CN110450953A - A kind of unmanned flight's device with heat sinking function for marine security protection patrol - Google Patents
A kind of unmanned flight's device with heat sinking function for marine security protection patrol Download PDFInfo
- Publication number
- CN110450953A CN110450953A CN201910744747.0A CN201910744747A CN110450953A CN 110450953 A CN110450953 A CN 110450953A CN 201910744747 A CN201910744747 A CN 201910744747A CN 110450953 A CN110450953 A CN 110450953A
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- Prior art keywords
- main body
- hole
- security protection
- fixing pipe
- venthole
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Studio Devices (AREA)
Abstract
The present invention relates to a kind of unmanned flight's devices with heat sinking function for marine security protection patrol, including main body, four rotors, four support rods and four cameras, the shape of the main body is cylinder, four rotors are circumferentially uniformly arranged in main body centered on the axis of main body, the support rod and rotor correspond, the support rod and body parallel, the top of the support rod is fixedly connected with main body, the camera and support rod correspond, the side of the separate main body of support rod is arranged in the camera, the main body is equipped with driving device, the main body controlling system and fault monitoring system, the main body is equipped with auxiliary body and cooling mechanism, the unmanned flight's device with heat sinking function for being used for marine security protection patrol realizes heat dissipation by cooling mechanism, it avoids being chronically at hot environment It damages down, moreover, function of the forced landing on the water surface is also realized by auxiliary body.
Description
Technical field
The present invention relates to intelligent security guard field, in particular to a kind of nothing with heat sinking function for marine security protection patrol
People's flight instruments.
Background technique
Intelligent safety and defence system is that intrusion alarm system, the view that product and other Related products are constituted are taken precautions against with application safety
The system of frequency safety defense monitoring system, gateway control system, anti-explosion safety inspection etc., or combined by these systems for subsystem
Or integrated electronic system or network, wherein security protection unmanned plane is one kind of intelligent security guard equipment, is equipped with high-definition digital and takes the photograph
The unmanned plane of camera and GPS positioning system can carry out positioning autonomous cruise, real-time transmission filmed image, monitoring personnel along power grid
It can synchronize on computers and watch and manipulate.
The existing unmanned plane for marine security protection patrol can not land in an emergency when a failure occurs in flight course,
Practicability is reduced, moreover, in flight course, more heat can be generated inside unmanned plane, especially in hot environment
Even more serious when lower flight, high temperature easily leads to unmanned plane inner wall component damage, shortens the working life.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, providing a kind of for marine security protection
Unmanned flight's device with heat sinking function of patrol.
The technical solution adopted by the present invention to solve the technical problems is: a kind of to have heat dissipation for marine security protection patrol
Unmanned flight's device of function, including main body, four rotors, four support rods and four cameras, the shape of the main body be
Cylinder, four rotors are circumferentially uniformly arranged in main body centered on the axis of main body, and the support rod and rotor one are a pair of
It answers, the top of the support rod and body parallel, the support rod is fixedly connected with main body, and the camera and support rod are one by one
Corresponding, the side of the separate main body of support rod is arranged in the camera, and the main body is equipped with driving device, the driving dress
It sets and is connect with rotary-wing transmission, the main body controlling system and fault monitoring system, the main body are equipped with auxiliary body and dissipate
Heat engine structure；
The cooling mechanism includes air inlet pipe, suction pump and fixing pipe, and the top of the main body is equipped with mounting hole, the peace
The axis for filling hole is parallel with support rod, the air inlet pipe and mounting hole coaxial arrangement, the outer diameter of the air inlet pipe and mounting hole
Aperture is equal, and the air inlet pipe is sealed and is fixedly connected with the inner wall of mounting hole, and the suction pump and fixing pipe are respectively positioned on main body
Interior, the suction pump is arranged in air inlet pipe, and the suction pump is fixed on the inner wall of main body, the axis of the fixing pipe with into
The axis of tracheae is vertical and intersects, and the bottom end of air inlet pipe is arranged in the middle-end of the fixing pipe, and the air inlet pipe and fixing pipe connect
Lead to and be fixedly connected, the fixing pipe setting is equipped at least two ventholes, institute at the intracorporal bottom of master, the top of the main body
It states venthole to be circumferentially uniformly distributed centered on the axis of mounting hole, the axis of the venthole and the axis of mounting hole are parallel；
The auxiliary body includes moving tube, seal disc, seal assembly and connection component, and the moving tube and main body are coaxial
Setting, the internal diameter of the moving tube are greater than the outer diameter of main body, and the main body passes through moving tube, the main body and moving tube slide and
It is tightly connected, the seal disc and moving tube are coaxially disposed, and the diameter of the seal disc and the outer diameter of moving tube are equal, described close
Closing disk is arranged in the bottom end of moving tube, the seal disc and the bottom end seal of moving tube and is fixedly connected, the bottom end of the main body
Equipped at least two connecting holes, the connecting hole and venthole are corresponded, the bottom end of the seal disc and main body against and it is close
Envelope connection, the seal assembly are arranged on venthole, and the component is arranged on seal disc.
