CN110510139A - A kind of method and device helping aircraft security landing or catapult-assisted take-off - Google Patents
A kind of method and device helping aircraft security landing or catapult-assisted take-off Download PDFInfo
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- CN110510139A CN110510139A CN201910889501.2A CN201910889501A CN110510139A CN 110510139 A CN110510139 A CN 110510139A CN 201910889501 A CN201910889501 A CN 201910889501A CN 110510139 A CN110510139 A CN 110510139A
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- raft device
- boat raft
- boat
- runway
- help
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/025—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using decelerating or arresting beds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
- B64F1/368—Arrangements or installations for routing, distributing or loading baggage
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Actuator (AREA)
Abstract
The present invention relates to the method and devices of a kind of help aircraft security landing or catapult-assisted take-off.Safety boat raft device is set on airfield runway, it, which is at least divided into, helps drop boat raft device and help-fly boat raft device two parts, help the structure of drop boat raft device are as follows: liquid cell and boat raft device are equipped on runway, the length of liquid cell is less than three kms, the downside of boat raft device is equipped with force-reducing unit, and upside is equipped with and helps drop plate.The structure of help-fly boat raft device are as follows: be provided with track on runway, be equipped with accumulator or booster in track both sides, boat raft device is connect with track or accumulator or booster.The booster is the piston that allows in air pressure part or hydraulic part in a manner of spiral lifting or pulley lifting mode or hoist engine lifting mode or burning fuel generates pushed at high pressure mode or the physical explosion way of propelling or the chemical explosion way of propelling comes shift position, to allow formation vacuum in the air pressure part or hydraulic part to generate atmospheric pressure, the atmospheric pressure is recycled to launch aircraft takeoff.
Description
Technical field
Aircraft lands are allowed the present invention relates to a kind of help aircraft lands or the method and device taken off, especially one kind
When steady deceleration or the method and device of catapult-assisted take-off can be capable of as early as possible.
Background technique
Currently, the method for allowing aircraft lands to be slowed down in the world mainly include the following types: 1, build up sufficiently long runway and allow
Aircraft voluntarily comes to a complete stop because motional inertia disappears.2, flap is installed on board the aircraft and counter pushes away deceleration device.3, with brake
Part slows down.4, slowed down with drag parachute.5, slowed down with hook or arrester wires.But these methods have a common drawback, are exactly not
Enough safely, when aircraft lands, due to being influenced by weather, wind direction, wind speed, landing angle and direction, even if having brake member, subtracting
The protection of fast umbrella also inevitably will appear the disaster of drift off the runway.Especially in the case where undercarriage can not be unfolded, safe landing
It is exactly a big problem.
At this stage, assisted aerocraft landing, preferably more common method has: steam catapult, linear motor and electromagnetism
Structure is complicated for formula ejector, VTOL, but these methods, and manufacture craft difficulty is very high, technical research and working service
Huge fund must all be put into.
Data shows that big passenger plane runway common at present generally will be 4 kilometers or so in the world.
The present inventor given in the invention of Publication No. CN109866937A it is a kind of using elastomeric objects by aircraft
The method that power savings after landing are got up, this method can make quickly to come to a complete stop and stored up when aircraft lands
It stores the strength got up and increases thrust to taking off for aircraft.But it is also only the side for storing power reinforcement to aircraft, steadily sliding
One of method.
Publication No. CN105314124B discloses a kind of vacuum using heavy caliber vertical type upper end opening lower end closed
Heavy caliber piston is pulled upwardly by cylinder by hoist engine, makes occur vacuum in vacuum reservoir, then by vacuum generate atmospheric pressure and
Piston own wt, the technology taken off through speed change gear and trailer wagon ejection fixed wing aircraft.Component needed for this technology is still
Show more, figure is more heavy, and not directly to power in taking off, energy can occur more in the transmitting of each component
Loss, in addition, being that can only but be not directed to how aircraft landing to be allowed to slow down to power-assisted is taken off there are one major defect.
Publication No. CN1348900A disclose it is a kind of solve the problems, such as the landing of aircraft with airplane load plate and take off, as
Described in its claims and specification: bearing or wheel being set below the load board, load board can be carried out
It quickly moves forward and backward, while a set of accelerator and brake apparatus for acting on airplane load plate is set.Aircraft landing is loading
On plate, the relative motion of protrusion the prevention aircraft and load board of the friction and load plate surface of load board and aero tyre,
Brake component can then make load board stop motion.When taking off, with the jet engine group or electromagnetic force being arranged in load board
Load board is pushed or pull on, in addition the engine of aircraft itself, can obtain double thrust.This design has distinct disadvantage: one,
When aircraft landing, by aero tyre friction and load plate surface protrusion come to a complete stop in load board by aircraft, then with brake
Part comes to a complete stop by load board, and this method is improper because being allowed to stop with brake component in load board high speed slide, with fly
It is about the same that the included brake component of machine brakes consumed brake block on runway, and the cost of this kind of brake block is very expensive,
So passenger plane does not generally consume brake block using brake component easily when landing.Two, jet engine is installed to help in load board
Fly, be not a kind of advanced method, allows jet engine just to have started in the distance of short km or so at once flame-out again,
Oil consumption waste is larger.If the cost of cost and ejection is bigger using electromagnetic launch.
Summary of the invention
The object of the present invention is to provide the method and devices of a kind of help aircraft security landing or catapult-assisted take-off.It is required
The technical issues of solution is mainly: 1, structure is relatively easy, manufacture craft difficulty is relatively low.2, facilitate operation, it is safe and practical,
It is high-efficient.3, can Intelligent control, can Reusability.
