CN100545038C

CN100545038C - Mountaintop transmitting aerodrome

Info

Publication number: CN100545038C
Application number: CNB2007100713066A
Authority: CN
Inventors: 黄金伦
Original assignee: Individual
Current assignee: Individual
Priority date: 2007-09-12
Filing date: 2007-09-12
Publication date: 2009-09-30
Anticipated expiration: 2027-09-12
Also published as: CN101234674A

Abstract

A kind of Mountaintop transmitting aerodrome, comprise that superconduction scolds floating type magnetic suspension car launcher, respective track, boarding place, aircraft passage and high building elevator, overline bridge, waste water storehouse, weight hammer type water pot and the mountain top lake (A, B) of passenger from the foot of the hill rising to boarding place, floating type magnetic levitation device is scolded in the cover superconduction that each side is provided with of car launcher, and double double supporting wheel each side is set and W type joist is respectively arranged, coupling T type beam has self adaptive even load support performance; The passenger is from the foot of the hill being elevated to the airport, mountain top, be that the water that utilizes the waste water storehouse is controlled the discharging corresponding water amount by computer and entered water pot by the total weight that enters the elevator personnel, water pot is descended, spur the elevator in cable wire and the high building, send the passenger to arrive overline bridge, directly enter the cabin.The aircraft that saves alighting gear is energy-conservation from heavy and light, and hill top takeoff has ceiling advantage, again because send aircraft with the magnetic suspension car launcher, highlights energy-saving and emission-reduction consumption reduction and efficient.

Description

Mountaintop transmitting aerodrome

Technical field

The present invention relates to a kind of Mountaintop transmitting aerodrome, be suitable for saving the large-scale airliner of alighting gear, use superconduction and scold floating type magnetic suspension car launcher, carrying out high efficiency launch plane on the original base of mountain top construction takes off, not only highlight energy-saving and emission-reduction but also make full use of the height on mountain, the characteristics that the mountain is how few, in friendly environment, sustainable development is useful.

Background technology

Existing airport need take large-area level land; The landing of aircraft needs alighting gear, increases the weight of aircraft.

Summary of the invention

The object of the present invention is to provide a kind of Mountaintop transmitting aerodrome, the airport that exists with the solution prior art need take large-area level land; The landing of aircraft needs alighting gear, increases the problem of the weight of aircraft.

Technical scheme of the present invention is: comprise that superconduction scolds floating type magnetic suspension car launcher, respective track, boarding place, aircraft passage and high building elevator, overline bridge, waste water storehouse, weight hammer type water pot and mountain top lake A and the B of passenger from the foot of the hill rising to boarding place, floating type magnetic levitation device is scolded in the cover superconduction that each side is provided with of car launcher, and double double supporting wheel each side is set and W type joist is respectively arranged, coupling T type beam has self adaptive even load support performance; The passenger is from the foot of the hill being elevated to the airport, mountain top, be that the water that utilizes the waste water storehouse is controlled the discharging corresponding water amount by computer and entered water pot by the total weight that enters the elevator personnel, water pot is descended, spur the elevator in cable wire and the high building, send the passenger to arrive overline bridge, directly enter the cabin.

Advantage of the present invention is: the aircraft that 1. saves alighting gear has the remarkable economical effect, and has more ceiling advantage at hill top takeoff from heavy and light, especially sends with the magnetic suspension car launcher and takes off, and highlights energy-saving and emission-reduction, consumption reduction and efficient; 2. possess the high mountain zone of building the mountain top reservoir, utilize water good, the air in the oxygen enrichment negative ion environment is good, be equipped with land route magnetic suspension traffic facility again, the good place that is certain to extremely poly-popularity is fit to greatly promote to develop mountain areas development flowers and fruits mountain and high-grade food plant export base; 3. goods and materials such as personnel, aircraft fuel oil rise on the mountain, and the weight effect of available waste discharge promotes (as the high building 5 of Fig. 1, waste water storehouse 7 devices such as grade); 4. can change existing airport and consume the level land, to save the soil.

Description of drawings

Fig. 1 is the block diagram of Mountaintop transmitting aerodrome.

Fig. 2 is the lateral plan of magnetic-levitation, car launcher, aircraft.

Fig. 3 is the section drawing of part ventral, car launcher, track.

Fig. 4 is that belly hook puts down the schematic diagram of (it is outer to stretch out ventral).

Fig. 5 is that belly hook is packed up the schematic diagram of (in the indentation ventral).

The specific embodiment

Referring to Fig. 1, comprise magnetic-levitation 1, carry aircraft on the car launcher 2,2 that is at a stop in its descending

termination boarding place

3,3; Expression car launcher 2 carries the aircraft emission that advances at utmost speed just in orbit among the figure.When car launcher 2 emissions close on the most significant end (upper left corner) of magnetic-levitation 1, the track PTO Power Take Off, the plumbing arm of cam 24 is blocked (referring to Fig. 2, but Fig. 2 represents that car launcher 2 is in boarding place 3), make the plumbing arm right-hand turning of cam cross an angle, cam 24 no longer withstands the back hook housing, making back hook 22 is that change downwards in the axle center with axle 23, (application number 200710070421.1 has been addressed to break away from belly hook D, Fig. 3 of application number 200710070081.2 has block diagram), when belly hook D stretches out outside the ventral, can bear the power to head, tail direction simultaneously, schematic diagram is at Fig. 4, Fig. 5.This moment, car launcher V＞500km/h added that aero-engine has reached full load thrust, so aircraft flies away from car launcher 2 very soon, enters cruising speed.

