CN106379508B - A kind of information collection that can be emptied for a long time and monitoring device - Google Patents
A kind of information collection that can be emptied for a long time and monitoring device Download PDFInfo
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- CN106379508B CN106379508B CN201610877873.XA CN201610877873A CN106379508B CN 106379508 B CN106379508 B CN 106379508B CN 201610877873 A CN201610877873 A CN 201610877873A CN 106379508 B CN106379508 B CN 106379508B
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- Prior art keywords
- control system
- air
- jet
- flank
- gas
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Classifications
-
- 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
-
- 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
A kind of information collection that can be emptied for a long time and monitoring device, belong to field of information acquisition, the horizontal movement and control system include gas puff Z-pinch valve, compressed air pipe system；The gas puff Z-pinch valve is multiple directional control valve, has multiple, is separately mounted in air-jet device, is connect with control system and compressed air pipe system, whether capable of controlling the jet of each air-jet device and jet direction and jet amount；The compressed air pipe system is mounted on by gas distributing valve between air-jet device and compressed air storage device；The compressed air pipe system is made of pipeline and connector；The compressed air pipe is made of light overpressure resistant material, and the long-time continuous observation to certain area can be kept and acquire corresponding information by having, and manufacture is low with operating cost, obtain the high feature of precision of information.
Description
Technical field
The invention belongs to field of information acquisition, more particularly to a kind of information collection that can be emptied for a long time and monitoring dress
It sets.
Background technology
Information collection is a material particular in people's live and work, and without information collection, people just can not be right
Extraneous affairs carry out judgement and decision；The sense organ of people is exactly most common information collecting device, and extraneous information is to human body
Sense organ generate stimulation, in sense organ leave the information marking, these information are sent to brain by nervous system, are carried out for people
Analysis, judgement and decision；The sensing capability of the sense organ of people is very limited in the Nature, is looked in the distance so people have invented
Mirror, camera, radar, pyroscan, artificial satellite etc. extend the sensing range of people's sense organ significantly, are given birth to for the mankind
Living create more understands natural means, also creates advantageous condition for human use's natural resources；But so far,
Still there are many natural regions that can not be detected or can not detect in detail by the mankind, for example, ocean, mountain range, desert, forest etc.
Region, since these regional extents are especially vast, existing detection device cannot detect or detailed cannot detect these
It is detailed inside region, and the state in these regions is in variable condition, changing rule need real-time collecting its
Information, and these information are compared, find out the state change rule in these regions；People acquire these regions at present
Means substantially have following methods, first, manually acquire, defect is that the range manually travelled is small, and speed is slow, and can enter
Depth is inadequate；It is short in the area above residence time second is that aircraft, defect are, letter that can not be in the continuous acquisition region
Breath variation；Furthermore it is exactly artificial satellite, defect is low precision, of high cost.
Invention content
For existing ocean, mountain range, desert, the above problem existing for the information collection of forest, the present invention proposes a kind of
The information collection that can be emptied for a long time and monitoring device, it is characterised in that：Including main gasbag, solar panel, flank, every
Film, skeleton, air-jet device, information collecting device, dynamical system, positioning system, horizontal movement and control system, information transmission and
Tele-control system, equipment compartment, control system, hoverheight control system, telescopic wing；The main gasbag is spherical shape, by light
The airtight thin-film material of matter is made；The solar panel is mounted on the top half surface of main gasbag and flank；It is described
Solar panel be flexible film form；The horizontal perimeter in main gasbag is arranged in the flank, radially distributes；Institute
The flank stated has multiple, is evenly distributed on main gasbag horizontal section periphery；The flank has 6 or 8；The diaphragm is set
Set inside main gasbag, flank, telescopic wing, by main gasbag, flank, telescopic wing inner space be separated into multiple spaces and each every
From the gas bag unit sealed against each other between space；The skeleton is arranged inside main gasbag and flank, supports main gasbag and side
The outer shape of the wing；The skeleton is made of light-weight high-strength material；The skeleton is by titanium alloy or carbon fibre material
It is made；The air-jet device is arranged in 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；The outer puff prot is arranged on the shell, oral area direction and flank radiation direction
Identical, tail portion is connect with outer air jet pipe；The described left puff prot setting on the shell, the oral area left side vertical with outer puff prot and
