CN109911208A - A kind of monitoring based on thermal image analysis and drive alarm unmanned plane - Google Patents
A kind of monitoring based on thermal image analysis and drive alarm unmanned plane Download PDFInfo
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- CN109911208A CN109911208A CN201910254599.4A CN201910254599A CN109911208A CN 109911208 A CN109911208 A CN 109911208A CN 201910254599 A CN201910254599 A CN 201910254599A CN 109911208 A CN109911208 A CN 109911208A
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Abstract
The invention discloses a kind of monitoring based on thermal image analysis and drive alarm unmanned plane, its structure includes urgent protection thermal image analysis fixing device, thermal image analysis camera, fixed foot prop, unmanned plane motor, rotate blade, unmanned plane wing, unmanned plane body, comprehensive adjuster, urgent protection thermal image analysis fixing device is set to thermal image analysis camera upper end and is connected by way of fixed installation, fixed feet is set up in unmanned plane body lower end and is connected by movable mode, the present invention is equipped with when unmanned plane breaks down in flight course, the equipment for having data automatically disengage and the structure of safe falling, help to prevent data in equipment from losing, monitoring work is impacted, simultaneously, equipped with the bird repellent structure started automatically by gravity, effectively prevent due to carelessness Forget to start, cause unmanned plane in flight course, is hit with birds.
Description
Technical field
The present invention relates to unmanned plane fields, more precisely, being a kind of monitoring based on thermal image analysis and driving alarm
Unmanned plane.
Background technique
With the development of science and technology, unmanned plane has been widely used in every field, mountable many equipment on unmanned plane are led to
It crosses and carries these equipment and work, the equipment of carrying has alarm device, monitor, thermal image analysis camera etc..But at present
This unmanned plane has the following disadvantages:
1, during unmanned plane works in the sky, when the interference by force majeure, unmanned plane breaks down, due to
Unmanned plane during flying is higher from the ground, and when falling, the thermal image analysis camera installed on unmanned plane can generate damage, leads to heat
Data in imaging analysis camera are lost, and are impacted to monitoring work.
2, simultaneously, unmanned plane before take-off, needs to manually start scarecrow device, is easy to forget to start because of carelessness, cause
Unmanned plane is hit in flight course with birds.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of monitoring based on thermal image analysis and driving
It alarms unmanned plane, to solve during the unmanned plane of the prior art works in the sky, when the interference by force majeure, nothing
It is man-machine to break down, since unmanned plane during flying is higher from the ground, when falling, the thermal image analysis camera installed on unmanned plane
Damage can be generated, causes the data in thermal image analysis camera to be lost, monitoring work is impacted, meanwhile, nobody
Machine before take-off, needs to manually start scarecrow device, is easy to forget to start because of carelessness, causes unmanned plane in flight course,
It is hit with birds.
To achieve the goals above, the present invention is to realize by the following technical solutions:
A kind of monitoring based on thermal image analysis and alarm unmanned plane is driven, structure includes urgent protection thermal image analysis
Fixing device, thermal image analysis camera, fixed foot prop, unmanned plane motor, rotation blade, unmanned plane wing, unmanned plane
Body, comprehensive adjuster, the urgent protection thermal image analysis fixing device are set to thermal image analysis camera upper end
And it is connected by way of fixed installation, the fixed feet is set up in unmanned plane body lower end and by movable mode
It is connected, the unmanned plane motor is set to rotation blade lower end and is connected by way of rotation, the unmanned plane horse
Up to being set to unmanned plane wing upper end and being connected by way of insertion installation, the unmanned plane wing is set to unmanned plane body
Left end and it is connected by welding, the unmanned plane body is set to comprehensive adjuster upper end and by fixed peace
The mode of dress is connected, and the comprehensive adjuster is set to urgent protection thermal image analysis fixing device upper end and passes through
Nested mode is connected, and the urgent protection thermal image analysis fixing device includes balance trigger mechanism, fixed limitation
Mechanism, fixed installation sector, the safe mechanism that comes, GPS positioning mechanism, lifting trigger mechanism, supersonic wave bird driving mechanism are described flat
With fixed limiting mechanism using being electrically connected, the fixed limiting mechanism is set to fixed installation sector lower end and leads to weighing apparatus trigger mechanism
The mode for crossing insertion installation is connected, and the safety comes mechanism set on fixed installation sector lower end and by transmission cooperation
Mode is connected, and the GPS positioning mechanism is set to below lifting trigger mechanism, the lifting trigger mechanism and supersonic wave bird driving machine
Structure is using electrical connection.