Preferably, the effect in order to realize sealing venthole, the seal assembly includes electromagnet, sealing-plug, magnet
Plate, two connecting rods and two through holes, the magnet plate is vertical with the axis of venthole, the sealing-plug matched with venthole and
Face setting, the sealing-plug are fixed on the side of the close venthole of magnet plate, the other side of the electromagnet and magnet plate
Against the electromagnet is fixed on the inner wall of main body, and gap is equipped between the sealing-plug and venthole, and through hole setting exists
On magnet plate, the electromagnet is located between two through holes, and the axis of the through hole and the axis of venthole are parallel, described
Connecting rod and through hole are coaxially disposed, and the diameter of the connecting rod and the aperture of through hole are equal, and the connecting rod passes through through hole, described
Connecting rod is slidably connected with through hole, and the top of the connecting rod is fixed on main intracorporal top.
Preferably, being coated with lubricating oil on the connecting rod to reduce the frictional force between magnet plate and connecting rod.
Preferably, the effect in order to realize fixing seal disk, the separate magnet of electromagnet is arranged in the connection component
The side of plate, the connection component include magnet block, spring, push rod and pilot hole, and the bottom end of main body is arranged in the pilot hole,
The pilot hole and venthole are coaxially disposed, and the push rod and venthole are coaxially disposed, the diameter of the push rod and pilot hole
Aperture is equal, and the push rod passes through pilot hole, and the inner wall of the push rod and pilot hole slidingly and sealingly connects, the bottom of the push rod
End is fixed on seal disc, and the magnet block is fixed on the top of push rod, the separate magnet plate of the magnet block and electromagnet
Side is against the spring is located between magnet block and main intracorporal bottom, and the magnet block passes through spring and main intracorporal bottom
Portion's connection, the distance between the magnet block and bottom in main body are less than the distance between top and main body bottom end of moving tube.
Preferably, being equipped with baroceptor and PLC, the suction pump, electromagnetism in the main body to realize intelligence
Iron, baroceptor are electrically connected with PLC.
Preferably, being set in the main body there are two accessory part, two accessory parts are distinguished to improve sealing effect
The both ends of fixing pipe are set, and the accessory part includes cylinder and block plate, and the block plate and fixing pipe are coaxially disposed, the gear
The diameter of disk and the outer diameter of fixing pipe are equal, and gap is equipped between the block plate and fixing pipe, and block plate is arranged in the cylinder
Side far from fixing pipe, the cylinder are fixed on the inner wall of main body, and the cylinder drives block plate along the axial direction of fixing pipe
Mobile, the cylinder is electrically connected with PLC.
Preferably, in order to reduce block plate and fixing pipe against when the impact force that generates, the making material of the block plate is
Rubber.
Preferably, being equipped with strainer in the air inlet pipe in order to avoid dust is entered in main body by air inlet pipe.
Preferably, the main body is equipped at least two solar panels for energy conservation, the solar panels are uniformly arranged
On the top of main body.
Preferably, being coated with stop-leak compound on the inner wall of the moving tube to reduce the gap between moving tube and main body.
