CN103129716A - Sea plane take-off, landing and accessory device - Google Patents

Abstract

A sea plane take-off, landing and accessory device is composed of piles 1, a middle compartment body 2, a deck 3, a front long compartment body 13, a rear long compartment body 14, an air energy storage device 15, a pressurized water generating device 16, a bothway single runway 17, a blocking device 18, a bullet resistant device 19, a photovoltaic power generation device 20, a transformer room 23, a hydraulic device 25, a commanding tower 31, a control room 32, a plane shed 33, an elevator 34, a dock compartment 35, a wind driven generator 36, a water diversion device 38 and the like. The sea plane take-off, landing and accessory device is characterized in that the devices mutually operate in a linkage mode.

Description

Open sea aeroplane landing and accessory device

Technical field

A kind of open sea aeroplane landing and accessory device belong to the military equipment field.

Background technology

On the less islands and reefs of area in China marine site, can not accomplish by traditional building an airport on land, therefore, exist the military aircraft that is taken off by airfield in wartime and can not in time obtain the problem of the mastery of the air in overhead, off-lying sea territory, simultaneously also exist local marine site and can not utilize the solar power of local area to change into electric energy, thereby increase the transportation device of long-distance transfer the fuel and numerous rear service personnels' shortcoming; Limit by physical features but also be to need huge fund input due to the airstrip of growing up being set on Reef in Chinese South Sea, therefore, arrange on islands and reefs that to have the short distance airport that aircraft was stopped and launched bouncing function be the selection of the best;

Summary of the invention

In order to solve above-mentioned existing problem, the invention provides a kind of be arranged on the fund of can saving on neritic zone, island and islands and reefs have again open sea aeroplane landing and an accessory device that aircraft is blocked landing and catapult-assisted take-off function.

The solution of the present invention is

open sea aeroplane landing and accessory device are by pile 1, middle envelope 2, deck 3, stage 4, screw 5, joint plate 9, connection connecting pore 10, screw rod 11, nut slot 12, front long envelope 13, rear long envelope 14, air energy-storage device 15, setting-out power generation assembly 16, two-way single flight road 17, block device 18, resistance bullet device 19, photovoltaic power generation equipment 20, output cable 21, connect grillage 22, transformer room 23, output cable 24, hydraulic efficiency gear 25, oil railway carriage or compartment 26, oil pipeline 27, oil can 28, arsenal 29, transport channel 30, direct tower 31, control cabin 32, hangarage 33, elevator 34, railway carriage or compartment, depressed place 35, aerogenerator 36, typhoon protection device 37, diversion equipment 38, military technology equipment 39 and weaponry 40 form, it is characterized in that, when open sea aeroplane landing and accessory device are arranged in the marine site, be provided with front resistance bullet device 19 in it, middle resistance bullet device 19 ' and rear resistance bullet device 19 ", three resistance bullet devices 19,19 ' 19 " topside of triple cylinder 168 of (convenient for making explanation, as only to be illustrated for embodiment take three resistance bullet devices 19) be separately positioned on several in neritic zone pile 1 above or around islands and reefs in several middle envelope 2 inner chambers pile 1 above before, during and after the position, and make progress separately that right deck 3 is top to be located, be respectively equipped with front tactile hook position 61, in tactile hook position 61 ' and rear tactile hook position 61 ", three resistance bullet devices 19,19 ', 19 " its in the submarine site that is separately positioned on the bottom of front long envelope 13 and rear long envelope 14 and is arranged on long envelope 13,14 sides with the sleeve 150 that hooks shellfish cylinder 149, be arranged on three resistance bullet devices 19,19 ', 19 of the open sea aeroplane landing of land, island and accessory device " its in all be separately positioned in the water pipe 238 relative with it of diversion equipment 38 with the sleeve 150 of hook shellfish cylinder 149, be arranged on the middle envelope 2 in two-way single flight road 17 of land and front long envelope 13 and afterwards long envelope 14 combine as a whole, the bottom section of middle envelope 2 be positioned at underground three resistance bullet devices 19,19 ', 19 " the topside of triple cylinder 168 combine as a whole, be arranged on the stage 4 with the front end of several screws 5 of envelope 2 in open sea aeroplane landing in the marine site and accessory device, be connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of front long envelope 13 rear ends, and the stage 4 with several screws 5 of middle envelope 2 rear ends is connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of rear long envelope 14 front ends, the place, outer end that is separately positioned on foredeck 54 on front long envelope 13 and rear long envelope 14 and aft deck 55 is provided with block device 18, in takeoff and landing at sea and accessory device the appropriate location be provided with air energy-storage device 15, setting-out power generation assembly 16, transformer room 23, output cable 24, hydraulic efficiency gear 25, with the oily railway carriage or compartment 26 of oil pipeline 27 and oil can 28 and with the arsenal 29 of transport channel 30, being positioned at appropriate locations above the railway carriage or compartment, depressed place 35 of open sea aeroplane landing and accessory device both sides is provided with it with the direct tower 31 of control cabin 32 and is provided with military technology and equip 39 and weaponry 40, be provided with photovoltaic power generation equipment 20 and several aerogenerators 36 on connection grillage 22 on depressed place, railway carriage or compartment 35, the interior relevant electrical equipment in the output cable 21 of photovoltaic power generation equipment 20 and several aerogenerators 36 and transformer room 23 links, also be provided with air energy-storage device 15 and setting-out power generation assembly 16 in railway carriage or compartment, depressed place 35, each output cable of setting-out power generation assembly 16 all with transformer room 23 in relevant electrical equipment link

The invention has the beneficial effects as follows:

1. the present invention has not only solved the problem of airport land occupation, can also be arranged on neritic zone, island and the islands and reefs away from the continent, has the effect that improves the military flight radius and strengthen the empty ability of system.

2. each airport in the present invention can store various goods and materials and military supplies.

Each airport, airport in 3 the present invention all has blocks the function that aircraft landing and cataplane take off.

4. the landing that can launch simultaneously and block some airplanes due to the fish-bone airport 05 in the present invention, therefore not only has the military secret of grasp advantage rapidly, even also have simultaneously after the airport is partially damaged, its remainder still can have the function that continues to launch and block takeoff and landing.

5. because the running of blocking and launch in the present invention does not need steam as power, therefore can saving fuel, can also avoid simultaneously providing the focus target to the heat-seeking missile of enemy's emission.

6. the less islands and reefs of area in the marine site, be also the optimal selection that open sea aeroplane landing and accessory device are set.

Due to resistance bullet device 010, squeezer 342 have the function of elasticity extruding, the generation that can avoid producing water hammer is to protect the safety of relevant parts and rope.

8. the air cavity ring 303,304 on resistance bullet device 010 has the function that can remove the seawater spray that rope is upwards taken out of.

9. the present invention can hinder several bullet device 19 compositions with joint efforts, therefore not only can hinder to play fighter plane but also can hinder to play early warning plane and bomber.

10. before airstrip landing aircraft, several electro-hydraulic drive water valves of control personnel control are in some high-pressure water inlet cylinders and cut out, control simultaneously some squeezers 342, make between the bullet of each squeezer 342 and water squeezing hole and produce suitable gap, hook a moment of firm check cable 187 until aircraft is stopped near this a section process of launching of airstrip from the aircraft pintle, also to control several squeezers 342 of personnel control all progressively to dwindle direct clearance between its bullet and water squeezing hole 331 to both mutually closely connected processes, this process can be according to aircraft weight, the size in sinking speed and squeezer bullet and 331 gaps, water squeezing hole and the key elements such as length of time are made computer software, make the computerized control landing of aircraft of staff.

11. owing to having played at front close rear several the thin permeable holes that hook shellfish cylinder front portion the effect that progressively increases surface pressure after hooking shellfish, make rope can not produce unexpected longitudinal impulse, to guarantee man-machine safety.

12. because resistance bullet device 19 is provided with booster electric machine, except hooking shellfish cylinder 149, other gas storage water storage device just can be made the specification of bearing superhigh pressure, therefore just can save substantial contribution.