Outer puff prot is vertical, and tail portion is connect with left air jet pipe；The left air jet pipe is mounted on left puff prot tail portion, one end and left jet
Mouth airtight connection, the other end are connect with gas puff Z-pinch valve；The outer air jet pipe is mounted on outer puff prot tail portion, one end and outer spray
Gas port airtight connection, the other end are connect with gas puff Z-pinch valve；The right air jet pipe be mounted on right puff prot tail portion, one end with
Right air jet pipe tail portion airtight connection, the other end are connect with gas puff Z-pinch valve；The shell be mounted on flank end, and with it is each
Puff prot connects；The right puff prot is arranged on the shell, the oral area direction right side vertical with outer puff prot, with outer jet
It is mouthful vertical and with left puff prot coaxial line；The gas puff Z-pinch valve is mounted on inside air-jet device, is located at air inlet pipe and jet
Among pipe；The information collecting device is rack-mount, is connect with the control system；The dynamical system installation
In equipment compartment, connect with the power input of solar panel and horizontal movement and control system and each functional component
It connects；The positioning system is mounted in equipment compartment, is connect with control system and dynamical system；The horizontal movement and control
System is mounted in equipment compartment, is connect with solar panel and air-jet device and horizontal movement and control system；The letter
Breath transmission and tele-control system are mounted in equipment compartment to be connect with the power supply of control system and dynamical system；The equipment compartment
It is arranged in the middle part of main gasbag；The equipment compartment is made of light-weight high-strength material；The control system is mounted on equipment compartment
It is interior to be connect with the power supply of dynamical system and each functional component；The hoverheight control system is mounted in equipment compartment and control
System processed and main gasbag, flank, the gas bag unit connection on telescopic wing；The telescopic wing is mounted between each two flank,
It can be unfolded and withdraw along flank.
The information collecting device is mounted 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；The image
Harvester is mounted on outside skeleton, is high-resolution picture pick-up device, is connect with control system；The infrared detection device is
IR imaging device is mounted on outside skeleton, is connect with control system；The laser ranging system is laser range finder,
Mounted on skeleton lower part, it is connect with control system；The acoustic detection device is mounted on outside skeleton or is suspended on skeleton
Lower section is connect using flexible cable with skeleton, and is connect with control system；The apparatus for measuring air quantity be mounted on skeleton lower part or
Flank end is anemometry, is connect with control system；The humidity detector is humidity measuring apparatus, is mounted on
Outside skeleton, it is connect with control system；The temperature-detecting device is temperature measuring set, is mounted on outside skeleton, with control
System connects；The radar system is mounted on skeleton, is connect with control system.
The dynamical system includes air compressor, compressed air storage device, accumulator, gas distributing valve；It is described
Air compressor be made of light-weight high-strength material, motor is matched and is connect with accumulator；The air inlet of air compressor
It can realize with air or main gasbag to include hoverheight control on air bag on flank and telescopic wing by gas distributing valve
System connection processed；The gas outlet of the compressor can be realized and air-jet device or hoverheight control by gas distributing valve
The middle pressure air accumulator of system connects；The compressed air storage device is mounted in equipment compartment, and import passes through pipeline and gas
Body distributing valve is connected to air compressor, and outlet is connect by gas distributing valve with horizontal movement and control system；Described
Accumulator is mounted in equipment compartment, including accumulator and power supply switch, is connect with solar cell and a consuming parts；Institute
The accumulator stated is high-efficient light accumulator, and the power supply switch can turn the electric energy of solar cell and accumulator
The power supply of the voltage and frequency that are changed to needed for each functional component, while to charge the battery by the electric energy of solar cell；Institute
The gas distributing valve stated is mounted in equipment compartment, is the assembly being combined by multiple solenoid electric valves, gas passage difference
It connect with the middle pressure air accumulator of air and compressed air storage device and hoverheight control system, and connects with control system
It connects.
The positioning device is mounted in equipment compartment, including satellite positioning device, and location information output device, position is repaiied
Equipment；The satellite positioning device uses big-dipper satellite positioning terminal, is connect with control system；The location information is defeated
Go out device in equipment compartment, is connect with big-dipper satellite positioning terminal and position correcting apparatus；The position correcting apparatus
In equipment compartment, it is connect with location information output device and control system.
