CN1666927A - Aviation passenger accident-reducing method - Google Patents

Abstract

The invention relates the method reducing the accidents of the aero passengers. The structure of the invention comprises the outline structure, the weight reducing method, the constructions of the airport. The characteristics are: the invention adopts the starting off structure of the slope inertia resistance, which is simple and stable. The constructions adopt electricity prevention technology to avoid lightening and the earthquake caused by the abnormal current.

Description

The method that aviation passenger accident reduces

The present invention relates to the structure on aircraft and airport, this structure comprises the main surface structure of aircraft, the main surface structure of adrm, machinery weight alleviate method, the Architectural Equipment on airport.

The runway that existing adrm must be built the place on more flat level ground or airport in is more flat, thus be not used to devote every effort to help more greatly and take off because of flat, so because of flat not big (gradient) resistance prevention aircraft landing.

The noise of existing helicopter and vibrations are bigger, influence passenger's health.

The aircraft of the application number 0211960915 that I invent does not have the damping explanation on the pipe link of this engine and non-engine.

The damping of existing Aerodrome Construction (earthquake) effect is lower.

When existing over-water floats (comprising hydroairplane) need leave water surface maintenance, often need lifting, difficulty is bigger when lifting than weight (ship etc.).

Existing airport position is difficult for building on the mountain, waterborne, take up an area of more.

Existing carrier aircraft aircraft carrier (also a kind of at last seadrome) is a ship, cannot dispersed combination, and the difficulty of manufacturing is big.

Be difficult for close, combination between existing ship and the ship.

Existing mechanical bearing, various wheel, materials such as axle rod are in the place that does not influence result of use, and the no lightening hole of great majority makes the own wt of machinery big.

My purpose of invention is to reduce aviation passenger's fatal accident rate, therefore need alleviate aircraft weight, improves the ascending, descending condition of aircraft, improves airfield and facility.

My inventive embodiments: airstrip is had certain slope, it is descending (it is bigger to be used to power) that this gradient makes when taking off, during landing go up a slope (resistance is bigger), this gradient can 1 to 50 degree (and horizontal surface), but 5 to 30 degree better, this gradient be by 0 the degree (level road) progressively excessively to 30 to 50 the degree, progressively excessively spending by 30 to 50 degree to 0, the distance of slope change can 1000 to 6 kms, but it is better about 3 kms, also can be shaped on the tire runway on the runway on airport, this tire can be arranged 2 to 10 rows, but 3 to 5 rows better, the length distance of each tire can 01 meter to 10 meters, but 0.25 to 2 meter better.Can there be arc on the horizontal road surface of this runway, that is to say that the center on road is low, the roadside height, and the tire height on the runway is uneven, can be connected to moving on this tire; (as motor) by the control of power is helped take off or land, should have support, electrical motor of axle, bearing, bearing etc. on this tire.This runway mainly is adapt to not have wheel to take off and land, comprising hydroairplane, the adrm of this slope road airstrip is preferably built nature eminence (mountain) or artificial eminence (building in, roof), this aircraft landing runway also can be built in the shallow pool, the pond deeply generally can 0.5 to 3 meter, but it is better about 0.8 to 1.5 meter, basin bottom is a dry concrete, this pond is wide general 6 to 40 meters, but about 30 meters better, pond length can 50 to 500 meters, but it is better about 200 meters, should there be the slope in the pond when leading to anhydrous runway, this slope should be from 0 excessive to 10 to 30 degree progressively, by 30 degree progressively excessively to 0 degree (level land).This shallow pool runway adapts to the wheel aircraft landing, and with dark 4 to 35 meters of pond system, length 2 to 5 kms, this runway adapt to does not have wheel (comprising hydroairplane) aircraft lifting and landing.

The airport of this hydroairplane can be built in waterborne, this airport also is most economical, convenient, but the airport of quick travel, this airport can (be risen by control vessel, falling tone degree commander etc.), ferryboat, towboat, hang ship, dive and rise the ship composition, the pressurized air principle that available Submarine is managed in the lifting that being somebody's turn to do dives rise ship, but but at the top of this ship vee shape ditch, this vee shape ditch can be built in wide upward (side have been seen V word ditch) of ship, also can be on the length of ship (in the past, after seen V word ditch), this ditch has the fixedly purposes of over-water floats (ship or aircraft etc.), rise along with submarine, object (ship or aircraft) on the V word ditch on this ship can emerge, because the object that need float (ship etc.) is heavier, this submarine is difficult to be competent at, need be shaped on the bigger underwater ship of buoyancy, the air feed of this ship can be provided by water surface buoyancy tube, before this ship, after, a left side, right, on, under can be shaped on inflatable objects (balloon, pipe gas), water inlet by ship, draining, pressurized air, venting, inflation (to balloon etc.), air-breathing (by buoyancy gas etc.) can make ship that big buoyancy is arranged, the length of this underwater ship, widely can be shaped on V word ditch, utilize this ditch can stablize by floating thing, but underwater ship and quilt are floated ship lateral cross across, and a plurality of underwater ships can transversely arrangedly float big hull.