Description of drawings

Fig. 1 is the plan structure schematic diagram of open sea aeroplane landing and accessory device;

Fig. 2 is the side-looking structural representation of open sea aeroplane landing and accessory device;

Fig. 3 is the side-looking structural representation of the block device 18 of open sea aeroplane landing and accessory device;

Fig. 4 is the local structure schematic top plan view of the block device 18 of open sea aeroplane landing and accessory device;

Fig. 5 is the local structure schematic top plan view of the block device 18 of open sea aeroplane landing and accessory device;

Fig. 6 is the side-looking structural representation of the expansion net arrangement 133 of block device 18;

Fig. 7 is the only side-looking structural representation of rope device 71 on two-way single flight road 17 and block device 18;

Fig. 8 is the side-looking structural representation that draws device 68 that revolves on two-way single flight road 17;

Fig. 9 is the side-looking structural representation of the squeezer 212 on resistance bullet device 19;

Figure 10 is the side-looking structural representation of the hydrodynamic(al) air valve 205 on resistance bullet device 19;

In figure:

pile 1, middle envelope 2, deck 3, stage 4, screw 5, spin slot 6, limit stage 7, screw 8, joint plate 9, connecting pore 10, screw rod 11, nut slot 12, front long envelope 13, rear long envelope 14, air energy-storage device 15, setting-out power generation assembly 16, two-way single flight road 17, block device 18, resistance bullet device 19, photovoltaic power generation equipment 20, output cable 21, connect grillage 22, transformer room 23, output cable 24, hydraulic efficiency gear 25, oil railway carriage or compartment 26, oil pipeline 27, oil can 28, arsenal 29, transport channel 30, direct tower 31, control cabin 32, hangarage 33, elevator 34, railway carriage or compartment, depressed place 35, aerogenerator 36, diversion equipment 38, military technology equipment 39, weaponry 40, machine room 41, electric air compressor 42, diesel compressor 43, H Exch 44, high-pressure gas railway carriage or compartment 45, high pressure water railway carriage or compartment 46, high pressure fills draining railway carriage or compartment 47, level sensor controller 48, exhaust railway carriage or compartment 49, atmosphere check device 50, water output cylinder 51, electricity liquid water valve 52, hydroelectric installation 53, foredeck 54, aft deck 55, body 56 is expanded in the railway carriage or compartment, structural slab 57, end railway carriage or compartment 58, markings 59, marker lamp 60, front tactile hook position 61, in touch hook position 61 ', rear tactile hook position 61 ", break slot 62, holder rope spring 63, deck open-work 64, open-work groove 65, inboard anticreep pulley 66, the perpendicular pulley 67 of outside anticreep, revolve and draw device 68, check cable 69, standby check cable 69 ', launch position 70, stop rope device 71, landing guiding device 72, weather cock 73, lift well 74, elevator 75, hangar 76, aircraft gate 77, tractor truck 78, fork rope device 79, reorganize and outfit chamber 80, cover plate 81, direct tower 82, control cabin 83, structure grillage 84, deck 85, gap 86, slide guide cylinder 87, gap 88, lifting column 89, cat net abduction rod 90, connection post plate 91, turn side plate 92, inserted link cylinder 92 ', horizontal anticreep pulley 93, pulley support 94, vertical anticreep pulley 95, pulley support 96, dragline pulley 96 ', post jamb permeable hole 97, post jamb joint plate 98, electro-hydraulic drive device 99, expansion link 100, connection seat board 101, upper fixed wheel 103, lacing grommet 104, anticreep fixed pulley 105, shaft stool 106, block 107, selvage rope 108, anticreep pulley 109, foot piece 110, the hole 111 of reeving, it is rete cord 112, cord junction joint 113, dog hole 113 ', lashing pulley 114, lock hook 114 ', hole enlargement cable 115, mobile anticreep pulley 116, hook shellfish cylinder 117, cylinder top board 118, the hole 119 of reeving, permeable hole 120, ring yoke plate 126, connecting pore 127, hook shellfish 128, lacing grommet 130, rope 131, noose ring 132, expand net arrangement 133, equipment railway carriage or compartment 146, compartment top plate 147, wear railway carriage or compartment cylinder 148, hook shellfish cylinder 149, sleeve 150, vertical joint plate 151, stomidium plate 152, pipe spreader 153, bearing frame 154, shaft seal 155, arc flap 157, packing seal 158, screw 159, screw rod 160, ring yoke plate 161, connecting pore 161 ', structure grillage 162, cylinder prosopyle 164, permeable hole 165, stop plate 166, spring 167, triple cylinder 168, anticreep sister block 169 in cylinder, conical baffle 170, coil 171 is led on a left side, coil 172 is led on the right side, flight 173, enlarging 174, drain hose 175, dividing plate 176, the hole 177 of reeving, a left side, the hole 178 of reeving, the right side, left air cavity ring 179, right air cavity ring 180, connect ring flat-plate 181, air inlet pipe 182, deflation hole 183, upper drain hose 184, epicone dividing plate 185, rear triple cylinder 186, tail pipe 187, lower back panel 188, pipe spreader 189, bearing 190, shaft seal 191, expansion water railway carriage or compartment, side 192, railway carriage or compartment base plate 193, permeable mouthful 194, open-work plate 195, inboard partition 196, permeable cylinder 197, flange 198, twin shaft folding plates 198 ', annular groove 199, seal ring 200, water squeezing hole 201, compartment top plate 202, water inlet 203, coolant outlet pipe 204, hydrodynamic(al) air valve 205, permeable control water railway carriage or compartment 206, external partition 207, mounting hole 208, connecting pore 209, rubber cushion 210, bolt 211, squeezer 212, UNICOM's cylinder 213, railway carriage or compartment 214 is installed, gangway 215, staircase 216, poling hole 217, hook shellfish 218, pulling rod 219, left lacing grommet 220, right lacing grommet 221, left rope 222, right rope 223, left lacing grommet 224, right lacing grommet 225, high-pressure water inlet cylinder 226, electro-hydraulic drive water valve 227, electrical motor 228, coupler 229, drive link 230, propeller 231, bracing strut 231 ', transformer room 232, output cable 233, hydraulic efficiency equipment 234, flume 235, hydraulic accumulator 236, pumping plant 237, water pipe 238, joint plate 239, front triple cylinder 240, rear triple cylinder 241, tail pipe 242, lower back panel 243, bar pipe 244, bearing 245, shaft seal 246, electro-hydraulic drive device 247, expansion link 248, ring yoke plate 249, connecting pore 250, spring strut 251, cylinder base plate 252, spring 253, pressure spring plate 254, link rod 255, bullet 256, spring strut 257, water inlet 258, spring 259, pressure spring plate 260, brace rod 261, pole perforating hole 262, slide valve sleeve 263, air inlet pipe 264, admission port 265, air extractor duct 266, guiding valve 267, breather hole 268, dish seat 270, plate bracket 271, lateral shaft 272, bearing 273, roller 274, the hole 275 of reeving, load-bearing bearing 276, swivel mount 277, the hole 278 of reeving, anticreep pulley 279, bracing strut seat 280, two fork bodies 281, coupling spindle 282, middle part coupling spindle 283, electro-hydraulic drive device 284, first line of a couplet spindle 285, second line of a couplet spindle 286, two plate axis holes 287, pulley 288, two plate axis holes 289, the deck is cylinder 290 thoroughly, electro-hydraulic drive device 291, expansion link 292, lifting body 293, take rope plate 294, flange 295, holder rope rank 296, sleeping hook rank groove 297, Kao Hook plate 298, stage 299, front guide frame 300, lower expansion net bar 301, rear guide frame 302, upper expansion net bar 303, dovetail furrow 304, lifting lath 305, tooth bar 306, turn outward and expand net bar 308 on joint plate 307, gear 309, gear wheel shaft 310, bracing strut seat 311, link rod 312, crank 313, dull and stereotyped 314, wheel 315, hook ring 316, cable 317, divide guy 318, anti-drop hook 319.

The specific embodiment:

The invention will be further described below in conjunction with drawings and Examples:

