CN206068190U - Multipurpose dynamic energy storage type carrier-based aircraft ejector system - Google Patents
Multipurpose dynamic energy storage type carrier-based aircraft ejector system Download PDFInfo
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- CN206068190U CN206068190U CN201620922278.9U CN201620922278U CN206068190U CN 206068190 U CN206068190 U CN 206068190U CN 201620922278 U CN201620922278 U CN 201620922278U CN 206068190 U CN206068190 U CN 206068190U
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Abstract
This utility model provides a kind of multipurpose dynamic energy storage type carrier-based aircraft ejector system, including ejection module, playback module and external power-equipment, ejection module is identical with playback modular structure, playback module is coordinated with more than one ejection module to be carried out disperseing dynamic accumulation of energy and concentrates whole kinetic energy to drive the acting of steel wire rope bivector traction shuttle straight line, carrier-borne aircraft ejection is gone up to the air, the system structure is simple, low cost, capacity usage ratio is high, entirely modularity and programme-controlled, ejection quality is adjustable, ejection speed is adjustable, it is convenient to process, install and train, it is military school's training and public place of entertainment necessary equipment, the quantity for increasing ejection module or the power for increasing accumulation of energy motor and external power-equipment, the ejection of aircraft carrier is can be directly used for just, it is the essential equipment of Chinese aircraft carrier.
Description
Technical field
This utility model is related to military project or naval equipment technical field, specifically a kind of multipurpose dynamic energy storage type warship
Carrier aircraft ejector system.
Background technology
Steam catapult is used on ten meter Ni Zi level nuclear aircraft carriers in the U.S., and Electromagnetical ejector is in continental rise machine
On test successfully just on Ford level nuclear aircraft carrier test, above two ejector present in application process it is fatal not
Foot is complex structure, expensive, power consumption height, so can only use on nuclear aircraft carrier or super nuclear aircraft carrier or try
Test, on aircraft carrier powered by conventional energy, carrier-borne aircraft can only be taken off using sliding jump formula at present, due to no ejector, it is carrier-borne that sliding jump formula is taken off
Machine can not be fullyed loaded takeoff, and large-scale fixed wing airplane such as antisubmarine plane, early warning plane and shipping fixed-wing aircraft can not all go up aircraft carrier, restriction
The fight capability of aircraft carrier constrains the development of Chinese aircraft carrier.
In prior art, the present inventor is in 201310272662.X patents, a kind of denomination of invention " belt carrier-borne aircraft boosting
A kind of ejector module is disclosed herein for device system and the random boosting work method of dispersion accumulation of energy concentration " one and dispersion accumulation of energy is concentrated
All using external power-equipment, the method for acting, the ejection module have the drawback that the power density of ejection module is little,
Dynamic accumulation of energy power is little, meets 60 tons of ejection with the more ejection module of the carrier-borne aircraft needs integrated configuration improved quality, thus accounts for
It is big with space, it is impossible to power to be launched according to the flexible reasonable distribution of different ejection quality, it is impossible to meet domestic aircraft carrier ejection
The needs of device.
The content of the invention
The purpose of this utility model is to provide a kind of multipurpose dynamic energy storage type carrier-based aircraft ejector system.