In response to the above problems, the present invention is solved using following method:
A kind of method and device helping aircraft security landing or catapult-assisted take-off, the method and device are run on airport
Safety boat raft device is set on road, and the safety boat raft device, which is at least divided into, helps drop boat raft device and help-fly boat two portions of raft device
Point；It is described that drop boat raft device is helped at least to be made of boat raft device and liquid cell or force-reducing unit or accumulator；The help-fly boat raft device
At least it is made of boat raft device with booster or accumulator；One end of the help-fly boat raft device is equipped with bumper or accumulator；
The boat raft device is connect by wheel or bar with the runway or liquid cell, and the bar includes track
Part, groove part, shaft-like object, tube, column.The connection type can be in various ways, such as: set in the bottom of boat raft device
Groove sets track on runway；For another example: setting tube in the bottom of boat raft device or two sides, shaft-like object is set on runway, navigate raft device
The tube of bottom is covered in the outside of the shaft-like object of runway, can slide longitudinally.On the boat raft device or it is provided with discourager
Or brake component, the discourager may act as the drawing article that assisting flight device takes off.The discourager is scalable or rotates or folds,
It can be popped up when stretching on the table top of the boat raft device, when contraction can retract under the table top of the boat raft device；It stops
Part under table top towards popping up on table top, with discourager as gate from the right and left of runway towards the effect of intermediate bit
Equally, the rear-wheel for being provided to stop aircraft is allowed to slow down, or accumulator is driven to store power.The discourager or it is flexible or
It is equipped with bearing or idler wheel or conveyer belt on discourager or stops pawl or elastomeric objects；On or near the discourager or set
There is detection part；The detection part includes pressure detection part or speed detection part or distance measurement part or shake frequency detection part or infrared ray
Detection part or optical detection part or magnetic detection part or radar wave detection part；
Between the boat raft device and the runway, or between the discourager, or can in electromagnetic levitation type or
Wheel-track type or slidingtype connection.
Preferably, the structure for helping drop boat raft device are as follows: in runway, including being set on or below the ground of runway
There is a liquid cell, the length of the liquid cell is gushed or anticollision dress less than three kms, four sides of the liquid cell or both sides or equipped with anti-
It sets；Bar is provided in the liquid cell, the boat raft device is connect with the bar；
The downside of the boat raft device or side are equipped with force-reducing unit, the upper surface of described boat raft device or equipped with helping drop plate, described to help
It drops plate and passes through elastomeric objects or air pressure part or hydraulic part or water damping or deceleration in gas-liquid casting die or the liquid cell；
The side of the boat raft device is synthesized by air pressure part or hydraulic part or gas-liquid casting die or elastomeric objects, and effect is anti-
It hits；The shape of the side or arc-shaped or acute angle or obtuse angle shape, either, by the periphery for rotating or stretching or fold boat raft device
Object and the shape for changing boat raft device either change boat raft device by peripheral objects inflation to boat raft device or filling liquid and
Shape；The raft device that navigates should be to need not needing resistance under water to determine according to it in what kind of shape.
It is described help drop boat raft device structure or are as follows: bar is provided on the runway, the two of the bar
Other or downside is provided with accumulator, and the boat raft device is connect with the bar or accumulator.
The structure of the help-fly boat raft device are as follows: bar is provided on the runway, in the both sides of the bar
Or downside is provided with accumulator or booster, the boat raft device is connect with the bar or accumulator or booster.
Preferably, the force-reducing unit is in hinge shape, and the force-reducing unit is at least composed of two boards and an axis；It is described
One end of two boards and the movable connection of axis, the other end are provided with turning or tooth or convex block or magnet, the axis and boat raft
The downside of device or side connection；
Either, the downside of the boat raft device or side are provided with electromagnet, which has magnetic state or without magnetic
The transformation of state or magnetic pole is controlled by intelligent converter, which can be connected with the magnet of described force-reducing unit one end by magnetic
It connects.That is, the electromagnet can change magnetic pole by power-off continuous electricity or change conducting direction, make script and the two boards
One end magnet magnetic state together, change into because mutually magnetic identical therefore generate mutually exclusive and separated
State.Design effect to be achieved in this way is: when the raft device that navigates, which accepts aircraft, needs deceleration, the electromagnet passes through
Change conducting direction and change magnetic pole, repels electromagnet mutually with the magnet on the two boards and separate, then, it is in hinge shape
One end of the two boards be unfolded to two sides, increase the resistance that slides under water along track extending direction of boat raft device.It is helping
It helps after the completion of the work of aircraft deceleration, boat raft device needs to return to origin by the elastic reset of elastomeric objects, is in hinge
The two boards of shape will be arranged because of its turning or convex block, the both ends being unfolded again the active force through water flow and close up in
At this moment the two sides of the electromagnet adjust the magnetic pole of electromagnet, the electromagnet again can be with the magnetic of one end of the two boards
Ferromagnetic suction is together；
Either, the force-reducing unit is made of one piece or one piece or more of baffle, and the baffle can be in the boat raft device
Downside or side it is flexible or fold or rotation.The baffle can be in random geometry, and the volume or area of the baffle can
With different.Its function is: if boat raft device is allowed to slow down, the baffle, which just trails, stops water flow to realize deceleration；And if
Allow boat raft device homing, the baffle just retract or be transferred to boat raft device inside, or fold be attached to boat raft device under
End face or both sides of the face keep the reseting procedure of boat raft device without hindrance.
Either, the force-reducing unit is by the one or more anti-pump group that pushes away at the anti-pump that pushes away is arranged in the boat
The downside of raft device or side.