The horizontal movement and control system includes gas puff Z-pinch valve, compressed air pipe system；The jet control
Valve processed is multiple directional control valve, has multiple, is separately mounted in air-jet device, is connected with control system and compressed air pipe system
It connects, whether capable of controlling the jet of each air-jet device and jet direction and jet amount；The compressed air pipe system is logical
Gas distributing valve is crossed to be mounted between air-jet device and compressed air storage device；The compressed air pipe system is by pipeline
It is formed with connector；The compressed air pipe is made of light overpressure resistant material.
The control system includes central processing unit, storage unit, communication unit, pressure sensor, control solenoid valve；
The central processing unit is connect with communication unit and storage unit, and is by communication unit and information collecting device and positioning
System and dynamical system and horizontal movement and the transmission of control system and information and remote control control system and hoverheight control system
System connection；The storage unit installation in the controls, is connect with communication unit and central processing unit；The communication list
Member is installed in the controls, including information input unit and information output unit；The information input unit is adopted with information
Acquisition means are transmitted with information and tele-control system connects, and connect the pressure being located in air bag and each gas storage and pass
The sensor connection information output unit is transmitted with information and tele-control system and on each air bag and flue
The control solenoid valve of road connects；The pressure sensor has multiple, is separately mounted to main gasbag and flank air bag, and flexible
In wing air bag；The control solenoid valve have it is multiple, be separately mounted to each air bag into the gentle body storage facilities of outlet pipe
On, the break-make and uninterrupted of gas can be controlled.
The information transmission and tele-control system include Satellite Communication System, signal output system, communication antenna；
The Satellite Communication System is mounted in information transmission and tele-control system, can realize the present invention and long-distance remote control station
Between communication and data exchange and compiling；The signal output system connects respectively at Satellite Communication System and central processing unit
It connects；The communication antenna is the skeleton in the present invention.
The hoverheight control system includes high pressure tank, middle pressure air accumulator, gas distributing valve, gas bag unit,
Light gas, by gas port；The high pressure tank is mounted in equipment compartment, is that the thin-walled made of light-weight high-strength material is close
Container is closed, inside is equipped with high pressure light gas；The high pressure tank outlet is equipped with high-voltage electromagnetic control valve, passes through pipeline
It is connect with middle pressure air accumulator；Pressure sensor is installed in the high pressure tank, which connects with control system
It connects；The middle pressure air accumulator is the thin-walled closed container made of light-weight high-strength material, import with pass through pipeline with it is high
The outlet connection of air accumulator is pressed, outlet is connect by pipeline and gas distributing valve with gas bag unit and air compressor；It is described
Middle pressure air accumulator in pressure sensor is installed, connect with control system；The gas distributing valve is mounted on gas bag unit
Between middle pressure air accumulator, the light gas in middle pressure air accumulator can be assigned in different gas bag units；The gas
Capsule unit is the independent confined space gone out in main gasbag and flank and telescopic wing internal insulation by diaphragm, passes through pipeline and gas
Distributing valve connects；The light gas is helium, is filled in gas bag unit and generates suspending power in air；Described is bullied
It at the top of a mouth flank end installed therein or air bag, can be docked with external air source, receive external light gas supplement.
The telescopic wing includes slide-driving device, hauling rope, gas bag unit group, sliding block, pulley, pulley yoke, sliding block
Guide rail；The slide-driving device is mounted on equipment compartment, including motor and driving wheel, driving wheel are connect with hauling rope；Institute
The hauling rope stated is fixedly connected with a slide block, and is connect by forming closed loop with slide-driving device after pulley；The air bag list
What multiple closed cells that tuple is made of the diaphragm and flexible alar wall were combined into, it heaves, does not fill after inner inflatable
It is collapsed when gas；The pressure sensor and gas control solenoid valve of control system are installed inside each closed cells, led to
Piping in hoverheight control system gas distributing valve and control system connect；The sliding block is mounted on gas bag unit
The outer end both sides of group, and coordinate with slide block guide rail, it can be moved in a straight line in slide block guide rail, the sliding block has multiple along cunning
Block guide rail is arranged and is connect respectively with the gas bag unit group outer layer of telescopic wing in the same direction；The pulley is mounted on pulley yoke end,
It being capable of the rotation on pulley yoke；The pulley yoke is mounted on slide block guide rail outer end, is fixedly connected with slide block guide rail；The cunning
Block guide rail is installed near the two sides center line of flank, and the whole length of flank is penetrated through.
Advantageous effect
The beneficial effects of the present invention are can keep the long-time continuous observation to certain area and acquire corresponding
Information, manufacture is low with operating cost, and it is high to obtain precision of information.