Address in application number 200710070982.1 about car launcher and the floating principle of magnetic.Launch the car launcher 2 behind the aircraft, the system that is cushioned when arriving magnetic-levitation 1 limes superiors is lived, and returns to boarding place 3 (Fig. 1) with deadweight, prepares to accept another aircraft emission.The magnetic suspension rail is led 1 propulsion coil 1a, little support roller 1b is located on the track, little support roller 1b is when holding car launcher 2 lacking enough magnetic suspension forces because of speed is low when just starting, all lean on little support roller 1b to roll when launching aircraft when car launcher and retreat, so all arranging propulsion coil 1a and little support roller 1b on the total length that rail is led.2 of Fig. 2 is car launchers, and the upper layer of car is arranged many support rollers 20, and extends in forward on two arms 21 that (left of Fig. 2 to) stretch out, so support roller 20 is double double supporting wheels (consulting Fig. 3) of holding the ventral left and right sides always.

25 of Fig. 2 is U type ribs, the 26th, and liquid nitrogen container, the 27th, liquid nitrogen is connected valve disc, and the 28th, refrigerator pipes, circulating liquid nitrogen cooling superconductive system, the 29th, superconducting coil; 1C on cam 24 right sides is bounce cylinder (but irrelevant with cam), is the shock absorber of making when firmly car launcher 2 returns to the smallest limit position; The 8th, traction rubber tire (air pressure can be adjusted), the traction rubber tire can have several, the 80th, swing arm, the 81st, axle, the 82nd, balancing device (illustrating with extension spring among the figure), purpose makes 8 pairs of ventrals of traction rubber tire that suitable friction force be arranged, towing aircraft rolls on car launcher 2, and traction rubber tire 8 is by synchronous strap drive, but forward and backward revolution and fine motion, the 83rd, roller is provided in a side of the raceway in the aircraft passage 4 (Fig. 1).

Fig. 3 is three's cross section structure figure of aircraft ventral c, car launcher 2, magnetic-levitation 1 (referring to dark-coloured position).D is belly hook (head-on to), the 20th, and support roller, W are W type joists (vertically), T is a T type beam, 2a is curved square tube (laterally), and U is a U type beam (vertically), and 1b is little support roller (holding U type beam), 1a is a propulsion coil, the 29th, superconducting coil, the 25th, U type rib, the 26th, liquid nitrogen container, the 28th, refrigerator pipes, 25a is the roller slide rail.

Fig. 4, Fig. 5 are belly hook D folding and unfolding schematic diagrams.Fig. 4 belly hook D down state is tight against the G block, and D1 is an axle, and C1 is a covering, connecting plate E, rocking arm F, F1 are axles, G1 block, F2 are hole (this moments inserted in the hole fasten by lateral pin), so belly hook D from head to or the slave Caudad stressed, all be firm.

Fig. 5, after lateral pin among the F2 of hole was extracted in expression, rocking arm F was the axle center with axle F1, and upwards swing drives connecting plate E and belly hook D, and D takes in ventral until belly hook.

The A of Fig. 1 is that the big lake is the water source that cleans most, and B is that lakelet is a daily water consumption; The 7th, the waste water storehouse, 7a is a gate, and 7b is annular dewatering outlet, and 7c is a water pot, and 7d is a guide wheel, 7e is a cable wire, the 6th, reservoir dike face road, the 5th, high building, 5a are overline bridges.Come the passenger of transmitter field, all be in high building 5, to rise to overline bridge 5a from the inferior vertical conveyor in the foot of the hill, enter boarding place 3 from overline bridge 5a again, directly enter the cabin, so there is not the passenger from the mountain, to go down toward the foot of the hill, when therefore gathering the passenger of certain number in the elevator at the end of high building 5, computer can instruct starting gate 7a, the water yield of putting into corresponding weight enters annular dewatering outlet 7b, flow into water pot 7c, 7c descends rapidly and spurs cable wire 7e, makes the elevator fast rise in the high building 5, up to the entrance that the passenger is risen to overline bridge 5a; This moment, the passenger all left elevator, and water pot 7c seems more heavy and end valve is rushed open in further decline, had put water (this water is further purifying treatment in the wetland wooden land of the foot of the hill), and empty water pot 7c is lighter and rise to shown position once more than elevator.

Claims

1, a kind of Mountaintop transmitting aerodrome, it is characterized in that, comprise that superconduction scolds floating type magnetic suspension car launcher, respective track, boarding place, aircraft passage and high building elevator, overline bridge, waste water storehouse, weight hammer type water pot and the mountain top lake (A, B) of passenger from the foot of the hill rising to boarding place, floating type magnetic levitation device is scolded in the cover superconduction that each side is provided with of car launcher, and double double supporting wheel each side is set and W type joist is respectively arranged, coupling T type beam has self adaptive even load support performance; The passenger is from the foot of the hill being elevated to the airport, mountain top, be that the water that utilizes the waste water storehouse is controlled the discharging corresponding water amount by computer and entered water pot by the total weight that enters the elevator personnel, water pot is descended, spur the elevator in cable wire and the high building, send the passenger to arrive overline bridge, directly enter the cabin.

2, Mountaintop transmitting aerodrome according to claim 1 is characterized in that, at the belly that is launched aircraft the belly hook (D) relevant with described car launcher is housed, and forms with connecting plate, rocking arm, hole (F2) and pin; When belly hook is put down and is stretched out, the working direction of belly hook (D) or step back direction, two-way can both bearing load.