CN103183121A - Close-fitting aircraft carrier equipped with hull bottom aerial carrier and split bearing beds - Google Patents

Abstract

The invention relates to a close-fitting aircraft carrier equipped with a hull bottom aerial carrier and split bearing beds, and aims to solve the problems of conventional enthusiasm about ocean hegemony, pursuing of tricky technology, inappropriate design concept, complex aerial carrier structure, misleading into a dead end of danger production and vicious stress, danger incidents caused by the fact that the aerial carrier takes off and lands on a limited deck, trouble to elites and life risks of heroes. The aircraft carrier adopts extensible wings; the hull bottom aerial carrier which changes three wheels into three crow plates stretches the neck, bulges the abdomen, holds back the wings, bends down to the sea surface, and floats in the bearing bed extending from a tail dock of the aircraft carrier; soft landing recovery is implemented; due to a seaward floating bed stretched out of the head dock, the aerial carrier takes off, floats on the sea surface, and rises straightly into the sky; the original ecological structure of the aerial carrier is improved to be light; the survival and fighting capacities of natural lives are elevated; and the deck area of the aircraft carrier is reduced remarkably, the structure is simplified, and the aircraft carrier becomes a combination body with the advantages of good coordination, safety, orderliness and high efficiency.

Description

The hull bottom carrier aircraft with split the supporting close-fitting aircraft carrier of pocket bed

The present invention relates to a kind of hull bottom carrier aircraft and split the supporting close-fitting aircraft carrier of pocket bed, is the significant composite entity of the integrated optimum coordination comprehensive benefit of air-sea.

As everyone knows, the deduction of last 100 years already of modern aircraft carrier, but copied and done to become that power is dominated exclusively and commercial monopoly, sell goods at a high figure, and the user implemented follow-up kidnapping instrument of ensuring supply, to do things creatively the cunning inappropriate Design Conception of pursuit technology, artificial manufacturing technology is high-leveled and difficult, structure is numerous and diverse, the material requirements harshness, fund input, the maintenance expense is great, and mislead and lure into pernicious stressed, do the insignificant problem of playing with fire in the danger, highlight in the carrier aircraft landing of taking off on limited deck very dangerous, shake is feared in the extreme, and accident is on the point of and is sent out, the elite that turning from side to side, unnatural death the person of outstanding talent---and the present invention just arises at the historic moment.

In order to get rid of above-mentioned drawback, the present invention suits measures to local conditions, the ocean as the carrier aircraft land platform that takes off, lead according to snobbish, proposition (is called for short the tail depressed place) in aircraft carrier afterbody work depressed place and stretches out maritime pocket bed, stretch out maritime floating bed with head work depressed place (being called for short first depressed place), carrier aircraft land and take-off process are transferred to the sea carry out.Namely take extensible machine wing, changing three-wheel is the hull bottom carrier aircraft that three sleds support, during land, according to tail depressed place indicator signal, determine landing point across the sea, the carrier aircraft abdomen of craning one is very held back wing, bow and cut the sea, stagnant speed is cut and is floated, and the one or many degradation floats, and exhausts until momentum, become an arrow at the end of its flight--a spent force, just stop fuel feeding, float and put in the pocket bed, realize that soft land reclaim.When taking off, rely on first depressed place guide rail gradient power-assist to take off and obtain to face the speed that is situated between, leave floating bed, cut the face of going overseas, length is raised straight drawing high, and is calm high up in the air.Also make aircraft carrier dwindle floor space significantly and close-fitting vest is healthy and strong, form optimum coordination, safety, in order, composite entity efficiently.