The purpose of this utility model is realized in the following manner, is set including ejection module, playback module and external power
Standby, ejection module is identical with playback modular structure, wherein：
Ejection module structure be by cabinet, power transmission shaft, steel wire rope, disk brake, built-in accumulation of energy motor, clutch,
Accumulation of energy power takeoff, ejection controller composition, power transmission shaft are arranged on the centre of cabinet by bearing, and wirerope-winding is positioned at cabinet
In power transmission shaft on, disc brake, accumulation of energy motor, clutch and accumulation of energy are symmetrically arranged with the power transmission shaft that cabinet both sides are stretched out
Power takeoff；
Disc brake includes brake disc and caliper, and the center of brake disc is connected with power transmission shaft, the edge of brake disc with
It is arranged on the caliper on the outside of cabinet to coordinate, on the outside of disc brake, is provided with built-in accumulation of energy motor；
Built-in accumulation of energy motor is made up of rotor and stator winding, and rotor center is provided with bearing and is connected with drive axis
Connect, stator winding is connected with cabinet both sides by electric machine casing；
Clutch is arranged on the outermost end of power transmission shaft, and internal friction disc center and the power transmission shaft of clutch are fixed, clutch
The medial surface of external friction disk is connected with the rotor lateral surface of built-in accumulation of energy motor；
Accumulation of energy power takeoff includes spill accumulation of energy disk and power takeoff, and the inner circle of spill accumulation of energy disk is outer with clutch external friction disk
Circle links together, and power takeoff is connected with the power output shaft of external power-equipment；
Playback module is only responsible for for shuttle drawing return to origin, small power consumption, and built-in accumulation of energy power of motor is enough without connection
External power-equipment；
Runway ditch is provided with the top of cabinet, guide roller in runway ditch, is provided with, slip rope connecting plate is fixed on steel wire rope
Centre, steel wire rope Jing guide rollers extend into runway ditch and pass through from the middle of two carrying rollers of idler machining, Jing reverse rollers and each idler machining
The carrying roller top at top is slided and is returned, then the guide roller on Jing playback module cabinets is connected with the power transmission shaft of playback module；
Ejection controller adopts wireless remote control mode, the Disk brake device in control ejection module and playback module by single-chip microcomputer
Device and clutch work, the beginning and end setting position sensor for launching runway provide control signal for ejection controller；
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, when external power-equipment refers to increase ejection quality
It is motor, diesel engine or the turboshaft engine that extra power is obtained outside built-in accumulation of energy motor slave module by accumulation of energy power takeoff
One or more power-equipments assembly.
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, accumulation of energy power takeoff be belt pulley, shaft coupling or from
One kind in clutch.
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, clutch is pneumatic clutch or electromagnetic clutch
In one kind.
The using method of multipurpose dynamic energy storage type carrier-based aircraft ejector system is as follows,
Ejection system is by ejection module, playback module, runway ditch module, electric energy scheduling module and power storage module group
Into in order to prevent multi rack carrier-borne aircraft while catapult-assisted take-off generation collision accident, four on aircraft carrier set ejection system is to enter in turn mostly
Row carrier-borne aircraft catapult-assisted take-off operation, most two frame carrier-borne aircrafts of catapult-assisted take-off simultaneously, so more than two sets of ejection system is constituted
One big system, is used to the electric energy unified allocation of resources that the built-in generator of each ejection module sends using electric energy scheduling module,
By in electric energy unified allocation of resources to the ejection system for launch operation or store it is standby in power storage module；
Built-in motor in ejection module is dynamoelectric and power generation dual-purpose motor, and the built-in motor in module is launched per platform external
It is exactly a Compact Power Plant that power-equipment drives lower, and a set of ejection system is made up of multiple stage ejection module, an ejection module
At least 10,000 kilowatts of external aerodynamic power, at least 30,000 kilowatts of three ejection modules, this is launch 60 tons of load basic
Energy reversal, an aircraft carrier are four sets of ejection systems, and generated energy is 120,000 kilowatts, and ejection system is not only without the electricity of consumption aircraft carrier
Electric energy can also be provided for aircraft carrier, by unified allocation of resources electric energy, four sets of ejection systems carry out ejection operation, i.e., a set of ejection in turn
System carries out ejection operation, and three sets of ejection systems launch operation for which using the electric energy that ejection gap sends and provide abundance in addition
Electric energy, makes the mutual redundancy of electric energy of four sets of ejection systems generations, the electric energy produced during non-ejection training by unified allocation of resources electric energy
Other electricity systems for aircraft carrier can also be concentrated to use, by the scientific and reasonable allotment of electric energy, can further improve the utilization of the energy
Rate, makes the more efficient energy-conservation of domestic aircraft carrier.
