CN106892131A - A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology - Google Patents
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology Download PDFInfo
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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
- B64F1/04—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
- B60—VEHICLES IN GENERAL
- B60P—VEHICLES ADAPTED FOR LOAD TRANSPORTATION OR TO TRANSPORT, TO CARRY, OR TO COMPRISE SPECIAL LOADS OR OBJECTS
- B60P3/00—Vehicles adapted to transport, to carry or to comprise special loads or objects
- B60P3/06—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles
- B60P3/11—Vehicles adapted to transport, to carry or to comprise special loads or objects for carrying vehicles for carrying aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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Abstract
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology,Including car body,Left center,Left rear wheel,The near front wheel,Driver's cabin,Hydraulic pressure main frame,Launching cradle,Shooting return device,Sound-controlled apparatus,Body,Band parachute empennage,Emitter,Control room,Head,Unmanned plane antenna,Translator combined type screw propeller,Off hind wheel,Taken turns in the right side,Off-front wheel,Its unmanned plane emitter is mounted on car body,With good concealment,Highly versatile,It is easy to maintenance,Battlefield adaptability is good,Maneuverability,The characteristics of reliability is high,And can be suitably used for launching the small and medium size unmanned aerial vehicles of different take-off weights and takeoff speed requirement,As a kind of new vehicle-mounted ejection type unmanned plane,Improve the general technical level of existing unmanned plane,The application prospect of unmanned plane is widened,It is simultaneously special as teenager's research in defense-related science and technology,The frontier science and technology level in defence equipment field is illustrated for teenager,Promote the popularization and development of defence education.
Description
Technical field
The present invention relates to defence education model field, more particularly to a kind of special vehicle-mounted bullet of teenager's research in defense-related science and technology
Penetrate formula unmanned plane.
Background technology
Since the thirties in 20th century, the development of unmanned plane and using the history for having had more than 90 years experienced for 20th century
Very long budding period and after fermenting the phase, unmanned plane welcomes the fast growth phase at the beginning of 21 century, and progressively extends from military domain
Civil area is arrived, nowadays, civilian unmanned plane is in emergency management and rescue, environment measuring, power-line patrolling, take photo by plane mapping, agricultural plant protection
It is used widely etc. multiple fields.
The country is engaged in the enterprises and institutions of unmanned plane industry just more than 200, in the time of short half a year, unmanned plane from
Blue sea becomes Red sea, and at the same time, unmanned plane demand will also be increased rapidly, it is contemplated that the dual-use unmanned plane of China will be by
6.2 hundred million dollars in 2013 increase to 22.8 hundred million dollars in 2022, and demand total value will be more than 13,400,000,000 dollars, average annual compound growth
Up to 15.57%, unmanned plane developing prospect is become better, and the civilian unmanned plane market of China substantially experienced three phases, first stage
The early stage market demand by military monopolization, inertia is set up, control system technology is immature, high cost, the beginning of the eighties in last century, west
Northern polytechnical university D-4 fixed-wings unmanned plane is that ground mapping and geological prospecting are attempted.Second stage is the nineties in last century
To the beginning of this century, Some Enterprises are explored to unmanned plane, and market starts to civilian " infiltration ", occur in that low side civil small-scale without
It is man-machine.1998, " Xiang bird " depopulated helicopter that South Airways puts on display in the airplane exhibition of Zhuhai, its purposes just included forest fire detection
Gone on patrol with fishing ground.Phase III is exactly current situation, i.e., while military demand is full, civil area is in full flourish, simply
Not yet find suitable profit model.Future portion military enterprise will set foot in civil area, and part city is occupied by technical advantage
, private enterprise also will compete the survival of the fittest by technology, market, qualification, develop Ji Jia leading enterprises.
