the corner radii provided for stabilization and against crack formation 8
see detail x
the telescopically resilient collecting rods 10 shown folded on the cabin floor 9
the pivot points 11
for this purpose, all can be blasted off quickly (ie in a matter of seconds) or mechanically by means of a main lever via fixing / holding bolts 12 for connecting the aircraft and
rescue cabin
those in the parachute room / balloon room 4 ,
stowed / folded large parachutes 13 ,
and or indicated the folded helium balloons 14 , which are attached to the rescue cabin 3 , by a central emergency switch / main lever (without drawing) all at the same time quickly (ie in seconds) mechanically / hydraulically / pneumatically, separable / or. by means of a calculated small explosive charge (not shown) that can be detonated / (made from the sealed cabin) special couplings 15 , which serve as a load-bearing connection between the cabin and parachutes or balloons.
indicated on the cabin floor 9
Detaching aid 16 (in the form of gas pressure pistons, steel springs, hydraulic ejectors or any other type), these detaching aids 16 press the cabin together from the rest of the missile, so that a flawless, safe disconnection from the rest of the aircraft is ensured.
Detail Y shows impression aid in the extended state

Fig. 1a, the roof cover 5 a (blasted off, falls freely to the ground) parachute is of course techn. also feasible here (this applies analogously to all large parts that fall to the ground separately)

Fig. 2, separated from the plane rescue cabin 3 shows in descent
without the roof cover 5 a (is already separated)
with the open large parachutes 13 a, and or indicated the helium-filled balloons 14 a as an additional flight aid
the telescopic resilient collecting rods 10 a extended towards the ground
the emergency control missiles 17 attached to the sides and at the ends of the rescue cabin
the obliquely indicated at both ends 7 cabin end walls 7 a
with the quick-closing air / watertight doors 7 b (not visible), which of course can be locked securely
the seals, not shown (for the purpose of sealing the cabin from the aircraft)
Unlocked detachable fixing / retaining bolts 12 (connecting bolts) (which normally hold the cabin and aircraft together)
lateral recesses 18 with closed lid 18 a for the floating body 19 packed therein (not shown)

Fig. 3 also the floating rescue cabin 3 with only indicated parachute 13 b / balloon lines 14 b
the laterally open recesses 18 with the opened covers 18 a (for storing the floats 19 )
those (from the side depressions) that are hanging on the cabin floor 9
and inflated (several) floats 19 a

Fig. 4 entire plane II shown outlined:
with window 1
shown with doors 2 ,
with the occupant cabin 3 b used below in the fuselage also called the rescue cabin 3 b
Parachute / balloon room 4 a
Detachable roof cover 5 b in the area of the parachute room / balloon room 4 a with the oblique end face 6 , at the cabin end 7 , at the rear and, in contrast to FIG. 1, at the tip of the aircraft (to the front) straight out and this time also including the pilot's cockpit / control cabin , s. Contour K (visible as an oblique / straight line) the corner radii 8 provided for stabilization and against crack formation (analogously at all corners)
see detail x
the telescopically resilient collecting rods 10 shown folded on the cabin floor 9
the pivot points 11
detachable or otherwise fast, process-safe uncoupling of the fixing / holding bolts 12 for connecting aircraft II and rescue cabin 3 b (exact position and number of connecting bolts depends on the construction of the aircraft and is statically / dynamically calculated by experts, like the other aircraft parts too)
those in the parachute room / balloon room 4 a,
stowed / folded large parachutes 13 , and or indicated the folded helium balloons 14 , which are attached to the rescue cabin 3 b,
through an emergency switch / main lever or similar to the car central locking (without drawing) quickly mechanical / hydraulic / pneumatic, detachable or. by means of calculated small explosive charges that can be detonated, centrally ignited (made from the sealed cabin) special couplings 15 which serve as a load-bearing connection between the cabin and parachutes or balloons.
indicated on the cabin floor 9 ,
Detaching aid 16 (in the form of gas pressure pistons, steel springs, hydraulic ejectors or other types)
Detail Y shows impression aid in the extended state

