GB2371034A

GB2371034A - Jet powered pontoon

Info

Publication number: GB2371034A
Application number: GB0113446A
Authority: GB
Inventors: Lubeck Shamsutdinov
Original assignee: Individual
Current assignee: Individual
Priority date: 2001-01-16
Filing date: 2001-01-16
Publication date: 2002-07-17
Anticipated expiration: 2021-01-16
Also published as: GB0113446D0; GB0101099D0; GB2371034B

Abstract

A jet powered pontoon has a fuselage 57 comprising an outer tube 1, with a smaller diameter inner tube 3 mounted concentrically within the outer tube, the outer tube being longer than the inner tube. The ends of the tubes are linked with frusto-conical sections 2 providing a funnel shaped inlet at one end of the pontoon and a funnel shaped outlet at the other end of the pontoon. The annular space 23 between the tubes is ballastable so that the buoyancy of the pontoon can be varied. At least one propeller 4, 5, 6 is provided within the frusto-conical section of the inlet end which on rotation creates a vacuum within the inlet. The vacuum draws the surrounding fluid mass into the inlet and accelerates it along the inner tube until it is expelled from the outlet end creating a propulsive force on the pontoon.

Description

237 1 034

D E S C R I P T I O N

/Technical field'/

This invention relaties to a new technologie to design a torpedo, a submarine, a dirigible and chasses for vessele, means for movement its by unlimited speed.

/Backgrdund/ The technologies of shipbuilding, airlinerbuilding are well known school of design which comprise a modern technologies inc-

luding the theorem of great DanieIle Bernoully. There is a speci-

al type of airliners and ships known such as high level of ' -th e-. scientific and engineering achievements e.g. a submarin Delta class or airliner Concord. But this techologies are gives disadvantage such as over-expenditure of engine Effort per unit knots and aircrash.Density fi;'acceler ting air or water mass increases proportionally velocity and becomes hard such as con- i caret'. The Effort of vessels is useless spending for 'overcome the resistance of coming to meet stream mass.

An advantage the Jet Pontoon technologie comprise the sucks and propul'sion a water or air mass, means for removal a resistan-

ce contrary flow mass.

E.G. Fig.3;13. The Delta class submarine spends Effort = F1=3386tn.sec for achieve 24knots. The Jet Pontoon submarine such as tancer spends Effort F=1588tn sec for achieve 130knots.

/Essenttial Technical features/ The Jet Pontoon technologie bases on theorem great Danielle Bernoully '!rcluding modern scientific and enginiering achievements.

There is known -a Potential Energy exists,between a Gravity Energy oppositQan Inertia energy, in the form of Spere.

A Kinetic Energy exist seen the Gravity and Potential Energies such as Sector of the Sphere and have a shape in the form of Cone.

A circular base of the cone is tapering to a point proport o-

nally tahgens of this point.

acceleration = 3,14 R2. tan The Jet mass exists into the Kinetic Energy and have a shape in the form of cut out cone It bases is increasing or decreasing proportionally the tangens of point This cone.

A cylinder copmprise an is-accelerated mass condition by tan = 0. The bases of cylinders is tapering proportionally ts Velosityes.,and acceleration.

K = coefficient of acceleration K = A == S = 3,14. R2 A = area A1S1 3,14 R2 V = volume S = base R = radius A Vacuum Lifting Volume exists between volumes differen is acce-

lerated Jets bodys proportionally its tangenses. This phenomen is called Disturbance Jet Body Plot. Fig.1;2.

U = acceleration = vi-v = Hl_H H = L = v = Velosity v1 V V _ _ _ _ _ _ _ _ _ = _

LY = Lifting Volume K S A h = height of cut out cone LV =/(3,14. R1. tang) - (3,14. 8 À tanl)/-H + h An accelerated Jet body do not thrust the Lifting Volume space.