Constitute ejection module, playback module, runway ditch module, electric energy mixing system module and the power storage of ejection system
Module, also can not only assemble on continental rise airport, islands and reefs airport in nuclear power and aircraft carrier over-assemble powered by conventional energy into ejection system
Into ejection system, moreover it can be used to navigate institute and various public places of entertainment are assembled into simulation entertainment training system.
The beneficial effects of the utility model are：Simple structure, low cost, capacity usage ratio are high, entirely modularity and journey
Controlization, ejection quality is adjustable, and ejection speed is adjustable, convenient processing, installation and training, increases the quantity increase simultaneously of ejection module
The power of accumulation of energy motor and external power-equipment, so that it may be directly used in the ejection of aircraft carrier, will be Science in Future in China aircraft carrier warship
The essential equipment of carrier aircraft ejector.
Description of the drawings
Fig. 1 is the overall structure diagram that a kind of multipurpose dynamic energy storage type carrier-based aircraft ejector launches module.
Fig. 2 is ejection system embodiment schematic diagram；
Fig. 3 is electric energy distribution principle block diagram；
Fig. 4 is external power equipment configurations schematic diagram.
Description of reference numerals：Cabinet 1, electric machine casing 2, power transmission shaft 3, power takeoff 4, accumulation of energy disk 5, clutch external friction disk 6,
Clutch internal friction disc 7, stator winding 8, rotor 9, caliper 10, brake disc 11, ejection deck 12, the connection of shuttle 13, shuttle
Plate 14, steel wire rope 15, linear bearing 16, guide roller 17, reverse rollers 18, idler machining 19, external power-equipment 20, runway ditch
21。
Specific embodiment
With reference to Figure of description multipurpose of the present utility model dynamic energy storage type carrier-based aircraft ejector ejection module is made with
Under explain.
Electromechanical integration dynamic energy storage type carrier-based aircraft ejector system of the present utility model, including ejection module, playback mould
Block, external power-equipment, ejection controller, electric energy scheduling module and power storage module, ejection module and playback modular structure
Identical, playback module is coordinated with more than one ejection module to be carried out disperseing dynamic accumulation of energy and concentrates whole kinetic energy to drive steel wire rope double
To the straight line acting of traction shuttle, carrier-borne aircraft ejection is gone up to the air by shuttle, wherein：
The structure of ejection module is by cabinet 1, power transmission shaft 3, steel wire rope 15, disk brake, built-in accumulation of energy motor, clutch
Device, accumulation of energy power takeoff composition, power transmission shaft 3 are arranged on the centre of cabinet 1 by bearing, and the end of steel wire rope 15 is held within
On power transmission shaft 3 in cabinet 1, the both sides of steel wire rope 15 are provided with brake disc 11, solid with the caliper 10 that brake disc 11 coordinates
The inner side of cabinet 1 is scheduled on, on the power transmission shaft 3 that 1 liang of outside of cabinet is stretched out, accumulation of energy motor, clutch and accumulation of energy power taking is symmetrically arranged with
Device；
Built-in accumulation of energy motor is made up of rotor 9 and stator winding 8, and rotor 9 is provided centrally with bearing and is rotated with power transmission shaft 3
Connection, stator winding 8 are connected with 1 both sides of cabinet by electric machine casing 2；
Clutch is arranged on the outermost end of power transmission shaft 3, and 7 center of internal friction disc and the power transmission shaft 3 of clutch are fixed, clutch
The medial surface of external friction disk 6 be connected with 9 lateral surface of rotor of built-in accumulation of energy motor；
Accumulation of energy power takeoff includes spill accumulation of energy disk 5 and power takeoff 4, inner circle and the clutch external friction disk of spill accumulation of energy disk
Cylindrical to link together, power takeoff is connected with the power output shaft of external power-equipment；
Runway ditch is provided with the top of cabinet, guide roller in runway ditch, is provided with, slip rope connecting plate is fixed on steel wire rope
Centre, steel wire rope Jing guide rollers extend into runway ditch and pass through from the middle of two carrying rollers of idler machining, Jing reverse rollers and each idler machining
The carrying roller top at top is slided and is returned, then the guide roller on Jing playback module cabinets is connected with the power transmission shaft of playback module；
Ejection controller adopts wireless remote control mode, the Disk brake device in control ejection module and playback module by single-chip microcomputer
Device and clutch work, the beginning and end setting position sensor for launching runway provide control signal for ejection controller；
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, when external power-equipment refers to increase ejection quality
It is motor, diesel engine or the turboshaft engine that extra power is obtained outside built-in accumulation of energy motor slave module by accumulation of energy power takeoff
One or more power-equipments assembly.