Fig. 4a, the roof cover 5 c, blown off, falls freely to the ground

Fig. 5 shows the rescue separated from the aircraft cabin in descent b 3,
without the roof cover 5 c (is already separated)
with the open large parachutes 13 a, and or indicated the helium-filled balloons 14 a as an additional flight aid
the telescopic resilient collecting rods 10 a extended towards the ground
the emergency control missiles 17 attached to the sides and at the ends of the rescue cabin (outlined in a radiation-like manner)
the obliquely indicated at the cabin end 7 end wall 7 a
with the quick-closing air / water-tight door 7 b (not visible), which can of course be locked securely,
the seals, not shown (for sealing the cabin to the aircraft).
Unlocked detachable fixing / retaining bolts 12 (connecting bolts) (which normally hold the cabin and aircraft together)
the lateral depressions 18 for the compactly packed floating bodies 19 (not visible here)

Fig. 5a also the floating (only outlined contours) / rescue cabin 3 b (designed as Fig. 5) with only indicated parachute 13 b / balloon lines 14 b
the lateral, now open recesses 18 with the covers 18 a opened (or because of the weight, which can be depreciated) (for storing the floating bodies 19 )
the ones that fell out (from the side depressions), hanging on the cabin floor 9 , moored by means of ropes
and inflated (several) floats 19 a

Fig. 6 also the floating (only outlined contours) rescue cabin 3 b and 3 c with only indicated parachute 13 b / balloon lines 14 b as another variant as outlined in Fig. 6, analogous to Fig. 4, but almost the same covering the entire length of the fuselage, but the front wings have already been thrown off the fuselage by means of separating devices as described above.

Here, the rescue cabin consists of occupant compartment 3 b and the luggage compartment 3 c underneath, so that passengers and luggage can be saved in an emergency when descending.

This variant is separated to the rear by a partition as the partition wall S, which closes but the entire cross section (see "A") of the aircraft fuselage and the passenger deck located quickly closable door 7 b from the residual carcass and the outside (in case of emergency crash case), closely divides.

In the luggage compartment (in the event of an accident) the bulkhead is always closed.

So for the sake of clarity, the occupant cabin 3 b and the luggage compartment 3 c underneath are sealed off from this outside by this bulkhead wall S, so that in this variant the occupants and also the relatively important luggage can be saved together in a descent. In this variant, the higher weight must be compensated for by more or larger parachutes / balloons. Possibly also by so-called brake rockets (without display) which have to be directed downwards.

Fig. 7 outlined as a further variant to Fig. 6.

Here also the floating (only contours indicated) rescue cabin 3 c, but only regarding the luggage compartment part, with only indicated parachute 13 b / balloon lines 14 b and the luggage compartment door 3.1 . This variant is intended to serve as a separate option for baggage rescue and thus damage limitation.

Fig. 8 outlined as a further variant to Fig. 7, hanging on the parachute, but as an example only outlines the expensive chassis 20 (or, accordingly, also separately relating to the engine, electronics or other expensive or important aircraft parts). Of course, a floating body corresponding to the respective weight can also be provided here (not outlined).

Claims (29)