As the present invention, further scheme, the balance trigger mechanism include trigger switch, steel ball loose collar, loose collar
Fixed block, balance steel ball, crust of the device, terminal control unit, connecting cable, the trigger switch are used with terminal control unit and are electrically connected
It connects, the trigger switch is set to inside steel ball loose collar and is connected by way of fixed installation, and the loose collar is fixed
Block is set to steel ball loose collar right end and is connected by welding, and the balance steel ball is set to inside steel ball loose collar simultaneously
And be connected by movable mode, the terminal control unit is set to inside crust of the device and the phase by way of fixed installation
Connection, with terminal control unit using being electrically connected, the connecting cable is used with fixed limiting mechanism and is electrically connected the connecting cable.
As the present invention, further scheme, the fixed limiting mechanism include fixed limiting mechanism shell, powerful electromagnetic
Iron, spring card slot, sliding groove, linking spring, linking movable plate, the strong electromagnet are set to fixed limiting mechanism interior of shell
And it is connected by way of fixed installation, the spring card slot is set to linking movable plate right end and is integrated,
The linking movable plate is set to sliding groove upper end and is connected by way of sliding, and the sliding groove is set to fixed limitation machine
It structure interior of shell and is integrated, the linking spring is set to spring card slot right end and by way of transmission cooperation
It is connected, the linking spring is set to fixed limiting mechanism interior of shell and is connected by welding.
As the present invention, further scheme, the fixed installation sector include insertion fixed block, block, limitation are fixedly mounted
Kelly, shifting chute, the insertion fixed block, which is set to, to be fixedly mounted block lower end and is integrated, and the limitation kelly is set to
It is embedded in fixed block left end and is connected by way of insertion installation, the limitation kelly is set to inside shifting chute and passes through
The mode of sliding is connected.
As the present invention further scheme, the safety mechanism that comes includes chute pack positioning ring, mechanical spring, drop
Fall umbrella capsule, effect push plate, linking rope, rope locating piece, rope storage tray, centralized positioning axis, the chute pack positioning ring
It is located at same axle center with chute pack and uses transition fit, the mechanical spring is set to effect push plate upper end and passes through biography
The mode of dynamic cooperation is connected, and the effect push plate is set to chute pack lower end and is connected by way of fitting, described
Linking rope is connected through rope locating piece center and by movable mode, and the rope locating piece is received set on rope
It receives and disk upper end and is connected by welding, the rope storage tray in same axle center and leads to centralized positioning axle position
The mode for crossing rotation is connected.
As the present invention, further scheme, the GPS positioning mechanism include SIM card fixing groove, SIM card, fix pasting board,
The SIM card is set to inside SIM card fixing groove and is connected by way of insertion installation, and the fixed pasting board is set to SIM
Card front end face and it is connected by way of fitting.
As the present invention, further scheme, the lifting trigger mechanism include lifting trigger mechanism shell, spring limitation
Slot, extension spring, shock start switch, hit trigger ball, hit shutdown switch, and the spring limiting groove is set to lifting triggering machine
It structure interior of shell and is integrated, the spring limiting groove is set to extension spring left end and by the side of transmission cooperation
Formula is connected, and the extension spring, which is set to, hits trigger ball left end and be connected by welding, the shock starting
Switch is set to lifting trigger mechanism outer casing inner wall and is connected by way of fixed installation, and the shock, which starts switch, to be located at
It hits immediately below shutdown switch, the shock shutdown switch is used with supersonic wave bird driving mechanism and is electrically connected.