Preferably, the accumulator or booster are at least by bigbore air pressure part or hydraulic part or gas-liquid casting die or electrical
Part or mechanical parts or elastomeric objects are composed, and the mechanical parts include connector or fastener；The bigbore air pressure part
Or diversion pipe or deflector hole are provided on hydraulic part or gas-liquid casting die；On the diversion pipe or it is provided with small-bore air pressure part
Or hydraulic part or gas-liquid casting die.In fact, the bigbore air pressure part or hydraulic part or gas-liquid casting die and small-bore air pressure
Part or hydraulic part or gas-liquid casting die are separately positioned on the two sides of diversion pipe, all with diversion pipe communications and liaison, small-bore air pressure part or liquid
The gas bleeding or when liquid from bigbore air pressure part or hydraulic part or gas-liquid casting die by diversion pipe of casting die or gas-liquid casting die
It is laborsaving.
Preferably, the accumulator stores power by the way of elastomeric objects or use compressed gas, or utilizes from institute
It states the gas flowed into and out in diversion pipe or deflector hole or liquid drives electric power generation, then store the electric energy issued
Come；
The booster be by the piston in the air pressure part or hydraulic part or gas-liquid casting die in a manner of spiral lifting
Or pulley lifting mode or hoist engine lift mode or air pressure push-pull fashion or hydraulic push-pull fashion or burning fuel generates high pressure
The way of propelling or the physical explosion way of propelling or the chemical explosion way of propelling come shift to allow the air pressure part or hydraulic part or
Vacuum is formed in gas-liquid casting die generates atmospheric pressure.
Preferably, the boat raft device or help drop plate or boat raft device on be provided with transmission belt or roller bearing or elastomeric objects, institute
Drive shaft or bearing are stated on transmission belt or are provided with, the transmission belt is in band-like or cloth-like or chain or roll shaft shape；
The different rotation directions of the roller bearing or transmission belt, are steadily slided, either after capable of helping aircraft lands
Increasing friction force or thrust when to aircraft takeoff；
The roller bearing or roll shaft or transmission belt or can it is described boat raft device or help drop plate on go up and down.The liter,
I.e. rise in boat raft device table top or help drop plate upper surface on, the drop, i.e., landing in the table top or the upper table
Under face.
The roller bearing or roll shaft or transmission belt that are arranged on the boat raft device potentially act as discourager and allow the aircraft
Pintle hooking；
One end of the boat raft device is equipped with slope, the slope or liftable；
Between the boat raft device and the runway or liquid cell or bar or be equipped with elastomeric objects, the elastomeric objects or
With pulley combination.
Preferably, the boat raft device is using the strength or energy of accumulator accumulation either using on the booster
Atmospheric pressure push or pull on the aircraft catapult and take off.
Preferably, the catapult-assisted take-off mode are as follows: dock at aircraft on boat raft device, then by the item is arranged in
The accumulator or booster of shape object side launch the boat raft device, then accumulator or booster by being set on the boat raft device
Launch the aircraft.
Preferably, described that drop boat raft device is helped to connect with help-fly boat raft device by connector or help described
Drop boat raft device and help-fly boat raft device are integrated into an entirety, the connector include pneumatic drives or hydraulic drives or
Mechanical transmissioning piece or Electrified Transmission part, the mechanical transmissioning piece include pulley or hawser or connecting rod or gear or hoist engine.
Preferably, takeoff runway and landing runway is respectively set on the both sides at a right angle, is provided on takeoff runway
Help-fly boat raft device, setting helps drop boat raft device on landing runway；
In the angle region of the takeoff runway and landing runway, be arranged airdrome control tower or airplane parking area or airport lounge or
Ticket lobby or ticketing spot or exit or integrated service area, the integrated service area include guidance reception area or baggage check delivery
Area or the public place of entertainment or rest area or shopping area or diet area or diagnosis and treatment area or emergency reaction area.It the angle region can be in any several
What shape.
Elastomeric objects of the present invention are divided into metallic elastic object and non-metal elastic object, the metallic elastic object
Body includes spring, and the non-metal elastic object includes rubber, silica gel, plastics, plastic cement, and the elastomeric objects include elasticity rolling
Axis.The bumper includes rubber pad, plastic pad, silicagel pad.The fastener include nail, screw, bolt, nut,
Pin or joinery and its construction and axis, chain, rope, tightener, folder, fastener.The connection include contact connection, bonding, welding,
Fastener connection, clip connection, cassette connection, bondage connection, movable connection and with mold connection cast in block.It is described
Discourager allows from the pintle hooking under aircraft upthrow, and the discourager can be hard objects or be soft object, the resistance
The shape for blocking part can be strip, bulk, including rope form, netted, cloth-like, paliform, including arrester wires, barrier, obstruction wall, resistance
Block pawl.The liquid cell includes pond or chemical solution liquid pool.The aircraft includes aircraft, rocket or other aircrafts, boat
Its device.
The invention has the advantages that after using the above method and device:
(1) aircraft lands can avoid using the cumbersome of drag parachute, or even brake block zero is allowed to be lost.
(2) aircraft lands, it is no longer necessary to worry safety problem, because aircraft is once land in boat raft device, inertia is rushed
Power will be immediately transferred to boat raft device, track, waterborne in accumulator or pond, even if aircraft occurs partially in landing
From runway, the mistakes such as undercarriage, wing dropping can not be unfolded, as long as having fallen on boat raft device, there is no need to worry safety problem again:
It is the shock-absorbing protecting for helping drop plate first.If the undercarriage of aircraft can not be unfolded, the bullet for helping drop plate or navigating on raft device is set
Property roller bearing can temporarily substitute the wheel of aircraft, so that aircraft security be allowed to force-land.Followed by the reduction of speed and anticreep of discourager
From protection, followed by the impact force transfer protection of navigate raft device and track, it is in the storage power buffer protection or pond of accumulator later
The power buffer protection that disappears that is played of water.Aircraft takeoff has the elastic force saved or air to come through power caused by overcompression
Boosting has the ready atmospheric pressure of booster institute to provide power, has boat raft device to provide the elevation angle, even wind direction and wind velocity when taking off
It is not right, safety of taking off will not be influenced.