A kind of buoyancy aid waterborne airport, this airport is to be assembled by a plurality of ships, identical or inequality between each assembling shipyard, the size shape of ship can be decided according to the overall shape that will build the airport, but the shape side of these a plurality of ships, oblong, polygon, various circles, abnormity, the shape of each fabricated ship can have multiple as building blocks (a kind of toy), but kind is less best, combined method between this fabricated ship can be with bolt etc., a plurality of hull bottom are preferably flat, there is interconnected pipeline to interlink between ship and the ship, the water pump power system is arranged, by suction draining (the many outer directions of Xiang Shuizhong), reach the purpose of travelling in the overall airport of control, this stack-mounted hull can be made with cement concrete, also but metal is made, but the most handy cement concrete in the top of this ship (lid) is made, salable or foam is housed in the ship, balloon etc., it is engaged like that the unitized construction of this ship and ship also can be made into teeth (angle gear tooth), groove, also can be made into groove or dovetail furrow, by these grooves, use bolt after the interlock of teeth again, this bolt can also replace with rubber column, with rubber column by screw hole (hole that hull is shaped on), two of this post can be the sky body, also rubber column two can be shaped on the hole, pin with pin retaining and to fix rubber column, the plate of rubber is shaped on the hole, upright with same block of rubber plate to pasting aboard ship, in bolt, that is to say that rubber plate can connect the both sides ship by the ship limit, the connection that makes two ships or many ships is to flexibly connect, individual air-filled pore is arranged at the bottom of this ship, and this inflation inlet can be to the balloon inflation of hull bottom, utilizes this balloon can reconcile height between ship and the ship.

Can also connect with magnetic force between this fabricated ship; this has the ship limit of magnetic force ship that individual slope is preferably arranged, and this place, slope preferably is shaped on one deck rubber, and the magnetic force on slope is by electricity (electromagnet) control; can be according to the difference of existing ship side slope face; with matching of this slope system,, can make to attract mutually between two ships to connect by the effect of electromagnetism with existing ship; before this ship can be adsorbed on the ship that is adsorbed; the back, about, this ship has lifesaving, the purposes of recovering, and also can be used in the protection of important ships and light boats.

For the building that makes airport and airport has stronger antidetonation (earthquake) property, can have big pond about 5 meters below the constructure ground, each column of upright supports (the ground degree of depth can adopt prior art) in this reliable pond of building load-bearing all has the metal caput (electric conductivity is better) of a plurality of protrusions on the surface of pool portion, at pond and column, the lower curtate of pond enclosure wall also should have the metal bars (conduction) that protrude more, these metal bars can have with the concrete reinforcement in the building and are connected, the metal caput of this protrusion also is a kind of lightning protection ground wire, in a word, whole airport, or some important buildings are led to mutually, electric current passes through smoothly from all directions up and down, this also is a kind of earthquake-proof method, above-mentioned pond can not have yet, if but do not have, the metal of above-mentioned all directions metal club head body should have connection mutually, and electric current can pass through from all directions of reinforcing bar.

A kind of with two aircraft bonded assembly pipe links, the connection situation of this aircraft be one in the above, another below, top aircraft is an engine, the main cabin machine flight that this machine can play following, the main cabin machine can be unpowered, but the operation of can gliding, the available a plurality of Metallic rod of the connection of this two machine connect, vibration-proof structure (weak spring or hydraulic shock-absorption) is arranged in this bar, also available rope connects two machines two, this motor plane comprises helicopter, this rope comprises steel wire, rubber rope, chemical fibre, the composite material rope, the composite material rope, but connect the main cabin machine lifting rope one or more, can to the main cabin machine vibration absorbing usage be arranged because of the elasticity of this rope, the profile of this main cabin machine can be as the aircraft to have, also can look like flying saucer, flat-bottomed boat-shape, car shape, guided missile shape (long semicircular body), can make this that retractility is arranged rope scrolling (existing machine), spacing can be adjusted, reduce vibrations and noise as needs, that the spacing between two machines can be transferred is far away, there is a net this helicopter following, and this mesh-shaped and traditional net are basic identical, and different is that the net internal upper part is fixed with a solid circle, this circle can make net open, by making of net being opened or closing of lifting rope (stay cord), this net has the lifesaving purposes, and can there be air suctiton inlet at each passenger seat nearby in the machine of main cabin, this air suctiton inlet can pass through pipeline, through filtering bodies the fresh air outside the main cabin is drawn into the air suctiton inlet place, on this pipeline valve can be arranged, can have flat bowl-type to become recess in word air-breathing, mouth can be air-breathing near this place, and this air suction structure (pipe) is used in existing car, be feasible on the ship.

