CN106364659A - Information collecting and monitoring device capable of staying in air for long time - Google Patents
Information collecting and monitoring device capable of staying in air for long time Download PDFInfo
- Publication number
- CN106364659A CN106364659A CN201610877874.4A CN201610877874A CN106364659A CN 106364659 A CN106364659 A CN 106364659A CN 201610877874 A CN201610877874 A CN 201610877874A CN 106364659 A CN106364659 A CN 106364659A
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- Prior art keywords
- control system
- flank
- skeleton
- air jet
- puff prot
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/36—Arrangement of jet reaction apparatus for propulsion or directional control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/30—Lighter-than-air aircraft, e.g. aerostatic aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
- G01D21/00—Measuring or testing not otherwise provided for
- G01D21/02—Measuring two or more variables by means not covered by a single other subclass
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
The invention provides an information collecting and monitoring device capable of staying in air for a long time, and belongs to the field of information collection. An information collection device is mounted on a framework and comprises an image collection device, an infrared detection device, a laser ranging device, an acoustic detection device, a wind measurement device, a humidity detection device, a temperature detection device and a radar system, wherein the image collection device is mounted outside the framework; the infrared detection device is infrared imaging equipment and is mounted outside the framework; the laser ranging device is a laser range finder; the acoustic detection device is mounted outside the framework or hung below the framework and connected with the framework through a flexible rope; the temperature detection device is a temperature measurement instrument, mounted outside the framework and connected with a control system; and the radar system is mounted on the framework and connected with the control system. The information collecting and monitoring device has the characteristics of being capable of keeping observing certain areas continuously for a long time and collecting corresponding information, low in manufacturing and operating cost, and high in information obtaining precision.
Description
Technical field
The invention belongs to field of information acquisition, particularly to a kind of information gathering that can be empty for a long time and monitoring dress
Put.
Background technology
Information gathering is a material particular in the middle of people's live and work, does not have information gathering, people just cannot be right
Extraneous affairs are judged and decision-making；The sense organ of people is exactly modal information collecting device, and extraneous information is to human body
Sense organ produce stimulate, thus leaving the information marking in sense organ, these information deliver to brain by nervous system, carry out for people
Analysis, judges and decision-making；The perception of the sense organ of people is very limited amount of in the Nature, so people have invented looking in the distance
Mirror, photographing unit, radar, infrared detector, artificial satellite etc., significantly extend the sensing range of people's sense organ, be mankind's life
Work creates the natural means of more understanding, also creates favourable condition for human use's natural resourcess；But so far,
The mankind still have many can not detect or can not detection in detail natural region, for example, ocean, mountain range, desert, forest etc.
Region, because these regional extents are especially vast, existing detection device can not detect or can not be detailed detect these
Intra-zone in detail, and the state in these regions is in variable condition, its Changing Pattern need real-time collecting its
Information, and these information are compared, find out the state change rule in these regions；People gather these regions at present
Means substantially have following methods, and one is artificial collection, and its defect is that the scope manually travelled is little, and speed is slow, and can enter
Depth is inadequate；Two is airborne vehicle, and its defect is, the area above holdup time short it is impossible to letter in enough this regions of continuous acquisition
Breath change；Furthermore it is exactly artificial satellite, its defect is low precision, high cost.