At present, the civilian unmanned plane of China has 130 Yu Jia research institutes and 15000 frame usage amounts, the kind of civilian unmanned plane
Class is also gradually enriched, including fixed-wing unmanned plane, rotor wing unmanned aerial vehicle, dirigible unmanned plane etc..And above-mentioned achievement, largely
When being high-altitude, high speed, medium-long range, boat long, the military unmanned air vehicle technology such as big load is gradually to the result of civilian " infiltration ".By several
The development in year, the range of application of current unmanned plane has been directed to the multiples such as survey of territorial resources, environmental monitoring, water regime monitoring, the disaster relief
Field.According to incompletely statistics, probably there is several hundred million yuan of magnitude unmanned plane only commercial market in the country's at present, is risen in face of this
Market, relevant enterprise and scientific research institution also move into civilian unmanned plane field one after another, and wherein agricultural plant protection and electric power energy is patrolled and examined
The two fields possess more considerable market scale prospect having shown more urgent demand trend at present, and examine
Considering unmanned plane technology at this stage can meet greatly, therefore the compatible degree of estimated supply and demand is higher.It is civilian with respect to minority at other
Field aspect, unmanned plane relies on its advantage, it is contemplated that also will be in fire control and disaster rescue, public security system, land mapping, meteorological environmental protection prison
Survey, parcel the aspect such as is sent with charge free and given full play to one's skill.
Unmanned plane industry future development has three main trend.Be first civilian unmanned plane field speedup will more than military domain,
With the intensification to the unmanned plane application value degree of awareness, unmanned plane remote sensing mapping, land and sea border defense, forest fire protection, pipeline line walking,
The application of the aspects such as police execution has started to starting, and shows the gesture of fast development.It was predicted that the city of global civilian unmanned plane
Field demand will be quickly incremented by with average annual nearly 30% speed.Secondly, following development of unmanned plane, will persistently reduce manufacturing cost, learns
Cost is practised, with the continuous ripe of technology and progress, the cost of body manufacture will be reduced constantly, and price also will be closeer
The people；The autonomous performance of unmanned plane is improved constantly simultaneously, and user learning cost declines, and operation becomes simpler easy-to-use.Finally, nobody
Machine enterprise will change single management mode, and business revenue source is more polynary, reduces business risk, expands business revenue scale；Current nothing
Man-machine is still an excessive risk, the industry of loss high, and service life is shorter, there is professional requirement to operating personnel, therefore
Can routinely be taken in later stage customer care.
Current unmanned aerial vehicle ejecting mode is mainly launched using Gas fluid pressure, by the way of electromagnetic launch and rato, gas
Hydraulic catapult is a kind of advanced unmanned plane radiation pattern for occurring in the world in recent years, compared with conventional mode, with peace
The advantages of full good concealment, good economy performance, good adaptability, the signals such as light, sound, heat, smog will not be produced, be easy to take-off venue
It is hidden, storage, transport and problem of management in the absence of fire control equipment, and consumable supplies and branch when unmanned plane is launched are carried out every time
The expense for helping guarantee is relatively low, is just adaptable to not by adjusting charging pressure of accumulator and precharge pressure within the specific limits in addition
With unmanned plane take-off weight and the use requirement of takeoff speed.Gas fluid pressure catapult launcher is mountable to carry on car, is easy to machine
Action war and transport transfer, thus device is again with good maneuverability.Foreign countries are at first Gas fluid pressure catapult-assisted take-off technology
Unmanned aerial plane launching system is applied to, because technical sophistication, difficulty are larger, only several countries such as the U.S., Britain and Switzerland grasp
Technique, China has also carried out the research work of unmanned plane Gas fluid pressure catapult-assisted take-off technology.Unmanned plane Gas fluid pressure ejection system
Mainly by Gas fluid pressure energy resource system, slide trolley system, buffering energy-absorbing system, launching cradle system, pulley acceleration system, off-load control
The multiple subsystem composition such as mechanism processed, relieving mechanism, unmanned plane locking mechanism, electric control system, its operation principle is by gas
Hydraulic energy system provides power for unmanned aerial vehicle ejecting, is accelerated on launching cradle as motion carrier with slide trolley system
Unmanned plane safe take-off speed, when the speed that slide trolley is moved together with unmanned plane reaches takeoff speed, unloading control machine
Structure cuts off power source, and slide trolley is buffered absorption systems to be stopped and be a significant slowdown, and unmanned plane is then pushed away in inertia and engine
Separated from slide trolley with takeoff speed in the presence of power and taken off.