open sea aeroplane landing and accessory device are by pile 1, middle envelope 2, deck 3, stage 4, screw 5, joint plate 9, connection connecting pore 10, screw rod 11, nut slot 12, front long envelope 13, rear long envelope 14, air energy-storage device 15, setting-out power generation assembly 16, two-way single flight road 17, block device 18, resistance bullet device 19, photovoltaic power generation equipment 20, output cable 21, connect grillage 22, transformer room 23, output cable 24, hydraulic efficiency gear 25, oil railway carriage or compartment 26, oil pipeline 27, oil can 28, arsenal 29, transport channel 30, direct tower 31, control cabin 32, hangarage 33, elevator 34, railway carriage or compartment, depressed place 35, aerogenerator 36, typhoon protection device 37, diversion equipment 38, military technology equipment 39 and weapon form 40 of equipments, it is characterized in that, when open sea aeroplane landing and accessory device are arranged in the marine site, be provided with front resistance bullet device 19 in it, middle resistance bullet device 19 ' and rear resistance bullet device 19 ", three resistance bullet devices 19,19 ' 19 " topside of triple cylinder 168 of (convenient for making explanation, as only to be illustrated for embodiment take three resistance bullet devices 19) be separately positioned on several in neritic zone pile 1 above or around islands and reefs in several middle envelope 2 inner chambers pile 1 above before, during and after the position, and make progress separately that right deck 3 is top to be located, be respectively equipped with front tactile hook position 61, in tactile hook position 61 ' and rear tactile hook position 61 ", three resistance bullet devices 19,19 ', 19 " its in the submarine site that is separately positioned on the bottom of front long envelope 13 and rear long envelope 14 and is arranged on long envelope 13,14 sides with the sleeve 150 that hooks shellfish cylinder 149, be arranged on three resistance bullet devices 19,19 ', 19 of the open sea aeroplane landing of land, island and accessory device " its in all be separately positioned in the water pipe 238 relative with it of diversion equipment 38 with the sleeve 150 of hook shellfish cylinder 149, be arranged on the middle envelope 2 in two-way single flight road 17 of land and front long envelope 13 and afterwards long envelope 14 combine as a whole, the bottom section of middle envelope 2 be positioned at underground three resistance bullet devices 19,19 ', 19 " the topside of triple cylinder 168 combine as a whole, be arranged on the stage 4 with the front end of several screws 5 of envelope 2 in open sea aeroplane landing in the marine site and accessory device, be connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of front long envelope 13 rear ends, and the stage 4 with several screws 5 of middle envelope 2 rear ends is connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of rear long envelope 14 front ends, the place, outer end that is separately positioned on foredeck 54 on front long envelope 13 and rear long envelope 14 and aft deck 55 is provided with block device 18, in takeoff and landing at sea and accessory device the appropriate location be provided with air energy-storage device 15, setting-out power generation assembly 16, transformer room 23, output cable 24, hydraulic efficiency gear 25, with the oily railway carriage or compartment 26 of oil pipeline 27 and oil can 28 and with the arsenal 29 of transport channel 30, being positioned at appropriate locations above the railway carriage or compartment, depressed place 35 of open sea aeroplane landing and accessory device both sides is provided with it with the direct tower 31 of control cabin 32 and is provided with military technology and equip 39 and weaponry 40, be provided with photovoltaic power generation equipment 20 and several aerogenerators 36 on connection grillage 22 on depressed place, railway carriage or compartment 35, the interior relevant electrical equipment in the output cable 21 of photovoltaic power generation equipment 20 and several aerogenerators 36 and transformer room 23 links, also be provided with air energy-storage device 15 and setting-out power generation assembly 16 in railway carriage or compartment, depressed place 35, each output cable of setting-out power generation assembly 16 all with transformer room 23 in relevant electrical equipment link.

By top described, the air energy-storage device 15 of open sea aeroplane landing and accessory device is comprised of machine room 41, electric air compressor 42, diesel compressor 43, H Exch 44, high-pressure gas railway carriage or compartment 45 and the various pipeline of prior art and various gas, water valve, it is characterized in that, the above-mentioned various devices of air energy-storage device 15 be separately positioned on separately in open sea aeroplane landing and accessory device suitable position and and the relative assembly right with it of setting-out power generation assembly 16 link.

by top described, the setting-out power generation assembly 16 of open sea aeroplane landing and accessory device is the high pressure water railway carriage or compartment 46 by prior art, high pressure fills draining railway carriage or compartment 47, level sensor controller 48, exhaust railway carriage or compartment 49, atmosphere check device 50, water output cylinder 51, electricity liquid water valve 52, hydroelectric installation 53 and various pipeline, air valve, water valve, electricity liquid G﹠W valve rope forms, it is characterized in that, the above-mentioned various devices of setting-out power generation assembly 16 are separately positioned on separately the suitable position in open sea aeroplane landing and accessory device and link with the relative assembly relative with it of air energy-storage device 15.

by top described, open sea aeroplane landing and the two-way single flight road 17 that is installed with device are by foredeck 54, aft deck 55 (for making explanation convenient, intending take the deck that is in windward side as foredeck 54, take the deck that is in leeward end as aft deck 55), deck 85 on block device 18, body 56 is expanded in the railway carriage or compartment, structural slab 57, end railway carriage or compartment 58, markings 59, marker lamp 60, front tactile hook position 61, in touch hook position 61 ', rear tactile hook position 61 ", break slot 62, holder rope spring 63, deck open-work 64, open-work groove 65, inboard anticreep pulley 66, the perpendicular pulley 67 of outside anticreep, revolve and draw device 68, check cable 69, make a concerted effort to join rope 69 ', launch position 70, stop rope device 71, landing guiding device 72, weather cock 73, lift well 74, elevator 75, hangar 76, aircraft gate 77, tractor truck 78, fork rope device 79, reorganize and outfit chamber 80, cover plate 81, direct tower 82 and control cabin 83 form, and it is characterized in that the deck 54 in two-way single flight road 17, deck 3 and aft deck 55 are separately positioned on the front long envelope 13 that is arranged on open sea aeroplane landing and accessory device, above middle envelope 2 and rear long envelope 14, the railway carriage or compartment that deck 3 is arranged on resistance bullet device 19 expand body * above, be provided with the direct tower 201 that is provided with control cabin in it on deck 3, expand on the central deck 170 of bodies 171 with direct tower 201 opposite side railway carriage or compartments and be provided with several aircraft gates 196, in the middle of each tactile hook position 62 of three the tactile hook positions 62 that arrange at 3 middle parts, deck, the place is provided with the break slot 62 that all is placed with holder rope spring 63 in several its, only be respectively arranged with rope device 71 below inner place, position and both sides and reorganize and outfit chamber 80 launching of forward and backward deck 54,55 outer end places, below each tactile hook position 61 at 3 middle parts, deck and the deck 3 of both sides, tactile hook position below, be respectively arranged with two symmetrical inboard anticreep pulleys 66 and two perpendicular pulleys 67 of symmetrical outside anticreeps, be provided with to revolve in each the open-work groove 65 above deck open-work 64 that touches 61 both sides, hook position and draw device 68, above deck 85 on proostracum 54, deck 3 and aft deck 55 and block device 18, all be decorated with the markings 59 of runway longitudinal centerline and be provided with marker lamp 60 and be provided with landing guiding device 72, near the position that is provided with the close outer end on the deck 85 of stopping rope device 71 block devices 18 each is launching an inboard also is provided with launches position 70, and 17 outsides, two ends, two-way single flight road are provided with the device 18 of blocking simultaneously, the following triple cylinder * top structure grillage * on every side with hindering bullet device 19 that two-way single flight road 17 touches the deck 3 at 61 places, hook position is coupled as one, be provided with hangar 76 and elevator 75 in the end railway carriage or compartment 58 that all arranges in foredeck 54 and aft deck 55 both sides, outer end, the front of the tractor truck 78 that arranges on two-way single flight road 17 is provided with fork rope device 79.

by top described, the block device 18 of open sea aeroplane landing and accessory device is by structure grillage 84, deck 85, gap 86, slide guide cylinder 87, gap 88, lifting column 89, cat net abduction rod 90, connection post plate 91, turn side plate 92, inserted link cylinder 92 ', horizontal anticreep pulley 93, pulley support 94, vertical anticreep sister block 95, pulley support 96, dragline pulley 96 ', post jamb permeable hole 97, post chamber 98, post jamb joint plate 98 ', electro-hydraulic drive device 99, expansion link 100, connection seat board 101, upper fixed wheel 103, lacing grommet 104, anticreep fixed pulley 105, shaft stool 106, block 107, selvage rope 108, anticreep pulley 109, foot piece 110, the hole 111 of reeving, it is rete cord 112, collection rope plate 113, dog hole 113 ', lacing grommet 113 ", lashing pulley 114, lock hook 114 ', hole enlargement cable 115, mobile pulley 116, hook shellfish cylinder 117, cylinder top board 118, the hole 119 of reeving, permeable hole 120, ring yoke plate 126, connecting pore 127, hook shellfish cylinder 128, lacing grommet 130, rope 131, noose ring 132 and expand net arrangement 133 and forms is characterized in that, the structure grillage 84 of device 18 both sides of blocking is the long envelope 13 below 17 two ends, two-way single flight road respectively, place, 14 outer end wall both sides is coupled as one, and all is linked with the lifting column 89 that all there is cat net abduction rod 90 its upper end on the expansion link 100 of the electro-hydraulic drive device 99 that all arranges with the bottom of the slide guide cylinder 87 of gap 88 of left and right, after the connection post plate 91 that combines as a whole with each lifting column 89 rear ends was passed backward by the gap 88 of slide guide cylinder 87 rear end, the outside of turning side plate 92 that its outside connects was respectively arranged with the horizontal anticreep pulley 93 of pulley support 94 with the vertical anticreep sister block 95 of pulley support 96, in each pile 1 inner chamber with post jamb permeable hole 97 of the left and right sides of the outermost end of left and right two several piles 1 of row below block device 18, be provided with the hook shellfish cylinder 117 with sleeve 121, and several of sleeve 121 outsides connect mutually with the ring yoke plate 126 of the connecting pore 127 post jamb joint plate 98 with pile 1, be respectively equipped with fixed wheel 103, lacing grommet 104 on the connection seat board 101 that arranges and with the anticreep fixed pulley 105 of shaft stool 106 on hook the cylinder top board 118 with the hole 119 of reeving of shellfish cylinder 117, selvage rope 108 covers that are arranged on block 107 dual-sides between both sides lifting column 89 rear portions have several all with the anticreep pulley 109 in foot piece 110 and the hole 111 of reeving, several anticreep pulleys 109 by be rete cord 112 with cord junction joint 113 on several all carry out flexagon ground with the lashing pulley 114 of lock hook 114 ' and connect, each lock hook 114 ' all with collection rope plate 113 on relative dog hole 113 ' phase structure connect, lacing grommet 113 with collection rope plate 113 " front end of the hole enlargement cable 115 that connects is connected with mobile anticreep pulley 116, the selvage rope that each that is separately positioned on both sides turns cat net abduction rod 90 front ends that all insert in the inserted link cylinder 92 ' that the inner top side of side plate 92 arranges and block 107 opposite side upper ends plugs, place, both sides on the deck 54,55 at 17 two ends, two-way single flight road is provided with respectively and expands net arrangement 133, but leaving its width between the front end of the rear end on the deck 85 that connects above with structure grillage 84 and relative foredeck 54 or aft deck 55 can pass block 107 not affect the gap 86 that wheel slides, the position 70 of launching of 85 longitudinal centerlines is provided with only rope device 71 on the deck.After the hole 119 of reeving in the upper end of the rope 131 that the lacing grommet 130 of the hook shellfish cylinder 128 of post chamber 98 interior settings connects through hooking 117 top boards 118 of shellfish cylinder, front portion, mobile pulley 116 rear portions and the upper fixed wheel 103 of cylinder top board 118 anticreep fixed pulleys, noose ring 132 and lacing grommet 104 that its end is made link.