Content of the invention
For existing ocean, mountain range, desert, the problems referred to above of the information gathering presence of forest, the present invention proposes a kind of
Information gathering and the supervising device that can be empty for a long time it is characterised in that: include main gasbag, solar panel, flank, every
Film, skeleton, air jet system, information collecting device, dynamical system, alignment system, horizontal movement and control system, information transfer and
Tele-control system, equipment compartment, control system, hoverheight control system, telescopic wing；Described main gasbag is spherical, by light
The airtight thin-film material of matter is made；Described solar panel is arranged on the top half surface of main gasbag and flank；Described
Solar panel be flexible film form；Described flank is arranged on the horizontal perimeter of main gasbag, radially distributes；Institute
The flank stated has multiple, is evenly distributed on main gasbag horizontal section periphery；Described flank has 6 or 8；Described barrier film sets
Put inside main gasbag, flank, telescopic wing, by main gasbag, flank, telescopic wing inner space be separated into multiple spaces and each every
The gas bag unit sealing against each other between space；Described skeleton is arranged on inside main gasbag and flank, supports main gasbag and side
The external shape of the wing；Described skeleton is made up of light-weight high-strength material；Described skeleton is by titanium alloy or carbon fibre material
Make；Described air jet system is arranged on the outer end of flank, including outer puff prot, left puff prot, left air jet pipe, outer jet
Pipe, right air jet pipe, shell, right puff prot；Described outer puff prot is arranged on shell, its oral area direction and flank radiation direction
Identical, afterbody is connected with outer air jet pipe；Described left puff prot is arranged on shell, the oral area left side vertical with outer puff prot with
Outer puff prot is vertical, and afterbody is connected with left air jet pipe；Described left air jet pipe is arranged on left puff prot afterbody, one end and left jet
Mouth airtight connection, the other end is connected with gas puff Z-pinch valve；Described outer air jet pipe is installed in outer puff prot afterbody, one end and outer spray
QI KOU airtight connection, the other end is connected with gas puff Z-pinch valve；Described right air jet pipe is arranged on the afterbody of right puff prot, one end with
Right air jet pipe afterbody airtight connection, the other end is connected with gas puff Z-pinch valve；Described shell is arranged on flank end, and and each
Puff prot connects；Described right puff prot is arranged on shell, its oral area direction right side vertical with outer puff prot, with outer jet
Mouthful vertical and with left puff prot coaxial line；Described gas puff Z-pinch valve is arranged on inside air jet system, positioned at air inlet pipe and jet
In the middle of pipe；Described information collecting device is rack-mount, is connected with described control system；Described dynamical system is installed
In equipment compartment, connect with the power input of solar panel and horizontal movement and control system and each functional part
Connect；Described alignment system is arranged in equipment compartment, is connected with control system and dynamical system；Described horizontal movement and control
System is arranged in equipment compartment, is connected with solar panel and air jet system and horizontal movement and control system；Described letter
Breath transmission and tele-control system are arranged in equipment compartment and are connected with the power supply of control system and dynamical system；Described equipment compartment
It is arranged in the middle part of main gasbag；Described equipment compartment is made up of light-weight high-strength material；Described control system is arranged on equipment compartment
The interior power supply with dynamical system and each functional part are connected；Described hoverheight control system is arranged in equipment compartment and control
Gas bag unit in system processed and main gasbag, flank, telescopic wing connects；Described telescopic wing is arranged between each two flank,
Can launch along flank and withdraw.
Described information collecting device is arranged on skeleton, including image acquisition device, infrared detection device, laser ranging
Device, acoustic detection device, apparatus for measuring air quantity, humidity detector, temperature-detecting device, radar system；Described image
Harvester is arranged on outside skeleton, is high-resolution picture pick-up device, is connected with control system；Described infrared detection device is
IR imaging device, is arranged on outside skeleton, is connected with control system；Described laser ranging system is laser range finder,
It is arranged on skeleton bottom, be connected with control system；Described acoustic detection device is arranged on skeleton outside or is suspended on skeleton
Lower section is connected with skeleton using flexible cable, and is connected with control system；Described apparatus for measuring air quantity be arranged on skeleton bottom or
Flank end, is anemometry, is connected with control system；Described humidity detector is humidity measuring apparatus, is arranged on
Outside skeleton, it is connected with control system；Described temperature-detecting device is temperature measuring set, is arranged on outside skeleton, with control
System connects；Described radar system is arranged on skeleton, is connected with control system.
Described dynamical system includes air compressor, compressed air storage device, accumulator, gas distributing valve；Described
Air compressor be made up of light-weight high-strength material, its motor is mated with accumulator and is connected；The air inlet of air compressor
It is capable of including the hoverheight control on the air bag on flank and telescopic wing with air or main gasbag by gas distributing valve
System processed connects；The gas outlet of described compressor is capable of controlling with air jet system or hoverheight by gas distributing valve
The middle pressure air accumulator of system connects；Described compressed air storage device is arranged in equipment compartment, and pipeline and gas are passed through in its import
Body distributing valve is connected to air compressor, and its outlet is connected with horizontal movement and control system by gas distributing valve；Described
Accumulator is arranged in equipment compartment, including accumulator and power supply switch, is connected with solaode and individual consuming parts；Institute
The accumulator stated is high-efficient light accumulator, and the electric energy of solaode and accumulator can be turned by described power supply switch
It is changed to the power supply of voltage needed for each functional part and frequency, be that accumulator charges by the electric energy of solaode simultaneously；Institute
The gas distributing valve stated is arranged in equipment compartment, is the assembly being combined into by multiple solenoid electric valves, and its gas passage is respectively
It is connected with the middle pressure air accumulator of air and compressed air storage device and hoverheight control system, and with control system even
Connect.
