CN102120493A

CN102120493A - Method and structure for assisting takeoff, landing and flying-unrelated operations of airplanes by using locomotive and railcar

Info

Publication number: CN102120493A
Application number: CN2010100002935A
Authority: CN
Inventors: 徐清华
Original assignee: Individual
Current assignee: Individual
Priority date: 2010-01-08
Filing date: 2010-01-08
Publication date: 2011-07-13

Abstract

The invention relates to a method and structure for assisting the takeoff, landing and flying-unrelated operations of airplanes by using a locomotive and a railcar. The mass of a landing gear system essential for completing the takeoff, landing and flying-unrelated operations of an airplane accounts for about 10% of the mass of a traditional airplane; in the method and structure disclosed by the invention, the landing gear system is omitted and replaced with a buffer and locking device equipped for the takeoff, landing and emergency landing of an airplane, and a locomotive, a railcar and other devices for assisting the takeoff, landing and flying-unrelated operations of the airplane, thereby reducing the mass of the airplane during flying, and facilitating the flying-unrelated operations such as repair, maintenance, upkeep and daily power supplies of the airplane. The locomotive and the railcar for assisting the takeoff, landing and flying-unrelated operations of an airplane run on a curvilinear orbit, thereby solving the problem that a fixed wing airplane is limited by a ship deck with a finite length; and the application of a twin ship body increases the turn radius of the orbit, and reduces the manufacturing cost of a ship body; meanwhile, the structures and features of the locomotive and the railcar make the continuous takeoff and landing of a plurality of airplanes possible.

Description

Locomotive, have the landing of railway vehicle second-mission aircraft and flight outside the operation method and structure

One, technical field

The invention belongs to locomotive, railcar; Being used for aircraft cooperates and installs to equipment on the airplane equipment; Aircraft carrier promptly is equipped with the warship of flight deck, and aircraft takes off and land thereon, and is used to keep in repair the fields such as hangar deck of aircraft.

Two, background technology

Speed per hour has entered actual operation stage greater than locomotive and the railcar of 300km/h; In the same way, all solve with the technical matters of speed, butt joint synchronously, wind tunnel experiment can partly solve the aerodynamics problem between locomotive in the docking operation, aircraft and the track under the first cosmic velocity.

Three, summary of the invention

The objective of the invention is: propose locomotive and the railcar second-mission aircraft takes off, operating method and structure outside land and the flight, when taking off, accelerate to the speed of taking off and unlock and take off by locomotive, railcar carrying aircraft; The aircraft of land operations and operating locomotive railcar in the same way, with speed, dock locking synchronously; slow down to reach and shut down the position; locomotive, railcar system provide necessary electric power for the aircraft that stops thereon; be convenient to aircraft daily service, maintenance, maintenance, rest on locomotive have on the railway vehicle or the separability pallet on aircraft be convenient to flight marshalling.

Technology contents of the present invention is: locomotive, railcar second-mission aircraft landing operational system are travelled on the curve track of ship deck, its locomotive, rail automotive system comprise: the side wheel rail system, anti-rollover system, belly and side brake system, reusable separable Fuel Tank, aircraft Support tray and jet power locomotive.

The railcar that travels at ship deck, drive by connecting rod, the superconductor that moves on this connecting rod and the linear electric motors is connected, superconductor, magnetic circuit, guide rail, stator coil are in together in liquid nitrogen or the liquid helium groove, described railcar is made of carbon fibre and light metal material, reduces the interference of electromagnetic linear motor Vent dew to the aircraft electromagnetic equipment.

The equipment that on curve track, moves, the radius of its centripetal force and operation is inverse relation, increases turn radius, reduces locomotive, the railcar normal pressure to the side direction track; Under ship length unmodified situation, adopt twin hull structure, increase beam over deck, increase turn radius, improve ship stability, reduce the naval vessel cost, reach on the finite length ship deck locomotive, the railcar second-mission aircraft purpose of taking off.

The locomotive that second-mission aircraft takes off that is used at land locomotion, railcar is to have the wing of the adjustable angle of attack and the vehicle of pressure capsule system, pressure capsule system cooperates with wing, adjust vehicle state of equilibrium and wheel adhesive ability to track, operating locomotive, railcar is looked its length can allow the continuous landing of many airplanes, visual its size of aircraft occupies a joint or a mutiple-unit engine, can separate at random between locomotive joint and the joint or combined characteristics is convenient to the flight marshalling, the shield gas flow wallboard can prevent that the scorching hot air-flow of aircraft from burning to aircraft and other mobile unit of its back.

Description of drawings

Fig. 1 is for jet power locomotive on the ship deck track and do not have alighting gear and have the aircraft of buffering and locking device.

Fig. 2 is a jet rail system braking scheme drawing.

Fig. 3 is the rail locomotive basic block diagram of linear electric motors and driving thereof on the ship deck curve track.

Fig. 4 is for increasing the required twin hull figure of ship deck track turn radius.

Fig. 5 is the jet locomotive second-mission aircraft that travels on the ship deck curve track scheme drawing that takes off.