ELECTROMAGNETIC LAUNCH TECHNOLOGY is to convert electrical energy into electromagnetic energy, and then is converted into projectile kinetic energy, is done work by electromagnetic force,
Object emission is gone out, so as to complete the technology to object propulsion, ELECTROMAGNETIC LAUNCH TECHNOLOGY all has a wide range of applications in multiple fields
Prospect.Make continental rise tactical weapon, can be used for antitank, tactical air defense, tackle enemy's strategic bomber, cruise missile, various tactics
Ballistic missile etc.；Make shipborne weapon, aircraft and sea skimmer of low-level penetration etc. can be tackled；Make space-based strategic arms, can intercept
Enemy's intercontinental ballistic missile, destroys enemy's military satellite etc.；Further, it is also possible to be installed to cataplane on aircraft carrier, its quality is only
/ 10th of traditional steam catapult；For launching unmanned plane, guided missile etc., precise control is capable of achieving；For tank, plate armour
The blocker of the Initiative Defence System of vehicle, is capable of achieving accurate point-to-point interception.Electromagnetic Launching and conventional radiation pattern phase
Than having the advantages that muzzle velocity high, efficiency high, controllability are good, launch cost is low, the preparatory period is short, transmitting is hidden.Therefore it
There is it to be widely applied in many fields such as scientific experiment, weaponry, missile defense systems, space application, airplane catapult
Prospect.
ELECTROMAGNETIC LAUNCH TECHNOLOGY combines numerous subjects such as power technology, switching technique, material technology and observation and control technology, each
The breakthrough of technology all can effectively advance the development of ELECTROMAGNETIC LAUNCH TECHNOLOGY.Corresponding power technology, switching technique, material technology,
The progress of armature bullet technology also governs the practical step of ELECTROMAGNETIC LAUNCH TECHNOLOGY.Electromagnetic launch lift-off technology is used as a kind of new
The unmanned plane lift-off technology of concept, its essence is that, based on linear electric motors principle, the launch mass of most of vehicle-mounted unmanned aerial vehicles is general
All within 1000 kg, emission rate is generally below 80 m/s, to such launch mass and emission rate, current straight line
Motor technology and high power pulsed source technology are entirely capable of providing technical guarantee for engineer applied, therefore, risen using electromagnetic launch
Winged mode is technically feasible.Electromagnetic ejection system is a kind of emerging transmitting optimization system, is to traditional catapult technique
Important breakthrough, change conventional radiation pattern.Electromagnetic launch application electromagnetic energy drives object, is exactly using the energy of electromagnetism
To promote the object for being launched to move out, theory analysis is proved, it can carry out high speed ejection to large-sized object.Existing electricity
Magnetic catapult technique and high power pulsed source technology are entirely capable of providing technical guarantee for engineer applied.Electromagnetic launch technology of unmanned aerial vehicle system
System can be generally divided into electrical system and mechanical system two parts, and wherein electrical system includes energy storage subsystem, electric adjustment point
System, ejection motor subsystem, tracking-telemetry and command subsystem and information interface subsystem；Mechanical system is by slide trolley system, slow
Rush the multiple subsystem composition such as absorption systems, launching cradle system, unloading control mechanism, relieving mechanism, unmanned plane locking mechanism.With
Existing unmanned plane air-liquid pressure ejection system is compared, and mechanical system is essentially identical, only exists size, the modification of the small range of profile,
Theory of mechanics need not be changed, inheritance is good.For electrical system, it is only necessary to which ejection motor is replaced into air-liquid pressure start
Device, power supply replaces air-liquid potential source, and changes corresponding measure and control device.Advanced electromagnetism hair is so on the one hand introduced
Penetrate technology；On the other hand original unmanned plane air-liquid pressure ejection mature technology has at utmost been used for reference, with good inheritance,
It is easily achieved.Unmanned plane takeoff speed is low, evaded be difficult to avoid that during electromagnetic launch system high speed velocity skin-effect, turn twist
The problems such as with track ablation, while observing and controlling problem when having evaded high speed.The relatively low takeoff speed of unmanned plane so that unmanned electromechanical
Magnetic catapult technique has inborn advantage on practical with respect to other ELECTROMAGNETIC LAUNCH TECHNOLOGYs, and electromagnetic launch technology of unmanned aerial vehicle technology is than it
His ELECTROMAGNETIC LAUNCH TECHNOLOGY has that takeoff speed is low, mass range of taking off is big, transmitting kinetic energy is small, tranmitting frequency is low, power supply is small, accelerate
Spend the technical characterstics such as small, electric current is small.These technical characterstics, with respect to other ELECTROMAGNETIC LAUNCH TECHNOLOGYs for, reduce to power supply, material
The technical requirements of material, switch, while low speed advantage and good inheritance all effectively support electromagnetic launch technology of unmanned aerial vehicle
It is practical.It is contemplated that electromagnetic launch technology of unmanned aerial vehicle technology (at least SUAV electromagnetic launch technology) will be in electromagnetic launch
Move towards practical in technology earliest, and the effectively progress of the related-art technology such as propulsion electromagnetic aircraft airplane catapult.