by top described, the front resistance bullet device 19 of open sea aeroplane landing and accessory device, middle resistance bullet device 19 ' and rear resistance bullet device 19 " by air energy-storage device 15, setting-out power generation assembly 16, equipment railway carriage or compartment 146, compartment top plate 147, wear railway carriage or compartment water channel 148, hook shellfish cylinder 149, sleeve 150, vertical joint plate 151, stomidium plate 152, pipe spreader 153, bearing frame 154, shaft seal 155, arc flap 157, packing seal 158, screw 159, screw rod 160, ring yoke plate 161, connecting pore 161 ', structure grillage 162, cylinder prosopyle 164, permeable hole 165, stop plate 166, spring 167, triple cylinder 168, anticreep sister block 169 in cylinder, conical baffle 170, coil 171 is led on a left side, coil 172 is led on the right side, flight 173, enlarging 174, drain hose 175, dividing plate 176, the hole 177 of reeving, a left side, the hole 178 of reeving, the right side, left air cavity ring 179, right air cavity ring 180, connect ring flat-plate 181, air inlet pipe 182, deflation hole 183, upper drain hose 184, epicone dividing plate 185, rear triple cylinder 186, tail pipe 187, lower back panel 188, pipe spreader 189, bearing 190, shaft seal 191, expansion water railway carriage or compartment, side 192, railway carriage or compartment base plate 193, permeable mouthful 194, open-work plate 195, inboard partition 196, permeable cylinder 197, flange 198, twin shaft folding plates 198 ', annular groove 199, seal ring 200, water squeezing hole 201, compartment top plate 202, water inlet 203, coolant outlet pipe 204, hydrodynamic(al) air valve 205, permeable control water railway carriage or compartment 206, external partition 207, mounting hole 208, connecting pore 209, rubber cushion 210, bolt 211, squeezer 212, UNICOM's cylinder 213, railway carriage or compartment 214 is installed, gangway 215, staircase 216, poling hole 217, hook shellfish 218, pulling rod 219, left lacing grommet 220, right lacing grommet 221, left rope 222, right rope 223, left lacing grommet 224, right lacing grommet 225, high-pressure water inlet cylinder 226, electro-hydraulic drive water valve 227, electrical motor 228, coupler 229, drive link 230, propeller 231, bracing strut 231 ', transformer room 232, output cable 233 and hydraulic efficiency equipment 234 form, it is characterized in that, front resistance bullet device 19, middle resistance bullet device 19 ' and rear resistance bullet device 19 " all with the hook shellfish cylinder 149 of sleeve 150 respectively upper, middle and lower be arranged on wearing in railway carriage or compartment water channel 148 that water pipe with diversion equipment 38 links vertically oppositely, and sleeve 150 with the ring yoke plate 161 of connecting pore 161 ' and wear railway carriage or compartment water channel 148 inner structure grillages 162 and combine as a whole, front resistance bullet device 19 (for making explanation convenient, the resistance bullet is two before only puts 19 and be illustrated for embodiment) is arranged on middle envelope 2 following front portion, be provided with air energy-storage device 15 and setting-out power generation assembly 16 in the equipment railway carriage or compartment 146 of front resistance bullet device 19, on its anterior barrel of each resistance bullet device 19 with being linked with several between the hook shellfish cylinder 149 of several permeable holes 165 and sleeve 150 inwalls all with vertical joint plate 151 of open-work, hook shellfish cylinder 149 welds from beginning to end with some sections stainless steel cylinders or links with flange and forms, sleeve 150 all combines as a whole with structure grillage 162 with connecting pore 163 respectively by bolt with the ring yoke plate 161 of connecting pore 161 ' by several on its outer wall, be provided with in the front that hooks the baffle plate 166 that arranges on shellfish cylinder 149 rear inside wall the spring 167 made from corrosion-resistant steel, above the hook shellfish cylinder 149 of front resistance bullet device 19, the front upper place of the connection place of the triple cylinder 168 of UNICOM is provided with an interior anticreep sister block 169, being linked with on conical baffle 170 on triple cylinder 292 all has flight 173, all has the left side of enlarging 174 to lead coil 171 on it and coil 172 is led on the right side in it, outwards passed drain hose 175 on barrel on conical baffle 170, two lead be provided with above coil 171,172 two respectively with the above two 171,172 vertically opposite dividing plates 176 on hole 177 and the right side hole 178 of reeving of reeving, a left side, be respectively arranged with all on two holes 177,178 top left air cavity ring 179 and the right air cavity ring 180 that several deflation holes 183 is all arranged with connecting in its of ring flat-plate 181, link with the another end mouth of pipe of two air cavity rings 179,180 air inlet pipes that link 182 and the air extractor duct 266 of hydrodynamic(al) air valve 205 respectively, drain hose 184 on outwards having passed on barrel on dividing plate 176, having the side of some open-work plates 195 to expand permeable mouthful 194 of water railway carriage or compartment 192 railway carriage or compartment base plates 193 in the top of rear triple cylinder 186 nozzle and its above it links, expand on 192 inboard partitions 196 of water railway carriage or compartment in the side, be provided with the other end that several its nozzles are linked with the permeable cylinder 197 of blank flange 198 and pass inboard partition 196 and extend in permeable control water railway carriage or compartment 206, be provided with seal ring 200 in annular groove 199 on 198 of flanges of each permeable cylinder 197, also be provided with several water squeezings hole 201 on inboard partition 196, the other end mouth of pipe of the coolant outlet pipe 204 of UNICOM and the water inlet 258 of hydrodynamic(al) air valve 205 link on the compartment top plate 202 in expansion water railway carriage or compartment, side 192, each water inlet 203 on the railway carriage or compartment wallboard at expansion 192 rear portions, water railway carriage or compartment, side all is linked with the high-pressure water inlet cylinder 226 with electro-hydraulic drive water valve 227, each its periphery that arranges on the external partition 207 between the installation railway carriage or compartment 214 of permeable control water railway carriage or compartment 206 and its front has the mounting hole 208 of several connecting pores 209 and rubber cushion 210, link with the sleeve 150 that hooks shellfish cylinder 149 with the nozzle of the other end of UNICOM's cylinder 213 of permeable control water railway carriage or compartment 206 UNICOMs, be arranged on connecting mutually with the ring yoke plate 249 of connecting pore 250 several connecting pores 209 by mounting hole 208 peripheries on bolt and external partition 207 of each squeezer 212 peripheries middle parts of installing in railway carriage or compartment 214, the tip of stretching into the bullet 256 in permeable control water railway carriage or compartment 206 of each squeezer 212 after installation, all with relative inboard partition 196 on the center of circle in water squeezing hole 201 face, be provided with staircase 216 in the bottom that the gangway 215 that arranges on railway carriage or compartment 214 is installed, be linked with several polings hole 217 at the suitable place that railway carriage or compartment 214 railway carriage or compartment walls are installed, the control cable of each squeezer 212 all links by the circuit of the relevant controlling electrical equipment in poling hole 217 and relative control cabin 32, the high pressure fuel pipe of each squeezer 212 through poling hole 217 after, all link with the relevant oil pipe of relative hydraulic efficiency equipment 25, there is the rear end of the pipe spreader 189 of bearing 190 to be provided with shaft seal 191 in rear triple cylinder 186 connection positions with in its of the lower back panel 188 center UNICOMs of the rear portion tail pipe 187 of the hook shellfish cylinder 149 of sleeve 150, pass backward the left side of the interior anticreep sister block 169 of cylinder of triple cylinder 168 front upper places, lower end with the left lacing grommet 220 of the pulling rod 219 that hooks the interior hook of shellfish cylinder 149 shellfishes 218 and left rope 222 that right lacing grommet 221 connects respectively and right rope 223, right pulley, coil 171 is led on a left side, coil 172 is led on the right side, the hole 177 of reeving, a left side, the hole 178 of reeving, the right side, left air cavity ring 179, right air cavity ring 180, the open-work 185 ' of upper spacer 185, two symmetrical inboard anticreep pulleys 184 below 3 centers, deck, two symmetrical outside anticreep pulleys 185, after revolving in the deck open-work 182 of 179 both sides, 17 tactile hook position, two-way single flight road and top two open-work grooves 183 thereof are drawn device 186, be connected with check cable 69 between the left lacing grommet 224 of left rope 222 and the right lacing grommet 225 of right rope 223, simultaneously left lacing grommet 224 and right lacing grommet 225 all can be flexibly link with the anti-drop hook 319 of making a concerted effort to join rope 69 ' two ends, be provided with bearing 190 in the pipe spreader 189 at tail pipe 187 lower back panel 188 middle parts, pipe spreader 189 rear ends are provided with shaft seal 191, after hook shellfish cylinder 149 after the front end warp beam sleeve pipe 189 of the drive link 230 that electrical motor 228 output shafts that arrange in outside, lower back panel rear portion connect by coupler 229 extend between triple cylinder 186 and triple cylinder 168 is interior, be linked with the propeller 231 with bracing strut 231 ', the circuit of each electric equipment on the output cable 233 of being drawn by transformer room 232 and front resistance bullet device 19 links.