A propeller,s wing transforms a revolving movement for Vacuum opposit Pressure Force, meansfor sucks and escape the water or air mass, means for admiting sea water or air mass to the cham-

ber and thereafter expelling it through the Narrow Tube and rear nozzle with substantial force to develop thrust for propelling the Jet Pontoon.

A measurement of acceleration and velocity could be accounted such as escape same capacity Jet mass across cat out cone to se-

cond cylinder (tube). Fig.1.

An ability the Jet Pontoon to lift the loads weight is accor-

ding to Density of Lifting Volume.

/Example/

Figure 1 shows a meted of measurements to the Disturbance Jet Body Plot.

b). - contour of jet ray in the form cylinder.

Cylinder N3 - jet body by tangens = 0 and velocity = 0 Cylinder N2 - H is accordance to the Jet Pontoon,s velocity Cylinder N1 - is accelerated jet.

Cylinder N2 and Cylinder N1 have same Volumes.

S - base or area of Cylinder N2 S - base or area of accelerated Cylinder N1 -A - vacuum force +P - pressure force E - effort accordance to vacuum Volume of the cone LV - Vacuum space exists between Volums Cylinder N3 and N1 oF

Figure 2 shows Disturbanse Jet Body Plot. Jet body N4 is accele rated into the jet body N3. The accelerating jet body narrows proportionally tangent at point f.

S;S1;S2 - base of cut out cone is narrowed proportionally ac celerate. Cut out cone N5 and N4 have the same capacity.

Figure 3 shows the method of analysis the effeciencydthe Delta class submarine. By Force F1 = 12119 tn. sec its F=1588tn. sec.

and achieved a velocity 24 knots only.

Figure 13 shows Delta class submarine after reconstruct it by the Jet Pontoon techology. There is withdrovn the useless Force F = 1588tn. sec. submarine achieved a velocity 183knots.

Figure 4 shows the Jet Pontoon comprising a Fuselage (57) in the form of Large Tube (1), the Lifting Volumeis located between the Large Tube(1) and the Narrow Tube(3). enables the Jet Pontoon(16) to sink or rise to the surface of water or air mass surrounding by. The Reactive Engine(54) consists of two Accelerators(2) in the form of cut out cone with Narrow Tube(3) indented to the sma ller end this, in two, contains a propeller(4) (5)(6) creates a vacuum in the cone and pressure opposit the vacuum(-P)(+ P) in the Narrow Tube(3) enables the acceleration of water or air mass,.

This force propells the Jet Engine(54), the Jet Pontoon(16). An accelerating jet body mass increases speed proportionally and does not thrust a cut out cone 2). This allows movement by unlimited speed. An automatic steering including a manual control, a Power station(e.g.15), a Reactive hydropuls underwater propulsion sis tem(54), a steering mechanisms(52)((34) is mount in an integral unit. Figure 5 shows a Container(40), tourism vessel, is mounted on the Jet Pontoon(16) chasses. It is in rice position over the Ocean surface. Packaging of sweeming pools construction(42) is mount on ship,s side.

Figure 6 shows a Container(40), tourism vessel, is in a position to sink by level an ocean,s surface and spreds the sweeping pool.

Figure 7 shows an Aircraft(40) Container is mounted on the Jet Pontoon chassis(16). It is able to sink and rise.

Weight = 25.000 tonn R2 = 1,5m AJ = 673m.sec Lenght = 600 m Velocity = 607,5 knots LV - 25.ooo m3 2 - nuclear reactor 4 - shafts R1 = 2,35m Figure 8 shows a used aeroplanes is mount on the Jet Pontoon cha-

sses. Figure 9 shows a Jet Pontoon modification, such as Dirigible.