Described positioner is arranged in equipment compartment, and including satellite positioning device, positional information output device, position is repaiied
Equipment；Described satellite positioning device adopts big-dipper satellite positioning terminal, is connected with control system；Described positional information is defeated
Go out device to be arranged in equipment compartment, be connected with big-dipper satellite positioning terminal and position correcting apparatus；Described position correcting apparatus
It is arranged in equipment compartment, be connected with positional information output device and control system.
Described horizontal movement and control system include gas puff Z-pinch valve, compressed air piping system；Described jet control
Valve processed is multiple directional control valve, has multiple, is separately mounted in air jet system, connects with control system and compressed air piping system
Connect, can control the jet of each air jet system whether with jet direction and jet amount；Described compressed air piping system is led to
Cross gas distributing valve to be arranged between air jet system and compressed air storage device；Described compressed air piping system is by pipeline
With joint composition；Described compressed air piping is made up of light overpressure resistant material.
Described control system includes central processing unit, memory element, communication unit, pressure transducer, controls electromagnetic valve；
Described central processing unit is connected with communication unit and memory element, and by communication unit and information collecting device and positioning system
System and dynamical system and horizontal movement and control system and information transfer and remotely control control system and hoverheight control system
System connects；Described memory element is installed in the controls, is connected with communication unit and central processing unit；Described communication list
Unit installs in the controls, including information input unit and information output unit；Described information input unit and information are adopted
Acquisition means and information transfer and tele-control system connect, and the pressure connecting in air bag and each gas storage passes
Sensor connects described information output unit and information transfer and tele-control system and is arranged on each air bag and gas tube
Control electromagnetic valve on road connects；Described pressure transducer has multiple, is separately mounted to main gasbag and flank air bag, and flexible
In wing air bag；Described control electromagnetic valve has multiple, and be separately mounted to each air bag enters outlet pipe gentle body storage facilities
On, break-make and the uninterrupted of gas can be controlled.
Described information transfer and tele-control system include, Satellite Communication System, signal output system, communication antenna；
Described Satellite Communication System is arranged in information transfer and tele-control system, is capable of the present invention and long-distance remote control station
Between communication and data exchange and compiling；Described signal output system connects respectively at Satellite Communication System and central processing unit
Connect；Described communication antenna is the skeleton in the present invention.
Described hoverheight control system includes, high pressure tank, middle pressure air accumulator, gas distributing valve, gas bag unit,
Light gas, by QI KOU；Described high pressure tank is arranged in equipment compartment, is that the thin-walled being made up of light-weight high-strength material is close
Close container, inside is equipped with high pressure light gas；Described high pressure tank outlet is provided with high-voltage electromagnetic control valve, by pipeline
It is connected with middle pressure air accumulator；In described high pressure tank, pressure transducer is installed, this pressure transducer is with control system even
Connect；Described middle pressure air accumulator is the thin-walled hermetic container being made up of light-weight high-strength material, its import with by pipeline with high
The outlet of pressure air accumulator connects, and its outlet is connected with gas bag unit and air compressor by pipeline and gas distributing valve；Described
Middle pressure air accumulator in pressure transducer is installed, be connected with control system；Described gas distributing valve is arranged on gas bag unit
And middle pressure air accumulator between, can by middle pressure air accumulator in light gas be assigned in different gas bag units；Described gas
Capsule unit is the independent confined space being gone out in main gasbag and flank and telescopic wing internal insulation by barrier film, by pipeline and gas
Distributing valve connects；Described light gas are helium, are filled in gas bag unit producing suspending power in atmosphere；Described is bullied
A mouth flank end installed therein or air bag top, can be docked with external source of the gas, accept external light gas and supplement.