The present invention solves the technical scheme one that its technical matters adopts:

1) close-fitting aircraft carrier, its hangar is face belowdecks, and head and the tail all have door to communicate with floating bed with front and back pocket bed.Front end still keeps the existing Soviet Union formula general layout of taking off that jumps of raising one's head and looking, and sets up Shou Wu in its left and right sides, tilts to stretch out to spread the wings to take off for carrier aircraft and floats the floating bed of cutting the sea; Its tail depressed place, rear portion also tilts to stretch out holds back the wing land for carrier aircraft and cuts the pocket bed that floats recovery;

2) frame hull bottom carrier aircraft, its machine wing is extensible, convergence, and its hull bottom is the location and is suspended on three trivets on the fuselage roof beam structure, upright support and diagonal brace, and their roots are positioned at like the duck chest that three skid plates of " product " Fabric office are attached on the web.During the carrier aircraft land, the abdomen of craning one is very held back wing, bows and cuts the sea, and stagnant speed is cut and floated, and floats to rest in the pocket bed, implements soft recovery, and necking down draws the abdomen, and is close to fuselage;

3) pocket bed is made up of three parallel file guide rails, dividing plate, bed frame, grid air cushion and air bag.These three guide rail tops are fluted, respectively with above-mentioned hull bottom carrier aircraft web on the skid plate bottom surface of " product " word Fabric office tangent the matching in file roller pearl pearl top of emerging, article three, lead the file rail and support by equidistant alternate line dividing plate intersection, be positioned in the frame, its base part seat drops on the grid air cushion.The pocket bed relies on the tail depressed place, and inclination is stretched out, and inserts the sea, and the floating holder of air bag is arranged.The floating bed in first depressed place is the same with the pocket bed, and just front end flushes with the sea.

4) the batch sortie that the new frame of close-fitting aircraft carrier, the functional efficiency of aircraft carrier are often taken off with the carrier aircraft unit time is weighed.Jump and fly also to set up Shou Wu in the left and right sides of raising one's head and looking for the specific use except keeping Soviet Union's formula, stretches many floating beds, number in order, set up 1,3,5 and 2,4,6 and take turns opening and take off.The same tail depressed place pocket bed quantity that enlarges is also numbered, and implements open recovery the in turn, improves the effect of aircraft carrier.

Positive beneficial effect of the present invention, by as figure-2 shown in, the hard land of wheel type carrier aircraft and hull bottom carrier aircraft soft the recovery running orbit to likening qualitative parsing to, the y-y coordinate is represented the height of carrier aircraft center of gravity among the figure, and the x-x coordinate is represented: s=tv, s are distance, t is the time, and v is speed.F1 is wheel type carrier aircraft run curve, and its underriding land are on the deck time, and tyre buffering plasticity is minimum, height of gravitational center h changes very little, and the time is of short duration rapid, and impact load stress is concentrated, and link is caused significant shear power and moment of torsion---the resistance rope of more seriously stumbling, except burst earn draw pernicious stressed, cause carrier aircraft link distortion, outside tearing even wrecking, hidden danger is difficult to be surveyed: if the resistance rope operation of stumbling is not in place, malfunctioning, can cause the difficult control of carrier aircraft and fall into the sea; The resistance rope fracture if stumble, the not only carrier aircraft horizontal self-destruction of rushing out of control,---the power of brushing lightly of returning of the resistance Suo Zishen that stumbles, also institute is to draping over one's shoulders gruel, and cutter is hacked axe and is cut!---and hull bottom type carrier aircraft land reclaim curve F2, the indicator signal that carrier aircraft is recognized aircraft carrier tail depressed place in the choosing of vast sea, the abdomen of craning one is very held back wing, bows and cuts the sea, when hull bottom compression water surface depth H and time length and apart from all significantly surpassing h, set burst momentum is broken the whole up into parts, break up, eliminate the consequence of pernicious load, and take stagnant fast one or many degradation to cut and float, exhaust into the length of strong crossbow until momentum, stop control lever, carrier aircraft is just put and is held in the palm in the pocket bed.

This structure deduction of suiting measures to local conditions to grow with each passing hour to the intrinsic ecosystem of carrier aircraft improves, and causes optimum coordination, produces comprehensive positive effect, and details are set forth as follows.