External power-equipment can also be the dual-function motor of electromotor and motor.
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, accumulation of energy power takeoff be belt pulley, shaft coupling or from
One kind in clutch.
Described multipurpose dynamic energy storage type carrier-based aircraft ejector system, clutch is pneumatic clutch or electromagnetic clutch
In one kind.
Embodiment 1
Ejector system dispersion accumulation of energy concentrates acting principle as follows：
1）Each ejection module arranges two built-in accumulation of energy motors, while turning by the built-in accumulation of energy motor of Frequency Converter Control
Speed, the rotor of built-in accumulation of energy motor are rotated into dynamic accumulation of energy shape in the dynamic accumulation of energy power takeoff of drive simultaneously of power transmission shaft overhead idling
State, the recessed disk of the accumulation of energy on power takeoff are a flywheels suitable with rotor diameter quality, and disk brake is in braking shape
State, clutch are in release conditions, and power transmission shaft is static, and the steel wire rope being wrapped on power transmission shaft does not do work to shuttle traction, static
Ejection race start above playback module；
When the module big mass objects of ejection are launched, two built-in accumulation of energy motors pass through two accumulation of energy power takeoffs and two respectively
Individual external power-equipment connection, obtains extra shaft power to increase the ejection power of module；
During two accumulation of energy motor no powers, which is driven to rotate by accumulation of energy power takeoff by two external power-equipments, two
Accumulation of energy motor makees flywheel use；
As shaft power can be separated or be closed by power takeoff by two built-in accumulation of energy motors and two external power-equipments
And, enable ejection module neatly to select different shaft power to launch the carrier-borne aircraft of different quality；
In the bottom of runway ditch, each ejection module has one group of steel wire rope to be connected to biography to some ejection module longitudinal arrangements
Between moving axis and shuttle, by boat tracker tow or everybody river in the way of all built-in accumulation of energy motors, accumulation of energy power takeoff and external
The rotation shaft power of power-equipment passes to shuttle, and shuttle then passes to carrier-borne aircraft traction power and hauling speed；
2）Carrier-borne aircraft slides into the initiating terminal of ejection runway, and draw bar and the shuttle of carrier-borne aircraft are hooked together into preparation
Ejection status；
3）Commander sends ejection signal, ejection controller control clutch adhesive, built-in accumulation of energy by Digiplex
Motor enters dynamic accumulation of energy workmanship state, and power transmission shaft is by rotor power taking of the clutch to built-in accumulation of energy motor, drive axis
Haulage cable is wound on power transmission shaft, and often winding one is enclosed, and steel wire rope just draws the length of shuttle one girth of traveling, while increasing
Plus an acceleration, when under rotating speed of the power transmission shaft in setting, 100 meters of long steel wire ropes are all wound on power transmission shaft in 3 seconds,
Carrier-borne aircraft simulation training car is just drawn to ejection runway terminal by shuttle, and carrier-borne aircraft can just accelerate to the acceleration of setting, adjust
The rotating speed of built-in accumulation of energy motor can just obtain required setting ejection speed；
4）When shuttle advances to ejection runway terminal, braking sensor is triggered, launch the disc type of module and playback module
Brake is braked simultaneously, and the clutch for launching module discharges simultaneously, and power transmission shaft is no longer from power taking on built-in accumulation of energy motor, power transmission shaft
Moment skidding, while steel wire rope reversely draws shuttle braking, the ejection inertia that shuttle quality is produced is by the elasticity of steel wire rope
Tension force is offset, and shuttle stops at ejection runway terminal；
5）The disk brake of ejection controller control ejection module and playback module simultaneously brake lag 1-3 seconds, then together
When discharge, the clutch adhesive of the module that playbacks is driven the built-in accumulation of energy rotor power taking of axial rotation, and drive axis are reverse
Winding ejection medium, when traction shuttle returns ejection race start, while triggered point sensor, ejection controller secondary control again
The disk brake of ejection module and playback module is braked simultaneously, and the clutch release of playback module, shuttle are still in ejection runway
Starting point, waits next ejection signal.