The invention has the advantages that the unmanned flight's device with heat sinking function for being used for marine security protection patrol passes through
Cooling mechanism realizes the function of heat dissipation, avoids being chronically under hot environment and damaging, should compared with existing cooling mechanism
Cooling mechanism structure is simple, and cost is lower, moreover, also realizes function of the forced landing on the water surface by auxiliary body
Can, compared with existing auxiliary body, auxiliary body's clever structure, practicability is stronger.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural representation of unmanned flight's device with heat sinking function for marine security protection patrol of the invention
Figure；
Fig. 2 is the cross-sectional view of unmanned flight's device with heat sinking function for marine security protection patrol of the invention；
Fig. 3 is the seal assembly of unmanned flight's device with heat sinking function for marine security protection patrol of the invention
Structural schematic diagram；
Fig. 4 is the portion the A enlarged drawing of Fig. 2；
In figure: 1. main bodys, 2. rotors, 3. support rods, 4. cameras, 5. air inlet pipe, 6. suction pumps, 7. fixing pipes, 8. move
Dynamic pipe, 9. seal discs, 10. electromagnet, 11. sealing-plugs, 12. magnet plates, 13. connecting rods, 14. magnet blocks, 15. springs, 16. push away
Bar, 17. baroceptors, 18. cylinders, 19. block plates, 20. strainers, 21. solar panels.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in Figs. 1-2, a kind of unmanned flight's device with heat sinking function for marine security protection patrol, including main body
1, the shape of four rotors, 2, four support rods 3 and four cameras 4, the main body 1 is cylinder, and four rotors 2 are with main body 1
Axis centered on be circumferentially uniformly arranged on the body 1, the support rod 3 is corresponded with rotor 2, the support rod 3 with it is main
Body 1 is parallel, and the top of the support rod 3 is fixedly connected with main body 1, and the camera 4 is corresponded with support rod 3, described to take the photograph
The side for the separate main body 1 that support rod 3 is arranged in as first 4, the main body 1 are equipped with driving device, the driving device and rotation
The wing 2 is sequentially connected, 1 controlling system of main body and fault monitoring system, and the main body 1 is equipped with auxiliary body and heat dissipation machine
Structure；
The cooling mechanism includes air inlet pipe 5, suction pump 6 and fixing pipe 7, and the top of the main body 1 is equipped with mounting hole, institute
The axis for stating mounting hole is parallel with support rod 3, and the air inlet pipe 5 is coaxially disposed with mounting hole, the outer diameter and peace of the air inlet pipe 5
The aperture for filling hole is equal, and the air inlet pipe 5 is sealed and is fixedly connected with the inner wall of mounting hole, and the suction pump 6 and fixing pipe 7 are equal
In main body 1, the suction pump 6 is arranged in air inlet pipe 5, and the suction pump 6 is fixed on the inner wall of main body 1, described solid
The axis for determining pipe 7 is vertical with the axis of air inlet pipe 5 and intersect, and the bottom end of air inlet pipe 5, institute is arranged in the middle-end of the fixing pipe 7
It states air inlet pipe 5 and is connected to and is fixedly connected with fixing pipe 7, the bottom in main body 1, the top of the main body 1 is arranged in the fixing pipe 7
Portion is equipped at least two ventholes, and the venthole is circumferentially uniformly distributed centered on the axis of mounting hole, the venthole
Axis is parallel with the axis of mounting hole；
The auxiliary body includes moving tube 8, seal disc 9, seal assembly and connection component, the moving tube 8 and main body 1
Coaxial arrangement, the internal diameter of the moving tube 8 are greater than the outer diameter of main body 1, and the main body 1 passes through moving tube 8, the main body 1 and shifting
Dynamic pipe 8 slidingly and sealingly connects, and the seal disc 9 is coaxially disposed with moving tube 8, diameter and the moving tube 8 of the seal disc 9
Outer diameter is equal, and the bottom end of moving tube 8, bottom end seal and fixation of the seal disc 9 with moving tube 8 is arranged in the seal disc 9
Connection, the bottom end of the main body 1 are equipped at least two connecting holes, and the connecting hole and venthole correspond, the seal disc 9
With the bottom end of main body 1 against and be tightly connected, the seal assembly is arranged on venthole, and the component is arranged in seal disc 9
On.