(3) runway will be saved substantially.
(4) if by it is described safety boat raft device be applied to aircraft carrier or other large surface warships, do not change aircraft carrier or its
Under the preceding topic of the floor space of its large surface warship, carrier-borne aircraft short distance can not only be allowed to rise as steam or electromagnetic launch
Drop, it is important that manufacturing cost and use cost is as far apart as heaven and earth, it can also extension landing runway, protects the safe landing of carrier-borne aircraft,
The safe falling of especially protection is injured, breaks down carrier-borne aircraft and new hand pilot.
Detailed description of the invention
Embodiments of the present invention are described further with reference to the accompanying drawing, but protection scope of the present invention be not limited to it is attached
Figure and embodiment.
Fig. 1 is a kind of schematic cross-sectional view of the first embodiment of the invention about booster structure.
Fig. 2 is second of embodiment of the invention about a kind of schematic cross-sectional view for storing power booster.
Fig. 3 is the third of the invention embodiment about aircraft landing helping drop boat raft device and help-fly to navigate raft dress
Set the explanatory view on the boat raft device combined.
Fig. 4 is explanatory view of the mode shown in Fig. 3 about aircraft standby for takeoff on boat raft device.
Fig. 5 is that the booster that mode shown in Fig. 3 has been set in orbit about aircraft and boat raft device is launched to left end,
The booster being arranged in boat raft device to be ready passing through explanatory view when discourager takes off aircraft catapult.
Fig. 6 is the signal that the 4th kind of embodiment of the invention stops aircraft rear-wheel about detection part Intelligent control discourager
Property cross section view.
Fig. 7 is that mode shown in Fig. 6 about discourager is changed into drawing article, by pulling aircraft rear-wheel by aircraft catapult
The schematic cross-sectional view taken off.
Fig. 8 be 5th kind of embodiment of the invention dropped to about aircraft be placed in pond helping it is schematic on drop plate
Side view.
Fig. 9 is schematic, bottom view of the mode shown in Fig. 8 about boat raft device.
Figure 10 is separately positioned on a right angle about by takeoff runway and landing runway for the 6th kind of embodiment of the invention
Both sides, by airdrome control tower, airplane parking area, airport lounge, ticket lobby, ticketing spot, exit, integrated service area setting taking off
The schematic plan of runway and landing runway angle region.
Wherein: in the first embodiment: heavy caliber air pressure part 101, piston 102, tooth 103, intelligent controller 104,
Bolt 105, diversion pipe 106, small-bore gas casting die 107, active cylinder 108, diversion pipe 109, small-bore gas casting die 110, piston
111, pass through connector 112, active cylinder 113, piston 114, discourager 115, sparge pipe 116, heavy caliber air pressure part 117, piston
118, positionable wall 119.In the second embodiment: heavy caliber hydraulic part 201, heavy caliber air pressure part 202, connector 203 are living
Plug 204, positionable wall 205, piston 206, diversion pipe 207, engine 208, battery 209, discourager 210, spring 211, intelligence
Controller 212, hoist engine 213, hawser 214, diversion pipe 215, hydraulic part 216, piston 217, liquid 218, intelligent controller
219, motor 220, piston rod 221, piston 222, brake component 223.In the third embodiment: runway 301, track 302 store
Power booster 303, rear end 304, navigate raft device 305, clip slot 306, discourager 307, discourager 308, helps drop help-fly plate 309, elasticity
Roller bearing 310, aircraft 311, piston 312, one end 313 of piston 312, brake component 314, vertical tooth 315, aircraft 316, motor
317, diversion pipe 318, intelligent controller 319, silicagel pad 320, hydraulic stem 321, arrow 322, junction 323.In the 4th kind of reality
Apply in mode: ground 601 stores power booster 602, piston rod 603, discourager 604, intelligent detecting control piece 605, aircraft
606, front-wheel 607, rear-wheel 608, right-hand end 609, brake component 610, arrow 611.In the 5th kind of embodiment: runway 701, water
Pond 702, tube 703, navigate raft device 704, pulley 705, brake component 706, lower end 707, force-reducing unit 708, and force-reducing unit 709 helps drop
Plate 710, elastic telescopic casing 711, the water surface 712, aircraft 713, elastic discourager 714, stretch cord 715, the anti-pump 716, interior of pushing away
Arc baffle 717, tubaeform diversion pipe 718, axis 719, turning 720, magnet 721, electromagnet 722, intelligent converter 723, power generation
Machine 724, battery 725, right side 726, bumper 727.In the 6th kind of embodiment: helping drop boat raft device 801, help-fly boat
Raft device 802, the aircraft 803 of landing, the aircraft 804 to take off, airdrome control tower 805, airplane parking area 806 to be flown, shutdown to be checked
Feed supplement area 808 is repaired on level ground 807, and channel 809 of taking off, channel 810 of landing, point of dropping off the guests 811, exit 812, claim place
813, outbound channel 814, diet area 815, rest area 816, love reception area 817, shopping area 818, ticketing area 819, luggage inspection
Delivery area 820 is looked into, entertains diagnosis and treatment emergency reaction integrated functional zonation 821, ticketing spot 822, airport lounge 823, boarding channel 824 helps
Flight raft device 825 helps drop boat raft device 826.