Described telescopic wing includes slide-driving device, hauling rope, gas bag unit group, slide block, pulley, pulley yoke, slide block
Guide rail；Described slide-driving device is arranged on equipment compartment, and including motor and drive, its drive is connected with hauling rope；Institute
The hauling rope stated is fixedly connected with a slide block, and is connected with slide-driving device formation closed loop after pulley；Described air bag list
Tuple is combined into by multiple closed cells that described barrier film and flexible alar wall form, and heaves, do not fill after its inner inflatable
Draw in during gas；The pressure transducer of control system is installed inside each described closed cells and gas controls electromagnetic valve, lead to
Piping is connected with the gas distributing valve in hoverheight control system and control system；Described slide block is arranged on gas bag unit
The outer end both sides of group, and coordinate with slide block guide rail, can move along a straight line in slide block guide rail, described slide block has multiple edges sliding
Block guide rail is arranged in the same direction and is connected with the gas bag unit group outer layer of telescopic wing respectively；Described pulley is arranged on pulley yoke end,
Being capable of rotation on pulley yoke；Described pulley yoke is arranged on slide block guide rail outer end, is fixedly connected with slide block guide rail；Described cunning
Near two side center lines of block guide rails assembling flank, the whole length of insertion flank.
Beneficial effect
The beneficial effects of the present invention is, the long-time Continuous Observation to certain area can be kept and gather corresponding information,
Manufacture and operating cost is low, obtain precision of information high.
Brief description
Fig. 1 is the longitudinal profile schematic diagram of the present invention
1. main gasbag, 2. solar panel, 3. flank, 4. barrier film, 5. skeleton, 6. air jet system, 7. information collecting device,
8. dynamical system, 9. alignment system, 10. horizontal movement and control system, 11. information transfers and tele-control system, 12.
Equipment compartment, 13. control systems, 14. hoverheight control systems.
Fig. 2 is the top view of the present invention
1. main gasbag, 3. flank, 6. air jet system, 15. telescopic wings.
Fig. 3 is the structural representation of information collecting device
5. skeleton, 71. image acquisition devices, 72. infrared detection devices, 73. laser ranging systems, 74. acoustic detection devices,
75. apparatus for measuring air quantity, 76. humidity detectors, 77. temperature-detecting devices, 78. radar systems.
Fig. 4 is the structural representation of dynamical system
81. air compressors, 82. compressed air storage devices, 83. accumulator, 84. gas distributing valves.
Fig. 5 is the structural representation of horizontal movement and control system
101. gas puff Z-pinch valves, 102. compressed air piping systems.
Fig. 6 is the structural representation of control system
131. central processing units, 132. memory element, 133. communication units, 134. pressure transducers, 135. control electromagnetic valves, 7.
Information collecting device, 8. dynamical system, 9. alignment system, 10. horizontal movement and control system, 11. information transfers and remote
Process control system, 14. hoverheight control systems.
Fig. 7 is the structural representation of hoverheight control system
141. high pressure tanks, pressure air accumulator in 142., 143. gas distributing valves, 144. gas bag units, 145. light gas,
146. are subject to QI KOU, 81. air compressors.
Fig. 8 is the structural representation of telescopic wing
12. equipment compartments, 151. slide-driving devices, 152. hauling ropes, 153. gas bag unit groups, 154. slide blocks, 155. pulleys,
156. pulley yokes, 157. slide block guide rails.
Fig. 9 is the structural representation of air jet system
61. outer puff prots, 62. left puff prots, 63. left air jet pipes, 64. outer air jet pipes, 65. right air jet pipes, 66. shells, 67. is right
Puff prot.
Specific embodiment
In order to further illustrate technical scheme, in conjunction with the specific embodiment of the brief description present invention；As
Fig. 9, selects the titanium alloy sheet of 1 millimeter of thickness, is made into shell 66, be equally respectively prepared that diameter is identical to be 200 in this example
The outer puff prot 61 of cylindrical shape of millimeter, left puff prot 62, right puff prot 67, and be installed on shell 66, its exporter
To vertical with left puff prot 62, right puff prot 67 for outer puff prot 61, left puff prot 62, right puff prot 67 are located at outer jet respectively
The both sides of mouth 61；From 30 millimeters of diameter thin-wall titanium alloy tubing respectively as left air jet pipe 63, outer air jet pipe 64, right jet
Pipe 65, and by its one end respectively with outer puff prot 61, left puff prot 62, right puff prot 67 afterbody airtight connection, the other end with
Gas puff Z-pinch valve 101 connects；On shell 61, setting mounting structure is fixedly connected with the end of flank 3, ensures outer spray after connection
The direction of QI KOU 61 is identical to end expansion direction with the root of flank 3；This completes the enforcement of air jet system 6.