Now engage drawings and Examples and set forth combination accessory scheme of the present invention and structure, wherein:

Fig. 1-hull bottom carrier aircraft with split the supporting close-fitting aircraft carrier of pocket bed just, the top scheme drawing

Fig. 2-hard land of carrier aircraft wheel type and hull bottom type are cut to float and are reclaimed running orbit contrast scheme drawing

Fig. 3-carrier aircraft machine wing stretches, shrinks partial schematic diagram

Fig. 4-carrier aircraft hull bottom just, top and partial exploded view

Fig. 4 a-hull bottom web very supports decomposing schematic representation

Fig. 4 b-hull bottom web decomposing schematic representation of drawing the abdomen

Fig. 5-head and the tail depressed place floating bed pocket bed take off land Fabric office just, the top scheme drawing

Fig. 5 a-pocket bed and floating bed are stored lateral plan

Among the figure: A-wheel type carrier aircraft, the A1-hull bottom carrier aircraft of spreading the wings, A2-holds back wing hull bottom carrier aircraft, A3-web, A4-skid plate, A5-triangle bracket, the upright support of A6-, A7-diagonal brace, A8-top chock, A9-step, clamp among the A10-, A11-tail clamp

B-pocket bed, B0-floating bed, B1-guide rail, B2-dividing plate, B3-bed frame, B4-grid air cushion, B5-air bag

The C-aircraft carrier, C1-deck, C2-hangar, C3-tail depressed place, the first depressed place of C4-, C5-flat truck, C6-sleeper guide rail, C7-storehouse door

1) the present invention is shown in figure-1, and by close-fitting aircraft carrier (C), hull bottom carrier aircraft (A1) and pocket bed (8) are formed the new entity of optimum coordination, it is characterized in that: undertaken by carrier aircraft land and take-off process are transferred to the sea from the aircraft carrier deck.The tail depressed place (C3) of aircraft carrier tilts to stretch out for carrier aircraft (A1) cuts the pocket bed (B) that floats recovery, front end still keeps the general layout that the existing formula wing head of Soviet Union jumps and takes off, but increase three parallel files and push up the sleeper guide rail (C6) of tangent kissing with the three row ball pearls of emerging at the bottom of carrier aircraft hull bottom three skid plates, and set up Shou Wu (C4) in its right left both sides and also tilt to stretch out the floating bed (B0) of spreading the wings and taking off for carrier aircraft (A2).And hangar (C2) is below deck (C1), and first Wu Weiwu all has gate open toward hangar, and shifts the flat truck (C6) that carrier aircraft is used;

2) hull bottom carrier aircraft

A, it has the dipteron that can launch simultaneously and draw in, shown in figure-3, right left machine wing all is four of P with the width: P1, P2, the nested overlap joint of P3, P4 order, and gang up each sheet waist by the wing TK that spreads out, top T is firmly at the waist of P1 sheet and the wing spreads out, after ganging up P2, P3, P4 sheet in regular turn, terminal K assembles the fuselage control mechanism, realize that a right left side launches simultaneously and restrain, the nested overlap joint of each sheet is width half (being P/2), the difference of launching with convergence is 1.5P, namely holds back the width that reduces 3P behind the wing than spademan;