1. Rescue cabin for passengers threatened by the plane crash, characterized in that the passenger cabin can be quickly separated from the rest of the heavy aircraft body in the event of an impending crash and then as an independent, airtightly sealed body and with the occupants on your seats, hanging on sufficiently large parachutes and thus can survive safely on earth. 2. Rescue cabin according to claim 1 characterized in that the cabin is seen on the long side, as is usual with all aircraft, Window and depending on the size of the aircraft has one or two passenger doors and on the End faces so beveled and rounded in the beveled corners to be quick in an emergency being able to be separated from the rest of the heavy aircraft body; Tensions and risk of tears avoided. 3. Rescue cabin according to claim 1 to 2 characterized in that air / watertight and pressure-resistant swivel Folding or sliding doors, which are shaped so that they lock securely and rigidly seal with min. a small pressure-resistant window for emergency flight orientation, installed which are open to staff and passengers during normal flight operations, but with imminent crash of the entire missile in a flash by hand and or automatically after all occupants are gathered in the cabin, sealed pressure-tight, and reliable can be locked. 4. rescue cabin according to claim 1 to 3 characterized in that the cabin seen on the longitudinal side only on the rear end faces is chamfered, but also includes the pilot's cockpit on the pilot Emergency landings still have control functions for the descent of the rescue cabin. 5. Rescue cabin or passenger cabin also called, according to claim 1 to 4 characterized in that the cabin made of the latest lightweight materials such. B. Titanium, aircraft aluminum and or in carbon fiber-wood-plastic composite because of that Flying weight as a weight-saving, but nevertheless as a stable and stiff construction suitable for flying is designed. 6. rescue cabin according to claim 1 to 5 characterized in that the cabin in the roof during normal flight with min. 2 or several folded large parachutes and auxiliary parachutes for emergencies (at impending crash). 7. rescue cabin according to claim 1 to 6 characterized in that the cabin when landing on water by quick connectors can be separated from the parachutes pulling down into the water. 8. rescue cabin according to claim 1 to 7 characterized in that the cabin in the roof with min. a detachable Roof cover is provided to prevent the parachutes from unfolding during an emergency flight hinder, and at the same time to reduce the descent speed by reducing weight reduce so that a gentle impact can be ensured. 9. rescue cabin according to claim 1 to 8 characterized in that the cabin in the roof with min. one or more folded gas balloons also connected via quick disconnect couplings and the required also detonable helium gas bottles for the rapid filling of the balloons is provided, in addition to the parachutes in the load capacity during emergency landing support. 10. Rescue cabin according to claim 1 to 9 characterized in that the cabin at the critical points additional separation aids owns in the form of gas pressure pistons, steel springs, or other Ejector, similar to injection molds and drawing presses for ejecting the finished part designed. 11. Rescue cabin according to claim 1 to 10 characterized in that the cabin is normally unlockable with several simultaneously or detachable fixing or retaining bolts with the aircraft body torsionally rigid connected, but in an emergency together or in a specific order to disconnect by means of a pressure medium, mechanically or, in the case of a problem, also by hand, or via one Central lever simultaneously operated the bolt separations in seconds or faster can be. 12. Rescue cabin according to claim 1 to 11 characterized in that the cabin also with a Breathing air tank is equipped for ventilation of the occupants in an emergency for descent. 13. Rescue cabin according to claim 1 to 12 characterized in that the cabin also has emergency lighting in the event of an emergency, Cell phone, rescue missiles, life jackets, bandages, drinking water and other necessary Devices, such as cutting knife / hatchet and emergency provisions. 14. Rescue cabin according to claim 1 to 13 characterized in that the parachutes and the auxiliary parachutes at the moment or also time-dependent and / or also the balloon envelopes, which are then automatically filled with helium will fall out of the roof in the event that the fixing / retaining bolts when impending Crash can be unlocked, with the help of the opened parachutes also the cabin the remaining heavy fuselage is torn out and separated so that the heavy remaining fuselage (with the heavy luggage and the heavy engines the full fire-prone fuel tanks etc. in short, everything in an emergency for the pure Rescue occupants and no longer needed for a slow descent) without hindering the rescue cabin from falling faster to earth, possibly before serving the remaining aircraft is still at a safe altitude, depending on the time / air pressure by means of a separating or Explosive device disintegrates into relatively small and therefore less dangerous crash parts. 15. Rescue cabin according to claim 1 to 14 characterized in that the cabin is light, but still waterproof and airworthy is built to float. 16. rescue cabin according to claim 1 to 15 characterized in that lateral depressions with also detachable into the cabin Covers are molded into which inflatable floats are inserted for the water landing are inflated, serve as impact absorbers when needed and also for a long time Keeps the cabin afloat. 17. Rescue cabin according to claim 1 to 16 characterized in that the cabin can be folded out on the bottom side, also several Telescopic resilient collecting rods hanging down for several meters to reduce the Impacts are attached to the floor, which usually add unnecessary weight save, so mounted in brackets in the aircraft, so that they also the normal Stiffen the fuselage or increase or improve the statics. 