Description of the drawings
Fig. 1 is the longitudinal profile schematic diagram of the present invention
1. main gasbag, 2. solar panels, 3. flanks, 4. diaphragms, 5. skeletons, 6. air-jet devices, 7. information collections dress
It sets, 8. dynamical systems, 9. positioning systems, 10. horizontal movements and control system, the transmission of 11. information and tele-control system,
12. equipment compartment, 13. control systems, 14. hoverheight control systems.
Fig. 2 is the vertical view of the present invention
1. main gasbag, 3. flanks, 6. air-jet devices, 15. telescopic wings.
Fig. 3 is the structural schematic diagram of information collecting device
5. skeleton, 71. image acquisition devices, 72. infrared detection devices, 73. laser ranging systems, 74. acoustic detections dress
It sets, 75. apparatus for measuring air quantity, 76. humidity detectors, 77. temperature-detecting devices, 78. radar systems.
Fig. 4 is the structural schematic diagram of dynamical system
81. air compressor, 82. compressed air storage devices, 83. accumulators, 84. gas distributing valves.
Fig. 5 is the structural schematic diagram of horizontal movement and control system
101. gas puff Z-pinch valve, 102. compressed air pipe systems.
Fig. 6 is the structural schematic diagram of control system
131. central processing unit, 132. storage units, 133. communication units, 134. pressure sensors, 135. control electromagnetism
Valve, 7. information collecting devices, 8. dynamical systems, 9. positioning systems, 10. horizontal movements and control system, 11. information pass
Defeated and tele-control system, 14. hoverheight control systems.
Fig. 7 is the structural schematic diagram of hoverheight control system
141. high pressure tanks press air accumulator, 143. gas distributing valves, 144. gas bag units, 145. lightweight gas in 142.
Body, 146. by gas port, 81. air compressors.
Fig. 8 is the structural schematic diagram of telescopic wing
12. equipment compartment, 151. slide-driving devices, 152. hauling ropes, 153. gas bag unit groups, 154. sliding blocks, 155. slide
Wheel, 156. pulley yokes, 157. slide block guide rails.
Fig. 9 is the structural schematic diagram of air-jet device
61. outer puff prot, 62. left puff prots, 63. left air jet pipes, 64. outer air jet pipes, 65. right air jet pipes, 66. shells,
67. right puff prot.
Specific implementation mode
Technical solution in order to further illustrate the present invention, in conjunction with the specific implementation mode of the description of the drawings present invention；Such as
Fig. 9 selects the titanium alloy sheet of 1 millimeter of thickness in this example, is made into shell 66, it is 200 that it is identical that diameter, which is equally respectively prepared,
Cylindric outer puff prot 61, left puff prot 62, the right puff prot 67 of millimeter, and be installed on shell 66, 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
The both sides of mouth 61；Select the thin-wall titanium alloy tubing of 30 millimeters of diameter respectively as left air jet pipe 63, outer air jet pipe 64, right jet
Pipe 65, and by the one end tail portion airtight connection with outer puff prot 61, left puff prot 62, right puff prot 67 respectively, the other end with
Gas puff Z-pinch valve 101 connects；Mounting structure is arranged on shell 61 to be fixedly connected with the end of flank 3, ensures outer spray after connection
The direction of gas port 61 is identical to end expansion direction as the root of flank 3；This completes the implementations of air-jet device 6.
Such as Fig. 8, select light-high-strength fabric as the outer layer of the gas bag unit group 153 of telescopic wing and in it in this example
Gas tight seal material is adhered in side, and connects diaphragm 4 made of multiple identical materials inside it, and gas bag unit group 153 is divided
It is cut into 50 compartments of selection in multiple space this example；It selects titanium-alloy thin-plate that equipment compartment 12 is made, stepper motor is selected to add
Pulley combination is installed in 12 inside of equipment compartment, selects light-high-strength rope as traction as slide-driving device 151
Rope 152 selects titanium alloy that sliding block 154 and pulley 155 and pulley yoke 156 and slide block guide rail 157 is made；Sliding block is selected to lead in this example
The cross sectional shape of rail 157 is spill, that is, has the rectangle of opening on one side, is installed in the center line of flank 3 and penetrates through entire
Its opening direction of the length of flank 3 is located at the outside of flank 3；Step is set on sliding block 154, and the width of step is less than or equal to slide
The width being open on block guide rail 157；There is the hauling rope mounting hole of perforation sliding block 154 in the middle part of the section of sliding block 154；By pulley yoke
156 are mounted on the outer end of slide block guide rail 157, and pulley 155 is mounted on pulley yoke 156, ensure that pulley 155 can be free
Rotation；152 both ends of hauling rope are closed to form closed loop, one side passes through and fixes with the hauling rope mounting hole on sliding block 154, this
It is selected in example per the sliding block 154 of side 20, sliding block 154 is fixedly connected with the interval of gas bag unit group 153, the end difference of hauling rope
It is wound on pulley 155 and the pulley of driving device 151, this completes the implementations of telescopic wing 15.