B, its hull bottom shown in figure-4, by skid plate (A4) and paracone then web (A3) and identical three triangle brackets (A5) that can do longitudinal oscillation synchronously like the wide duck chest, and upright support (A6), diagonal brace (A7) composition.And the AB of triangle bracket support, with upright support, the root of diagonal brace all is positioned on the web, and its top suspension is positioned on the longeron frame.Wherein, on web, main skid plate is forward between two parties with " product " word Fabric office for three skid plates, after the side sled is symmetrical in.The straight trough of skid plate bottom all is embedded with file roller pearl, and Zhu Ding is all emerged and is attached to the sled web plate face at the end, and matches with three guide rails (B1) phase merit of the pocket bed of addressing later.Correspondingly three each joint of triangle bracket interface point A, B, C pivot pin insert all separately that corresponding jaw link in the hole with the falcon head, link so from beginning to end, surround leg-of-mutton.Thirty years of age support then is made up of upper limbs GH and lower limb HE, and H is the joint link pivot pin of joint interface point.Though and diagonal brace is upper limbs MN and lower limb NF composition, but N then is dovetail and nested section of falcon, be the market-head of lower limb, insert upper limbs dovetail cover, can only make the fabricate block of directed flexible slippage, and its lower limb root F tilts firmly at web foremost, and M joint, upper limbs top pivot pin then hangs the location roof beam structure and is inverted in the bearing saddle bore.And three triangle brackets have only AB support root B pivot pin to be positioned at separately in corresponding skid plate step (A9) axis hole, and each A joint pivot pin of its top then hangs and is positioned at inversion firmly in corresponding fuselage roof beam structure top chock (A8) axis hole.The lower limb of upright support are upright, the web center that its root E is firm, and with main skid plate, diagonal brace arranges the 3rd on same line of centers.G joint, upright support upper end pivot pin also is to hang to be positioned in the bracket holes of the inverted bearing seat of fuselage roof beam structure.The equal line of the line of centers of all pivot pins is parallel.The AB of triangle bracket support is variable only, and it is by the fabricate block of cylinder and piston, and upper limbs is that cylinder, lower limb are the fabricate block of piston, is that the control web is endured out and the main part of drawing the abdomen, and all the other two support BC and CA are fixed length.

When carrying, shown in figure-4a, this moment, primer fluid compressed switch, and the cylinder of three AB supports reaches pitch length, triangle bracket is the positive right-angled triangle of handstand, and namely CA is crisperding, and AB is a burst limit, BC is profound, and the CA support all is attached to the fuselage roof beam structure, and hull bottom is all uprightly withstood in the AB support.This moment upright support center direct bearing, diagonal brace is also completely stretched tiltedly, is the carrier aircraft land very attitudes of tripe of craning one.When closing back original position, shown in figure-4b, AB support cylinder is withdrawn into limit, contraction in length, so the ABC distortion is equicrural triangle, the BC support becomes the base, is attached on the web.Upright support is meanwhile turned back, and upper limbs GH attaches the fuselage roof beam structure, upright lower limb H point pivot pin back timber frame, and touch switch, clamp (A10) is clamped in the quilt; Diagonal brace also tiltedly slides to, and lower limb are inserted in upper limbs, during its pivot pin back timber frame, also touches fuselage tail clamp (A11), and clamping is held firmly, the attaching ventral so whole hull bottom is locked.This is carrier aircraft flight and stops the state that the stopping time necking down is drawn the abdomen.

4) pocket bed (B) is made up of three guide rails (B1) dividing plates (B2), bed frame (B3), grid air cushion (B4) and air bag (B5) shown in figure-4.These three parallel file guide rail tops are fluted, respectively tangent the matching in file roller pearl top of begining to crop up with the skid plate of carrier aircraft " product " word Fabric office bottom.Article three, guide rail supports by equidistant alternate line dividing plate intersection, and firm position is at the bed frame, and its base part seat drops on the grid air cushion.The pocket bed also relies on the tail depressed place, and slant dilation inserts the sea, and the floating holder of gas Bian is arranged.The floating bed that stretch out in first depressed place is the same with it, no essential distinction, and just front end flushes with the sea.The guide rail of raising one's head and looking (C6) adopts sleeper directly to fix above deck.