Embodiment 2
The using method of multipurpose dynamic energy storage type carrier-based aircraft ejector system, ejection system are by ejection module, playback
Module, runway ditch module, electric energy scheduling module and power storage module composition, in order to prevent multi rack carrier-borne aircraft while catapult-assisted take-off
Generation collision accident, four on aircraft carrier set ejection system are to carry out carrier-borne aircraft catapult-assisted take-off operation in turn mostly, are at most launched simultaneously
Take off two frame carrier-borne aircrafts, so more than two sets of ejection system is constituted into a big system, using electric energy scheduling module to each
The electric energy unified allocation of resources that the built-in generator of ejection module sends is used, by electric energy unified allocation of resources to the ejection for launching operation
In system or store it is standby in power storage module；
Built-in motor in ejection module is dynamoelectric and power generation dual-purpose motor, and the built-in motor in module is launched per platform external
It is exactly a Compact Power Plant that power-equipment drives lower, and a set of ejection system is made up of multiple stage ejection module, an ejection module
At least 10,000 kilowatts of external aerodynamic power, at least 30,000 kilowatts of three ejection modules, this is launch 60 tons of load basic
Energy reversal, an aircraft carrier are four sets of ejection systems, and generated energy is 120,000 kilowatts, and ejection system is not only without the electricity of consumption aircraft carrier
Electric energy can also be provided for aircraft carrier, by unified allocation of resources electric energy, four sets of ejection systems carry out ejection operation, i.e., a set of ejection in turn
System carries out ejection operation, and three sets of ejection systems launch operation for which using the electric energy that ejection gap sends and provide abundance in addition
Electric energy, makes the mutual redundancy of electric energy of four sets of ejection systems generations, the electric energy produced during non-ejection training by unified allocation of resources electric energy
Other electricity systems for aircraft carrier can also be concentrated to use, by the scientific and reasonable allotment of electric energy, can further improve the utilization of the energy
Rate, makes the more efficient energy-conservation of domestic aircraft carrier.
Described method, the ejection module of composition ejection system, playback module, runway ditch module, electric energy mixing system mould
Block and power storage module, can not only in nuclear power and aircraft carrier over-assemble powered by conventional energy into ejection system, also can continental rise airport,
Islands and reefs airport is assembled into ejection system, moreover it can be used to navigate institute and various public places of entertainment are assembled into simulation entertainment training system.
Preferred embodiment of the present utility model is the foregoing is only, this utility model is not limited to, although ginseng
This utility model is described in detail according to previous embodiment, for a person skilled in the art, which still can be with
Technical scheme described in foregoing embodiments is modified, or equivalent is carried out to which part technical characteristic.It is all
Any modification, equivalent or improvement for being made etc. within the spirit of the present utility model and principle, should be included in practical
Within new protection domain.
The known technology of those skilled in the art is in addition to technical characteristic disclosed in description of the present utility model.