Selected such as Fig. 7, in this example titanium alloy be made high pressure tank 141, middle pressure air accumulator 142, gas distributing valve 143,
By gas port 146, air compressor 81；By high pressure tank 141, middle pressure air accumulator 142, gas distributing valve 143, by gas port 146,
Air compressor 81 is mounted in equipment compartment, and pressure sensor is installed inside high pressure tank 141 and middle pressure air accumulator 142,
High-voltage electromagnetic control valve is installed and is connect with control system 13 in its exit；High pressure tank 141 and middle pressure air accumulator 142 are adopted
It is connected with pipeline；Middle pressure air accumulator 142 is connect by pipeline with gas distributing valve 143, is by gas distributing valve 143 and control
13 connection of system, gas outlet are connect gas bag unit 144 with gas bag unit 144 by pipeline and include main gasbag 1 and flank 3 and stretch
All gas bag units on the wing 15；It is filled with light gas in high pressure tank 141, middle pressure air accumulator 142, gas bag unit 144
145, select helium as light gas 145 in this example；1 top of main gasbag or 3 end of flank will be mounted on by gas port 146,
Check valve is installed in by gas port 146, gas is merely able to be externally entering and cannot flow out from the inside；In this example in order to
The load for mitigating the present invention, using hoverheight control system 14 and 8 public air compressors of dynamical system；It is thus complete
At the implementation of hoverheight control system 14.
Such as Fig. 6, the central processing unit of selecting the industry general in this example, storage unit, communication unit, pressure sensor,
Solenoid valve is controlled respectively as central processing unit 131, storage unit 132, communication unit 133, pressure sensor 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 is fixed
Position system 9, horizontal movement and control system 10, information transmission and tele-control system 11, hoverheight control system 14 connect
It connects, and consistent communications protocol is formed with ground control centre；Pressure sensor 134 and control solenoid valve 135 are installed respectively
It is connect inside each gas bag unit 144, and with central control module, just completes the implementation of control system 13.
Such as Fig. 5, select titanium alloy that the general gas solenoid directional control valve of the industry is made as gas puff Z-pinch valve in this example
101, compressed air pipe system 102 is made using light-high-strength plastic conduit, by compressed air pipe system 102 and power
The gas distributing valve 84 of system 8 connects, and connects with the gas puff Z-pinch valve 101 inside the air-jet device 6 of 3 outer end of flank
It connects, completes the implementation with regard to horizontal movement and control system 10.
Such as Fig. 4, an air compressor 81 is shared using dynamical system 8 and hoverheight control system 14 in this example, is adopted
It is manufactured with titanium alloy material；Select titanium alloy that the general air accumulator of the industry is made as compressed air storage device 82；It is pressing
Pressure sensor is installed, exit is equipped with solenoid electric valve, and is connect with control system 13 in contracting air storage arrangement 82；
Accumulator 83 is used as using assembling lithium ion battery power inverter in this example, by accumulator 83 and solar panel 2 and
The power input portion of the functional components such as control system 13 connects；Gas distributing valve 84 is stored up with compressed air respectively by pipeline
Cryopreservation device 82, horizontal movement and control system 10 connect, and just complete the implementation of dynamical system 8.