By top described, the diversion equipment 38 of open sea aeroplane landing and accessory device is comprised of flume 235, hydraulic accumulator 236, pumping plant 237, water pipe 238, joint plate 239, front triple cylinder 240, rear triple cylinder 241, tail pipe 242, lower back panel 243, bar pipe 244, bearing 245 and shaft seal 246, it is characterized in that, the other end and the seawater with the flume 235 of the hydraulic accumulator 236 of pumping plant 237 of diversion equipment 38 link; The water pipe 238 of hydraulic accumulator 236 is arranged in the bottom section of the open sea aeroplane landing that is located in the land, island and accessory device, and has the sleeve 150 of hook shellfish cylinder 149 to connect mutually by in its of joint plate 239 and resistance bullet device 19 in it; At the rear portion of water pipe 238, be linked with respectively front triple cylinder 240, rear triple cylinder 241 and tail pipe 242; Be provided with bearing 245 in the bar pipe 244 at lower back panel 243 middle parts of tail pipe 242, bar pipe 244 rear ends are provided with shaft seal 246.

By top described, squeezer 212 on resistance bullet device 19 is comprised of electro-hydraulic drive device 247, expansion link 248, ring yoke plate 249, connecting pore 250, spring strut 251, cylinder base plate 252, spring 253, pressure spring plate 254, link rod 255 and bullet 256, it is characterized in that, expansion link 248 ends of the electro-hydraulic drive device 247 of squeezer 212 and the cylinder base plate 252 of spring strut 251 combine as a whole; Connect mutually one with the mounting hole 208 with rubber cushion 210, bolt 211 and connecting pore 209 around its on the ring yoke plate 249 of connecting pore 250 and permeable control water railway carriage or compartment 206 external partitions 207 on electro-hydraulic drive device 247 drum outer walls; After the expansion link 255 that the pressure spring plate 254 that touches with the front side pressure of spring 253 in spring strut 251 connects passed forward, the center of circle in the water squeezing hole 201 on the cone point of the bullet 256 of its end connection and the inboard partition 196 at 206 rear portions, permeable control water railway carriage or compartment faced; The cable poling of electro-hydraulic drive device 247 is linked by the circuit that the poling hole 217 of installing on the plate of railway carriage or compartment, railway carriage or compartment passed and caused the relevant relay in relative control cabin; After the high pressure fuel pipe of being drawn by electro-hydraulic drive device 247 and the oil return pipe poling hole 217 through railway carriage or compartment 214 is installed passes, the oil pipe relative with hydraulic efficiency equipment 25 links.

By top described, the hydrodynamic(al) air valve 205 of resistance bullet device 19 is comprised of spring strut 257, water inlet 258, spring 259, pressure spring plate 260, brace rod 261, pole perforating hole 262, slide valve sleeve 263, air inlet pipe 264, admission port 265, air extractor duct 266, guiding valve 267 and breather hole 268, it is characterized in that, the coolant outlet pipe that the side of the water inlet 258 of spring strut 257 ends of hydrodynamic(al) air valve 205 and resistance bullet device 19 expands on the compartment top plate of water railway carriage or compartment links; The brace rod 261 that the pressure spring plate 260 that pressure in spring strut 257 is touched spring 259 connects penetrates the guiding valve 267 that the interior also connecting belt of slide valve sleeve 263 has circular groove 268; The freeing pipe in the other end of the air inlet pipe 264 of admission port 265 UNICOMs on slide valve sleeve 263 barrels and high-pressure gas railway carriage or compartment links; Air extractor duct 266 on slide valve sleeve 263 barrels links with the air inlet pipe of resistance bullet device 19.

By top described, revolving on two-way single flight road 17 draws device 68 to be comprised of subbase 270, plate bracket 271, lateral shaft 272, bearing 273, roller 274, the hole 275 of reeving, load-bearing bearing 276, swivel mount 277, the hole 278 of reeving, anticreep pulley 279 and 280 of bracing strut seats, it is characterized in that, revolve in the open-work groove 65 above the deck open-work 64 that draws device 68 to be arranged on each 61 both sides, tactile hook position on deck 3, and its bottom is with the bottom connection one of subbase 270 with the open-work groove 65 in the hole 275 of reeving; Be provided with load-bearing bearing 276 above subbase 270 peripheries and between below swivel mount 277 peripheries; Several pressing plates that combine as a whole above with subbase 270 peripheral panels prop up all touching with pressing mutually above swivel mount 277 peripheries with the roller 274 of bearing 273 on 2471 inside lateral shafts 272; Revolve on the eccentric face with the swivel mount 277 in the hole 278 of reeving that draws device 68, be linked with the anticreep pulley 279 with bracing strut seat 280.

By top described, the fork rope device 79 of the tractor truck 78 on two-way single flight road 17 is comprised of two fork bodies 281, coupling spindle 282, middle part coupling spindle 283, electro-hydraulic drive device 284, first line of a couplet spindle 285, second line of a couplet spindle 286, two plate axis hole 287, pulley 288 and two plate axis hole 289, it is characterized in that, the coupling spindle 282 of two fork body 281 rear ends of fork rope device 79 combines as a whole with the front of tractor truck 78; Two plate axis holes 287 at each side front end place of two fork bodies 281 both sides all are equipped with pulley 288; The coupling spindle 282 that arranges on two fork bodies 281 branch junctions links with the second line of a couplet spindle 286 of electro-hydraulic drive device 284, and two plate axis holes 289 of the first line of a couplet spindle 285 of electro-hydraulic drive device 284 and its first line of a couplet spindle and tractor truck 78 fronts combine as a whole.

by top described, only rope device 71 on two-way single flight road 17 is by the saturating cylinder 290 in deck, electro-hydraulic drive device 291, expansion link 292, lifting body 293, take rope plate 294, flange 295, holder rope rank 296, sleeping hook rank groove 297 He Kao Hook plates 298 form, it is characterized in that, , stage 299, front guide frame 300, lower expansion net bar 301, rear guide frame 302, upper expansion is by electro-hydraulic drive device 573, expansion link 574, lifting body 575, convex body 576, holder rope rank 577, sleeping hook groove 578, Kao Hook wall 579 and deck be 250 compositions of cylinder thoroughly, it is characterized in that, only the electro-hydraulic drive device 291 of rope device 71 is arranged on two-way single flight road 17 and launches near position 70 deck thoroughly in cylinder 290, the front portion that on the expansion link 292 on electro-hydraulic drive device 291 tops, each of lifting body 293 left and right sides of client link is taken rope plate 294 all is linked with flange 295, two take and are provided with sleeping hook rank groove 297 between the rope plate.Plate 295 is equipped with the upper back and is provided with Kao Hook plate 298; Be provided with holder rope rank 577 below Kao Hook plate 298 front portions; Be provided with sleeping hook groove 578 on convex body 576 and Tuo Suo rank 577; Be provided with Kao Hook wall 579 in convex body 576 rear ends; The circuit of the relevant controlling device in the automatically controlled cable of electro-hydraulic drive device 291 and control cabin * links; The oil pipe that the high pressure fuel pipe of electro-hydraulic drive device 291 is relative with hydraulic efficiency equipment * links.