Specific embodiment
As shown in Figure 1, the structure of booster are as follows: piston 102 in heavy caliber air pressure part 101 is equipped with tooth 103, intelligence on one side
Can control device 104 can control tooth 103 by bolt 105, to control the sliding distance of piston 102.Heavy caliber air pressure
Part 101 is connect with heavy caliber air pressure part 117, and piston 118 is connect with positionable wall 119.Heavy caliber air pressure part 101 is equipped with diversion pipe
106, diversion pipe 106 is equipped with small-bore gas casting die 107, and 107 side of small-bore gas casting die is equipped with active cylinder 108.Heavy caliber gas
Diversion pipe 109 is additionally provided on casting die 101, diversion pipe 109 is equipped with small-bore gas casting die 110, the piston 111 in air pressure part 110
It is linked together by connector 112 and the piston 114 in active cylinder 113.When discourager 115 is pullled by aircraft, piston 102
When moving to the right end of air pressure part 101, i.e., positioned by bolt 105.From the gasoline liquid of the spray form into active cylinder 113 of sparge pipe 116
It lights a fire after body, high pressure gas just will push piston 114 and be moved to the right with piston 111 the gas pumping in air pressure part 101
Piston 102 and discourager 105 send as an envoy to because atmospheric pressure generates pulling force to the left.
Mainly led to by a heavy caliber hydraulic part 201 and a heavy caliber air pressure part 202 as shown in Fig. 2, storing power booster
It crosses connector 203 and is mutually linked composition, be equipped with piston 204 in air pressure part 202, the left end of piston 204 is connect with positionable wall 205.
Piston 206 is equipped in hydraulic part 201, the right end of piston 206 is connect with discourager 210, and left end is connect with spring 211.Work as flight
Device drives discourager 210 to lead piston 206 when side direction is mobile to the right, will stiff spring 211 it is mobile towards right direction, spring
211 pulling force will allow aircraft quick deceleration through discourager 210, meanwhile, spring 211 is in a manner of elastic force by the inertia of aircraft
Impulse force allows the positioning of piston 206 to store by brake component 223.
If wanting for hydraulic part 201 to be evacuated and being allowed to generate powerful atmospheric pressure, the starting of intelligent controller 212 can be allowed to roll up
It raises machine 213 and tightens hawser 214, the piston 217 in the hydraulic part 216 being arranged on diversion pipe 215 is pulled towards right direction, thus
Extract the liquid 218 in hydraulic part 201 out.Meanwhile intelligent controller 219 also being allowed to start motor 220 by spiral way piston
Bar 221 moves right to move right with piston 222, also extracts the liquid 218 in hydraulic part 201 out.In practical applications, as enclosing
Be wound on 201 appearance of heavy caliber hydraulic part small-bore hydraulic part 216 can be set it is multiple, when these small-bore hydraulic parts all into
After the work of row drawing liquid, the liquid in heavy caliber hydraulic part 201 will form vacuum by pumping.
If piston 206 has been displaced to the right end of hydraulic part 201, and discourager 210 is also by aircraft with continuation
It moving right, air pressure part 202 will and then move right, gas will be flowed rapidly into from diversion pipe 207, what this was quickly flowed
Gas can drive engine 208 to generate electricity, and generated electric energy can be stored in battery 209.
As shown in figure 3, runway 301 is equipped with track 302, it is equipped with by track 302 and stores power booster 303, store power booster
303 rear end 304 is fixedly connected with the side of track 302, and boat raft device 305 is connect by clip slot 306 with track 302, and navigate raft device
305 inside is equipped with the connection of discourager 307,308 for storing power booster and two sides, and junction 323 can be sliding in magnetic suspension state
It is dynamic.The face of boat raft device 305, which is equipped with, helps drop help-fly plate 309, helps the elastic roller bearing 310 that strip is equipped in drop help-fly plate 309, bullet
Property roller bearing 310 can be down to, be namely retracted into help drop help-fly plate 309 plate face under, can also rise that is, be raised to institute
State the pintle hooking for being convenient for aircraft above plate face at 5cm.As shown, aircraft 311 can not be opened up because there was a mechanical failure
Gear down wheel is opened, therefore can only force-land and help on drop help-fly plate 309, after pintle has caught on elastic roller bearing 310,
Its inertia impulsive force has been immediately transferred to boat raft device 305 and has stored on power booster 303, therefore the clip slot 306 for the raft device 305 that navigates heads on work
One end 313 of plug 312 is slided to the right along track 302, and sliding is stopped when reaching the maximum development distance of piston 312,
Referring to fig. 2 to store power booster description it is known that, at this point, store power booster 303 in spring also have been unfolded into most
Greatly, store expired elastic force, brake component 314 is stuck on the vertical tooth 315 that 302 one side of track is arranged in, prevent piston 312 from once to
Left reset.In conjunction with Fig. 4, when needing to launch aircraft 316, first the hoist engine of discourager 307,308 can be drawn to boat raft
The rightmost of device 305 starts motor 317, the air in storage power booster 303 is pumped to form vacuum through diversion pipe 318, then
Aircraft 316 is dragged to before discourager 307,308, is allowed on rear side of its rear-wheel and is resisted the discourager 307,308, and elasticity is rolled
Axis 310 be down to almost with help drop the upper surface of help-fly plate 309 it is concordant, allow elastic roller bearing 310 be set to help drop help-fly plate 309 in
Drive shaft driving under towards shown in arrow 322 clockwise turn to rotation, then start starting for the aircraft 316 itself
Machine, starting intelligent controller 319 release the locking control of brake component 314, as shown in connection with fig. 5, among storage power booster 303
Spring storage power and vacuum generate atmospheric pressure double action under, one end 313 of piston 312 will push clip slot at once
Therefore 306 namely push boat raft device 305 launches towards left side, impinge upon the silicagel pad 320 of the rear end 304 when clip slot 306 and
Because touched switch while all standing, hydraulic stem 321 jacks up rapidly upward, helping the one end for dropping help-fly plate 309 to rise, institute
It states the storage power booster being arranged in inside boat raft device 305 and also releases braking at once, pulled and flown by 307,308 strength of discourager
The rear-wheel of device 316 by aircraft 316 launch, ski-jump take-off.In practical application, the table top for the raft device 305 that navigates and 301 ground of runway
It is flat.