Such as Fig. 3, select titanium alloy that skeleton 5 is made in this example, the high definition camera device for selecting satellite system general is as shadow
As harvester 71；The infrared detection device for selecting satellite system general is as infrared detection device 72；Using satellite or fly
The general laser range finder of machine system selects aircraft or the general sonar contact device of naval vessels to make as laser ranging system 73
For acoustic detection device 74, filled using the general apparatus for measuring air quantity of weather monitoring system and humidity detector and temperature detection
It sets respectively as apparatus for measuring air quantity 75, humidity detector 76 and temperature-detecting device 77；Select aircraft airborne radar conduct
The information collection of above-mentioned apparatus is partially installed on skeleton by radar system 78 respectively, and is distributed rational position and do not generated mutually
Interference, information processing and transmitting device are mounted in equipment compartment 12 and are connect with control system 13, and this completes information to adopt
The implementation of acquisition means 7.
Such as Fig. 1, Fig. 2 selects light-high-strength fabric as the cladding material of main gasbag 1 and diaphragm 4 and at it in this example
Internal layer adheres to airtight thin-film material and collectively constitutes main gasbag 1 and diaphragm 4；Commercially available thin-film type solar cell is selected in this example
Its piecemeal is fixedly mounted on the upper surface of main gasbag 1 and flank 3 as solar panel 2 by plate, and with dynamical system 8
Accumulator 83 connects；It is triangle that 8 flanks 3, horizontal cross sectional geometry are selected in this example, is evenly distributed on the water of main gasbag 1
Flat periphery；It selects titanium alloy tubular material to be connected with each other in this example to be made and main gasbag 1 and the matched skeleton of 3 shape of flank
5, it is used to support and installs each functional component, the antenna of the information that also serves as transmission and tele-control system 11, in skeleton 5
The stabilizer blade for the adjustment that can stretch is arranged in corresponding position and draw hook is landed for the present apparatus and drawn by other power plants；This example
The length of the middle hemispherical for selecting main gasbag 1 as 50 meters of diameter, flank 3 is 20 meters, and 10 meters of height is located in 1 hemisphere of main gasbag
Heart plane top；The air-jet device 6 is mounted on to the outer end of flank 3；Information collecting device 7 is mounted under main gasbag 1
It connect on the skeleton 5 in portion and with control system 13, dynamical system 8 is mounted in equipment compartment 12 and connects with each functional component
It connects；Positioning system 9 is mounted in equipment compartment 12, the BDStar navigation system terminal conduct for selecting the industry general in this example
Positioning system 9；Horizontal movement and control system 10 are mounted in equipment compartment 12, satellite control system or nothing are selected in this example
Man-machine control system and the industry it is general information transmission and tele-control system as information transmission and control system 11, and
It is installed in equipment compartment 12, and is connect with the power supply of dynamical system 8 and control system 13；The titanium alloy plate system of selection
Forming apparatus cabin 12 is simultaneously fixedly connected with skeleton 5；Control system 13 and hoverheight control system 14 are mounted in equipment compartment 12,
And it is connected with corresponding component；8 telescopic wings 15 are selected in this example, are separately mounted between flank 3；Just complete the present invention one
The implementation for the information collection and monitoring device that kind can empty for a long time.
In application, the mounted present apparatus is placed field, being injected by gas port in hoverheight control system 14
High-pressure helium, by injecting each gas bag unit after decompression, due to the buoyancy of light gas, the present apparatus can suspend in the air,
Different according to the geomorphologic conditions of acquired information, ground control centre sends out instruction, sets corresponding parameter, and control system 13 is sent out
Go out instruction, adjusts the blowing pressure in each gas bag unit and be filled with the air bag quantity and the regularity of distribution of light gas helium；By
Different in the air bag quantity difference and pressure for being filled with helium, generated buoyancy is different, it will be able to adjust corresponding hoverheight；
While adjusting hoverheight or after, start horizontal movement and control system 10, control system 13 and controlled according to ground
