CN100551779C

CN100551779C - Destination on the intermediate ship

Info

Publication number: CN100551779C
Application number: CNB2007100704211A
Authority: CN
Inventors: 黄金伦
Original assignee: Individual
Current assignee: Individual
Priority date: 2007-07-31
Filing date: 2007-07-31
Publication date: 2009-10-21
Anticipated expiration: 2027-07-31
Also published as: CN101234675A

Abstract

Destination on a kind of intermediate ship, be fit to the blimp landing of no alighting gear, aircraft ventral during landing stretches out a hook, and along the glide of energy storage band upward slope direction, a fusiformis frame that is located on the energy storage band is arranged below first section span (A), hooked with convenient, dragged flywheel, and drive synchronous pulley and synchronous band, flower wheel, drive frequency conversion generator (not shown) electrification energy storage in the bow again with the beam warp centrifugal clutch by the energy storage band that hooked with flywheel, very fast deceleration in aircraft being gone up a slope slide, force of inertia is by energy storage, upward slope counteract gravity forces.This airport helps expanding the ocean and utilizes and save land land used.

Description

Destination on the intermediate ship

Technical field

The invention belongs to the adrm that lands on the ship of medium-sized size, be only applicable to use on blimp or small commercial aircraft or scientific research, the national defence.The present invention is not suitable for all aircrafts with alighting gear, only is fit to the aircraft (as application number 200710070081.2 and application number 200710067410.8) of no alighting gear.

Background technology

Existing aircraft adopts alighting gear landing, the problem that exist the kinetic energy of aircraft landing not store, landing takies the large tracts of land soil.

Summary of the invention

The invention provides destination on a kind of intermediate ship, can save alighting gear, its purpose: energy-saving and emission-reduction, saving soil, expansion ocean utilize, the development ocean science schools; Change and get used to land school-running modes.Solve the problem that kinetic energy can not store, landing takies the large tracts of land soil of aircraft landing.

Technical scheme of the present invention is: comprise energy storage band, flywheel, first deflector roll and second deflector roll, energy storage band envelope first section span and second section span, first section span is provided with the fusiformis frame that is hooked the energy storage band and slow down and glide by landing aircraft belly hook in order to convenient; The energy storage band is a band synchronously, and the two ends at its open loop mouth place all are connected on the fusiformis frame, and energy storage band and fusiformis frame are supported on flywheel, roller and first deflector roll and second deflector roll, and the fusiformis frame is on flywheel, first deflector roll and second deflector roll; The flight force of inertia that described second section span is aircraft by the energy storage band hold, be converted into storage can runway, also be aircraft at short square from interior quick deceleration, impulse force is climbed the gravitational low slake up to the upslope runway that closes on the hardstand advancing; This hardstand is in horizontality a little less than the vertex of second section span during shutdown, running-fit is being adorned a synchronous pulley and an elevator wheel parallel with one another on the pivot of this hardstand, and this synchronous pulley is by the synchronous strap drive second energy storage frequency conversion generator; The cable wire of reeling on this elevator wheel, the end of cable wire is being fixed the lasso of two glue belt one classes, can entangle the driving engine or the left and right of aircraft; The energy storage band that is hooked by aircraft drives described flywheel and axle thereof, and with the synchronous pulley that connects with centrifugal clutch of this coaxial line and band synchronously, and the flower wheel of running-fit on balance staff, again with the synchronous pulley in parallel with flower wheel, transmission gives that the first energy storage frequency conversion generator generates electricity, the electric power storage energy storage.

The present invention has the following advantages:

1, destination is adapted at developing on each ocean surface our ocean science schools on the intermediate ship, teacher, coach, police be teacher, professor, also be the defender of motherland's national defence simultaneously, the student after the several years, promptly become carry on more advanced studies, the talent of fresh combatants aspect military service or aquatic products processing, marketing, aviation, the navigation;

2, destination on the intermediate ship is established the amorphous silicon membrane cell photovoltaic power generation system more and is covered on the ship, prevent or fewly spied upon supervision by satellite, safeguard simultaneously Chinese fishing boat prevent by the pirate plunder may;

3, cooperate scientist's ocean scientific investigation ship and growth troop camp, ocean;

4, select the poor student of a collection of moral qualities, intellectual ability, physical fitness and aesthetic appreciation and other aspiration juvenile students to go to school ocean science schools, preferably allow them assist fishery, marine fishery and steer a ship, flight attachment, and subsidize students by enterprise or national charity organization and fully freely go to school; Can save land like this and run a school, do factory and training base, the resource that reduces in the territorial waters is stalked exploitation by other country;

5, during aircraft landing, be to have angle of attack climbing to glide, just in case can not land, aircraft can leap straight, can not land with the alighting gear aircraft that lands as land, draws high head again with regard to dangerous and long runway very;

6, the A of Fig. 1, B span are not to equal airport runway length, and it is the picture square edge, and the true length of runway is the camber line near hypotenuse.