A surface is mount a Solar battery. LV - Lifting Volume is fill in a gaz by density 0,09 g.sm3

I = H = 130m Beam = 16m R2 = 1m - density - air 1,3kg.m3 - gas 0,09kg.m3 = 1,21kg.m3 UP - Lifting Power 20tn - 20000kg. 1,21kg.m3 = 24200m3 =LV va velocity2accelerated jet = 1400m.sec H1 volume = R2.3,14. 1400m.sec = 3, 13m2. 1400m.sec = 4396m3 S1 = 3,14m2 Volume a Narrow Tube = 3,14m2. 130m = 408m3 = VNT Ly = Lifting Volume = 24200m3 N3 - volume of Dirigible = LP + VNT = 24200m3 + 408m3= 24608m3 S - A - area = 24608: 130m = 189m2 R1 radius = 189m2: 3,14 = 602 = 7,7m Beam = 16m K - coefficient = S: 51 = R1:R22 = 60 vJP - velosity of Jet Pontoon (Dirigible) = 1400m.sec: 60 = 23,3m.sec= = 23,3m.sec. 3600sec = 83880m.sec = 83,8. 1.6 = 52.425mph Variety 2.

va = 3000msec vJP = 3000m.sec: 60 = 50 m.sec = 180000^m.sec = 180km.h = 112,5mph Variety 3.

R2 = 1 '2m S1 = 7m K = 189m2: 7m2 = 27 vJP = 1400m.sec: 27 = 51,8m.sec = 186,6km.h = 116mph Figure 10 shows the secong modification of Dirigible comprising the Jet Pontoon is mounted a turbine engine, means for accelerate an air mass and propelling the Dirigible. The heat up air fills in the Lifting Volume for rise the Dirigible.

R2 = 1,Sm va = 2400m.sec vJP = 2400m.sec: 27 = 88,88m.sec. 3600sec = 319, 96km.h = 199.97mph Figure 11 (cut off), Figure 12 shows the scheme of Jet Pontoon,s modification, such as Submarine. The protection armour provide a without breakdowns an undersea action it fuselage. The Accelera-

tor is mounted two propellers is rewolving,to opposit each other.

Figure 14 shows the Jet Pontoon s modiffication, such as Tanker.

It is mounted the vari-able length Oil rig, means for drilling operations and obtain the oil undersea.

Figure 15 (cut off) shows action the Tanker, such as drill rig, means for obtain the oil in deep undersea. It Chamber(56) is use-

ful for revolving the drill rig and the Accelerator(2) for making the conkret foundation.

Figure 16 shows a power station e.g. Turbine Engine is mounted -

o side of the Fuselage(57) the Jet Pontoon. (15) Jet Turbine eng ne is enable to accelerate va = 2400m.sec.

/ - - {- -:

The sort of jet turbine engine tha can apply on a Jet Pontoon.

At the front of the engine a compressor sucks in air, acting rather like a propeller, but the air is compressed and as result it becomes accelerated narrow and hot. Some of the heated air goes through into the combustion chamber and is mixed with the fuel (kerosene). The fuel burns and causes a great increase in the pressure of the gases. The hot gases are then forced out at high speed e.g. 2440 meter per second through the connective tube, a Valve for regulate a pressure in combustion chamber and nozzle.

The escaping gases prvide a rotate the Wheeled propeller of Acce-

lerator. and neutralis an air resistance in front.

The engine needs to be started with an electric motor to rotate the compressor, but once the engine is canning some of the energy from the exhaust gases is used to drive a turbine. The turbine is mounted on the same shaft as the compressor so air can now be sucked in without the help of an electric motor.

An heat up gazes comes in the Lifting Volume of Dirigible, means for rise it.

Figure 17 shows (cut out) Circular Propeller comprise circular chamber is mount the Wings(9) and couple on pairs Valves,means for for rotate it by pressure, e.g. gaz, water.

(55) Between Wings Abe Gateway is provided, means for safety a sea animals. Between Wings(7)(8)(9) a Force is equally distri-

butes over gaz or water agents.

Figure 19 shows fragment of sweeming pool (cut out). (44) Barrier.

(43) Float comprise a ball, means for support the (46) Netting floor of sweeping pool. (43) Trap comprise a pneumatic construct for walk.

Examples.

Figure 5;6 By GUINNES world records 2001. page 140.