With the main load-bearing of aircraft or stressed support with flat, or the rectangular tube material is made, can lead between these many tubing, at Guan Shangke by the intake ﹠ exhaust valves door is arranged, in this pipe, add air, tubing can have the purposes of high pressure air bottle, because it is bigger to take off the power that into needs, the quick discharge of gas in when taking off, will managing to the rear of aircraft or below, this gas helps aircraft to be risen, this aircraft comprises hydroairplane (not having wheel) or land plane (wheel is arranged), if will in this pipe fuel oil be housed, this bolster extremely, the purposes that fuel tank also can be arranged, the structural principle of this skeleton pipe fuel tank can also be used in car, on the ship, preferably being shaped on normal temperature on civil aviaton's airliner has on case and low temperature fuel tank (5 degree are to subzero 30 degree) the low temperature fuel tank heat-insulation layer can be arranged, and normal temperature oil can be used for taking off, igniting usefulness, low temperature oil can be used for reducing the temperature of driving engine.

Can be in the tire of aircraft by radiator is arranged, this thermal source can be electro heat or air (hot air) heating, the source of hot air can be outer by several endothermic tubes are arranged with engine block, this pipeline is to tire cabin (place of dress aircraft wheel), can be on the pipeline by air pump is arranged, hot air can be discharged in the cabin by air pump, electro heat can be with electrical heating wire directly by on the hydraulic pressure draw-bar (skin) of tire, on the electric heater (heating wire) of this pull bar, preferably wrap one deck insulation fire retardant, should be to tire heating and the purpose that heats to pull bar, be the concentration that reduces hydraulic oil, improve the sensitieness of tyre hydraulic pull bar, reliability.

A kind of loss of weight operation of aircraft manufacturing mainly is to realize with boring, and the diameter in this hole generally can 1 to 10 millimeter, but 1.5 to 3.5 millimeters better because the more possible loss of weight problem out in the cold of less area often.Distance between hole and the hole can 1 to 10 millimeter (in the place that needs loss of weight), but it is better between 2 to 6 millimeters, this needs the parts of loss of weight to comprise the mechanics of aircraft, structure facility part, mechanics comprises bearing, axostylus axostyle, the various wheel, motor etc., the structure facility comprises sheet material etc., one cover bearing in use, what have needs fixed jacket, cover (not rotating) in the needs that have are fixing, total some load-bearing or stressed many of overcoat and interior cover, and another part load-bearing or stressed few (friction force), with this load-bearing or stressed few in, put outward and be shaped on the hole, this hole can be through hole or non through hole, a hundred per cent of hole overcoat area in the area (this area is meant that porose place also comprises the limit between hole and the hole) of branch of interior overcoat institute can account for, but percentage 10 to 40 is better, there is the purposes to bearing oiling (oilhole) in this hole, the hole in piece part that the straight shape drill bit that diameter is little is difficult for getting into, can utilize the bending drill bit that bores tooth as medical-dental, the less hole of hole drill if desired, can use laser drill, the end face of the solid retainer in the bearing, radially, horizontal and all can hole, above-mentioned bearing part in addition all can be holed under the situation that does not influence result of use, and this boring method also can be used in other the wheel shape mechanical component, as gear, moving state or non-power conduction wheel etc.

When various axostylus axostyles are pressed various bearings or wheel at cover, preferably be shaped on lightening hole by the wheel place, because the protection of wheel is arranged; so wheel place comparatively robust of this axostylus axostyle; the boring loss of weight can not influence the use of axostylus axostyle, and this loss of weight structure also can be used on the sheet material, with board fiber board; five-ply board; cardboard is shaped on porous on the metal sheet, stick with glue, gluing nail; spot welding (electric welding a kind of), method with the plate of two atresias be fixed on the following of this perforated plate and above.Can alleviate the weight of sheet material like this, above-mentioned loss of weight operation also is adapted in the production of other machinery and building materials.