Fig. 6 is the jet locomotive second-mission aircraft land scheme drawing on the ship deck curve track that travels.

Fig. 7 is the locomotive railcar basic block diagram of land second-mission aircraft landing.

Fig. 8 is the land locomotive, the railway vehicle second-mission aircraft scheme drawing that takes off is arranged.

Fig. 9 is the land locomotive, railway vehicle second-mission aircraft land scheme drawing is arranged.

Concrete implementation step

Further specify below in conjunction with accompanying drawing

Fig. 1 shows jet locomotive on the ship deck curve track, no alighting gear and has the basic block diagram of buffering and locking device aircraft; Among the figure 1-passive rail running and can with body portion from reusable Fuel Tank module; 2-is removable be used for Fuel Tank and body portion from, be used for the explosive module that locomotive main is slowed down; 3-jet power locomotive; 4-can with body portion from or the combination the aircraft Support tray that has wheel flutter; 5-have adjustable linear velocity and and Friction disk between the inertia wheel of distance; The 6-lateral rails; The 7-side wheels; 8-prevents the removable Friction disk of locomotive rollover system: 9-; The 10-belly has the aircraft of buffering and locking device.

Fig. 2 shows and is used for jet rail locomotive brake or passive operational system scheme drawing, wherein Vo＞V1＞V2 ... Vn; Vo is the locomotive linear velocity, V1, V2 ... Vn is the inertia wheel linear velocity, between the Friction disk of locomotive in service and the inertia wheel by the friction positive energy exchange, finish the moderating process of locomotive, the linear velocity of every inertia wheel and can do dynamic adjustment separately apart from the distance of Friction disk, this system can drive between locomotive and the equipment thereof and dock.

Fig. 3 shows that linear motor driving has the railway vehicle basic block diagram; This car body has also alleviated the interference of linear electric motors track electromagnetism Vent dew to the aircraft electromagnetic equipment by light metal and carbon fiber manufacturing when reducing the car body quality.1-has the pull bar of Telescopic among the figure; The 2-magnetic pole; 3-track electrode; The superconductor that 4-moves on electrode track; 5-liquid nitrogen or liquid helium; The 6-car body; 7-liquid nitrogen or liquid helium groove, wherein the superconductor that moves on drive stay and the track is connected, and is used for finishing operation and the braking of self-propelled vehicle on curve or rectilinear orbit.

Fig. 4 is shown twin ship structure scheme drawing, the purpose of doing like this is in order to increase the turn radius of rail locomotive on ship deck, reduce the normal pressure of locomotive to the side direction track, reach the auxiliary fixed wing aircraft of the finite length ship deck railcar purpose of taking off, this practice has reduced the cost on naval vessel; This kind naval vessel still has good stable under the less situation of floating line.

Fig. 5 is shown the jet locomotive second-mission aircraft that travels on the ship deck curve track scheme drawing that takes off, and the jet locomotive with carrying aircraft of initial velocity Vo accelerates to V by bend ₁Aero-engine starts and accelerates to takeoff speed V jointly with the jet locomotive of track at this moment ₂, unlock, to take off, jet locomotive is flame-out, blast module work between Fuel Tank and the main body, Fuel Tank is accelerated to V ₄Continue operation forward, and cooperate with brake system, slowing down by bend stops; The jet supersonic plane vehicle main body is reduced to V by blast module work recoil with speed ₃, the main body locomotive air resistance after the separation obviously increases, the matching track brake system, and deceleration stops.The purpose of doing like this is to alleviate the local pressure of track equipment in service to the side direction track, advancing the track service life.

Fig. 6 is shown the jet locomotive second-mission aircraft land scheme drawing that travels on the ship deck curve track, the jet locomotive that has initial velocity and be a Vo by bend accelerate to the land aircraft synchronously, with fast V ₁Aircraft and jet rail locomotive in the same way, with speed, dock synchronously, docking time is that 0.5-1 is about second, after the butt joint locking, aircraft and jet locomotive are flame-out simultaneously, blast module work between Fuel Tank and the main body, Fuel Tank are accelerated to that V4 continues operation forward and cooperate to be decelerated to brake system and stops; The jet supersonic plane vehicle main body relies on the work of blast module with the aircraft that is carried, and speed reduces to V3, and the matching track brake system stops by the bend deceleration.

More than be used for Fuel Tank and body portion from and be used for explosive carrier that main body slows down and explosive modularization, normalisation; And can change at any time, the cargo-carring module of jet locomotive each run will be according to the equivalents of the operational outfit biggest quality, F-Zero, the blast of stopping distance selection recently module, control system will be according to the equipment quality on the orbit, the speed of operation and stopping distance are ignited some blasts module, prevent unexpected the generation.

Above-described passive travel in orbit and can be with main body the Fuel Tank of separable or combination, will be according to the task amount quantitative loading fuel of finishing at every turn, guarantee once to use up, can reduce the operating consumption of fuel of jet locomotive like this, increase jet locomotive simultaneously in the orbital motion process safe.