BIGGEST CRUISE LINER

311 m (1.020 ft) long and 48 m (157.5 ft) wide. with a gross toon-

nage of 142.000. It can accomodate 3.114 passengers and 1.181 crew.

Reconstruct 4 - shafts - chasses of Jet Pontoon 350 m- length - L-

LV - Livting Volume = 142.000 tn. = 142.000 m3.: 4 = 35.500 m3 R2 - of propeller = 2 m S2 - area of Narrow Tube = R22-3,14 = 12,56 m2 aJV accelerated Jet,s Volume (Narrow Tube) = 12,56m2 350 m = = 4396 m3 YJP Volume of Jet Pontoon = 35.500 m3 + 4396 m3 = 39.896 m3 S1 - area of Large Tube = 39.896 m3: 350 m = 113,9 m2 K - coefficient = S1: S2 = 113, 9m2: 12,56m2 = 9 vaJ - velosity of accelerated Jet (into Narrow Tube) = e. g. 673m.sec v - velisity of Liner = vaJ: K = 673m.sec: 9 = 74,77m.sec = = 269.200mph = 168, 25mph Figure 7; Aircraft Length = 600m. Tonnage = 50. 000 tn. 4 chasses.

R2 = lm S2 = R2 3,14 = 3,14 m2 Lifting Volume = 50.000 tn: 4 = 12500 m3 S1 = 12500m3: 600 m = 20,8 m2 K = S1: S2 = 20,8 m2: 3,14 m2 = 6,6 vaJ velosity of accelerated Jet (into Narrow Tube) = e.g. 673m.sec v velosity of aircraft = 673m.sec: 6,6 = 101,96m.sec = 367kmph = = 229,37 mph D - diametr of Large Tube = 20,8 m2: 3,13 = 6,62 m

l l a. Air Jet ray b. Stability velocity Jet ray c. Moving Jet ray e. Accelerate Jet ray g. Accelerated Jet ray S. Circular base, of cylinder or cone S1. Circular base, tapering to a point of cone P. Inertial neutral power -P. Vacuum power +P. Pressure power 1. Body in the form of cylinder. L'arge Tube 2. Accelerator '' 3. Narrow tube of accelerated Jet 4. First propeller 5. Suplementary propeller 6. Maight and main propeller 7. Wings of first propeller 8. Wings of suplementary propeller 9. Wings of might and main propeller 1O. Ventilator Or-

11. Combustion chamber by high pressure, 12. Turbine for rotatethe ventilator -:,, 13. Connective channel 14. Fan 15. Power stationed det, iturbine e g n,e.

16. Jet Pontoon 17. Circular cylinder for moving to street 18. Circular cylinder for moving to back 19. Exhaust channel 20. Propellers wheel, circular basis 21. Basis wheel of propeller 22. Valve for regulate a pressure in combustion chamber, 23. Lifting Volume 24. Body of accelerator in the form of cut out cone 25. Wheeled propeller compiling circular cylinder, wings, ball bearing, piston valves.

26. Chamber for high pressure 27. Stop valve 28. Piston valve 29. Protection armour 30. Turret 31. Weapon, torpedo 32. Eleron 33. Drawing room 34. Channel for neutralization a Jets weight and vertically ste aring 35. Alternative propeller 36.Central propeller 37. Valves for hot air 38. Casing 39. Aeroplane 40. Container, vessels body

41. Support 42, Packaging of sweeming pools construction 43. Trap 44. Barrier 45. Float 46. Netting floor of sweeming pool 47. Rope 48. Temperaturely gap 49. Ball bearing 50. Vent 51. Reactive engine 52. Tube for horizontal /left or right/ steering 3., -r ur> Len th'. -

5.4! Rp,a,ct,i e,,eNgine. Ch amber ',.

55. Gateway <is.,, Ca̳ 5tr..N,v! 1 57., Fuselage it, " I tak,,,-.

....