5) general layout that reclaims is taken off shown in figure-5 in close-fitting aircraft carrier head and the tail depressed place.So-called close-fitting vest is the elimination of following the transfer of carrier aircraft landing point and impulsive force thereof, just reduces aircraft carrier floor space and structure significantly, also further improves the service efficiency of aircraft carrier.The batch sortie that the functional efficiency of aircraft carrier often takes off with the unit time is weighed.Jump and take off for the specific use except still keeping former Soviet Union formula in the new Fabric office, also set up in the left and right sides of raising one's head and looking and put many floating beds, number in order and set up 1,3,5 and 2,4,6 open taking off in turn, enlarge pocket bed quantity equally in the tail depressed place, also serial number is also set up 1,3,5 and 2,4,6 and is implemented open recovery the in turn.

So in concrete the utilization, when the hull bottom carrier aircraft lines up to take off, enter each first depressed place floating bed website from hangar by predetermined 1,3,5 or 2,4,6 numberings, borrow guide rail gradient power-assist to take off and obtain to face the speed that is situated between, leave floating bed, cut the face of going overseas, straight length is raised slowly and is drawn high, calm high up in the air, open continuously, line up to get inside the character that one is playing; Hull bottom carrier aircraft colony or single-row return, same, the organizational system by 1,3,5 and 2,4,6, send the numbering signal of pocket bed in vast sea affirmation tail depressed place, the landing point of determine complying with one's wishes, the aviator starts office, and the hull bottom carrier aircraft tripe of craning one is very held back wing, bow and cut the sea, the fast one or many degradation that stagnates floats to be cut, and exhausts until momentum, becomes an arrow at the end of its flight--a spent force, just stop fuel feeding, put holder in the pocket bed.Pocket bed air bag this moment (B5) inflation is risen, and carrier aircraft is submitted and entered guide rail, and just necking down is drawn the abdomen, and slides to the tail depressed place, and Ku Men (C10) is wide open, draws in hangar in a steady stream by dull and stereotyped (C5) and sweeps and disorderly change scene round and round when taking off land on the original deck as heat pot ant.---brag about " the taking off vertically " of " smart point " now; " launch lift-off ", just design real the genus, causes pernicious stressed model.Looking takes off than jumping wins several seconds advantage, but therefore have serious consequences: one, the ecosystem of aircraft is to be the product of feature with the wing, highlight split into or contract to go into air-flow be that fixed its of vital functions casting bears structure---nowadays lift with vertical vertical the throwing, wing meets with the strong anti-resistance of plate face fully loaded, and the weakness (being wing and fuselage junction) that its concentrated stress causes supporting is out of shape, is torn even wrecks; Vertical throwing is lifted and is required powerful assembly to send out energy, consumption of fuel is greatly also given and is started the same serious burst of wormwheel blade stressed, and accident is on the point of and is sent out, and to aircraft carrier deck high temperature sintering, hot-fluid is billowing, and the ear that shakes that screams worsens environment etc., it is compared with carrier aircraft sexual function at the same level, all will deduct points, such as combat radius obviously reduces---more seriously take off vertically to not bright the turning from side to side of aviator's physiology and psychology, i.e. burst is thrown and is lifted, heart is subjected to terrestrial attraction and throws hoisting force to anti-pull, suddenly, lose one's head, be absorbed in a trance dizzy fan's state, and suffer from military strategist in ancient China's taboo, it is man-machine in pairs from frustrating forfeiture dash not fight.And like this chronic fatigue self inflicted injury, must be on the point of detection, easily worn part is replaced in maintenance, and because of complex structure, and is too fat to move, and the corresponding huge millstone around one's neck on equipment and the servo ， Back of colony of launching.