Claims (5)
1. multipurpose dynamic energy storage type carrier-based aircraft ejector system, it is characterised in that including ejection module, playback module, external dynamic
Power equipment, ejection controller, electric energy scheduling module and power storage module, ejection module are identical with playback modular structure, playback
Module is coordinated with more than one ejection module to be carried out disperseing dynamic accumulation of energy and concentrates whole kinetic energy to drive steel wire rope bivector traction to slide
Shuttle straight line does work, and carrier-borne aircraft ejection is gone up to the air by shuttle, wherein：
The structure of ejection module is by cabinet, power transmission shaft, steel wire rope, disk brake, built-in accumulation of energy motor, clutch, accumulation of energy
Power takeoff is constituted, and power transmission shaft is arranged on the centre of cabinet by bearing, and the end of steel wire rope is held within the biography in cabinet
On moving axis, the both sides of steel wire rope are provided with brake disc, and the caliper coordinated with brake disc is fixed on the inner side of cabinet, cabinet two
Accumulation of energy motor, clutch and accumulation of energy power takeoff are symmetrically arranged with the power transmission shaft that outside is stretched out；
Built-in accumulation of energy motor is made up of rotor and stator winding, and rotor center is provided with bearing and is connected with drive axis, fixed
Sub- winding is connected with cabinet both sides by electric machine casing；
Clutch is arranged on the outermost end of power transmission shaft, and internal friction disc center and the power transmission shaft of clutch are fixed, and the outer of clutch rubs
The medial surface for wiping disk is connected with the rotor lateral surface of built-in accumulation of energy motor；
Accumulation of energy power takeoff includes spill accumulation of energy disk and power takeoff, the inner circle of spill accumulation of energy disk and the cylindrical company of clutch external friction disk
It is connected together, power takeoff is connected with the power output shaft of external power-equipment；
Runway ditch is provided with the top of cabinet, guide roller in runway ditch, is provided with, slip rope connecting plate is fixed on the centre of steel wire rope,
Steel wire rope Jing guide rollers extend into runway ditch and pass through from the middle of two carrying rollers of idler machining, at the top of Jing reverse rollers and each idler machining
Carrying roller top is slided and is returned, then the guide roller on Jing playback module cabinets is connected with the power transmission shaft of playback module；
Ejection controller by single-chip microcomputer adopt wireless remote control mode, control ejection module and playback module in disc brake and
Clutch works, and the beginning and end setting position sensor for launching runway provides control signal for ejection controller.
2. multipurpose according to claim 1 dynamic energy storage type carrier-based aircraft ejector system, it is characterised in that external power
It is the electricity that extra power is obtained outside built-in accumulation of energy motor slave module by accumulation of energy power takeoff when equipment refers to increase ejection quality
The assembly of one or more power-equipments of motivation, diesel engine or turboshaft engine.
3. multipurpose according to claim 1 dynamic energy storage type carrier-based aircraft ejector system, it is characterised in that accumulation of energy power taking
Device is the one kind in belt pulley, shaft coupling or clutch.
4. multipurpose according to claim 1 dynamic energy storage type carrier-based aircraft ejector system, it is characterised in that clutch is
One kind in pneumatic clutch or electromagnetic clutch.
5. multipurpose according to claim 1 dynamic energy storage type carrier-based aircraft ejector system, it is characterised in that built-in electricity
Machine is to generate electricity and electric dual-purpose machine, is motor, is electromotor during non-ejection operation during ejection operation.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620922278.9U CN206068190U (en) | 2016-08-23 | 2016-08-23 | Multipurpose dynamic energy storage type carrier-based aircraft ejector system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620922278.9U CN206068190U (en) | 2016-08-23 | 2016-08-23 | Multipurpose dynamic energy storage type carrier-based aircraft ejector system |
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| CN206068190U true CN206068190U (en) | 2017-04-05 |
Family
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| CN201620922278.9U Expired - Fee Related CN206068190U (en) | 2016-08-23 | 2016-08-23 | Multipurpose dynamic energy storage type carrier-based aircraft ejector system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697123A (en) * | 2021-09-17 | 2021-11-26 | 安徽工业大学 | Aircraft carrier shipboard aircraft catapult |
-
2016
- 2016-08-23 CN CN201620922278.9U patent/CN206068190U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113697123A (en) * | 2021-09-17 | 2021-11-26 | 安徽工业大学 | Aircraft carrier shipboard aircraft catapult |
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Granted publication date: 20170405 Termination date: 20170823 |