The instruction at center, control air-jet device 6 in gas puff Z-pinch valve 101 unlatching quantity and position, to control jet direction and
The quantity that speed and puff prot are opened, to determine the horizontal movement direction and movement velocity of the present apparatus, in order to accelerate the present apparatus
The present apparatus is drawn to specified region using helicopter or naval vessel and carried out by movement velocity, the setting traction hook on skeleton 5
It launches；It reaches after specifying region, ground control centre（Satellite ground control system or unmanned aerial vehicle control are selected in this example
System is as ground control centre）Command control system 13, opening imformation harvester 7, according to different needs, by present apparatus institute
In the geographical location in region, image, temperature, humidity, wind-force, landforms, whether there are underwater moving sound or animal activity, electromagnetism
The information such as wave source are transmitted by information and the dynamic ground control centre of the transmission of control system 11, when needs are mobile or convert the height that suspends
Degree, ground control centre send out instruction at any time, and control system 13 starts horizontal movement and control system 10 and hoverheight control
System 14 is shifted one's position；Since present apparatus working region is suitable for the depopulated zone of large area, solar panel 2 can be this dress
It sets and the sufficient energy is provided, powered for each functional component by accumulator 83；Since horizontal movement and control system 10 use
Be compressed air, be that the present apparatus is in suspension inexhaustible, therefore does not need the extra power energy；Air compressor 81 will be empty
Air pressure, which is contracted, to be formed pressure-air and enters in the compressed air storage device 82 of dynamical system 8, and compressed air storage device 82 is passed through
It is discharged into again in horizontal movement and control system 10, the insufficient defect of 81 air demand of air compressor is avoided, in horizontal movement
And control system 10, when not working, air compressor 81 can be measured according to the pressure sensor of compressed air storage device 82 and be pressed
Force information works at any time；As a result of more airbag structures, the danger for causing whole device to fall due to air bag gas leakage is avoided,
When single air bag gas leakage, control system 13 is able to detect that the airbag aeration time is exceeded, can close the air bag；When need
When adjusting hoverheight, ground control centre command control system 13, each gas bag unit into main gasbag 1 and flank 3
It fills such as helium, when needing significantly to adjust hoverheight, control system 13 sends out instruction, and hoverheight control system 14 is to stretching
Gas bag unit inflation in the contracting wing 15, while starting the slide-driving device 151 of telescopic wing 15, telescopic wing 15 is unfolded or is received
Hold together；When needing to reduce hoverheight, start air compressor 81, by gas distributing valve 143, by the flue of gas bag unit
Road is connected to the air inlet of air compressor 81, and the gas outlet of air compressor 81 is connect with middle pressure air accumulator 142, starts air
Compressor 81, this makes it possible to recycle light gas, such light gas waste is small, can ensure emptying for the present invention
Time；It is lost when due to light gas, when leading to gas pressure reduction in middle pressure air accumulator 142, control system 13 instructs high pressure
141 outlet solenoid valve of air accumulator is opened, and helium is supplemented for middle pressure air accumulator 142, ensures 14 normal work of hoverheight control system
Make；After emptying for a long time, when the gas pressure in high pressure tank 141 is reduced to setting value, can send aircraft or
By being filled with helium into high pressure tank 141 by gas port 146, this makes it possible to ensure this for person's naval vessels or other delivery vehicles
Device it is longer empty the time；Due to that can empty for a long time, the information status of region can be continuously monitored, is overcome winged
Machine and personnel are unable to the defect of continuous work；Since hoverheight is lower than artificial satellite, satellite monitoring is overcome apart from remote information
Inaccurate defect；It is moved in region due to that can control, overcomes the small defect of stationary monitoring website monitoring range,
Simultaneously multiple present apparatus can be discharged in continuum, can forming region chain, expand monitoring range, simultaneously because structure is simple
It is single, extra power is not needed, the manufacture and operating cost relative to the existing information collecting device such as aircraft and artificial satellite are low.