By top described, the expansion net arrangement 133 of block device 18 is expanded bar 306, is turned plate 307, two plate axis hole 309, gear 310, gear wheel shaft 311, link rod 312, crank 313, dull and stereotyped 314, wheel 315 and 316, hook ring outward and form by stage 299, front guide bracket 300, lower expansion net bar 301, rear saddle 302, upper expansion net bar 303, dovetail furrow 304, lifter rack 305, dovetail, it is characterized in that, two expansion net arrangements 133 are placed on respectively on the deck 85 of 17 left and right, two ends, two-way single flight road; In the front and back saddle 300 that the front portion of each expansion net arrangement 133 all arranges, the 302 interior dovetail furrows 304 that all arrange, the lifter rack 305 that expands bar with dovetail is installed; The upper side of the lower end side of the lifter rack 305 of front and the lifter rack 305 of back is linked with lower expansion net bar 301 and upper expansion net bar 303 by turning plate 307 outward respectively; Be arranged on two plate axis holes 309 between two saddles 300,302 with the gear 310 of sprocket drive spindle 311, link rod 312 and crank 313; Intracavity bottom in stage 299 is provided with wheel; Be linked with several flat boards 315 in front and back saddle 300,302 middle and upper parts.

By top described, joining rope 69 ' making a concerted effort on two-way single flight road 17 is comprised of cable 317, minute guy 318 and anti-drop hook 319, it is characterized in that, the anti-drop hook 319 that two each of making a concerted effort to join rope 69 ' make a concerted effort to join rope 69 ' front end links with the left lacing grommet 224 of the left rope 222 of 61 sides, front tactile hook position relative with it or the right lacing grommet 225 of right rope 223; Anti-drop hook 319 on minute guy 318 at middle part with relative with it in touch the left lacing grommet 224 of left rope 222 of 61 ' side, hook position or the right lacing grommet 225 of right rope 223 links; The anti-drop hook 319 of making a concerted effort to join rope 69 ' rear end links with the left lacing grommet 224 of the left rope 222 of 61 sides, rear tactile hook position relative with it or the right lacing grommet 225 of right rope 223; Minute guy 318 (convenient for making explanation, as to intend being illustrated as embodiment so that minute guy to be set) and the middle part of cable 317 combine as a whole; At the two ends of cable 317 and minute guy 318 ends all be connected with anti-drop hook 319; Article two, the specification of making a concerted effort to join rope 69 ' is identical, and each makes a concerted effort to join 1/3rd left and right that distance between two adjacent anti-drop hooks 319 of rope 69 ' is check cable 69 length.

By top described, the military technology of open sea aeroplane landing and accessory device equipment 014 is comprised of existing advanced relevant technologies equipment.

By top described, the weaponry 015 of open sea aeroplane landing and accessory device is comprised of existing advanced relevant weaponry.

Claims (7)

1. open sea aeroplane landing and accessory device are by pile 1, middle envelope 2, deck 3, stage 4, screw 5, joint plate 9, connection connecting pore 10, screw rod 11, nut slot 12, front long envelope 13, rear long envelope 14, air energy-storage device 15, setting-out power generation assembly 16, two-way single flight road 17, block device 18, resistance bullet device 19, photovoltaic power generation equipment 20, output cable 21, connect grillage 22, transformer room 23, output cable 24, hydraulic efficiency gear 25, oil railway carriage or compartment 26, oil pipeline 27, oil can 28, arsenal 29, transport channel 30, direct tower 31, control cabin 32, hangarage 33, elevator 34, railway carriage or compartment, depressed place 35, aerogenerator 36, typhoon protection device 37, diversion equipment 38, military technology equipment 39 and weaponry 40 form, it is characterized in that, when open sea aeroplane landing and accessory device are arranged in the marine site, be provided with front resistance bullet device 19 in it, middle resistance bullet device 19 ' and rear resistance bullet device 19 ", three resistance bullet devices 19,19 ' 19 " topside of triple cylinder 168 of (convenient for making explanation, as only to be illustrated for embodiment take three resistance bullet devices 19) be separately positioned on several in neritic zone pile 1 above or around islands and reefs in several middle envelope 2 inner chambers pile 1 above before, during and after the position, and make progress separately that right deck 3 is top to be located, be respectively equipped with front tactile hook position 61, in tactile hook position 61 ' and rear tactile hook position 61 ", three resistance bullet devices 19,19 ', 19 " its in the submarine site that is separately positioned on the bottom of front long envelope 13 and rear long envelope 14 and is arranged on long envelope 13,14 sides with the sleeve 150 that hooks shellfish cylinder 149, be arranged on three resistance bullet devices 19,19 ', 19 of the open sea aeroplane landing of land, island and accessory device " its in all be separately positioned in the water pipe 238 relative with it of diversion equipment 38 with the sleeve 150 of hook shellfish cylinder 149, be arranged on the middle envelope 2 in two-way single flight road 17 of land and front long envelope 13 and afterwards long envelope 14 combine as a whole, the bottom section of middle envelope 2 be positioned at underground three resistance bullet devices 19,19 ', 19 " the topside of triple cylinder 168 combine as a whole, be arranged on the stage 4 with the front end of several screws 5 of envelope 2 in open sea aeroplane landing in the marine site and accessory device, be connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of front long envelope 13 rear ends, and the stage 4 with several screws 5 of middle envelope 2 rear ends is connected as one with the gusset piece 9 with connecting pore 10, nut slot 12 and screw rod 11 of rear long envelope 14 front ends, the place, outer end that is separately positioned on foredeck 54 on front long envelope 13 and rear long envelope 14 and aft deck 55 is provided with block device 18, in takeoff and landing at sea and accessory device the appropriate location be provided with air energy-storage device 15, setting-out power generation assembly 16, transformer room 23, output cable 24, hydraulic efficiency gear 25, with the oily railway carriage or compartment 26 of oil pipeline 27 and oil can 28 and with the arsenal 29 of transport channel 30, being positioned at appropriate locations above the railway carriage or compartment, depressed place 35 of open sea aeroplane landing and accessory device both sides is provided with it with the direct tower 31 of control cabin 32 and is provided with military technology and equip 39 and weaponry 40, be provided with photovoltaic power generation equipment 20 and several aerogenerators 36 on connection grillage 22 on depressed place, railway carriage or compartment 35, the interior relevant electrical equipment in the output cable 21 of photovoltaic power generation equipment 20 and several aerogenerators 36 and transformer room 23 links, also be provided with air energy-storage device 15 and setting-out power generation assembly 16 in railway carriage or compartment, depressed place 35, each output cable of setting-out power generation assembly 16 all with transformer room 23 in relevant electrical equipment railway carriage or compartment connect.

2. according to claim 1, the two-way single flight road 17 of open sea aeroplane landing and accessory device is by foredeck 54, aft deck 55, deck 85 on block device 18, body 56 is expanded in the railway carriage or compartment, structural slab 57, end railway carriage or compartment 58, markings 59, marker lamp 60, tactile hook position 61, break slot 62, holder rope spring 63, deck open-work 64, open-work groove 65, inboard anticreep pulley 66, the perpendicular pulley 67 of outside anticreep, revolve and draw device 68, check cable 69, make a concerted effort to join rope 69 ', launch position 70, stop rope device 71, landing guiding device 72, weather cock 73, lift well 74, elevator 75, hangar 76, aircraft gate 77, tractor truck 78, fork rope device 79, reorganize and outfit chamber 80, cover plate 81, direct tower 82 and control cabin 83 form, it is characterized in that, the deck 54 in two-way single flight road 17, deck 3 and aft deck 55 are separately positioned on the front long envelope 13 that is arranged on open sea aeroplane landing and accessory device, above middle envelope 2 and rear long envelope 14, the railway carriage or compartment that deck 3 is arranged on resistance bullet device 19 expand body * above, be provided with the direct tower 201 that is provided with control cabin in it on deck 3, expand on the central deck 170 of bodies 171 with direct tower 201 opposite side railway carriage or compartments and be provided with several aircraft gates 196, in the middle of each tactile hook position 62 of three the tactile hook positions 62 that arrange at 3 middle parts, deck, the place is provided with the break slot 62 that all is placed with holder rope spring 63 in several its, only be respectively arranged with rope device 71 below inner place, position and both sides and reorganize and outfit chamber 80 launching of forward and backward deck 54,55 outer end places, below each tactile hook position 61 at 3 middle parts, deck and the deck 3 of both sides, tactile hook position below, be respectively arranged with two symmetrical inboard anticreep pulleys 66 and two perpendicular pulleys 67 of symmetrical outside anticreeps, be provided with to revolve in each the open-work groove 65 above deck open-work 64 that touches 61 both sides, hook position and draw device 68, above deck 85 on proostracum 54, deck 3 and aft deck 55 and block device 18, all be decorated with the markings 59 of runway longitudinal centerline and be provided with marker lamp 60 and be provided with landing guiding device 72, near the position that is provided with the close outer end on the deck 85 of stopping rope device 71 block devices 18 each is launching an inboard also is provided with launches position 70, and 17 outsides, two ends, two-way single flight road are provided with the device 18 of blocking simultaneously, the following triple cylinder * top structure grillage * on every side with hindering bullet device 19 that two-way single flight road 17 touches the deck 3 at 61 places, hook position is coupled as one, be provided with hangar 76 and elevator 75 in the end railway carriage or compartment 58 that all arranges in foredeck 54 and aft deck 55 both sides, outer end, the front of the tractor truck 78 that arranges on two-way single flight road 17 is provided with fork rope device 79.