The rail locomotive of linear motor driving is described below by Fig. 5 at second-mission aircraft take-off process on the curve track: the locomotive of carrying aircraft begins to accelerate to V1 by bend with initial velocity Vo under the promotion of linear electric motors pull bar, this moment, the aero-engine starting accelerated to takeoff speed V2 to kinematic scheme jointly with orbit motor, unlock and take off, linear electric motors feed counter-current, the intensity of counter-current is according to the distance of residue rectilinear orbit, the maximum normal pressure of the speed of kinematic scheme and quality and bend carrying is selected suitable numerical value, the direction that counter-current feeds motor back stay generation power F is opposite with the rail locomotive velocity reversal, and rail locomotive slows down under the effect of variable braking power F and stops.

Linear motor driving rail locomotive second-mission aircraft land process on curve track is described below by Fig. 6: the promotion lower railway locomotive at the linear electric motors pull bar is accelerated to and land aircraft synchronous same-speed V1 by bend by speed Vo; aircraft and locomotive are in the same way; with speed; butt joint synchronously; butt joint locking back aircraft is flame-out; linear electric motors feed counter-current; counter-current intensity is according to the kinematic scheme quality; remaining rectilinear orbit distance; the maximum normal pressure of the local carrying of the speed of kinematic scheme and bend is selected rational numerical, is decelerated under the braking of kinematic scheme earthquake power F to shut down the position.

Fig. 7 is shown the land second-mission aircraft and takes off, lands and the outer locomotive that moves of flight, and railcar basic structure, 1-is the power vehicle that has management information system and rail pressure sensor-based system among the figure; But the 2-independent adjustment angle of attack or increase air resistance reach the wing that slows down for car body; 3-has management information system, the locomotive of device such as pressure capsule system, but the 4-independent adjustment angle of attack or to increase air resistance be that car body slows down or adjusts and cooperate and rests on locomotive and board a plane and change the wing of its air dynamic behaviour, 5-has the shield gas flow wallboard of elevating function, this wallboard and rear vehicle wall panel are used, the scorching hot air-flow that prevents aircraft burn thereafter aircraft or other mobile unit.

Fig. 8 shows the locomotive of land carrying aircraft, and railcar accelerates to the speed of taking off, and rises the shield gas flow wallboard, and aircraft unlocks and takes off.

Fig. 9 shows the land locomotive, the aircraft of railcar and landing in the same way, with speed, dock locking synchronously and is decelerated to and shuts down the position, separate then and organize into groups.

On land in locomotive, the railcar second-mission aircraft landing process, the angle of attack that locomotive railcar pressure sensor is in time adjusted each wing according to wheel to the pressure or the cooperation stop aircraft aerodynamics characteristic thereon of track, prolong the service life of wheel and track, this wing also has deceleration simultaneously.

Locomotive, the track of railcar operation can be laid on areas such as shallow sea, marsh, river, beach by bridge.

Aircraft after every land occupies a joint or mutiple-unit engine or occupies a pallet that has wheel flutter according to its needs, is convenient to the flight marshalling like this.Locomotive, the railcar second-mission aircraft land of taking off reduce the aircraft vibratory impulse that alighting gear brings aircaft configuration when taking off land in the past, prolong the aircraft utilization life-span.

Claims

1. operating method and the structure outside locomotive, the landing of railcar second-mission aircraft and the flight, comprise that no alighting gear belly has the aircraft of buffering and blocking device, orbital motion system and equipment, it is characterized in that: the process of taking off reaches takeoff speed by locomotive, railcar carrying aircraft, and unlocking reaches the purpose of taking off; The aircraft of locomotive, railcar and land with speed, synchronously dock locking, run slowly to the shutdown position.

2. method according to claim 1 and structure is characterized in that: operate in the locomotive on the ship deck, railcar second-mission aircraft landing operational system has side rails, side and belly brake system, blast recoil deceleration system, separable aircraft pallet and the rail jet power locomotive of being convenient to the aircraft flight marshalling.

3. method according to claim 1 and structure, it is characterized in that: the locomotive of operation is the locomotive of unpowered systems outside landing of orbital motion second-mission aircraft and the flight, its operation scheme promotes by pull bar, the linear electric motors power system related with pull bar, all being included in liquid nitrogen becomes in the liquid helium groove, pull bar moves in the slit above groove, finishes the propelling or the braking of guideway vehicle, and pull bar has Telescopic.

4. method according to claim 1 and structure is characterized in that: the naval vessel of the orbital motion system of carrying second-mission aircraft landing can be twin hull.

5. method according to claim 1 and structure is characterized in that: locomotive and railcar be for there being movable wings, pressure capsule system, and automatic lifting functional shielding air-flow wallboard is arranged; Pressure capsule system cooperates with wing, adjusts car body balance and the wheel adhesive ability to track.Movable wings and shield gas flow wallboard can be used for increasing the air resistance of locomotive.

6. method according to claim 1 and structure is characterized in that: operating locomotive, motor-drivenly have locomotive can assist the continuous landing of many airplanes, locomotive, railcar is separable and combined characteristics at random, helps the flight marshalling.