Rotor 2 is rotated by driving device, so that main body 1 be made to realize the effect of flight, video is acquired by camera 4
Signal, and terminal is transmitted to by control system, it realizes patrol, during flight, is run by suction pump 6, make external air
Entered in fixing pipe 7 by air inlet pipe 5, then is discharged from the both ends of fixing pipe 7, and the air in main body 1 is discharged from venthole, leads to
The directed flow of air is crossed, the heat in main body 1 can be made to be discharged, realize the function of heat dissipation, during which, seal disc 9 passes through company
Connected components and main body 1 keep opposing stationary positional relationship, when fault monitoring system monitors fault-signal, pass through sealing group
Part is realized venthole and is sealed, and connection component stops realizing seal disc 9 fixation, after the air pressure in main body 1 increases, seal disc
9 is mobile away from 1 direction of main body under the influence of air pressure, and drives connecting tube mobile, and the bottom end of main body 1 is made to generate a sky
Chamber, the characteristic that can be floated by cavity in the water surface allow the device to float the function of realizing forced landing across the sea.
As shown in figure 3, the seal assembly includes electromagnet 10, sealing-plug 11,12, two connecting rods 13 of magnet plate and two
Through hole, the magnet plate 12 is vertical with the axis of venthole, and the sealing-plug 11 is matched with venthole and face is arranged, described
Sealing-plug 11 is fixed on the side of the close venthole of magnet plate 12, the other side of the electromagnet 10 and magnet plate 12 against,
The electromagnet 10 is fixed on the inner wall of main body 1, and gap is equipped between the sealing-plug 11 and venthole, and through hole setting exists
On magnet plate 12, the electromagnet 10 is located between two through holes, and the axis of the through hole and the axis of venthole are parallel,
The connecting rod 13 is coaxially disposed with through hole, and the diameter of the connecting rod 13 is equal with the aperture of through hole, and the connecting rod 13 passes through
Through hole, the connecting rod 13 are slidably connected with through hole, and the top of the connecting rod 13 is fixed on the top in main body 1.
When fault monitoring system monitors fault-signal, electric current is passed to by electromagnet 10, makes electromagnet 10 and magnet
Mutually exclusive active force is produced between plate 12, to make magnet plate 12 that sealing-plug 11 be driven to be moved in venthole, is realized
The effect of venthole is sealed, when fault monitoring system does not monitor fault-signal, 10 reverse current of electromagnet makes electromagnet 10
The active force to attract each other is generated between magnet plate 12, to make magnet plate 12 that sealing-plug 11 be driven to reset.
Preferably, being coated with lubricating oil on the connecting rod 13 to reduce the frictional force between magnet plate 12 and connecting rod 13.
The effect of lubricating oil is the frictional force reduced between magnet plate 12 and connecting rod 13, improves the mobile smoothness of magnet plate 12
Property.
As shown in figure 4, the side of the separate magnet plate 12 of electromagnet 10, the connection component is arranged in the connection component
Including magnet block 14, spring 15, push rod 16 and pilot hole, the pilot hole is arranged in the bottom end of main body 1, the pilot hole with go out
Stomata coaxial arrangement, the push rod 16 are coaxially disposed with venthole, and the diameter of the push rod 16 is equal with the aperture of pilot hole, institute
Push rod 16 is stated across pilot hole, the push rod 16 is slidingly and sealingly connect with the inner wall of pilot hole, and the bottom end of the push rod 16 is solid
It is scheduled on seal disc 9, the magnet block 14 is fixed on the top of push rod 16, the separate magnet of the magnet block 14 and electromagnet 10
The side of plate 12 is against the spring 15 is located between the bottom in magnet block 14 and main body 1, and the magnet block 14 passes through spring
15 connect with the bottom in main body 1, the distance between the magnet block 14 and bottom in main body 1 be less than the top of moving tube 8 with
The distance between 1 bottom end of main body.