And the present invention follows and suits measures to local conditions, as the taboo of ending of getting, nexhaustible immense ocean, unscrupulous utilization, platform as the land of taking off, grow with each passing hour to the structure deduction improvement of the intrinsic ecosystem of carrier aircraft, cause optimum coordination and positive effect: one, owing to eliminate pernicious stressed, so structure manufacturing technology, material requirements all significantly reduces, and particularly weight falls sharply, as replacing three tire frameworks with file roller pearl, give the carrier aircraft handsome body of making light of one's life by commiting suicide, promote life, viability and fistfight power, they are two years old, human factor first, obtain powerful technical support, for giving full play to dynamic role, can increase the deal that determines meaning on the integrated stage of air-sea.For example, it is extreme low-altitude to carry out enforcement, even pastes the sea long-range raid, quick clever making profit of can't be held back in battling in the air, be only success or failure victory or defeat key element determined by fate, rather than other any single thing, its three, aircraft carrier reduces floor space significantly, tonnage, reduce the power magnitude, and close-fitting vest is healthy and strong, and promotes motor-driven agility energy; Increase the head and the tail floating bed, the pocket bed promotes the land of taking off and provides the effect of playback, forms optimum coordination, safe and orderly composite entity---in fact, the hull bottom carrier aircraft has been arranged, the island seashore just be the aircraft carrier that never sinks of real meaning.Anyly come to attack the prey that the beast of prey all will become hornet.

Claims (4)

1. A hull bottom carrier aircraft with split the supporting close-fitting aircraft carrier of pocket bed (Fig. 1), by close-fitting aircraft carrier (C), the optimum coordination entity that hull bottom carrier aircraft (A1) and pocket bed (B) are formed is characterized in that: undertaken by carrier aircraft land and take-off process are transferred to the sea from the aircraft carrier deck.The tail depressed place (C3) of aircraft carrier tilts to stretch out for carrier aircraft (A1) cuts the pocket bed (B) that floats recovery, front end still keeps the general layout that the existing formula wing head of Soviet Union jumps and takes off, but increase three parallel files and push up the sleeper guide rail (C6) of tangent kissing with the three row ball pearls of emerging at the bottom of carrier aircraft hull bottom three skid plates, and set up Shou Wu (C4) in its right left both sides and also tilt to stretch out the floating bed (B0) of spreading the wings and taking off for carrier aircraft (A2), and hangar (C2) is below deck (C1), first Wu Weiwu all has gate open toward hangar, and shifts the flat truck (C6) that carrier aircraft is used;
2. According to the described hull bottom carrier aircraft of claim 1 with split the supporting close-fitting aircraft carrier of pocket bed, its hull bottom carrier aircraft is characterised in that:

   A, it has the dipteron (Fig. 3) that can launch simultaneously and restrain, right left machine wing all is four of P with the width: P1, P2, the nested overlap joint of P3, P4 order, and gang up each sheet waist by the wing TK that spreads out, top T is firmly at the waist of P1 sheet and the wing spreads out, after ganging up P2, P3, P4 sheet in regular turn, terminal K assembles the fuselage control mechanism, realizes that a right left side launches to hold back with closing simultaneously.The nested overlap joint of each sheet is half (being P/2) of width, and the difference of launching with convergence is 1.5P, namely holds back the width that reduces 3P behind the wing than spademan;

   B, its hull bottom (Fig. 4), by skid plate (A4) and paracone then web (A3) and identical three triangle brackets (A5) that can do longitudinal oscillation synchronously like the wide duck chest, and upright support (A6), diagonal brace (A7) is formed.And the AB of triangle bracket support, with upright support, the root of diagonal brace all is positioned on the web, and its top suspension is positioned on the fuselage roof beam structure.Wherein, on web, main skid plate is forward between two parties with " product " word Fabric office for three skid plates, after the side sled is symmetrical in.The straight trough of skid plate bottom all is embedded with file roller pearl, and Zhu Ding is all emerged and is attached to the sled web plate face at the end, and with tangent the matching of three guide rails (B1) of the pocket bed of addressing later.Correspondingly three each joint of triangle bracket interface point A, B, C pivot pin insert all separately that corresponding jaw link in the hole with the falcon head, so from beginning to end pivot pin link surround leg-of-mutton.Thirty years of age support then is made up of upper limbs GH and lower limb HE, and H is the joint link pivot pin of joint interface point.Though and diagonal brace is upper limbs MN and lower limb NF composition, but N then is dovetail and nested section of falcon, it is the falcon head of lower limb, insert upper limbs dovetail cover, can only make the fabricate block of directed flexible slippage, and its lower limb root F tilts firmly at web foremost, and M joint, upper limbs top pivot pin then hangs the location roof beam structure and is inverted in the bearing saddle bore.And three triangle brackets have only AB support root B pivot pin to be positioned under the bearing seat of corresponding skid plate separately in (A9) axis hole, and each A joint pivot pin of its top then hangs and is positioned at inversion firmly in corresponding fuselage roof beam structure top chock (A8) axis hole.The lower limb of upright support are upright, the web center that its root E is firm, and with main skid plate, diagonal brace arranges the 3rd on same line of centers; G joint, upright support upper end pivot pin also is to hang to be positioned in the bracket holes of the inverted bearing seat of fuselage roof beam structure, and the equal line of the line of centers of all pivot pins is parallel.