As shown in fig. 6, storing power booster 602 in having for the ground of runway 601, the piston rod of power booster 602 is stored
603 right-hand end 609 is equipped with discourager 604, and discourager 604 can stretch among the right-hand end 609, works as intelligent detecting
Control piece 605 detects the moment that the front-wheel 607 of aircraft 606 is skimmed over from the top of discourager 604, i.e. starting discourager 604
The rear-wheel 608 for stopping aircraft 606 is popped up at a terrific speed, and rear-wheel 608 is made to drive discourager 604 and piston rod
603 move right until coming to a complete stop.
As shown in fig. 7, when needing with the power laid in power booster 602 is stored by 606 catapult-assisted take-off of aircraft, it can be flight
Device 606 is parked in the left side of discourager 604, and the head of aircraft 606 makes discourager 604 be against the right side of the rear-wheel 608 towards left side
Side, that is, it is against the rear side of rear-wheel 608, braking of the brake component 610 to piston rod 603 is then released, in this way, on piston rod 603
The elastic force saved already and the atmospheric pressure having had been prepared for can allow piston rod 603 quickly to move downward, and drive discourager
604 pull the aircraft 606 on the ground of runway 601 towards left direction that is, arrow i.e. by the rear-wheel 608 is pulled
First 611 direction catapult-assisted take-off.
As shown in figure 8, digging out a pond 702 in runway 701, tube 703 is equipped in pond 702, navigate raft device 704
707 sets of lower end can be slided to left and right direction on tube 703, brake component 706 be arranged in the lower end 707 and tube
703 joining place.The left side pool wall in pond 702 is equipped with pulley 705, and the left end of stretch cord 715 is connect with boat raft device 704, right
End is connect through pulley 705 with the right side pool wall in pond 702.The right side pool wall in pond 702 is equipped with bumper 727.Navigate raft device 704
Bottom surface be equipped with the lesser force-reducing unit 708 of figure and the biggish force-reducing unit 709 of the bodily form, boat raft device 704 upper surface be equipped with thickness compared with
Drop plate 710 but is helped for hollow greatly, drop plate 710 is helped to connect by elastic telescopic casing 711 with the upper surface for the raft device 704 that navigates.It helps
Drop plate 710 is kept afloat on 712, and boat raft device 704 is then submerged under the water surface 712 completely.
As shown in figure 9, the bottom surface of boat raft device 704 is equipped with, counter to push away the lesser force-reducing unit 708 of pump 716, the bodily form, the bodily form biggish
Force-reducing unit 709, telescopic inner arc baffle 717, tubaeform diversion pipe 718.One end of the force-reducing unit 708 can be 719 turns around axis
Dynamic, the other end is equipped with turning 720 and magnet 721.The axis 719 is connect with the bottom surface of boat raft device 704.It is arranged by axis 719
The electromagnet 722 on side can be controlled the transformation of its magnetic pole by intelligent converter 723.When the raft device 704 that navigates is mobile towards left direction, water
The pressure of stream can be attached to magnet 721 on the electromagnet 722 by the turning 720, and at this moment, intelligent converter 723 can
The magnetism of adjustment electromagnet 722 sucks magnet 721 mutually with electromagnet 722.When the raft device 704 that navigates is mobile towards right direction, one
Denier is in need, and the magnetism that electromagnet 722 can be adjusted in intelligent converter 723 keeps magnet 721 and electromagnet 722 mutually exclusive, from
And separate blocking water flow.Osculum one end of tubaeform diversion pipe 718 is equipped with generator 724 and battery 725, diversion pipe
718, which can rapidly flow through water flow its osculum one end, allows generator 724 to generate electricity and stores electric energy by battery 725 in case counter push away pump
716 use.The arc-shaped face in right side 726 of boat raft device 704, but its arc-shaped face is to make because of inflation so, is inflated if emptied
Body is then plane.
In conjunction with Fig. 8 Fig. 9, when aircraft 713, which drops to, to be helped on drop plate 710 and stopped by elastic discourager 714, institute's band
The impact force and inertia impulsive force come have been immediately transferred to the water helped in drop plate 710, boat raft device 704, tube 703 and pond 702
On, initially, the arc-shaped face in right side 726 for the raft device 704 that navigates, force-reducing unit 708,709 is all undeployed, and inner arc baffle 717 does not extend out,
It is counter that push away pump 716 inactive.In this way, elastic discourager 714 would not be by great impact force.Boat raft device 704 moves in water
A distance to elastic discourager 714, helps drop plate 710, aircraft 713 to be equivalent to and be integrated, so that it may which first expansion subtracts
Then force-reducing unit 709 is successively unfolded in power device 708, stretch out inner arc baffle 717, and the valve for opening the right side 726 empties wherein
Right side 726 is become plane by gas, this succession of measure, is provided to that boat raft device 704 and aircraft 713 is allowed to slow down.Most
Afterwards, start counter push away and pump 716 and brake component 706, boat raft device 704 is allowed to reach exactly to come to a complete stop when the right-hand end in pond 702.To flight
After device 713 is removed from boat raft device 704, the control of brake component 706 is released, boat raft device 704 again can be because of stretch cord 715
Elastic force automatically returns to the left-hand end in pond 702.