Advantage of the present invention is: this invention is adopted the gradient to be used to devote every effort to help and is taken off structure, this is simple in structure, the reliable and stable safety of principle, be difficult for et out of order, this structure is particularly useful for less area, level land, this adrm can be built on the mountain, reduce cost, this building adopts electricity-preventing technique, but the anti-thunder and lightning of actv. is prevented the earthquake that causes because of current anomaly, the reason that earthquake takes place is disputable, it will be argued that earthquake is mobile because of storing of underground current, strong and weak antagonism causes, this builds the conducting metal that horizontal vertical direction is arranged in underground 5 meters, can be with the electric current in 5 meters of the surface seismic smoothly by the destruction that do not have a resistance, this seadrome not only can be saved the soil, but also can make aircraft remove tire, reduce aircraft weight, save the tire fault that the energy thoroughly solves aircraft, the latent ship that rises of this invention, this ship has will have breakdown plane and ship to float off the purposes of the water surface fast.

This aircraft can be built aboard ship, can set up a big adrm with many ships, this ship also can be shaped on the magnetic ship, this has peculiar to vessel the recovering on the water of suction also is feasible, the seismaesthesia of helicopter and noise are influential to passenger's health, but this hanging main cabin actv. addresses this problem, visiting on the hanging main cabin has aspirate tube, outer air can be sucked human body, this aspirate tube structure also can be used on car, on the vehicle such as ship, main frame structure on the aircraft can be made of tubing, this pipe can be worked as fuel tank and be used, when taking off, the high pressure air in this pipe helps the purposes of taking off, and the cabin of this aircraft and physical construction can be shaped on porous, this hole can alleviate aircraft weight about 5 percent, but this loss of weight bearing and loss of weight axostylus axostyle be expendable weight not only, also can prolong their service life, this drilling weight losing method also can be used on the sheet material, and this loss of weight bearing also can be used in other the machinery (comprising other vehicle).