Claims

-: C L A I M S

1. A maintenance technical Jet Pontoon comprising a housing, of the fuselage in the form of Large Tubet reactive engine mounted inside thereof means for sucks accelerate and force out through a Narrow Tube3a water or air mass. The inertia of escaping mass provides a forvard thrust on the Jet Pontoon. The Lifting Volu-

me is located between the Large Tubeland the Narrow Tuber enables the Jet Pontoon to sink or rise to the surface of water or air mass surrounding by. The Reactive Engine 4consists of two Accelerators2in the form of a cut out cone with Narrow Tube inden-

ted to the smallerend this, in two, contains a propeller. The propeller creates a vacuum in the cone and pressure opposite the vacuum in the Narrow Tube3enables the acceleration of water or air mass. This force propells the Jet engine, the Jet Pontoon. An accelerating mass jet body increases speed proportionally and does not thrust a cut out coned This allows movement by unlimited speed. A high speed increase is made possible through the discharged Effort of exists power engines. An automatic steering including a manual control, a power station, a Reactive hydro-

pulse underwater propulsion system, a steering mechanisms is mount in an integral unit.

2. The fuselage as claimed in Claim 1, have an even strength

straight streamlined surface means for sink or rise and move on high velocity.

3. An everyone measurements of Jet Pontoon body as claimed in Claim 1, means for desigh, transforms by velocity, load, Effort and modification, such as equivalent equipments a cut out cone, cylinder N1, cylinder N2, Cylinder N3. Fig.1; Fig.2; Fig.3 4. A measurement of velocity as claimed in Claim 3, means for design, accounts as same volume fluid removes across cut out cone.

57 1 5. The fuselage in the form of Large Tube as claimed in Claim 1, comprise a Reactive Jet acceleration mechanisms, a Lifting Volume be located between it volumes, an automatic steering sister and me-

chanism, power station, detection, homing and control systems and underwater propulsion system, the means for sucks sea water to the cut out cone accelerate and thereafter expelling the sea water through the Narrow lube and rear cut out cone (nozzle) with sub-

statial force to develop thrust for propelling the Jet Pontoon.Fig 4, 6. The Lifting Volume as claimed in Claim 5, comprise an empty pace for load e.g. the petrolium or explosive, means for sink or rise the Lifting Pontoon by density it.

7. A new technology as claimed in Abstract, comprise the truths: a). an accelerating jet body narrows proportionally speed; b). between volums, into Stahl speed jet body, volume-and is narrowed accelerating jet body,s volume, exists a vacuum Lifting Volume c]. an accelerated jet body don't thrust to the Jet Pontoon body; means for 100X utilization an Effort for unlimited accelera

tion Jet Pontoon; d). a weight of loaded Jet Pontoon don,t stand in the way of for movement it; Fiq.13;7.

e). the compulsion accelerating mechanism transforms an engine energy to the vacuum opp si pressure volume, means for with sus-

tantial force to develop thrust for propelling the Jet Pontoon; 9). a wave's of seasurface don,t stand in the way of for move-

menting Jet Pontoon; Fig.13;7.

f). an ability the vessel to sink and rise enables to create a new technologie of sea tourism business Fig.5;6;15.

h). the Jet Pontoon technologie is able to rebirth the Dirigible such as most safety and cheap method the air force by high speed.

Fig.1;2;3;4;5;6;7;8;9;10; i). is enable to create new tecnologie comprise undersea works such as obtain and transport the Oil. Fig.13;14;15.

8. A steering mechanism as claimed in Claim 1, comprise a chan-

nels, valves and elerons is acton by force accelerated jet.

9. A power station as claimed in Claim 1, comprise a technical maintenance, such so nuclear reactor, steam turbine, engine, turbine engine and els into the Lifting Volume or outside the Jet Pontoon,s fuselage. Fig.16.

10. The turbine engine as claimed in Claim 9 is distinguish to mount a connective channel and valve for regulate a pressure in combustion chamber. Fig.16.