Description of drawings

Fig. 1 is " destination on the intermediate ship " lateral plan.

Fig. 2 is the top view of fusiformis frame F, energy storage band G, roller J.

Fig. 3 is the sectional position figure of airframe cross section, roller, energy storage band.

The specific embodiment

Referring to Fig. 1, when the aircraft on right side was arrived in bow by plane in the A section span, the aviator emitted belly hook D, went up a slope by white arrow and prepared to land, and the A section span 18m of this section is the landing first step that belly hook D hooks fusiformis frame F.Fusiformis frame F is the picture prism mesh a bit, when it is hooked by belly hook D, " mesh " be elongated draw flat, in drawing flat process because the frame elasticity of fusiformis frame F, give one in aircraft well buffering, flexibility started energy storage band G, when hooking energy storage band G and carry out energy storage by aircraft, flying speed lowers, lift divergence, part weight is pressed to energy storage band G, and the effect of the amount of deflection of energy storage band G and spring 5, spring 25, spring 32 guarantees flexible deceleration of aircraft and building better soft landing performance.Above-mentioned each spring is signal, and reality all is to keep flexible the landing or maintenance constant tension power and the shock absorption device established.

B section span (B ≈ 130m) be aircraft the flight force of inertia by energy storage band G hold, be converted into storage can runway, also be aircraft at short square from interior quick deceleration, impulse force is climbed the gravitational low slake up to the upslope runway that closes on the hardstand advancing.

C section span (C ≈ 15m) is the hardstand.It is in horizontality a little less than the vertex of B section during shutdown; Running-fit is being adorned two wheels in parallel---synchronous pulley on pivot C1, and synchronous pulley can transmission energy storage frequency conversion generator C2 with synchronous band; One is the elevator wheel, the cable wire of reeling on the elevator wheel, and the end of cable wire is being fixed the lasso of two glue belt one classes, can entangle the driving engine or the left and right of aircraft.

When aircraft will enter storage canopy C4, be the heart hardstand C, by pivot C1 earlier, cw turns over a θ angle, receive descending roller road obliquely down, the tail that makes aircraft downwards, with descending shown in the dotted arrow, retreat and roll down, if unclamp the brake of elevator wheel, with gravity, drive elevator wheel and wheel (synchronous pulley) on pivot C1 the running-fit rotation in parallel with it of aircraft, (this is energy storage for the second time to make second frequency conversion energy-reserving generator C2 generating by synchronous band at this moment; Energy storage for the first time is to drive energy storage band G, energy storage when just landing at aircraft).Store canopy 4C up to allowing aircraft back off to.

If take off: the magnetic suspension of extending deck K from storage canopy 4C outside the sideslip runway moves on on the ship is taken off on the guide rail, can be by take off on the K1 (" taking off " please allow apply for next time again).

Fig. 2, fusiformis frame F have former and later two " people " fonts elastic shelf F1, F3 and about two frame F2 surround, (this energy storage band that is different from application number 200710070081.2 is only by a direction cycle operation) of running time image loom shuttle commute, fusiformis frame F is overcome the elastic force of elastic shelf F1, F3 by the inertia ahead power of aircraft, about two frame F2 draw over to one's side almost and together, so that fusiformis frame F is elongated, draws is flat (this brings a fine buffer action when hooking the energy storage band to aircraft).

Elastic shelf F1, F3 (Fig. 2) use high tensile steel wire to make as the rubber of " embedding method silk " liner, and front and back are connected with hinge pin F4 with energy storage band G respectively; F2 also be lined with high tensile steel wire, mould pipe fitting with transparent polyurethane (PU), the low-voltage LED light-emitting device is installed in the pipe, make and send sheen evening; Also be connected with elastic shelf F1, F3 with hinge pin.

Offshore conditions is stable unlike land, so serve the belly hook D of landing aircraft to hook with very big fusiformis frame.