Contrast description of drawings: Fig. 1, be the birds-eye view of airstrip, number in the figure is illustrated: runway (1), tire (2), tire axle (3) landing airdrome length omits setting-out.(4), the wide part of this runway can have arc, and the centre, road should be hanged down, both sides, road height, and this tire (2) can be arranged two at this runway and drain into 10 rows; This multi-row figure does not draw in the drawings, and the support (seat) of tire axle (3) does not draw in the drawings yet, available loss of weight bearing (bearing outside has the loss of weight through hole) on this tire axle.Fig. 2 is a damping helicopter front view, number in the figure is illustrated: aircraft body (5) the machine lifting rope (6) that stretches, pulling force bumper (7), hanging passenger plane body (flying saucer shape) (8), body window (9), this motor plane is not limited to helicopter, the aircraft that also comprises other kind, preferably a little bit smaller (can carry one to 2 chaufeur) of system of this helicopter, the details in helicopter and main cabin does not draw in the drawings, can adopt weight-reducing material on this passenger plane, Fig. 3 is the cutaway drawing of existing undercarriage hydraulic pressure draw-bar, figure grade is illustrated: pull bar body (10), the horizontal end face of electrical heating wire (11), trombone slide length is omitted line (12), this electrical heating wire can keep the temperature (3 to 50 degree) of hydraulic pressure draw-bar, helps the maintenance sensitivity of hydraulic pressure draw-bar, makes the property retention of undercarriage stable, the cloth of bag electrical heating wire does not draw among this figure, Fig. 4 is the transverse sectional view of underwater ship, and number in the figure is illustrated: hard tube admission port (13), light proportion buoyancy aid (14), spirally flexible pipe (15), air compression (16), these (16) can have a plurality of, and admission port (13) buoyancy aid (14) spirally flexible pipe (15) also can have a plurality of, inflation software (17), this software also has 5 in the drawings.Vee shape ship top (18), air inlet, gas exhaust duct (19), this pipeline can be to soft buoyancy aid (balloon) inflation, and the most handy jet, the water-bound of the power of this ship does not draw in the accompanying drawings.This ship will slip into the below of over-water floats, and the function that the helpful over-water floats of this ship emerges also has the function of salvaging a sunken ship.Fig. 5 is the transverse sectional view of ambulance ship; number in the figure is illustrated: hull (20); domatic (21), the best and existing ship side slope of this domatic gradient face matches, and just this ship is domatic leans against on the hull that has ship; this ship is domatic preferably to be magnetic; existing ship is inhaled mutually with this ship, and a plurality of these ambulance ships can protect existing ship not sink, and are difficult for being hit by submarine mine; help the stability of existing ship, help water survival.Hull bottom (22), this hull bottom (22) also can be W fonts etc.Fig. 6 is that seadrome buoyancy aid symmetry is cutd open figure, number in the figure is illustrated: buoyancy aid mouth (23), the available multiple material of the lid of this mouthful, buoyancy aid (24), making such as this buoyancy aid (24) and buoyancy aid lid available metal, concrete product, connecting bore (25) can fuse a plurality of buoyancy aids by this hole (25) with bolt etc., make airport dimensions, there is downward gas filed purposes hull bottom hole (26), this hole, inflation downwards, can be to the balloon inflation under the hull bottom, this balloon does not draw in the drawings.Can adorn air in this hull, also can adorn plastic foam, the object that proportions such as rubber balloon are lighter, is the airport pavement slope map at Fig. 7,8,9, and Fig. 7 is the domatic figure in airport, picture guyot; Fig. 8 is the domatic figure in pond; Fig. 9 is domatic airstrip figure; To illustration: airport, guyot (27), say on guyot and can have various airport facilities; Do not draw among the figure, domatic airstrip (28), pond length is omitted line (29); At the bottom of the pond (30), the water surface (31), water-bed slope (32), ramp (33), level line (34), dark general about 1.5 meters of this pond, can drop to hydraulic accumulator earlier during aircraft landing, so enter ramp (33), enter the airport sailing level road (34) into by in the pond, running stretch (20 to 200 meters), take off level road (35), the clivia road (36) of taking off, big slope (37), the level road that takes off (38), this highway section helps taking off, if but to be used in also be feasible on the aircraft landing.Figure 10 is the aspirate tube figure of passenger plane, and this figure is a birds-eye view, and number in the figure is illustrated: external admission mouth (39), press valve outer (40), press filtered air thing (41), air suctiton inlet (42), description of operation: outside external admission mouth (39) is connected on, this mouth can be evened up preferably outward, also can protrude a bit, everyone seat that air suctiton inlet is connected on the main cabin by pipeline nearby, when outside when good air is arranged, open valve, can be with fresh air conveying out of my cabin to each passenger (air suctiton inlet) nearby.In order to reduce the resistance of flight, suitably reduce the main cabin volume, also to make full use of the space in the visitor.Reduce the air quality problems of utilizing space (overloading visitor) to bring, this air air suction structure helps addressing this problem, and this structure is used on existing other vehicle, also is feasible.Figure 11 is the section plan at underground 5 meters of anti-earthquake airport building, number in the figure is illustrated: cement concrete, pond body of wall (43), pass body of wall steel bar end (44), building bearing column (45), pass column steel bar end (46), vertical upright to bar cross section (47), the pond is upright to bar cross section steel bar end (48), upright in the pond to bar cross section (49), at the bottom of the pond (50), building outside (51), the electric current during this underground earthquake laterally (a plurality of direction) are upright to the ground by building smoothly.Figure 12 is the plane symmetry cutaway view of bearing outside, number in the figure is illustrated: the diameter through hole on the lasso (52), lasso the first half (53), small diameter bore on the lasso (54), rolling body raceway (55), non through hole (56), the latter half of lasso (57), generally the overcoat of bearing is fixed on that (as motor) needs fixed jacket by the time on the bearing support, this overcoat is motionless, at this moment the load-bearing of overcoat mainly is half (the latter half) of overcoat, and this part preferably is shaped on non through hole (56), the supporting part of second half (the first half) can be shaped on through hole (52), the degree of depth in above-mentioned this hole, diameter can have multiple, Figure 13 is the symmetrical cutaway view of interior cover of bearing, figure grade is illustrated: non-heavy the holding of interior cover (the first half) be (58) partly, interior cover non through hole (59), cover non through hole (60) in a plurality of, interior cover load-bearing (the latter half) part large diameter hole (61), interior cover rolls ditch (62), a plurality of through holes (63), minor diameter through hole (64), interior cover non-bearing (the first half) is (65) partly, and cover through hole can be used on the mechanical axis of fixing interior cover in this, as axletree, this axle does not rotate at machinery (on the car), rotates by the bearing on the axle and rotates (as unpowered axletree), and the first half of the bearing inner sleeve on the axle just is the non-bearing part.Figure 14 is the retainer section plan in the bearing; Figure grade is illustrated: outside hole, the footpath of retainer (66), this hole can have a plurality ofly only draws one in the drawings.Keep support body (67), cross-drilled hole (68) radially, radial bore (69), this hole can have a plurality of, only draws one among the figure, end face cross-drilled hole (70), this hole also can have a plurality of, small end face (71), the degree of depth in above-mentioned hole, diameter is identical, or inequality.Figure 15 is the front view of mechanical wheel figure, number in the figure is illustrated: the external diameter of wheel rim (72), this external diameter can have teeth on (72), and this is taken turns can be gear, and the external diameter of this wheel rim can have belt tunnel on (72), but this is taken turns also belt pulley etc., can be other mechanical runner, but the structure on the external diameter not be drawn in the drawings yet, wheel end face aperture (73), wheel semiaxis hole (74), wheel end face macropore; This can have many people, also can have multiplely, and there is the purposes that alleviates runner weight in this hole, web (76).Figure 16 is the symmetrical cutaway view of axostylus axostyle, and figure grade is illustrated: axis body (77), the hole of locating by bearing (also can be other mechanical runner) (78) of axle, deep hole (79), the above-mentioned hole of small diameter bore (80) can have a plurality of, size but inequality.Press the protruding axle place of arbor wheel (81).Figure 17, the 18th, weight-reducing material, sheet material figure, Figure 17 is a birds-eye view, Figure 18 is Figure 17 A-A cutaway drawing, figure grade is illustrated: plate hollow hole (82), this hole can process with boring bar tool, also makes of other technology, upper decorative (83), but this plate aluminium sheet, plank, plastic flagstone etc., porous plate body (84), this plate body can be used timber, composite material, board fiber board, cardboard, aluminium sheet is waited until metallic material, below dull and stereotyped (85), the also available multiple material of this plate, up and down surface plate and porous plate body be connected and fixed can go up gluing, the nail nail, spot welding with electric drill boring, is adorned glue on the hole, use little wood, plastics, cylinder inserts this, and also the hole is gluing fixing, this plastic cylinder head can have a flat sand of picture flat head screw, if metal also is feasible with spot welded method.