As shown in Figure 10, drop boat raft device 801 and help-fly boat raft device 802 is helped to be respectively arranged on the both sides at a right angle, i.e.,
Help-fly navigates raft device 802 in laterally setting, and help-fly navigates raft device 825 for the catapult-assisted take-off from left to right of aircraft 804；Help drop boat raft device
801 in longitudinally disposed, helps drop boat raft device 826 that aircraft 803 is landed from top to bottom to coming to a complete stop, makes the aircraft 803 of landing and take off
Aircraft 804 heading it is different, to avoid the danger interfered with or disturb each other.Helping drop boat raft device 801 and help-fly boat raft device
Airdrome control tower 805, channel 809 of taking off, airplane parking area to be flown 806, to be checked can be set in the rectangular region of 802 angle
It is airplane parking area 807, maintenance feed supplement area 808, landing channel 810, point of dropping off the guests 811, exit 812, the place 813 that claims, outbound
Area is consigned in channel 814, diet area 815, rest area 816, love reception area 817, shopping area 818, ticketing area 819, baggage check
820, diagnosis and treatment emergency reaction integrated functional zonation 821, ticketing spot 822, airport lounge 823, boarding channel 824 are entertained.
If desired, double down or round trip flight boat raft device can also be respectively set in right-angle side.
Claims (10)
1. a kind of method and device for helping aircraft security landing or catapult-assisted take-off, it is characterized in that:
Safety boat raft device is provided on airfield runway, the safety boat raft device, which is at least divided into, helps drop boat raft device and help-fly
Boat two parts of raft device；
It is described that drop boat raft device is helped at least to be made of boat raft device and liquid cell or force-reducing unit or accumulator；
The help-fly boat raft device is at least made of boat raft device with booster or accumulator；One end of help-fly boat raft device or
Equipped with bumper or accumulator；
The boat raft device is connect by wheel or bar with the runway or liquid cell, and the bar includes orbital member, recessed
Slotware, shaft-like object, tube, column；
On the boat raft device or it is provided with discourager or brake component, the discourager may act as the pulling that assisting flight device takes off
Part；The discourager can stretch or rotate or fold, the discourager it is flexible or on discourager be equipped with bearing
Or idler wheel or conveyer belt or stop pawl or elastomeric objects；
On or near the discourager or be equipped with detection part, the detection part include pressure detection part or speed detection part or
Distance measurement part or shake frequency detection part or infra-red detection part or optical detection part or magnetic detection part or radar wave detection part；
The boat raft device and runway connect between discourager, or in electromagnetic levitation type or wheel-track type or slidingtype.
2. the method according to claim 11 and device, it is characterized in that:
The structure for helping drop boat raft device are as follows: liquid cell, the length of the liquid cell are equipped on or below the ground of runway
Degree gushes or anticollision device, collision-prevention device less than three kms, four sides of liquid cell or both sides or equipped with anti-；
Bar is provided in the liquid cell, the boat raft device is connect with the bar；
The downside of the boat raft device or side are equipped with force-reducing unit, the upper surface of described boat raft device or equipped with helping drop plate, described to help drop plate
Pass through the water damping or deceleration in elastomeric objects or air pressure part or hydraulic part or gas-liquid casting die or the liquid cell；
The side of the boat raft device is synthesized by air pressure part or hydraulic part or gas-liquid casting die or elastomeric objects, the shape of the side or is in
Arc or acute angle or obtuse angle shape either change boat raft device and rotating or stretching or fold the peripheral objects of boat raft device
Shape the shape of boat raft device is either changed by peripheral objects inflation to boat raft device or filling liquid and；
It is described help drop boat raft device structure or are as follows: be provided with bar on the runway, the bar both sides or
Downside is provided with accumulator, and the boat raft device is connect with the bar or accumulator；
The structure of help-fly boat raft device are as follows: be provided with bar on the runway, the bar both sides or under
Side is provided with accumulator or booster, and the boat raft device is connect with the bar or accumulator or booster.
3. the method according to claim 11 and device, it is characterized in that: the force-reducing unit is in hinge shape, the force-reducing unit is extremely
It is few to be made of two boards and an axis；
One end of the two boards and the movable connection of axis, the other end is provided with turning or tooth or convex block or magnet, described
Axis is connect with the downside of boat raft device or side；
Either, the downside of the boat raft device or side are provided with electromagnet, which has magnetic state or without magnetic state
Or the transformation of magnetic pole is controlled by intelligent converter, which can be connected with the magnet of described force-reducing unit one end by mutual magnetic
It connects；
Either, the force-reducing unit is made of one piece or one piece or more of baffle, and the baffle can be under the boat raft device
Side or side stretch or fold or rotate；
Either, the force-reducing unit is by the one or more anti-pump group that pushes away at the anti-pump that pushes away is arranged in the boat raft device
Downside or side.
4. the method according to claim 11 and device, it is characterized in that:
The accumulator or booster are at least by bigbore air pressure part or hydraulic part or gas-liquid casting die or electricity piece or mechanical parts
Or elastomeric objects are composed, the mechanical parts include connector or fastener；The bigbore air pressure part or hydraulic part or
Diversion pipe or deflector hole are provided on gas-liquid casting die；On the diversion pipe or be provided with small-bore air pressure part or hydraulic part or
Gas-liquid casting die.
5. the method according to claim 11 and device, it is characterized in that:
The accumulator stores power by the way of elastomeric objects or use compressed gas, or utilizes from the diversion pipe or lead
The gas or liquid flowed into and out in discharge orifice drives electric power generation, then stores electric energy；
The booster be by the piston in the air pressure part or hydraulic part or gas-liquid casting die in a manner of spiral lifting or cunning
It takes turns lifting mode or hoist engine lifting mode or air pressure push-pull fashion or hydraulic push-pull fashion or burning fuel generates pushed at high pressure
Mode or the physical explosion way of propelling or the chemical explosion way of propelling come shift position, thus allow the air pressure part or hydraulic part or
Vacuum is formed in gas-liquid casting die generates atmospheric pressure.