When fault monitoring system does not monitor fault-signal, electromagnet 10 passes to electric current, makes electromagnet 10 and magnet block
The active force to attract each other is generated between 14, so that magnet block 14 be made to be moved by 16 seal disc 9 of push rod by towards close to main body 1
Dynamic pulling force, to make to keep opposing stationary positional relationship between seal disc 9 and main body 1, when fault monitoring system monitors
When fault-signal, reverse current is passed to by electromagnet 10, makes to generate mutually exclusive work between electromagnet 10 and magnet block 14
Firmly, so that magnet block 14 be made to push seal disc 9 away from the movement of 1 direction of main body by push rod 16, and compress spring 15,
Realize the mobile function of driving seal disc 9.
Preferably, in order to realize intelligence, it is equipped with baroceptor 17 and PLC in the main body 1, the suction pump 6,
Electromagnet 10, baroceptor 17 are electrically connected with PLC.
When fault monitoring system does not monitor fault-signal, fault monitoring system issues signal to PLC, and PLC is that is, programmable
Logic controller, it is used for its internally stored program using a kind of programmable memory, execute logical operation, sequential control,
Periodically, count with the user oriented instruction such as arithmetical operation, and it is various types of by number or analog pattern input, output control
Mechanical or production process, its essence is a kind of computer for being exclusively used in Industry Control, hardware configuration substantially with miniature calculating
Machine is identical, is generally used for the reception and output of processing and the instruction of data, for realizing center control, to make PLC control
Suction pump 6 is run, and electromagnet 10 is powered, and when fault monitoring system monitors fault-signal, fault monitoring system is given again
PLC issues signal, and PLC control electromagnet 10 passes to reverse current, when the atmospheric pressure value in main body 1 is greater than the setting of pressure sensor
When value, pressure sensor issues signal to PLC, and PLC control suction pump 6 is out of service, realizes intelligence.
Preferably, being set in the main body 1 there are two accessory part, two accessory parts divide to improve sealing effect
The both ends of fixing pipe 7 are not set, and the accessory part includes cylinder 18 and block plate 19, and the block plate 19 and fixing pipe 7 are coaxial
Setting, the diameter of the block plate 19 is equal with the outer diameter of fixing pipe 7, and gap is equipped between the block plate 19 and fixing pipe 7, described
The side of the separate fixing pipe 7 of block plate 19 is arranged in cylinder 18, and the cylinder 18 is fixed on the inner wall of main body 1, the cylinder
18 drive block plates 19 along the axial movement of fixing pipe 7, and the cylinder 18 is electrically connected with PLC.
When pressure sensor issues signal to PLC, PLC controls cylinder 18 and runs, and makes block plate 19 and fixing pipe 7 against real
The effect for now blocking fixing pipe 7, improves leakproofness.
Preferably, in order to reduce block plate 19 and fixing pipe 7 against when the impact force that generates, the production material of the block plate 19
Material is rubber.
Rubber quality is more soft, can reduce block plate 19 and fixing pipe 7 against when the impact force that generates, realize buffering
And effectiveness in vibration suppression.
Preferably, being equipped with strainer 20 in the air inlet pipe 5 in order to avoid dust is entered in main body 1 by air inlet pipe 5.
The effect of strainer 20 is that dust is avoided to enter in main body 1 by air inlet pipe 5, realizes dust-proof effect.
Preferably, the main body 1 is equipped at least two solar panels 21, and the solar panels 21 are for energy conservation
The even top that main body 1 is set.
Solar panels 21 can be absorbed light and realize photovoltaic power generation, and institute's generated energy provides device operation, plays energy conservation
The effect of environmental protection, also improves cruising ability.
Preferably, being coated with sealing on the inner wall of the moving tube 8 to reduce the gap between moving tube 8 and main body 1
Rouge.
The effect of stop-leak compound is the gap reduced between moving tube 8 and main body 1, improves leakproofness.
The device, by making the air in main body 1 and the air outside main body 1 realize directed flow, makes during flight
Heat discharge in main body 1, realizes the function of heat dissipation, when a failure occurs it, moves seal disc 9 away from 1 direction of main body
It is dynamic, so that the bottom of main body 1 is generated cavity, so that main body 1 be allow to float across the sea, realizes forced landing；
Compared with prior art, which passes through heat dissipation
Mechanism realizes the function of heat dissipation, avoids being chronically under hot environment and damaging, compared with existing cooling mechanism, the heat dissipation
Mechanism structure is simple, and cost is lower, moreover, also realizes function of the forced landing on the water surface by auxiliary body, with
Existing auxiliary body compares, auxiliary body's clever structure, and practicability is stronger.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to which the technical scope thereof is determined according to the scope of the claim.