As Fig. 8, select light-high-strength fabric in this example as the outer layer of the gas bag unit group 153 of telescopic wing and in it
Gas tight seal material is adhered in side, and connects the barrier film 4 that multiple identical materials are made inside it, by 153 points of gas bag unit group
It is slit in this example of multiple spaces and select 50 compartments；Make equipment compartment 12 from titanium-alloy thin-plate, from motor plus
Pulley combination, as slide-driving device 151, is installed in inside equipment compartment 12, from light-high-strength rope as traction
Rope 152, makes slide block 154 and pulley 155 and pulley yoke 156 and slide block guide rail 157 from titanium alloy；Led from slide block in this example
The cross sectional shape of rail 157 is spill, that is, has the rectangle of opening, is installed in the center line of flank 3 and insertion is whole
Its opening direction of the length of flank 3 is located at the outside of flank 3；Step is arranged on slide block 154, the width of step is less than or equal to slide
The width of block guide rail 157 upper shed；There is the hauling rope fixing hole of insertion slide block 154 in the middle part of the section of slide block 154；By pulley yoke
156 outer ends being arranged on slide block guide rail 157, and pulley 154 is arranged on pulley yoke 156 it is ensured that pulley 154 can be free
Rotation；Hauling rope 152 two ends are closed and forms closed loop, its side passes through and fixes with the hauling rope fixing hole on slide block 154, this
Select 20 slide blocks 154 in every side in example, slide block 154 is fixedly connected with gas bag unit group 153 interval, the end of hauling rope is respectively
The pulley of pulley 154 and driving means 151 is wound around, this completes the enforcement of telescopic wing 15.
As Fig. 7, in this example from titanium alloy make high pressure tank 141, middle pressure air accumulator 142, gas distributing valve 143,
It is bullied, 146, air compressor 81；By high pressure tank 141, middle pressure air accumulator 142, gas distributing valve 143, it is bullied, 146, empty
Air compressor 81 is arranged in equipment compartment, installs pressure transducer inside high pressure tank 141 and middle pressure air accumulator 142, its
Exit is installed high-voltage electromagnetic control valve and is connected with control system 13；High pressure tank 141 and middle pressure air accumulator 142 are adopted
Pipeline connects；Middle pressure air accumulator 142 is connected with gas distributing valve 143 by pipeline, by gas distributing valve 143 and control system
13 connections, its gas outlet is connected gas bag unit 144 by pipeline and includes main gasbag 1 and flank 3 and telescopic wing with gas bag unit 144
All gas bag units on 15；It is filled with light gas in high pressure tank 141, middle pressure air accumulator 142, gas bag unit 144
145, select helium in this example as light gas 145；Main gasbag 1 top or flank 3 end will be arranged on by QI KOU 146,
In by QI KOU 146, check valve is installed, gas is merely able to be externally entering and can not flow outwardly from inside；In this example in order to
Mitigate the load of the present invention, using hoverheight control system 14 and the public air compressor of dynamical system 8；Thus complete
Become the enforcement of hoverheight control system 14.
As Fig. 6, select in this example the general central processing unit of the industry, memory element, communication unit, pressure transducer,
Control electromagnetic valve respectively as central processing unit 131, memory element 132, communication unit 133, pressure transducer 134, control electricity
Magnet valve 135；Above as the central control module of control system, by it respectively at information collecting device 7, dynamical system 8, determine
Position system 9, horizontal movement and control system 10, information transfer and tele-control system 11, hoverheight control system 14 is even
Connect, and form consistent communications protocol with ground control centre；Pressure transducer 134 and control electromagnetic valve 135 are respectively mounted
Inside each gas bag unit 144, and it is connected with central control module, just complete the enforcement of control system 13.
As Fig. 5, in this example, make the general gas solenoid directional control valve of the industry as gas puff Z-pinch valve from titanium alloy
101, compressed air piping system 102 is made using light-high-strength plastic conduit, by compressed air piping system 102 and power
The gas distributing valve 84 of system 8 connects, and with the gas puff Z-pinch valve 101 being arranged within the air jet system 6 of flank 3 outer end even
Connect, complete the enforcement with regard to horizontal movement and control system 10.
As Fig. 4, adopt dynamical system 8 to share an air compressor 81 with hoverheight control system 14 in this example, adopt
Manufactured with titanium alloy material；Make the general air accumulator of the industry from titanium alloy as compressed air storage device 82；In pressure
Pressure transducer is installed in contracting air storage arrangement 82, exit is provided with solenoid electric valve, and is connected with control system 13；
Adopt assembling lithium ion battery power inverter in this example as accumulator 83, by accumulator 83 and solar panel 2 and
The power input portion of control system 13 grade functional part connects；Gas distributing valve 84 is passed through pipeline store up with compressed air respectively
Cryopreservation device 82, horizontal movement and control system 10 connect, and just complete the enforcement of dynamical system 8.