6. method according to claim 1 or 2 and device, it is characterized in that in the boat raft device or helping on drop plate and being provided with biography
Dynamic band or roller bearing or elastomeric objects on the transmission belt or are provided with drive shaft or bearing, and the transmission belt is in band-like or cloth
Shape or chain or roll shaft shape；
The different rotation directions of the roller bearing or transmission belt, are steadily slided after capable of helping aircraft lands, or to winged
Increasing friction force or thrust when row device takes off；
The roller bearing or roll shaft or transmission belt or can it is described boat raft device or help drop plate on go up and down；
The roller bearing or roll shaft or transmission belt that are arranged on the boat raft device potentially act as discourager and allow the tail of the aircraft
Hook hooking；
One end of the boat raft device is equipped with slope, the slope or liftable；
Between the boat raft device and the runway or liquid cell or bar or be equipped with elastomeric objects, the elastomeric objects or with cunning
Wheel combination.
7. method and device according to claim 1 or 4 or 5, it is characterized in that: the boat raft device is stored using the accumulator
Long-pending strength or energy either pushes or pull on the aircraft catapult using the atmospheric pressure on the booster and takes off.
8. the method according to claim 11 and device, it is characterized in that the catapult-assisted take-off mode are as follows: park aircraft
In on boat raft device, the boat raft device is then launched by accumulator or booster that the bar side is arranged in, then by being arranged
In accumulator or the booster ejection aircraft on the boat raft device.
9. the method according to claim 11 and device, it is characterized in that described help drop boat raft device and help-fly boat raft to fill
Set to connect by connector either helps drop boat raft device and help-fly boat raft device to be integrated into an entirety, the connection for described
Part includes pneumatic drives or hydraulic drives or mechanical transmissioning piece or Electrified Transmission part, the mechanical transmissioning piece include pulley or
Hawser or connecting rod or gear or hoist engine.
10. method and device described according to claim 1 or 2 or 3 or 4 or 5 or 8 or 9, it is characterized in that: at right angle
Takeoff runway and landing runway is respectively set in both sides, and help-fly boat raft device is provided on takeoff runway, is set on landing runway
It is equipped with and helps drop boat raft device；
In the angle region of the takeoff runway and landing runway, airdrome control tower or airplane parking area or airport lounge or ticketing are set
The Room or ticketing spot or exit or integrated service area, the integrated service area include guidance reception area or the public place of entertainment or rest area or
Shopping area or diet area or diagnosis and treatment area.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910889501.2A CN110510139A (en) | 2019-09-12 | 2019-09-12 | A kind of method and device helping aircraft security landing or catapult-assisted take-off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910889501.2A CN110510139A (en) | 2019-09-12 | 2019-09-12 | A kind of method and device helping aircraft security landing or catapult-assisted take-off |
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| Publication Number | Publication Date |
|---|---|
| CN110510139A true CN110510139A (en) | 2019-11-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910889501.2A Pending CN110510139A (en) | 2019-09-12 | 2019-09-12 | A kind of method and device helping aircraft security landing or catapult-assisted take-off |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113335544A (en) * | 2021-06-30 | 2021-09-03 | 燕山大学 | Transmission system of landing assisting device of ship-based helicopter |
| CN114291283A (en) * | 2021-03-18 | 2022-04-08 | 何韧 | Aircraft gripping type recovery method and device |
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| GB563426A (en) * | 1942-07-11 | 1944-08-15 | Reid & Sigrist Ltd | Improvements in or relating to runways for aircraft |
| FR1048485A (en) * | 1950-09-21 | 1953-12-22 | Aircraft landing pads | |
| CN201459564U (en) * | 2009-08-14 | 2010-05-12 | 昆明理工大学 | Modified airport runway |
| CN108033032A (en) * | 2017-12-12 | 2018-05-15 | 佛山神航科技有限公司 | A kind of water landing runway |
| CN208947635U (en) * | 2018-09-18 | 2019-06-07 | 任福喜 | A kind of track electricity pushes away the device that quickly takes off |
| CN109866937A (en) * | 2017-12-02 | 2019-06-11 | 何韧 | A kind of method and device helping aircraft lands deceleration or the reinforcement that takes off |
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2019
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Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB563426A (en) * | 1942-07-11 | 1944-08-15 | Reid & Sigrist Ltd | Improvements in or relating to runways for aircraft |
| FR1048485A (en) * | 1950-09-21 | 1953-12-22 | Aircraft landing pads | |
| CN201459564U (en) * | 2009-08-14 | 2010-05-12 | 昆明理工大学 | Modified airport runway |
| CN109866937A (en) * | 2017-12-02 | 2019-06-11 | 何韧 | A kind of method and device helping aircraft lands deceleration or the reinforcement that takes off |
| CN108033032A (en) * | 2017-12-12 | 2018-05-15 | 佛山神航科技有限公司 | A kind of water landing runway |
| CN208947635U (en) * | 2018-09-18 | 2019-06-07 | 任福喜 | A kind of track electricity pushes away the device that quickly takes off |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114291283A (en) * | 2021-03-18 | 2022-04-08 | 何韧 | Aircraft gripping type recovery method and device |
| CN113335544A (en) * | 2021-06-30 | 2021-09-03 | 燕山大学 | Transmission system of landing assisting device of ship-based helicopter |
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Application publication date: 20191129 |