The present invention devises a kind of teenager by the research to existing unmanned aerial vehicle ejecting mode and future developing trend
The special vehicle-mounted ejection type unmanned plane of research in defense-related science and technology, and monitoring unmanned picture can be transmitted equipped with shooting return device, also
Being provided with parachute empennage protection unmanned plane can release a parachute reduction body injury in time after catching a packet, the transmitting of its unmanned plane
Device is mounted on car body, with good concealment, highly versatile, good easy to maintenance, battlefield adaptability, maneuverability, reliability
High the characteristics of, and can be suitably used for launching the small and medium size unmanned aerial vehicles of different take-off weights and takeoff speed requirement, and the present invention is to car
The design and research of ejection type unmanned plane is carried to the general technical level of raising China unmanned plane, the application of China's unmanned plane is widened
Prospect has very important significance, and has also filled up the blank of China's air science research field, and the present invention also serves as Buddhist simultaneously
Wish what torch education and science Co., Ltd edited in Shan Shi Sanshui District《Chinese middle and primary schools' research in defense-related science and technology reader》Supporting state
Anti- education and the model of teenager's research in defense-related science and technology, it is that teenager illustrates a kind of new vehicle-mounted ejection type unmanned plane letter
Listization operation, improves attention rate and cognition degree of the teenager to Defence business, is preferably to cultivate civil-military inosculation technology
The scientific research reserve in field.
The content of the invention
The invention provides a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology.
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology of the invention, its technical scheme is as follows：
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology of the invention, including it is car body, left center, left back
Wheel, the near front wheel, driver's cabin, hydraulic pressure main frame, launching cradle, shooting return device, sound-controlled apparatus, body, band parachute empennage, hair
Wheel, off-front wheel, the car in injection device, control room, head, unmanned plane antenna, translator combined type screw propeller, off hind wheel, the right side
Body lower end left side is sequentially provided with the near front wheel, left center, left rear wheel from front to back, and the car body lower end right side sets successively from front to back
There are wheel, off hind wheel in off-front wheel, the right side, the car body front end is provided with driver's cabin, control is provided with inside the hydraulic pressure main frame rear end
Room, the car body upper end is provided with hydraulic pressure main frame, and the hydraulic pressure main frame upper end is provided with launching cradle, and the launching cradle rear end is provided with
Emitter, the upper end is provided with body, and the body rear end is provided with band parachute empennage, and the launching cradle upper end is provided with machine
Body, the body rear end is provided with band parachute empennage, and the body front end is provided with head, and the head lower end is provided with shooting side by side
Return device and sound-controlled apparatus, the head upper end are provided with unmanned plane antenna, and the unmanned plane upper antenna end front is provided with powered
Machine combined type screw propeller.
Hydraulic pressure main frame described further is hydraulic means, the launch angle for adjusting launching cradle.
Launching cradle described further is catapult-launching gear, for quickly launching unmanned plane to being gone on patrol and portion in the air
Administration.
Shooting return device described further can instantaneous transmission unmanned plane monitored picture to ground command center.
Sound-controlled apparatus described further is provided with long-range acoustic control receiver, so as to can be completed to unmanned plane by sound instruction
Manipulation.
Band parachute empennage described further can protect the unmanned plane to be released a parachute in time after catching a packet reduction
Body is damaged.
Unmanned plane antenna described further can be used to receive mesh of the radio signal so as to remotely complete manipulation unmanned plane
's.
Emitter described further is ejection starter, when emitter starts, can start hydraulic pressure main frame
Adjust the launch angle of launching cradle and quickly launch unmanned plane to aerial.