Claims (10)

1, the present invention relates to the structure on aircraft and airport, this structure comprises the main surface structure of aircraft, the main surface structure of adrm, machinery weight alleviate method, the Architectural Equipment on airport, it is characterized in that: airstrip is had certain slope, it is descending (it is bigger to be used to power) that this gradient makes when taking off, be to go up a slope (resistance is bigger) during landing, this gradient can 1 to 50 degree (and horizontal surface), but 5 to 30 degree better, this gradient be by 0 the degree (level road) progressively excessively to 30 to 50 the degree, by 30 to 50 degree progressively excessively to 0 degree, the distance of slope change can 1000 to 6 kms, but better, on the runway on airport, also can be shaped on the tire runway about 3 kms, this tire can be arranged 2 to 10 rows, but 3 to 5 rows are better, and the length distance of each tire can 01 meter to 10 meters, but 0.25 to 2 meter better.Can there be arc on the horizontal road surface of this runway, that is to say that the center on road is low, the roadside height, and the tire height on the runway is uneven, can be connected to moving on this tire; (as motor) by the control of power is helped take off or land, should have support, electrical motor of axle, bearing, bearing etc. on this tire.This runway mainly is adapt to not have wheel to take off and land, comprising hydroairplane, the adrm of this slope road airstrip is preferably built nature eminence (mountain) or artificial eminence (building in, roof), this aircraft landing runway also can be built in the shallow pool, the pond deeply generally can 0.5 to 3 meter, but it is better about 0.8 to 1.5 meter, basin bottom is a dry concrete, this pond is wide general 6 to 40 meters, but about 30 meters better, pond length can 50 to 500 meters, but it is better about 200 meters, should there be the slope in the pond when leading to anhydrous runway, this slope should be from 0 excessive to 10 to 30 degree progressively, by 30 degree progressively excessively to 0 degree (level land).This shallow pool runway adapts to the wheel aircraft landing, and with dark 4 to 35 meters of pond system, length 2 to 5 kms, this runway adapt to does not have wheel (comprising hydroairplane) aircraft lifting and landing.

2, the airport according to claim 1 is characterized in that; The airport of this hydroairplane can be built in waterborne, this airport also is most economical, convenient, but the airport of quick travel, this airport can (be risen by control vessel, falling tone degree commander etc.), ferryboat, towboat, hang ship, dive and rise the ship composition, the pressurized air principle that available Submarine is managed in the lifting that being somebody's turn to do dives rise ship, but but at the top of this ship vee shape ditch, this vee shape ditch can be built in wide upward (side have been seen V word ditch) of ship, also can be on the length of ship (in the past, after seen V word ditch), this ditch has the fixedly purposes of over-water floats (ship or aircraft etc.), rise along with submarine, object (ship or aircraft) on the V word ditch on this ship can emerge, because the object that need float (ship etc.) is heavier, this submarine is difficult to be competent at, need be shaped on the bigger underwater ship of buoyancy, the air feed of this ship can be provided by water surface buoyancy tube, before this ship, after, a left side, right, on, under can be shaped on inflatable objects (balloon, pipe gas), water inlet by ship, draining, pressurized air, venting, inflation (to balloon etc.), air-breathing (by buoyancy gas etc.) can make ship that big buoyancy is arranged, the length of this underwater ship, widely can be shaped on V word ditch, utilize this ditch can stablize by floating thing, but underwater ship and quilt are floated ship lateral cross across, and a plurality of underwater ships can transversely arrangedly float big hull.