Claims (10)
1. a kind of unmanned flight's device with heat sinking function for marine security protection patrol, including main body (1), four rotors
(2), the shape of four support rods (3) and four cameras (4), the main body (1) is cylinder, and four rotors (2) are with main body
(1) it is circumferentially uniformly arranged on centered on axis on main body (1), the support rod (3) and rotor (2) correspond, the branch
Strut (3) is parallel with main body (1), and the top of the support rod (3) is fixedly connected with main body (1), the camera (4) and support
Bar (3) corresponds, and camera (4) setting is set on the side of the separate main body (1) of support rod (3), the main body (1)
There is driving device, the driving device and rotor (2) are sequentially connected, main body (1) controlling system and fault monitoring system,
It is characterized in that, the main body (1) is equipped with auxiliary body and cooling mechanism；
The cooling mechanism includes air inlet pipe (5), suction pump (6) and fixing pipe (7), and the top of the main body (1) is equipped with installation
The axis in hole, the mounting hole is parallel with support rod (3), and the air inlet pipe (5) and mounting hole are coaxially disposed, the air inlet pipe
(5) outer diameter is equal with the aperture of mounting hole, and the air inlet pipe (5) seals and is fixedly connected, the pumping with the inner wall of mounting hole
Sucking pump (6) and fixing pipe (7) are respectively positioned in main body (1), and the suction pump (6) is arranged on air inlet pipe (5), the suction pump
(6) it is fixed on the inner wall of main body (1), the axis of the fixing pipe (7) is vertical with the axis of air inlet pipe (5) and intersects, described
The middle-end of fixing pipe (7) is arranged in the bottom end of air inlet pipe (5), and the air inlet pipe (5) is connected to and is fixedly connected with fixing pipe (7),
The bottom that the fixing pipe (7) is arranged in main body (1), the top of the main body (1) are equipped at least two ventholes, it is described go out
Stomata is circumferentially uniformly distributed centered on the axis of mounting hole, and the axis of the venthole and the axis of mounting hole are parallel；
The auxiliary body includes moving tube (8), seal disc (9), seal assembly and connection component, the moving tube (8) and main
Body (1) coaxial arrangement, the internal diameter of the moving tube (8) are greater than the outer diameter of main body (1), and the main body (1) passes through moving tube (8),
The main body (1) slidingly and sealingly connect with moving tube (8), and the seal disc (9) and moving tube (8) are coaxially disposed, described close
The diameter of closing disk (9) is equal with the outer diameter of moving tube (8), and the seal disc (9) setting is described close in the bottom end of moving tube (8)
It closing disk (9) and the bottom end seal of moving tube (8) and is fixedly connected, the bottom end of the main body (1) is equipped at least two connecting holes, institute
Connecting hole and venthole is stated to correspond, the bottom end of the seal disc (9) and main body (1) against and be tightly connected, the sealing
Component is arranged on venthole, and the component is arranged on seal disc (9).
2. unmanned flight's device with heat sinking function as described in claim 1 for marine security protection patrol, feature exist
In, the seal assembly include electromagnet (10), sealing-plug (11), magnet plate (12), two connecting rods (13) and two through holes,
The magnet plate (12) is vertical with the axis of venthole, and the sealing-plug (11) matches with venthole and face is arranged, described close
Blocking (11) is fixed on the side of the close venthole of magnet plate (12), the other side of the electromagnet (10) and magnet plate (12)
Against, the electromagnet (10) is fixed on the inner wall of main body (1), gap is equipped between the sealing-plug (11) and venthole,
Through hole is arranged on magnet plate (12), and the electromagnet (10) is located between two through holes, the axis of the through hole with
The axis of venthole is parallel, and the connecting rod (13) and through hole are coaxially disposed, the diameter of the connecting rod (13) and the hole of through hole
Diameter is equal, and the connecting rod (13) passes through through hole, and the connecting rod (13) is slidably connected with through hole, the top of the connecting rod (13)
It is fixed on the top in main body (1).