   The AB of triangle bracket support is variable only, and it is by the fabricate block of cylinder and piston, and upper limbs is that cylinder, lower limb are the fabricate block of piston, is that the control web is endured out and the main part of drawing the abdomen, and all the other two support BC and CA are fixed length.

   (Fig. 4 a), this moment, primer fluid compressed switch, and the cylinder of three AB supports reaches pitch length, and triangle bracket is the positive right-angled triangle of handstand, and namely CA is crisperding, and AB be a burst limit, and BC is profound, and the CA support all is attached to the fuselage roof beam structure, and AB supports and all uprightly withstands web when carrying.This moment upright support center direct bearing, diagonal brace is also completely stretched tiltedly, is the carrier aircraft land very attitudes of abdomen of craning one.When closing recovery, (Fig. 4 b), AB support cylinder is withdrawn into limit, contraction in length, so the ABC distortion is equicrural triangle, the BC support becomes the base, is attached on the web.Upright support is meanwhile turned back, and upper limbs GH attaches the fuselage roof beam structure, upright lower limb H point pivot pin back timber frame, and touch switch, clamp (A10) is clamped in the quilt; Diagonal brace also tiltedly slides to, and lower limb are inserted in upper limbs, and during straight back timber frame, its pivot pin also touches tail clamp (A11), and clamped holding firmly is attached to ventral so whole hull bottom is locked.
3. According to the described hull bottom carrier aircraft of claim 1 with split the supporting close-fitting aircraft carrier of pocket bed, its pocket bed (Fig. 6) is characterised in that: be made up of three guide rails (B1), dividing plate (B2), bed frame (B3), grid air cushion (B4) and air bag (B5).These three parallel file guide rail tops are fluted, respectively tangent the matching in file roller pearl pearl top of begining to crop up with the skid plate of carrier aircraft " product " word Fabric office bottom.Article three, guide rail supports by equidistant alternate line dividing plate intersection, and firm position is at the bed frame, and its base part seat drops on the grid air cushion.The pocket bed relies on the tail depressed place, and slant dilation inserts the sea, and the floating holder of air bag is arranged.The floating bed that stretch out in first depressed place is the same with it, no essential distinction, and just front end flushes with the sea.The guide rail of raising one's head and looking (C6) then is to adopt sleeper directly to fix above deck.
4. According to claim 1 hull bottom carrier aircraft with split the supporting close-fitting aircraft carrier of pocket bed, its close-fitting aircraft carrier (Fig. 5) feature exists: still keep former Soviet Union formula and jump and take off for outside the specific use, also set up Shou Wu in the left and right sides of raising one's head and looking and stretch out many floating beds, number in order, set up 1,3,5 and 2,4,6 open taking off in turn, be located at the tail depressed place equally and enlarge pocket bed quantity, also serial number is set up 1,3,5 and 2,4,6 and is implemented open recovery the in turn.Pocket bed and floating bed are the multistage hinge, and be collapsible, and perhaps nested combination is scalable, be stored in its dock bottom portion (figure-5a).

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