As Fig. 3, in this example, make skeleton 5 from titanium alloy, from the general high definition camera device of satellite system as shadow
As harvester 71；From the general infrared detection device of satellite system as infrared detection device 72；Using satellite or fly
The general laser range finder of machine system, as laser ranging system 73, is made from the general sonar contact device of aircraft or naval vessels
For acoustic detection device 74, filled using the general apparatus for measuring air quantity of weather monitoring system and humidity detector and temperature detection
Put respectively as apparatus for measuring air quantity 75, humidity detector 76 and temperature-detecting device 77；From aircraft airborne radar conduct
Radar system 78, respectively the information gathering of said apparatus is partially installed on skeleton, and distributes rational position and do not produce mutually
Interference, its information processing and transmitting device are arranged in equipment compartment 12 and are connected with control system 13, and the information of this completes is adopted
The enforcement of acquisition means 7.
As Fig. 1, Fig. 2, select light-high-strength fabric in this example as the cladding material of main gasbag 1 and barrier film 4 and at it
Internal layer adheres to airtight thin-film material and collectively constitutes main gasbag 1 and barrier film 4；Commercially available thin-film type solar cell is selected in this example
Plate, as solar panel 2, its piecemeal is fixedly mounted on main gasbag 1 and the upper surface of flank 3, and with dynamical system 8
Accumulator 83 connects；8 flanks 3 are selected, its horizontal cross sectional geometry is triangle, is evenly distributed on the water of main gasbag 1 in this example
Flat periphery；It is connected with each other the skeleton made with main gasbag 1 and flank 3 form fit from titanium alloy tubular material in this example
5, for supporting and installing each functional part, also serve as information transfer and the antenna of tele-control system 11, in skeleton 5 simultaneously
Relevant position arranges the leg of adjustment of can stretching and hook lands for this device and drawn by other power set；This example
Middle selection main gasbag 1 is the hemispherical of 50 meters of diameter, and the length of its flank 3 is 20 meters, and highly 10 meters are located in main gasbag 1 hemisphere
Heart plane top；Described air jet system 6 is arranged on the outer end of flank 3；Information collecting device 7 is arranged under main gasbag 1
It is connected on the skeleton 5 in portion and with control system 13, dynamical system 8 is arranged in equipment compartment 12 and connects with each functional part
Connect；Alignment system 9 is arranged in equipment compartment 12, in this example, selects the general BDStar navigation system terminal conduct of the industry
Alignment system 9；Horizontal movement and control system 10 are arranged in equipment compartment 12, in this example, select satellite control system or nothing
Man-machine control system and the general information transfer of the industry and tele-control system as information transfer and control system 11, and
It is installed in equipment compartment 12, and the power supply with dynamical system 8 and control system 13 are connected；From titanium alloy plate system
Forming apparatus cabin 12 is simultaneously fixedly connected with skeleton 5；Control system 13 and hoverheight control system 14 are arranged in equipment compartment 12,
And connect with corresponding part；Select 8 telescopic wings 15 in this example, be separately mounted between flank 3；Just complete the present invention one
Plant the information gathering that can be empty for a long time and the enforcement of supervising device.