3. according to claim 1, the block device 18 of open sea aeroplane landing and accessory device is by structure grillage 84, deck 85, gap 86, slide guide cylinder 87, gap 88, lifting column 89, cat net abduction rod 90, connection post plate 91, turn side plate 92, inserted link cylinder 92 ', horizontal anticreep pulley 93, pulley support 94, vertical anticreep sister block 95, pulley support 96, dragline pulley 96 ', post jamb permeable hole 97, post chamber 98, post jamb joint plate 98 ', electro-hydraulic drive device 99, expansion link 100, connection seat board 101, upper fixed wheel 103, lacing grommet 104, anticreep fixed pulley 105, shaft stool 106, block 107, selvage rope 108, anticreep pulley 109, foot piece 110, the hole 111 of reeving, it is rete cord 112, collection rope plate 113, dog hole 113 ', lacing grommet 113 ", lashing pulley 114, lock hook 114 ', hole enlargement cable 115, mobile pulley 116, hook shellfish cylinder 117, cylinder top board 118, the hole 119 of reeving, permeable hole 120, ring yoke plate 126, connecting pore 127, hook shellfish cylinder 128, lacing grommet 130, rope 131, noose ring 132 and expand net arrangement 133 and forms is characterized in that, the structure grillage 84 of device 18 both sides of blocking is the long envelope 13 below 17 two ends, two-way single flight road respectively, place, 14 outer end wall both sides is coupled as one, and all is linked with the lifting column 89 that all there is cat net abduction rod 90 its upper end on the expansion link 100 of the electro-hydraulic drive device 99 that all arranges with the bottom of the slide guide cylinder 87 of gap 88 of left and right, after the connection post plate 91 that combines as a whole with each lifting column 89 rear ends was passed backward by the gap 88 of slide guide cylinder 87 rear end, the outside of turning side plate 92 that its outside connects was respectively arranged with the horizontal anticreep pulley 93 of pulley support 94 with the vertical anticreep sister block 95 of pulley support 96, in each pile 1 inner chamber with post jamb permeable hole 97 of the left and right sides of the outermost end of left and right two several piles 1 of row below block device 18, be provided with the hook shellfish cylinder 117 with sleeve 121, and several of sleeve 121 outsides connect mutually with the ring yoke plate 126 of the connecting pore 127 post jamb joint plate 98 with pile 1, be respectively equipped with fixed wheel 103, lacing grommet 104 on the connection seat board 101 that arranges and with the anticreep fixed pulley 105 of shaft stool 106 on hook the cylinder top board 118 with the hole 119 of reeving of shellfish cylinder 117, selvage rope 108 covers that are arranged on block 107 dual-sides between both sides lifting column 89 rear portions have several all with the anticreep pulley 109 in foot piece 110 and the hole 111 of reeving, several anticreep pulleys 109 by be rete cord 112 with cord junction joint 113 on several all carry out flexagon ground with the lashing pulley 114 of lock hook 114 ' and connect, each lock hook 114 ' all with collection rope plate 113 on relative dog hole 113 ' phase structure connect, lacing grommet 113 with collection rope plate 113 " front end of the hole enlargement cable 115 that connects is connected with mobile anticreep pulley 116, the selvage rope that each that is separately positioned on both sides turns cat net abduction rod 90 front ends that all insert in the inserted link cylinder 92 ' that the inner top side of side plate 92 arranges and block 107 opposite side upper ends plugs, place, both sides on the deck 54,55 at 17 two ends, two-way single flight road is provided with respectively and expands net arrangement 133, but leaving its width between the front end of the rear end on the deck 85 that connects above with structure grillage 84 and relative foredeck 54 or aft deck 55 can pass block 107 not affect the gap 86 that wheel slides, the position 70 of launching of 85 longitudinal centerlines is provided with only rope device 71 on the deck.After the hole 119 of reeving in the upper end of the rope 131 that the lacing grommet 130 of the hook shellfish cylinder 128 of post chamber 98 interior settings connects through hooking 117 top boards 118 of shellfish cylinder, front portion, mobile pulley 116 rear portions and the upper fixed wheel 103 of cylinder top board 118 anticreep fixed pulleys, noose ring 132 and lacing grommet 104 that its end is made link.