Claims (1)
1. a kind of information collection that can be emptied for a long time and monitoring device, including main gasbag, solar panel, flank, every
Film, skeleton, air-jet device, information collecting device, dynamical system, positioning system, horizontal movement and control system, information transmission and
Tele-control system, equipment compartment, control system, hoverheight control system, telescopic wing；The main gasbag is spherical shape, by light
The airtight thin-film material of matter is made；The solar panel is mounted on the top half surface of main gasbag and flank；It is described
Flank the horizontal perimeter in main gasbag is set, radially distribute；The diaphragm is arranged in main gasbag, flank, telescopic wing
The inner space of main gasbag, flank, telescopic wing is separated into and is sealed against each other between multiple spaces and each insulating space by inside
Gas bag unit；The skeleton is arranged inside main gasbag and flank, supports the outer shape of main gasbag and flank；The bone
Frame is made of light-weight high-strength material；The air-jet device is arranged in 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；The outer puff prot is arranged on the shell, oral area
Direction is identical as flank radiation direction, and tail portion is connect with outer air jet pipe；The described left puff prot setting on the shell, oral area with it is outer
The vertical left side of puff prot is vertical with outer puff prot, and tail portion is connect with left air jet pipe；The left air jet pipe is mounted on left jet
Mouth tail portion, one end and left puff prot airtight connection, the other end are connect with gas puff Z-pinch valve；The outer air jet pipe is mounted on outer spray
Gas port tail portion, one end and outer puff prot airtight connection, the other end are connect with gas puff Z-pinch valve；The right air jet pipe is mounted on the right side
The tail portion of puff prot, one end and right air jet pipe tail portion airtight connection, the other end are connect with gas puff Z-pinch valve；The shell installation
It is connect in flank end, and with each puff prot；On the shell, oral area direction is in outer puff prot for the right puff prot setting
Vertical right side, it is vertical with outer puff prot and with left puff prot coaxial line；The gas puff Z-pinch valve is mounted in air-jet device
Portion is located among air inlet pipe and air jet pipe；The information collecting device is rack-mount, connects with the control system
It connects；The dynamical system is mounted in equipment compartment, with solar panel and horizontal movement and control system and each function
The power input of component connects；The positioning system is mounted in equipment compartment, is connect with control system and dynamical system；
The horizontal movement and control system is mounted in equipment compartment, with solar panel and air-jet device and horizontal movement and control
System connection processed；The information transmission and tele-control system are mounted in equipment compartment the electricity with control system and dynamical system
Source connects；The equipment compartment is arranged in the middle part of main gasbag；The equipment compartment is made of light-weight high-strength material；The control
System processed is mounted in equipment compartment and is connect with the power supply of dynamical system and each functional component；The hoverheight control system
It is connect with the gas bag unit on control system and main gasbag, flank, telescopic wing in equipment compartment；The telescopic wing installation
Between each two flank, it can be unfolded and withdraw along flank, it is characterised in that：The horizontal movement and control system packet
Include gas puff Z-pinch valve, compressed air pipe system；The gas puff Z-pinch valve is multiple directional control valve, has multiple, is separately mounted to
In air-jet device, connect with control system and compressed air pipe system, whether capable of controlling the jet of each air-jet device and
Jet direction and jet amount；The compressed air pipe system is mounted on air-jet device and compressed air by gas distributing valve
Between storage device；The compressed air pipe system is made of pipeline and connector；The compressed air pipe is by lightweight
Pressure-resistant material is made.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877873.XA CN106379508B (en) | 2016-10-09 | 2016-10-09 | A kind of information collection that can be emptied for a long time and monitoring device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610877873.XA CN106379508B (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)
| Publication Number | Publication Date |
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| CN106379508A CN106379508A (en) | 2017-02-08 |
| CN106379508B true CN106379508B (en) | 2018-10-09 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610877873.XA Expired - Fee Related CN106379508B (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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| CN (1) | CN106379508B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN103587674A (en) * | 2012-08-13 | 2014-02-19 | 中国空间技术研究院 | Airship airbag with shape-control frames |
| CN103786863A (en) * | 2014-02-17 | 2014-05-14 | 李彦征 | Jet-propelled vertical-lift air bag aircraft |
| WO2014207732A1 (en) * | 2013-06-28 | 2014-12-31 | Paolo Bellezza Quater | A multi-rotor aircraft |
| CN105947169A (en) * | 2016-06-07 | 2016-09-21 | 王庆方 | Solar saucer-shaped floating aircraft provided with shrinkable airbag |
| CN206068119U (en) * | 2016-10-09 | 2017-04-05 | 华北水利水电大学 | A kind of information gathering that can be empty for a long time and supervising device |
-
2016
- 2016-10-09 CN CN201610877873.XA patent/CN106379508B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN103587674A (en) * | 2012-08-13 | 2014-02-19 | 中国空间技术研究院 | Airship airbag with shape-control frames |
| WO2014207732A1 (en) * | 2013-06-28 | 2014-12-31 | Paolo Bellezza Quater | A multi-rotor aircraft |
| CN103786863A (en) * | 2014-02-17 | 2014-05-14 | 李彦征 | Jet-propelled vertical-lift air bag aircraft |
| CN105947169A (en) * | 2016-06-07 | 2016-09-21 | 王庆方 | Solar saucer-shaped floating aircraft provided with shrinkable airbag |
| CN206068119U (en) * | 2016-10-09 | 2017-04-05 | 华北水利水电大学 | A kind of information gathering that can be empty for a long time and supervising device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106379508A (en) | 2017-02-08 |
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Granted publication date: 20181009 Termination date: 20191009 |