Translator combined type screw propeller described further, its propeller is configured with motor special for being provided to propeller
Driving force, drives unmanned plane during flying.
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology of the present invention, its advantage and excellent feature
It is：Monitoring unmanned picture can be transmitted equipped with shooting return device, parachute empennage is additionally provided with and is protected unmanned plane by beating
Can be released a parachute reduction body injury in time after hitting, and its unmanned plane emitter is mounted on car body, with good concealment, be led to
With property it is strong, easy to maintenance, battlefield adaptability is good, maneuverability, reliability high the characteristics of, and can be suitably used for that transmitting is different to play fly weights
Amount and takeoff speed requirement small and medium size unmanned aerial vehicles, and the present invention to the design and research of vehicle-mounted ejection type unmanned plane to improving me
The general technical level of state's unmanned plane, the application prospect for widening China's unmanned plane has very important significance, used as a kind of new
The vehicle-mounted ejection type unmanned plane of type, has also filled up the blank of China's air science research field, while as teenager's national defence section
Skill research special purpose model, is frontier science and technology level that teenager illustrates defence equipment field, promotes the popularization of defence education
And development.
Brief description of the drawings
Fig. 1 is a kind of left view structural representation of the special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology of the invention
Figure.
Fig. 2 is that a kind of right side of the special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology of the invention regards structural representation
Figure.
Illustrate：
Car body 1, left center 2, left rear wheel 3, the near front wheel 4, driver's cabin 5, hydraulic pressure main frame 6, launching cradle 7, shooting return device 8,
It is sound-controlled apparatus 9, body 10, band parachute empennage 11, emitter 12, control room 13, head 14, unmanned plane antenna 15, powered
Wheel 18, off-front wheel 19 in machine combined type screw propeller 16, off hind wheel 17, the right side.
Specific embodiment
Embodiment 1：
With reference to the accompanying drawings 1, a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology shown in accompanying drawing 2, including car
Body 1, left center 2, left rear wheel 3, the near front wheel 4, driver's cabin 5, hydraulic pressure main frame 6, launching cradle 7, shooting return device 8, acoustic control dress
Put 9, body 10, band parachute empennage 11, emitter 12, control room 13, head 14, the combination of unmanned plane antenna 15, translator
Wheel 18, off-front wheel 19 in formula propeller 16, off hind wheel 17, the right side, the lower end of the car body 1 left side is sequentially provided with the near front wheel from front to back
4th, left center 2, left rear wheel 3, the lower end of the car body 1 right side are sequentially provided with wheel 18, off hind wheel in off-front wheel 19, the right side from front to back
17, the front end of the car body 1 is provided with driver's cabin 5, and control room 13, the upper end of the car body 1 are provided with inside the rear end of hydraulic pressure main frame 6
Hydraulic pressure main frame 6 is provided with, the upper end of hydraulic pressure main frame 6 is provided with launching cradle 7, and the rear end of the launching cradle 7 is provided with emitter 12,
The upper end of the launching cradle 7 is provided with body 10, and the rear end of the body 10 is provided with band parachute empennage 11, and the front end of the body 10 is provided with
Head 14, the lower end of the head 14 is provided with shooting return device 8 and sound-controlled apparatus 9 side by side, and the upper end of the head 14 is provided with nobody
Machine antenna 15, the upper end of unmanned plane antenna 15 front is provided with translator combined type screw propeller 16, and the hydraulic pressure main frame 6 is liquid
Pressure device, the launch angle for adjusting launching cradle 7, the launching cradle 7 be catapult-launching gear, for unmanned plane is quickly launched to
Gone on patrol and disposed in the air, it is described shooting return device 8 can instantaneous transmission unmanned plane monitored picture to ground command center,
The sound-controlled apparatus 9 is provided with long-range acoustic control receiver, so that manipulation that can be by sound instruction completion to unmanned plane, the band drop
The umbrella empennage 11 that falls can protect unmanned plane can be released a parachute in time after catching a packet reduction body be damaged, the unmanned plane
Antenna 15 can be used to receive purpose of the radio signal so as to remotely complete manipulation unmanned plane, and the emitter 12 is opened for ejection
Dynamic device, when emitter 12 starts, can start hydraulic pressure main frame 6 and adjust the launch angle of launching cradle 7 and unmanned plane is fast
To aerial, the translator combined type screw propeller 16, its propeller is configured with motor special for being provided to propeller for speed ejection
Driving force, drives unmanned plane during flying.