During application, mounted device is placed field, being injected by QI KOU in hoverheight control system 14
High-pressure helium, injects each gas bag unit, due to the buoyancy of light gas, this device can suspend in the air after decompression,
Different according to the geomorphologic conditions of gathered information, ground control centre sends instruction, sets corresponding parameter, control system 13
Go out instruction, adjust the blowing pressure in each gas bag unit and the air bag quantity and the regularity of distribution that are filled with light gas helium；By
Different in the air bag quantity difference and pressure being filled with helium, produced buoyancy difference is it becomes possible to adjust corresponding hoverheight；
While adjusting hoverheight or after, start horizontal movement and control system 10, control system 13 is according to ground control
The instruction at center, control air jet system 6 in the unlatching quantity of gas puff Z-pinch valve 101 and position, thus control jet direction and
Speed and the quantity of puff prot unlatching, to determine horizontal movement direction and the movement velocity of this device, in order to accelerate this device
Movement velocity, on skeleton 5, this device is drawn to designated area using helicopter or naval vessel and carries out by setting traction hook
Throw in；After reaching designated area, ground control centre (selects satellite ground control system or unmanned aerial vehicle to control in this example
System is as ground control centre) command control system 13, opening imformation harvester 7, according to different needs, by this device institute
In the geographical position in region, image, temperature, humidity, wind-force, landforms, whether there are moving sound or animal activity, electromagnetism under water
The information such as wave source pass through information transfer and control system 11 transmits dynamic ground control centre, when needs are mobile or conversion suspension is high
Degree, ground control centre sends instruction at any time, and control system 13 starts horizontal movement and control system 10 and hoverheight controls
System 14 is shifted one's position；Because this device working region is applied to large-area depopulated zone, solar panel 2 can be this dress
Put and the sufficient energy is provided, powered for each functional part by accumulator 83；Because horizontal movement and control system 10 adopt
Be compressed air, be that this device is in suspension inexhaustible, therefore do not need the extra power energy；Air compressor 81 is by sky
Air pressure contracting forms in the compressed air storage device 82 that pressure-air enters dynamical system 8, by compressed air storage device 82
It is discharged in horizontal movement and control system 10, it is to avoid the not enough defect of air compressor 81 air demand, in horizontal movement again
And control system 10 is not when working, air compressor 81 can be according to the pressure transducer measurement pressure of compressed air storage device 82
Force information works at any time；Due to employing many airbag structures, it is to avoid because air bag gas leakage causes the danger that whole device falls,
When single air bag gas leakage, control system 13 is able to detect that this airbag aeration time is exceeded, just can close this air bag；When need
When adjusting hoverheight, ground control centre command control system 13, to each gas bag unit in main gasbag 1 and flank 3
Fill such as helium, when needing significantly to adjust hoverheight, control system 13 sends instruction, hoverheight control system 14 is to stretching
Gas bag unit inflation in the contracting wing 15, starts the slide-driving device 151 of telescopic wing 15 simultaneously, telescopic wing 15 is launched or receives
Hold together；When needing to reduce hoverheight, start air compressor 81, by gas distributing valve 143, by the gas tube of gas bag unit
Road is connected with the air inlet of air compressor 81, and the gas outlet of air compressor 81 is connected with middle pressure air accumulator 142, starts air
Compressor 81, this makes it possible to recycle light gas, such light gas waste is little, ensure that being empty of the present invention
Time；When being lost due to light gas, when leading to gas pressure reduction in middle pressure air accumulator 142, control system 13 instructs high pressure
Air accumulator 141 outlet solenoid valve is opened, and is that middle pressure air accumulator 142 supplements helium it is ensured that the normal work of hoverheight control system 14
Make；When after being empty for a long time, when the gas pressure in high pressure tank 141 reduces to setting value, can send aircraft or
Person's naval vessels or other vehicle, by being filled with helium by QI KOU 146 into high pressure tank 141, this makes it possible to ensure this
What device was longer is empty the time；Due to being empty for a long time, it is capable of the information status of continuous monitoring region, overcome winged
The defect that machine and personnel can not continuously work；Because hoverheight is lower than artificial satellite, overcome satellite monitoring apart from remote information
Inaccurate defect；Move in region due to controlling, overcome the little defect of stationary monitoring website monitoring range,
Multiple devices can be discharged in continuum simultaneously, can forming region chain, expand monitoring range, simultaneously because structure is simple
List is it is not necessary to extra power, low with respect to the manufacture of the existing information collecting device such as aircraft and artificial satellite and operating cost.