3. unmanned flight's device with heat sinking function as claimed in claim 2 for marine security protection patrol, feature exist
In being coated with lubricating oil on the connecting rod (13).
4. unmanned flight's device with heat sinking function as claimed in claim 2 for marine security protection patrol, feature exist
In the connection component is arranged in the side of the separate magnet plate (12) of electromagnet (10), and the connection component includes magnet block
(14), spring (15), push rod (16) and pilot hole, the pilot hole are arranged in the bottom end of main body (1), the pilot hole and outlet
Hole coaxial arrangement, the push rod (16) and venthole are coaxially disposed, and the diameter of the push rod (16) is equal with the aperture of pilot hole,
The push rod (16) passes through pilot hole, and the push rod (16) slidingly and sealingly connect with the inner wall of pilot hole, the push rod (16)
Bottom end be fixed on seal disc (9), the magnet block (14) is fixed on the top of push rod (16), the magnet block (14) and electricity
The side of the separate magnet plate (12) of magnet (10) is against the spring (15) is located at the bottom in magnet block (14) and main body (1)
Between portion, the magnet block (14) is connect by spring (15) with the bottom in main body (1), the magnet block (14) and main body
(1) the distance between interior bottom is less than the distance between top and main body (1) bottom end of moving tube (8).
5. unmanned flight's device with heat sinking function as claimed in claim 2 for marine security protection patrol, feature exist
In equipped with baroceptor (17) and PLC, the suction pump (6), electromagnet (10), baroceptor in the main body (1)
(17) it is electrically connected with PLC.
6. unmanned flight's device with heat sinking function as claimed in claim 5 for marine security protection patrol, feature exist
There are two accessory parts in setting in, the main body (1), and two accessory parts are separately positioned on the both ends of fixing pipe (7), described auxiliary
Helping component includes cylinder (18) and block plate (19), and the block plate (19) and fixing pipe (7) are coaxially disposed, the block plate (19) it is straight
Diameter is equal with the outer diameter of fixing pipe (7), and gap, cylinder (18) setting are equipped between the block plate (19) and fixing pipe (7)
In the side of the separate fixing pipe (7) of block plate (19), the cylinder (18) is fixed on the inner wall of main body (1), the cylinder
(18) drive block plate (19) along the axial movement of fixing pipe (7), the cylinder (18) is electrically connected with PLC.
7. unmanned flight's device with heat sinking function as claimed in claim 6 for marine security protection patrol, feature exist
In the making material of the block plate (19) is rubber.
8. unmanned flight's device with heat sinking function as described in claim 1 for marine security protection patrol, feature exist
In equipped with strainer (20) in the air inlet pipe (5).
9. unmanned flight's device with heat sinking function as described in claim 1 for marine security protection patrol, feature exist
In the main body (1) is equipped at least two solar panels (21), and the solar panels (21) are uniformly arranged on main body (1)
Top.
10. unmanned flight's device with heat sinking function as described in claim 1 for marine security protection patrol, feature exist
In being coated with stop-leak compound on the inner wall of the moving tube (8).