A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology described above is network game virtual
Intention animation army mould spin-off model in military equipment stage property, is made, without any using ceramics, metal, plastics, PVS materials
Gunpowder, without any machinery and gas percussion lock, without any practice emitter and function, a whole set of vehicle-mounted ejection type nobody
Machine as model equipment be used for teenager's research in defense-related science and technology it is pollution-free, nuisanceless, non-lethal.
The above, is only presently preferred embodiments of the present invention, is not the limitation for making other forms to the present invention, is appointed
What those skilled in the art changed possibly also with the technology contents of the disclosure above or be modified as equivalent variations etc.
Effect embodiment.But it is every without departing from technical solution of the present invention content, according to technical spirit of the invention to above example institute
Any simple modification, equivalent variations and the remodeling made, still fall within the protection domain of technical solution of the present invention.
Claims (9)
1. the special vehicle-mounted ejection type unmanned plane of a kind of teenager's research in defense-related science and technology, it is characterised in that：Including car body (1), a left side
Middle wheel (2), left rear wheel (3), the near front wheel (4), driver's cabin (5), hydraulic pressure main frame (6), launching cradle (7), shooting return device
(8), sound-controlled apparatus (9), body (10), band parachute empennage (11), emitter (12), control room (13), head (14), nothing
Wheel (18), off-front wheel (19), the car body in man-machine antenna (15), translator combined type screw propeller (16), off hind wheel (17), the right side
(1) lower end left side is sequentially provided with the near front wheel (4), left center (2), left rear wheel (3), car body (1) the lower end right side from front to back
Wheel (18), off hind wheel (17) in off-front wheel (19), the right side are sequentially provided with from front to back, and car body (1) front end is provided with driver's cabin
(5) control room (13), is provided with inside hydraulic pressure main frame (6) rear end, car body (1) upper end is provided with hydraulic pressure main frame (6),
Hydraulic pressure main frame (6) upper end is provided with launching cradle (7), and launching cradle (7) rear end is provided with emitter (12), the ejection
Frame (7) upper end is provided with body (10), and body (10) rear end is provided with band parachute empennage (11), and body (10) front end sets
There is head (14), head (14) lower end is provided with shooting return device (8) and sound-controlled apparatus (9), the head (14) side by side
Upper end is provided with unmanned plane antenna (15), and unmanned plane antenna (15) the upper end front is provided with translator combined type screw propeller (16).
2. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described hydraulic pressure main frame (6) is hydraulic means, the launch angle for adjusting launching cradle (7).
3. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described launching cradle (7) is catapult-launching gear, is gone on patrol and is disposed for quickly launching unmanned plane to aerial.
4. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described shooting return device (8) can instantaneous transmission unmanned plane monitored picture to ground command center.
5. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described sound-controlled apparatus (9) is provided with long-range acoustic control receiver, so as to the behaviour to unmanned plane can be completed by sound instruction
Control.
6. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described band parachute empennage (11) can protect unmanned plane to be released a parachute in time after catching a packet and reduce body institute
It is damaged.
7. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described unmanned plane antenna (15) can be used to receive purpose of the radio signal so as to remotely complete manipulation unmanned plane.
8. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described emitter (12) is ejection starter, when emitter (12) starts, can start hydraulic pressure main frame
(6) launch angle of adjustment launching cradle (7) and unmanned plane is quickly launched to aerial.
9. a kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology according to claim 1, its feature
It is：Described translator combined type screw propeller (16), its propeller is configured with motor special for providing driving to propeller
Power, drives unmanned plane during flying.
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| CN201710154540.9A CN106892131A (en) | 2017-03-15 | 2017-03-15 | A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology |
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| CN201710154540.9A CN106892131A (en) | 2017-03-15 | 2017-03-15 | A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106892131A true CN106892131A (en) | 2017-06-27 |
Family
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| CN201710154540.9A Pending CN106892131A (en) | 2017-03-15 | 2017-03-15 | A kind of special vehicle-mounted ejection type unmanned plane of teenager's research in defense-related science and technology |
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