4. the front resistance bullet device 19 of open sea aeroplane landing and accessory device according to claim 1, middle resistance bullet device 19 ' and rear resistance bullet device 19 " by air energy-storage device 15, setting-out power generation assembly 16, equipment railway carriage or compartment 146, compartment top plate 147, wear railway carriage or compartment cylinder 148, hook shellfish cylinder 149, sleeve 150, vertical joint plate 151, stomidium plate 152, pipe spreader 153, bearing frame 154, shaft seal 155, arc flap 157, packing seal 158, screw 159, screw rod 160, ring yoke plate 161, connecting pore 161 ', structure grillage 162, cylinder prosopyle 164, permeable hole 165, stop plate 166, spring 167, triple cylinder 168, anticreep sister block 169 in cylinder, conical baffle 170, coil 171 is led on a left side, coil 172 is led on the right side, flight 173, enlarging 174, drain hose 175, dividing plate 176, the hole 177 of reeving, a left side, the hole 178 of reeving, the right side, left air cavity ring 179, right air cavity ring 180, connect ring flat-plate 181, air inlet pipe 182, deflation hole 183, upper drain hose 184, epicone dividing plate 185, rear triple cylinder 186, tail pipe 187, lower back panel 188, pipe spreader 189, bearing 190, shaft seal 191, expansion water railway carriage or compartment, side 192, railway carriage or compartment base plate 193, permeable mouthful 194, open-work plate 195, inboard partition 196, permeable cylinder 197, flange 198, annular groove 199, seal ring 200, water squeezing hole 201, compartment top plate 202, water inlet 203, coolant outlet pipe 204, hydrodynamic(al) air valve 205, permeable control water railway carriage or compartment 206, external partition 207, mounting hole 208, connecting pore 209, rubber cushion 210, bolt 211, squeezer 212, UNICOM's cylinder 213, railway carriage or compartment 214 is installed, gangway 215, staircase 216, poling hole 217, hook shellfish 218, pulling rod 219, left lacing grommet 220, right lacing grommet 221, left rope 222, right rope 223, left lacing grommet 224, right lacing grommet 225, high-pressure water inlet cylinder 226, electro-hydraulic drive water valve 227, electrical motor 228, coupler 229, drive link 230, propeller 231, bracing strut 231 ', transformer room 232, output cable 233 and hydraulic efficiency equipment 234 form, and it is characterized in that front resistance bullet device 19, middle resistance bullet device 19 ' and rear resistance bullet device 19 " all with the hook shellfish cylinder 149 of sleeve 150 respectively upper, middle and lower be arranged on wearing in railway carriage or compartment water channel 148 that water pipe with diversion equipment 38 links, and the combining as a whole with the ring yoke plate 161 of connecting pore 161 ' the structure grillage 162 interior with wearing railway carriage or compartment water channel 148 of sleeve 150 vertically oppositely, front resistance bullet device 19 is arranged on the front portion below middle envelope 2, be provided with air energy-storage device 15 and setting-out power generation assembly 16 in the equipment railway carriage or compartment 146 of front resistance bullet device 19, on its anterior barrel of each resistance bullet device 19 with being linked with several between the hook shellfish cylinder 149 of several permeable holes 165 and sleeve 150 inwalls all with vertical joint plate 151 of open-work, hook shellfish cylinder 149 welds from beginning to end with some sections stainless steel cylinders or links with flange and forms, sleeve 150 all combines as a whole with structure grillage 162 with connecting pore 163 respectively by bolt with the ring yoke plate 161 of connecting pore 161 ' by several on its outer wall, be provided with in the front that hooks the baffle plate 166 that arranges on shellfish cylinder 149 rear inside wall the spring 167 made from corrosion-resistant steel, above the hook shellfish cylinder 149 of front resistance bullet device 19, the front upper place of the connection place of the triple cylinder 168 of UNICOM is provided with an interior anticreep sister block 169, being linked with on conical baffle 170 on triple cylinder 292 all has flight 173, all has the left side of enlarging 174 to lead coil 171 on it and coil 172 is led on the right side in it, outwards passed drain hose 175 on barrel on conical baffle 170, two lead be provided with above coil 171,172 two respectively with the above two 171,172 vertically opposite dividing plates 176 on hole 177 and the right side hole 178 of reeving of reeving, a left side, be respectively arranged with all on two holes 177,178 top left air cavity ring 179 and the right air cavity ring 180 that several deflation holes 183 is all arranged with connecting in its of ring flat-plate 181, link with the another end mouth of pipe of two air cavity rings 179,180 air inlet pipes that link 182 and the air extractor duct 266 of hydrodynamic(al) air valve 205 respectively, drain hose 184 on outwards having passed on barrel on dividing plate 176, having the side of some open-work plates 195 to expand permeable mouthful 194 of water railway carriage or compartment 192 railway carriage or compartment base plates 193 in the top of rear triple cylinder 186 nozzle and its above it links, expand on 192 inboard partitions 196 of water railway carriage or compartment in the side, be provided with the other end that several its nozzles are linked with the permeable cylinder 197 of blank flange 198 and pass inboard partition 196 and extend in permeable control water railway carriage or compartment 206, be provided with seal ring 200 in annular groove 199 on 198 of flanges of each permeable cylinder 197, also be provided with several water squeezings hole 201 on inboard partition 196, the other end mouth of pipe of the coolant outlet pipe 204 of UNICOM and the water inlet 258 of hydrodynamic(al) air valve 205 link on the compartment top plate 202 in expansion water railway carriage or compartment, side 192, each water inlet 203 on the railway carriage or compartment wallboard at expansion 192 rear portions, water railway carriage or compartment, side all is linked with the high-pressure water inlet cylinder 226 with electro-hydraulic drive water valve 227, each its periphery that arranges on the external partition 207 between the installation railway carriage or compartment 214 of permeable control water railway carriage or compartment 206 and its front has the mounting hole 208 of several connecting pores 209 and rubber cushion 210, link with the sleeve 150 that hooks shellfish cylinder 149 with the nozzle of the other end of UNICOM's cylinder 213 of permeable control water railway carriage or compartment 206 UNICOMs, be arranged on connecting mutually with the ring yoke plate 249 of connecting pore 250 several connecting pores 209 by mounting hole 208 peripheries on bolt and external partition 207 of each squeezer 212 peripheries middle parts of installing in railway carriage or compartment 214, the tip of stretching into the bullet 256 in permeable control water railway carriage or compartment 206 of each squeezer 212 after installation, all with relative inboard partition 196 on the center of circle in water squeezing hole 201 face, be provided with staircase 216 in the bottom that the gangway 215 that arranges on railway carriage or compartment 214 is installed, be linked with several polings hole 217 at the suitable place that railway carriage or compartment 214 railway carriage or compartment walls are installed, the control cable of each squeezer 212 all links by the circuit of the relevant controlling electrical equipment in poling hole 217 and relative control cabin 32, the high pressure fuel pipe of each squeezer 212 through poling hole 217 after, all link with the relevant oil pipe of relative hydraulic efficiency equipment 25, there is the rear end of the pipe spreader 189 of bearing 190 to be provided with shaft seal 191 in rear triple cylinder 186 connection positions with in its of the lower back panel 188 center UNICOMs of the rear portion tail pipe 187 of the hook shellfish cylinder 149 of sleeve 150, pass backward the left side of the interior anticreep sister block 169 of cylinder of triple cylinder 168 front upper places, lower end with the left lacing grommet 220 of the pulling rod 219 that hooks the interior hook of shellfish cylinder 149 shellfishes 218 and left rope 222 that right lacing grommet 221 connects respectively and right rope 223, right pulley, coil 171 is led on a left side, coil 172 is led on the right side, the hole 177 of reeving, a left side, the hole 178 of reeving, the right side, left air cavity ring 179, right air cavity ring 180, the open-work 185 ' of upper spacer 185, two symmetrical inboard anticreep pulleys 184 below 3 centers, deck, two symmetrical outside anticreep pulleys 185, after revolving in the deck open-work 182 of 179 both sides, 17 tactile hook position, two-way single flight road and top two open-work grooves 183 thereof are drawn device 186, be connected with check cable 69 between the left lacing grommet 224 of left rope 222 and the right lacing grommet 225 of right rope 223, simultaneously left lacing grommet 224 and right lacing grommet 225 all can be flexibly link with the anti-drop hook 319 of making a concerted effort to join rope 69 ' two ends, be provided with bearing 190 in the pipe spreader 189 at tail pipe 187 lower back panel 188 middle parts, pipe spreader 189 rear ends are provided with shaft seal 191, after hook shellfish cylinder 149 after the front end warp beam sleeve pipe 189 of the drive link 230 that electrical motor 228 output shafts that arrange in outside, lower back panel rear portion connect by coupler 229 extend between triple cylinder 186 and triple cylinder 168 is interior, be linked with the propeller 231 with bracing strut 231 ', the circuit of each electric equipment on the output cable 233 of being drawn by transformer room 232 and front resistance bullet device 19 links.

5. according to claim 2, the only rope device 71 in two-way single flight road 17 is by the saturating cylinder 290 in deck, electro-hydraulic drive device 291, expansion link 292, lifting body 293, take rope plate 294, flange 295, holder rope rank 296, sleeping hook rank groove 297 He Kao Hook plates 298 form, it is characterized in that, , stage 299, front guide frame 300, lower expansion net bar 301, rear guide frame 302, upper expansion is by electro-hydraulic drive device 573, expansion link 574, lifting body 575, convex body 576, holder rope rank 577, sleeping hook groove 578, Kao Hook wall 579 and deck be 250 compositions of cylinder thoroughly, it is characterized in that, only the electro-hydraulic drive device 291 of rope device 71 is arranged on two-way single flight road 17 and launches near position 70 deck thoroughly in cylinder 290, the front portion that on the expansion link 292 on electro-hydraulic drive device 291 tops, each of lifting body 293 left and right sides of client link is taken rope plate 294 all is linked with flange 295, two take and are provided with sleeping hook rank groove 297 between the rope plate.Plate 295 is equipped with the upper back and is provided with Kao Hook plate 298; Be provided with holder rope rank 577 below Kao Hook plate 298 front portions; Be provided with sleeping hook groove 578 on convex body 576 and Tuo Suo rank 577; Be provided with Kao Hook wall 579 in convex body 576 rear ends; The circuit of the relevant controlling device in the automatically controlled cable of electro-hydraulic drive device 291 and control cabin * links; The oil pipe that the high pressure fuel pipe of electro-hydraulic drive device 291 is relative with hydraulic efficiency equipment * links.

6. according to claim 2, joining rope 69 ' making a concerted effort on two-way single flight road 17 is comprised of cable 317, minute guy 318 and anti-drop hook 319, it is characterized in that, the anti-drop hook 319 that two each of making a concerted effort to join rope 69 ' make a concerted effort to join rope 69 ' front end links with the left lacing grommet 224 of the left rope 222 of 61 sides, front tactile hook position relative with it or the right lacing grommet 225 of right rope 223; Anti-drop hook 319 on minute guy 318 at middle part with relative with it in touch the left lacing grommet 224 of left rope 222 of 61 ' side, hook position or the right lacing grommet 225 of right rope 223 links; The anti-drop hook 319 of making a concerted effort to join rope 69 ' rear end links with the left lacing grommet 224 of the left rope 222 of 61 sides, rear tactile hook position relative with it or the right lacing grommet 225 of right rope 223; Minute guy 318 (convenient for making explanation, as to intend being illustrated as embodiment so that minute guy to be set) and the middle part of cable 317 combine as a whole; At the two ends of cable 317 and minute guy 318 ends all be connected with anti-drop hook 319; Article two, the specification of making a concerted effort to join rope 69 ' is identical, and each makes a concerted effort to join 1/3rd left and right that distance between two adjacent anti-drop hooks 319 of rope 69 ' is check cable 69 length.

7. according to claim 3, the expansion net arrangement 133 of block device 18 is expanded bar 306, is turned plate 307, two plate axis hole 309, gear 310, gear wheel shaft 311, link rod 312, crank 313, dull and stereotyped 314, wheel 315 and 316, hook ring outward and form by stage 299, front guide bracket 300, lower expansion net bar 301, rear saddle 302, upper expansion net bar 303, dovetail furrow 304, lifter rack 305, dovetail, it is characterized in that, two expansion net arrangements 133 are placed on respectively on the deck 85 of 17 left and right, two ends, two-way single flight road; In the front and back saddle 300 that the front portion of each expansion net arrangement 133 all arranges, the 302 interior dovetail furrows 304 that all arrange, the lifter rack 305 that expands bar with dovetail is installed; The upper side of the lower end side of the lifter rack 305 of front and the lifter rack 305 of back is linked with lower expansion net bar 301 and upper expansion net bar 303 by turning plate 307 outward respectively; Be arranged on two plate axis holes 309 between two saddles 300,302 with the gear 310 of sprocket drive spindle 311, link rod 312 and crank 313; Intracavity bottom in stage 299 is provided with wheel; Be linked with several flat boards 315 in front and back saddle 300,302 middle and upper parts.

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