11. A propeller as claimed in Claim 1, comprise a circular basis mounted a wings and circular cylinder is provided the-Gateway(55), means for safety a sea animals.Fig.17.

12. A circular cylinder as claimed in Claim 11, mounted a couple of pairs the valves, means for transforms tine pressure power for rotate movement the propeller.(27),(28) Fig.17.

13. A modifications of Jet Pontoon as claimed in Claim 3, compri se the Jet Pontoon, means for application this technologie in bu siness such as: a). The undersea Tanker, comprise the maintenance technical Jet Pontoon, means for drill the sea floor, obtain the Oil, load and transportation it. It is able to work such as drill rig in deep water. Fig.13;14;15.

b). The tourism vessel, comprise the vehicle mounted on the Jet Pontoon chases, means rise, float by high speed such as ouce ning ship, on wucean, s surface sinks and transforms to an island including a beach and swete'ming pools. Fig.5;6;15.

c) An aircraft comprising a platform is mounted on the Jet Pontoon shasses, means for on high speed float, sink and rise.F.7.

d). An used aeroplans comprising a vehicle is mounted on the Jet Pontoon c'hasses, means for on high speed travel along oceans space. Fig.8. '' e). A Dirigible comprising The Jet Pontoon is mounted a solar battery, propeller, the Lifting Volume is filing by means of light gaz, mount drawing room, for most safety by high speed fly.Fig.9;9a.

f). A Dirigable comprising the Jet Pontoon is mounted i' the' turbine engine, a draping room' the Liftinq Volume -'' filing An - ^ tne not air from- - the turbine engine, means for . À N If j,-: -,

: rise and fly by rocket speed, cheap and safetly.

g). Fig.11;12. A submarine as claimed in claim l comprising a Jet Pontoon is neared on protection armour, a propeller have Gateway, means for on unlimited speed move undersea, the Narrow Tube is used such as trunk of artilery for thrust a weapon.

h). A PUMP MOUNTED in Jet Pontoon means for withdrawal the lipids from Lifting Volume.

i Amendments to the claims have been filed as follows Claim 1 'A jet powered pontoon having a fuselage comprising an outer tube with a smaller diameter inner tube mounted concentrically within the outer tube, the outer tube being longer than the inner tube and the ends of the tubes being linked with frusto-conical sections, providing a funnel shaped inlet at one end of the pontoon and a funnel shaped outlet at the other end of the pontoon, the annular space between the tubes being ballastable such that the buoyancy of the pontoon can be varied, wherein at least one propeller is provided within the frusto-conical section of the inlet end which on rotation creates a vacuum within the inlet, drawing the surrounding fluid and gas mass into the inlet and accelerating it along the inner tube until it is expelled from the outlet end creating a propulsive force on the pontoon ' . -; - -rat - A - --I -

2. The annular space comprising the Jet Pontoon,s body as claimed in Clime 1 wherein guide means avoids to meet the frontal resistance of surrour ing fluid or gas mass.

3. The Main propeller as claimed in::laime 1 wherein guide means a i,ar,s, rorms the engin,s power to wacuum opposite the pressure means for sucse accelerate and thrust We fluids or gas mass means for avoid the frontal resistance and force the pontoon. There is compulsion ice acceleration process.

4. The Main propeller as claimed n Claime 1 wherein guide means creates a vacuum within the frusto onica! section of the inlet able to providing won a plurality add tionai propellers means for distribute the engines power by creates a vacuum.

5. A vacuum whithin the frusto conical section of the inlet as claimed in Chime 1, wherein guide means sucse - accelerate the fluid or gas mass, narrows the jet body means for avoid the ''rental resistance its.

6 The additional propellers as c'.ainec5 in Claime 4 is rotating opposite each other means for prevent to a centrifugal poor resistance in the frusto conical section Fume 7. By eompu'sion jet acceleration process as claimed in Claime 3 the e! mass moves unimpeded through the Jet Pontoon,s inner tube becouse the jet body narrows proportionally to acceleration it means for unimpeded movement the Jet Pontoon through the surrounding fluid or gas mass.