The width G 1 ≈ 38cm of the energy storage band G of this programme is an a ratio much bigger synchronous band commonly used, and the two ends, the left and right sides at its open loop mouth place all are connected on the fusiformis frame F.When waiting landing, fusiformis frame F is on this span of flywheel 4, first deflector roll 6 and second deflector roll 23 (please contrast Fig. 1, Fig. 2), flywheel 4 also is a kind of synchronous pulley, the auxiliary cylindrical shell in it and the left and right sides constitutes a big deflector roll---and hold fusiformis frame F, this and first deflector roll 6, second deflector roll 23 are in like manner.

During energy storage the like mesh of fusiformis frame be elongated, draw flat after, space among the left and right sides ranks of roller J that can be by holding ventral, the distance of the roller J and first deflector roll 6 is very big, there is very big glide power starting stage because aircraft has just landed, do not need roller J, roller all is to have certain elastomeric free gear---need not power or plunging joint.

The energy storage first time of Fig. 1: the energy storage band G that is hooked by aircraft, drive flywheel 4, axle 3, and with the synchronous pulley that connects with centrifugal clutch of axle 3 coaxial lines and band P1 flower wheel P2 (running-fit is on balance staff 1) is again with the synchronous pulley in parallel with flower wheel P2 (drawing) synchronously, transmission gives that the first energy storage frequency conversion generator (drawing) generates electricity, the electric power storage energy storage in bow.E is the polycarbonate translucent cover, can send out sheen caution aircraft evening and arrive in bow by plane in the sheen sky; E1 is an electromagnetic wave launcher, aircraft can be navigated outside hundreds of rice aim at fusiformis frame longitudinal central axis line.H1 is horizontal monitoring device, monitors that belly hook D hooks the signal of fusiformis frame F, in time passes to the power that control tower is adjusted frequency conversion generator, and the appliance computer control system guarantees safe landing.H, horizontal monitoring device H1 (laterally monitoring device) are at shipboard, and be all lighter, little, with composite materials manufacturing (being not used in battleship).

Fig. 3 is fuselage cross section, roller, energy storage band cross section; R is the fuselage cross section, and S is that wing, U, U1 are that turning rolls, V are roller, and T is driving engine carrying roller (if driving engine on fuselage then T is in the free time), and G is the energy storage band.

Claims

1, destination on a kind of intermediate ship, it is characterized in that, comprise energy storage band, flywheel, first deflector roll (6) and second deflector roll (23), energy storage band envelope first section span (A) and second section span (B), first section span (A) is provided with the fusiformis frame that is hooked the energy storage band and slow down and glide by landing aircraft belly hook in order to convenient; The energy storage band is a band synchronously, the two ends at its open loop mouth place all are connected on the fusiformis frame, energy storage band and fusiformis frame are supported on flywheel, roller and first deflector roll (6) and second deflector roll (23), and the fusiformis frame is on flywheel (4), first deflector roll (6) and second deflector roll (23); Described second section span (B) be aircraft the flight force of inertia by the energy storage band hold, be converted into storage can runway, also be that aircraft slows down in short range fast, impulse force is climbed the gravitational low slake up to the upslope runway that closes on the hardstand advancing; This hardstand is a little less than the vertex of second section span (B), be in horizontality during shutdown, running-fit is being adorned a synchronous pulley and an elevator wheel parallel with one another on the pivot of this hardstand, and this synchronous pulley is by the synchronous strap drive second energy storage frequency conversion generator (C2); The cable wire of reeling on this elevator wheel, the end of cable wire is being fixed the lasso of two glue belt one classes, can entangle the driving engine or the left and right of aircraft; The energy storage band that is hooked by aircraft drives described flywheel and axle thereof, and with the synchronous pulley that connects with centrifugal clutch of this coaxial line and band synchronously, and the flower wheel of running-fit on balance staff, again with the synchronous pulley in parallel with flower wheel, transmission gives that the first energy storage frequency conversion generator generates electricity, the electric power storage energy storage.

2, destination on the intermediate ship according to claim 1, it is characterized in that, described fusiformis frame (F) have former and later two " people " fonts elastic shelf and about two frames surround, running time image loom shuttle commute, this fusiformis frame is overcome the elastic force of elastic shelf by the inertia ahead power of aircraft, about two frames draw over to one's side almost and together, elongate, draw the fusiformis frame flat.