18. Rescue cabin according to claim 1 to 17 characterized in that on the cabin on the floor side a small if necessary Boat engine can be built out as a maneuvering aid when folding out water. 19. Rescue cabin according to claim 1 to 18 characterized in that in the event of a possible water landing with the large parachutes, which immediately become wet and heavy due to contact with the water, from the inside operated quick-release couplings on the cabin ceiling to separate the screens are attached, with which the now dangerous screens immediately after landing on can be separated once or centrally. 20. Rescue cabin according to claim 1 to 19 characterized in that for a makeshift Control of the cabin during descent at all important points small moving Missiles are attached to the cabin to target the cabin, as in the case of a spaceship Pressure surges in certain directions from the inhabited, as far as possible or other areas unsuitable for the emergency landing controlled by these pressure surges mop. 21. Rescue cabin according to claim 1 to 20 characterized in that for an emergency landing as often mentioned here, now easier ones Seats can be used, since usually no longer with a belly landing conventional and thus much heavier aircraft type must be expected, in which the seats were exposed to unprecedented centrifugal forces and therefore very stable and very were heavily designed and the now much lighter design of the seats means that the Compensate more complex and therefore somewhat heavier cabin. 22. Rescue cabin according to claim 1 to 21 characterized in that there is also the possibility of a pressure lock in the Cabin installed, the seats, unnecessary parts and hand luggage before descending to Discarding the reduction in flight weight, which slows down the descent speed. 23. Rescue cabin according to claim 1 to 22 characterized in that there is also the possibility of the front fuselage part, or the entire passenger area including the luggage compartment of the aircraft so with a rear tight end door (to be designed over the entire hull cross section so that in an emergency this entire part serves as a rescue cabin and also after the other parts have been quickly separated with rescue parachutes safely sinks down. 24. Rescue cabin or rescue system according to claim 1 to 23 characterized in that there is also the possibility of all important / and unimportant Aircraft parts such as B. engines, aircraft control / computer, landing gear, (same Fast emptying of the tanks, automatically triggered), which can then be triggered or unlockable adapter plates / bolts, or plugs are connected to the aircraft, but at impending plane crash via a signal from the cockpit by the pilot, or in a special / hopeless or flight angle-dependent aircraft position that leads to a crash, or in a special / hopeless or flight angle-dependent aircraft situation that causes the crash leads, are automatically blown off and also individually on large rescue parachutes analogous to the cabin, landing on the ground as undamaged as possible. 25. Rescue cabin or rescue system according to claim 1 to 24, characterized in that the fuselage for a weight-saving statics in the long side on the outer skin (from the front to the rear cucumber-shaped) is designed so that this sheet / plastic skin not smooth but in certain the same or depending on the needs of the statics, even in uneven shafts or grooves, or if combined, if necessary, can be carried out in different pressed sheet metal folds / depressions, in order to increase the statics or strength of the fuselage so that this again affects the material in favor of the aircraft construction according to the invention can be saved.
The embodiment according to the invention can thus somewhat or almost completely compensate for the additional technical outlay for the rescue cabin in weight. 26. Rescue cabin or rescue system according to claim 1 to 25, characterized in that all aircraft fuselage parts see Fig. 1-7 because of the lightweight construction and statics from a piece of light metal circuit board or steel / Allu sheet / plastic composite, etc. in one piece for each Partially produced large-scale steel tools, such as hollow deep-drawn cans, pressed, injection molded, in the large-blow molding process or hammered, similar to the manufacture of tubes or the conical tubular steel light masts. 27. Rescue cabin or rescue system according to claim 1 to 26 characterized in that the rescue cabin outside or inside, on the floor panel alongside, has one or more 90 ° and automatically fold-out metal web plates, which now separates the cabin from the rest of the fuselage in the event of an emergency (crash) Cab floor reinforced against the sagging force, which due to the weight of the Occupants, the seats and other parts loading the floor panel act on the floor. 28. Rescue cabin or rescue system according to claim 1 to 27 characterized in that the rescue cabin is additionally inside the cabin in an emergency seen between the floor panel and the ceiling alongside, against the deflection of the floor, which may arise after the separation, can be stiffened by min. one or more quickly attachable stiffening rods / steel cables and the like, made of metal or plastic, with snap hooks or other Connecting means at the ends of the rods / stiffening elements then hooked into eyelets, or are firmly screwed into the receiving thread, which is on the floor and ceiling in the cabin are located. 29. Rescue cabin or rescue system according to claim 1 to 28 characterized in that the rescue cabin in principle in its design, size, Shape, material, or in the case of large aircraft as a multi-part cabin for all types of aircraft, d. H. from large passengers / freight / military to small aircraft offers all possibilities, also in Regarding costs, or security for future aircraft designs.