3, the airport according to claim 1 is characterized in that; A kind of buoyancy aid waterborne airport, this airport is to be assembled by a plurality of ships, identical or inequality between each assembling shipyard, the size shape of ship can be decided according to the overall shape that will build the airport, but the shape side of these a plurality of ships, oblong, polygon, various circles, abnormity, the shape of each fabricated ship can have multiple as building blocks (a kind of toy), but kind is less best, combined method between this fabricated ship can be with bolt etc., a plurality of hull bottom are preferably flat, there is interconnected pipeline to interlink between ship and the ship, the water pump power system is arranged, by suction draining (the many outer directions of Xiang Shuizhong), reach the purpose of travelling in the overall airport of control, this stack-mounted hull can be made with cement concrete, also but metal is made, but the most handy cement concrete in the top of this ship (lid) is made, salable or foam is housed in the ship, balloon etc., it is engaged like that the unitized construction of this ship and ship also can be made into teeth (angle gear tooth), groove, also can be made into groove or dovetail furrow, by these grooves, use bolt after the interlock of teeth again, this bolt can also replace with rubber column, with rubber column by screw hole (hole that hull is shaped on), two of this post can be the sky body, also rubber column two can be shaped on the hole, pin with pin retaining and to fix rubber column, the plate of rubber is shaped on the hole, upright with same block of rubber plate to pasting aboard ship, in bolt, that is to say that rubber plate can connect the both sides ship by the ship limit, the connection that makes two ships or many ships is to flexibly connect, individual air-filled pore is arranged at the bottom of this ship, and this inflation inlet can be to the balloon inflation of hull bottom, utilizes this balloon can reconcile height between ship and the ship.

4, the airport according to claim 1 is characterized in that; Can also connect with magnetic force between this fabricated ship; this has the ship limit of magnetic force ship that individual slope is preferably arranged, and this place, slope preferably is shaped on one deck rubber, and the magnetic force on slope is by electricity (electromagnet) control; the difference that ship side slope face can be arranged according to oneself; with this slope system have ship to match with oneself, by the effect of electromagnetism, can make between two ships to attract mutually to connect; before this ship can be adsorbed on the ship that is adsorbed; the back, about, this ship has lifesaving, the purposes of recovering, and also can be used in the protection of important ships and light boats.

5, the airport according to claim 1 is characterized in that; For the building that makes airport and airport has stronger antidetonation (earthquake) property, can have big pond about 5 meters below the constructure ground, each column of upright supports (the ground degree of depth can adopt prior art) in this reliable pond of building load-bearing all has the metal caput (electric conductivity is better) of a plurality of protrusions on the surface of pool portion, at pond and column, the lower curtate of pond enclosure wall also should have the metal bars (conduction) that protrude more, these metal bars can have with the concrete reinforcement in the building and are connected, the metal caput of this protrusion also is a kind of lightning protection ground wire, in a word, whole airport, or some important buildings are led to mutually, electric current passes through smoothly from all directions up and down, this also is a kind of earthquake-proof method, above-mentioned pond can not have yet, if but do not have, the metal of above-mentioned all directions metal club head body should have connection mutually, and electric current can pass through from all directions of reinforcing bar.

6, the aircraft according to claim 1 is characterized in that; A kind of with two aircraft bonded assembly pipe links, the connection situation of this aircraft be one in the above, another below, top aircraft is an engine, the main cabin machine flight that this machine can play following, the main cabin machine can be unpowered, but the operation of can gliding, the available a plurality of Metallic rod of the connection of this two machine connect, vibration-proof structure (weak spring or hydraulic shock-absorption) is arranged in this bar, also available rope connects two machines two, this motor plane comprises helicopter, this rope comprises steel wire, rubber rope, chemical fibre, the composite material rope, the composite material rope, but connect the main cabin machine lifting rope one or more, can to the main cabin machine vibration absorbing usage be arranged because of the elasticity of this rope, the profile of this main cabin machine can be as the aircraft to have, also can look like flying saucer, flat-bottomed boat-shape, car shape, guided missile shape (long semicircular body), can make this that retractility is arranged rope scrolling (existing machine), spacing can be adjusted, reduce vibrations and noise as needs, that the spacing between two machines can be transferred is far away, there is a net this helicopter following, and this mesh-shaped and traditional net are basic identical, and different is that the net internal upper part is fixed with a solid circle, this circle can make net open, by making of net being opened or closing of lifting rope (stay cord), this net has the lifesaving purposes, and can there be air suctiton inlet at each passenger seat nearby in the machine of main cabin, this air suctiton inlet can pass through pipeline, through filtering bodies the fresh air outside the main cabin is drawn into the air suctiton inlet place, on this pipeline valve can be arranged, can have flat bowl-type to become recess in word air-breathing, mouth can be air-breathing near this place, and this air suction structure (pipe) is used in the car that oneself has, be feasible on the ship.