Claims (1)
1. a kind of information gathering that can be empty for a long time and supervising device, including main gasbag, solar panel, flank, every
Film, skeleton, air jet system, information collecting device, dynamical system, alignment system, horizontal movement and control system, information transfer and
Tele-control system, equipment compartment, control system, hoverheight control system, telescopic wing；Described main gasbag is spherical, by light
The airtight thin-film material of matter is made；Described solar panel is arranged on the top half surface of main gasbag and flank；Described
Flank be arranged on the horizontal perimeter of main gasbag, radially distribute；Described barrier film is arranged on main gasbag, flank, telescopic wing
Inside, the inner space of main gasbag, flank, telescopic wing is separated into and seals against each other between multiple spaces and each insulating space
Gas bag unit；Described skeleton is arranged on inside main gasbag and flank, supports the external shape of main gasbag and flank；Described bone
Frame is made up of light-weight high-strength material；Described air jet system is arranged on the outer end of flank, including outer puff prot, left jet
Mouthful, left air jet pipe, outer air jet pipe, right air jet pipe, shell, right puff prot；Described outer puff prot is arranged on shell, its oral area
Direction is identical with flank radiation direction, and afterbody is connected with outer air jet pipe；Described left puff prot is arranged on shell, and oral area is with outward
The vertical left side of puff prot is vertical with outer puff prot, and afterbody is connected with left air jet pipe；Described left air jet pipe is arranged on left jet
Mouth afterbody, one end and left puff prot airtight connection, the other end is connected with gas puff Z-pinch valve；Described outer air jet pipe is installed and is sprayed outside
QI KOU afterbody, one end and outer puff prot airtight connection, the other end is connected with gas puff Z-pinch valve；Described right air jet pipe is arranged on the right side
The afterbody of puff prot, one end and right air jet pipe afterbody airtight connection, the other end is connected with gas puff Z-pinch valve；Described shell is installed
In flank end, and it is connected with each puff prot；Described right puff prot is arranged on shell, its oral area direction and outer puff prot
Vertical right side, vertical with outer puff prot and with left puff prot coaxial line；Described gas puff Z-pinch valve is arranged in air jet system
Portion, in the middle of air inlet pipe and air jet pipe；Described information collecting device is rack-mount, with described control system even
Connect；Described dynamical system is arranged in equipment compartment, with solar panel and horizontal movement and control system and each function
The power input of part connects；Described alignment system is arranged in equipment compartment, is connected with control system and dynamical system；
Described horizontal movement and control system are arranged in equipment compartment, with solar panel and air jet system and horizontal movement and control
System processed connects；Described information transfer and tele-control system are arranged on the electricity with control system and dynamical system in equipment compartment
Source connects；Described equipment compartment is arranged in the middle part of main gasbag；Described equipment compartment is made up of light-weight high-strength material；Described control
System processed is arranged in equipment compartment and is connected with the power supply of dynamical system and each functional part；Described hoverheight control system
It is arranged in equipment compartment and be connected with the gas bag unit in control system and main gasbag, flank, telescopic wing；Described telescopic wing is installed
Between each two flank, can along flank launch and withdraw it is characterised in that: described information collecting device is arranged on skeleton
On, including image acquisition device, infrared detection device, laser ranging system, acoustic detection device, apparatus for measuring air quantity, humidity
Detection means, temperature-detecting device, radar system；Described image acquisition device is arranged on outside skeleton, is that high-resolution is taken the photograph
As equipment, it is connected with control system；Described infrared detection device is IR imaging device, is arranged on outside skeleton, with control
System processed connects；Described laser ranging system is laser range finder, is arranged on skeleton bottom, is connected with control system；Described
Acoustic detection device to be arranged on skeleton outside or be suspended on and be connected with skeleton using flexible cable below skeleton, and and control system
Connect；Described apparatus for measuring air quantity is arranged on skeleton bottom or flank end, is anemometry, with control system even
Connect；Described humidity detector is humidity measuring apparatus, is arranged on outside skeleton, is connected with control system；Described temperature inspection
Surveying device is temperature measuring set, is arranged on outside skeleton, is connected with control system；Described radar system is arranged on skeleton,
It is connected with control system.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877874.4A CN106364659B (en) | 2016-10-09 | 2016-10-09 | A kind of information collection that can be emptied for a long time and monitoring device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877874.4A CN106364659B (en) | 2016-10-09 | 2016-10-09 | A kind of information collection that can be emptied for a long time and monitoring device |
Publications (2)
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| CN106364659A true CN106364659A (en) | 2017-02-01 |
| CN106364659B CN106364659B (en) | 2018-10-09 |
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| CN1280937A (en) * | 1999-07-20 | 2001-01-24 | 林奎敏 | Controllable multifunctional suspended body with skeleton, air bag and film |
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2016
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| CN1280937A (en) * | 1999-07-20 | 2001-01-24 | 林奎敏 | Controllable multifunctional suspended body with skeleton, air bag and film |
| JP2003231499A (en) * | 2002-02-07 | 2003-08-19 | Masahiko Hayashi | Air jetting aircraft |
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| Publication number | Publication date |
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| CN106364659B (en) | 2018-10-09 |
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