8. By compulsion jet acceleration process as claimed in Claime 3 and the speed of the iet Pontoon is equally to tire Yetosity of let mass are rehousing from imagine arm- cilinder through the frusta-conical section into the inner tube to rear imagine cilynder.

9. The propellers as Claimed in C.laimes 1; 4 and 6 rotates by engine power on contact or hrough the agents power.

10. The imagine shed cilynder and the imagine rear cilynder as claimed in Claime have Ike same volumes. A diameter of imagir;e abed cilynder is equally to diameter of an outer tube, a ciiarneter of imagine rear cilynder is equally to diameter of inner tube. The length of imagine ahoy cilynder is equally to speed of Jet Pontoon, the length of imagine rear cilynder is equally to ueocitv of acceeraTea let mass.

tl. The ier.gthi of [nustc-oo?.icai section as claimed in Claime 1; 5; 6 is equally to pro - - S force according to enaires fir.

t2. The inner tube as claimed in Claime 1 provides of numbers additional dusts rot changing the direction of accelerating jet mass means for steering.

A. A fringe! shaper] inlet at one end of We pontoon and 3 funnel sharY'1 omit at Other em Qt tr!e pontoon 85 Claimed In C.iaime Provides the acceiera!'or.!pf? - nts as p!E?i in c',aime 4,.Seans T,0,,mo.,ernen, He Jet, or icor, queiy o., tooth 'irecticr.s.

A. A fDOCiiliCaE,Of?s of der Pontoon comprising a Iecnnoiogy.as claimed in' i iaimes t-' 3 can be varied:

- t3 aj. The undersea tanker comprisir g the Jet Pontoon means for drill the sea Door, obtain the ok toad and t aPsportat,on t There is able to work such as dril! rig in deep water. by The Mousse HESS?';,um,ising the vehicle mounted on the Jet Pontoon chassis, Ens to,-,aise, H - i, sink avid lraf\s o n s to an island on oucean surcharge.

c) An aircraft corr.prisin3 a platform is mounted on the Jew Pontoon chassis d). vehicle composing a USA aeropane is mounted on the Jet Pontoon chassis eJ. A dirigible comprising the Jet Pontoon If! sea motor vehicle on apt Pontoon chassis Y? A submarine cwnprising 'he -let Pontoon.

it'. A radlostearing Jet Pontoon comprising a submarine able to far from over the thousands milles to find and torpedo a Nap target.

5. ThR tourism vessel and aiom.;t as claimer in Claime 14 is mounted on the Jet Pontoon chassis providing 'the high support means for avoid the vaNes resistance.

16. she chassis fitted on high support as claimed ir' Claime 15 able to sink or raise on water surface 17. A dirigible as claimed in Claime 14 can be varied to the rnodifcation with annular space fill up the gas Gelium and to the modification with it annular space fill up the warm air creating from reactive engine fitted in inner tube.

18. The surface of dirigible basis on the gas Gelium as claimed in Claims 17 able to be covering with gelium battery means for providing an electric power to propeller fitted in inn tube 19. An used vessels e.g. nuceer power submarine as mentK>r d on description able to

reconstruct by Jet Pontoon techologie means for increasing its ef ciensy and speed by avoid frontal resistance its corpses.

20 A submanne as claimed, Elaine,4 provides to protective armour garment means for easie provide to control reparir As copses.

=1. A drill rig techology as claimed in Claims 14 accompanies by Jet Pontoon technology.

22. The additional propellers as clairred in Chime 4 rotates on different velocities accordong the acceleration Of Jet mass 23. The dirigible as claimed in Ciaime 14 should build by exists traditional techology to add in a new modem materials and technics of the Jet Pontoon technology.

24. The additional propellers as claimed in Claime 4 able providing to the circular cilynder equipped With pairs vanes means for revolving the citynder by agents power on high efficiency. The first valve travelling fitted in cilinder and second valve is travellir fitted on corpse