7, the aircraft according to claim 1 is characterized in that; With the main load-bearing of aircraft or stressed support with flat, or the rectangular tube material is made, can lead between these many tubing, at Guan Shangke by the intake ﹠ exhaust valves door is arranged, in this pipe, add air, tubing can have the purposes of high pressure air bottle, because it is bigger to take off the power that into needs, the quick discharge of gas in when taking off, will managing to the rear of aircraft or below, this gas helps aircraft to be risen, this aircraft comprises hydroairplane (not having wheel) or land plane (wheel is arranged), if will in this pipe fuel oil be housed, this bolster extremely, the purposes that fuel tank also can be arranged, the structural principle of this skeleton pipe fuel tank can also be used in car, on the ship, preferably being shaped on normal temperature on civil aviaton's airliner has on case and low temperature fuel tank (5 degree are to subzero 30 degree) the low temperature fuel tank heat-insulation layer can be arranged, and normal temperature oil can be used for taking off, igniting usefulness, low temperature oil can be used for reducing the temperature of driving engine.

8, the aircraft according to claim 1 is characterized in that; Can be in the tire of aircraft by radiator is arranged, this thermal source can be electro heat or air (hot air) heating, the source of hot air can be outer by several endothermic tubes are arranged with engine block, this pipeline is to tire cabin (place of dress aircraft wheel), can be on the pipeline by air pump is arranged, hot air can be discharged in the cabin by air pump, electro heat can be with electrical heating wire directly by on the hydraulic pressure draw-bar (skin) of tire, on the electric heater (heating wire) of this pull bar, preferably wrap one deck insulation fire retardant, should be to tire heating and the purpose that heats to pull bar, be the concentration that reduces hydraulic oil, improve the sensitieness of tyre hydraulic pull bar, reliability.

9, the aircraft according to claim 1 is characterized in that; A kind of loss of weight operation of aircraft manufacturing mainly is to realize with boring, and the diameter in this hole generally can 1 to 10 millimeter, but 1.5 to 3.5 millimeters better because the more possible loss of weight problem out in the cold of less area often.Distance between hole and the hole can 1 to 10 millimeter (in the place that needs loss of weight), but it is better between 2 to 6 millimeters, this needs the parts of loss of weight to comprise the mechanics of aircraft, structure facility part, mechanics comprises bearing, axostylus axostyle, the various wheel, motor etc., the structure facility comprises sheet material etc., one cover bearing in use, what have needs fixed jacket, cover (not rotating) in the needs that have are fixing, total some load-bearing or stressed many of overcoat and interior cover, and another part load-bearing or stressed few (friction force), with this load-bearing or stressed few in, put outward and be shaped on the hole, this hole can be through hole or non through hole, a hundred per cent of hole overcoat area in the area (this area is meant that porose place also comprises the limit between hole and the hole) of branch of interior overcoat institute can account for, but percentage 10 to 40 is better, there is the purposes to bearing oiling (oilhole) in this hole, the hole in piece part that the straight shape drill bit that diameter is little is difficult for getting into, can utilize the bending drill bit that bores tooth as medical-dental, the less hole of hole drill if desired, can use laser drill, the end face of the solid retainer in the bearing, radially, horizontal and all can hole, above-mentioned bearing part in addition all can be holed under the situation that does not influence result of use, and this boring method also can be used in other the wheel shape mechanical component, as gear, moving state or non-power conduction wheel etc.

10, the aircraft according to claim 1 is characterized in that; When various axostylus axostyles are pressed various bearings or wheel at cover, preferably be shaped on lightening hole by the wheel place, because the protection of wheel is arranged; so wheel place comparatively robust of this axostylus axostyle; the boring loss of weight can not influence the use of axostylus axostyle, and this loss of weight structure also can be used on the sheet material, with board fiber board; five-ply board; cardboard is shaped on porous on the metal sheet, stick with glue, gluing nail; spot welding (electric welding a kind of), method with the plate of two atresias be fixed on the following of this perforated plate and above.Can alleviate the weight of sheet material like this, above-mentioned loss of weight operation also is adapted in the production of other machinery and building materials.

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