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111147718A (en) * | 2019-12-24 | 2020-05-12 | 深圳市安思科电子科技有限公司 | Monitoring device convenient to accomodate based on block chain technique |
Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103108804A (en) * | 2010-06-29 | 2013-05-15 | 航空环境公司 | UAV having hermetically sealed modularized compartments and fluid drain ports |
| US20160288901A1 (en) * | 2015-03-31 | 2016-10-06 | Vantage Robotics, Llc | Propeller-motor assembly for efficient thermal dissipation |
| CN205971857U (en) * | 2016-08-30 | 2017-02-22 | 北方天途航空技术发展（北京）有限公司 | UAV (Unmanned aerial vehicle) for plant protection |
| JP6090407B1 (en) * | 2015-10-27 | 2017-03-08 | 三菱電機株式会社 | Storage movement device |
| CN107554763A (en) * | 2015-07-02 | 2018-01-09 | 深圳市大疆创新科技有限公司 | Unmanned plane, its control system and method, and unmanned plane landing control method |
| CN207106876U (en) * | 2017-07-27 | 2018-03-16 | 河南大域航空科技有限公司 | A kind of rain-proof unmanned plane |
| WO2018067499A1 (en) * | 2016-10-04 | 2018-04-12 | Wal-Mart Stores, Inc. | Systems and methods utilizing nanotechnology insulation materials in limiting temperature changes during product delivery |
| KR20180051270A (en) * | 2016-11-08 | 2018-05-16 | 한국항공우주연구원 | Motor cooling apparatus |
| CN108082400A (en) * | 2017-12-18 | 2018-05-29 | 佛山市神风航空科技有限公司 | Aerial photography aircraft airplane parking area waterborne |
| CN207990525U (en) * | 2018-03-30 | 2018-10-19 | 浙江杭一电器有限公司 | A kind of radiator for unmanned plane lighting device |
| CN108791833A (en) * | 2018-06-19 | 2018-11-13 | 郑州秉茂达电子科技有限公司 | A kind of unmanned plane amphibious landing gear |
| CN109552624A (en) * | 2017-09-25 | 2019-04-02 | 江苏华夏知识产权服务有限公司 | A kind of intelligent disaster relief unmanned plane for drug delivery based on Internet of Things |
| CN208775025U (en) * | 2018-08-28 | 2019-04-23 | 郑州光之源电子科技有限公司 | A kind of unmanned plane radiator |
| CN109823524A (en) * | 2019-02-18 | 2019-05-31 | 深圳市律远汇智科技有限公司 | A kind of highly-safe unmanned flight's device for agricultural |
-
2019
- 2019-08-13 CN CN201910744747.0A patent/CN110450953B/en active Active
Patent Citations (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103108804A (en) * | 2010-06-29 | 2013-05-15 | 航空环境公司 | UAV having hermetically sealed modularized compartments and fluid drain ports |
| US20160288901A1 (en) * | 2015-03-31 | 2016-10-06 | Vantage Robotics, Llc | Propeller-motor assembly for efficient thermal dissipation |
| CN107554763A (en) * | 2015-07-02 | 2018-01-09 | 深圳市大疆创新科技有限公司 | Unmanned plane, its control system and method, and unmanned plane landing control method |
| JP6090407B1 (en) * | 2015-10-27 | 2017-03-08 | 三菱電機株式会社 | Storage movement device |
| CN205971857U (en) * | 2016-08-30 | 2017-02-22 | 北方天途航空技术发展（北京）有限公司 | UAV (Unmanned aerial vehicle) for plant protection |
| WO2018067499A1 (en) * | 2016-10-04 | 2018-04-12 | Wal-Mart Stores, Inc. | Systems and methods utilizing nanotechnology insulation materials in limiting temperature changes during product delivery |
| KR20180051270A (en) * | 2016-11-08 | 2018-05-16 | 한국항공우주연구원 | Motor cooling apparatus |
| CN207106876U (en) * | 2017-07-27 | 2018-03-16 | 河南大域航空科技有限公司 | A kind of rain-proof unmanned plane |
| CN109552624A (en) * | 2017-09-25 | 2019-04-02 | 江苏华夏知识产权服务有限公司 | A kind of intelligent disaster relief unmanned plane for drug delivery based on Internet of Things |
| CN108082400A (en) * | 2017-12-18 | 2018-05-29 | 佛山市神风航空科技有限公司 | Aerial photography aircraft airplane parking area waterborne |
| CN207990525U (en) * | 2018-03-30 | 2018-10-19 | 浙江杭一电器有限公司 | A kind of radiator for unmanned plane lighting device |
| CN108791833A (en) * | 2018-06-19 | 2018-11-13 | 郑州秉茂达电子科技有限公司 | A kind of unmanned plane amphibious landing gear |
| CN208775025U (en) * | 2018-08-28 | 2019-04-23 | 郑州光之源电子科技有限公司 | A kind of unmanned plane radiator |
| CN109823524A (en) * | 2019-02-18 | 2019-05-31 | 深圳市律远汇智科技有限公司 | A kind of highly-safe unmanned flight's device for agricultural |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111147718A (en) * | 2019-12-24 | 2020-05-12 | 深圳市安思科电子科技有限公司 | Monitoring device convenient to accomodate based on block chain technique |
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