As the present invention, further scheme, the supersonic wave bird driving mechanism include supersonic generator fixed plate, ultrasound
Wave producer, the supersonic generator fixed plate are set to supersonic generator left end and are connected by way of fixed installation
It connects.
Invention beneficial effect
A kind of monitoring based on thermal image analysis of the invention and alarm unmanned plane is driven, when unmanned plane is by force majeure
And when breaking down, unmanned plane disequilibrium is inverted, and the balance steel ball in steel ball loose collar is rolled, and is being scrolled through
Cheng Zhongyu trigger switch is in contact, so that terminal control unit induces current into strong electromagnet, strong electromagnet is to metal material
The linking movable plate of matter generates adsorption capacity, drives limitation kelly to release the limit to insertion fixed block so that linking movable plate is mobile
System, thermal image analysis camera moment is detached from unmanned plane body, during disengaging, block is fixedly mounted and releases to chute pack
Limitation, the mechanical spring of compressive state releases elastic force limitation, sprung back, and induced effect push plate is by chute pack device for ejecting
Outside shell, the small-sized parachute in chute pack is opened, so that thermal image analysis camera gently lands in ground, staff
Can be carried out by the positioning to SIM card recycling thermal image analysis camera, when unmanned plane body takes off, hit trigger ball by
Moment generates overweight, is moved down, starts switch and be in contact with shock, so that supersonic generator is started to work, to sky
In birds expelled, when unmanned plane body lands, hit the weightlessness that is generated by moment of trigger ball, moved up, and hit
It hits shutdown switch to be in contact, supersonic generator stops working.
A kind of monitoring based on thermal image analysis of the invention and alarm unmanned plane is driven, equipped with flying when unmanned plane
When breaking down in journey, the equipment for having data automatically disengage and the structure of safe falling, helps to prevent number in equipment
According to losing, monitoring work is impacted, meanwhile, equipped with the bird repellent structure started automatically by gravity, effectively prevent
Forget to start because of carelessness, cause unmanned plane in flight course, is hit with birds.
Detailed description of the invention
By reading referring to attached drawing detailed description of non-limiting embodiments, other feature of the invention, purpose
It will be become more apparent upon with advantage.
In the accompanying drawings:
Fig. 1 is a kind of monitoring based on thermal image analysis of the present invention and the structural schematic diagram for driving alarm unmanned plane.
Fig. 2 is a kind of structural plan figure of urgent protection thermal image analysis fixing device of the present invention.
Fig. 3 is a kind of detailed construction schematic diagram of urgent protection thermal image analysis fixing device of the present invention.
Fig. 4 is a kind of detailed construction schematic diagram of fixed limiting mechanism of the present invention.
Fig. 5 is a kind of detailed construction schematic diagram for going up and down trigger mechanism of the present invention.
In figure: urgent protection thermal image analysis fixing device -1, thermal image analysis camera -2, fixed foot prop -3,
Unmanned plane motor -4, rotation blade -5, unmanned plane wing -6, unmanned plane body -7, comprehensive adjuster -8, balance triggering machine
Structure -11, fixed limiting mechanism -12, fixed installation sector -13, the safe mechanism -14 that comes, GPS positioning mechanism -15, lifting triggering
Mechanism -16, trigger switch -1101, steel ball loose collar -1102, loose collar fixed block -1103, is put down supersonic wave bird driving mechanism -17
Weigh steel ball -1104, crust of the device -1105, terminal control unit -1106, connecting cable -1107, fixed limiting mechanism shell -
1201, strong electromagnet -1202, spring card slot -1203, sliding groove -1204, linking spring -1205, linking movable plate -1206,
It is embedded in fixed block -1301, block -1302, limitation kelly -1303, shifting chute -1304, chute pack positioning ring-is fixedly mounted
1401, mechanical spring -1402, chute pack -1403, effect push plate -1404, linking rope -1405, rope locating piece -1406,
Rope storage tray -1407, SIM card fixing groove -1501, SIM card -1502, fixed pasting board -1503, rises centralized positioning axis -1408
Drop trigger mechanism shell -1601, spring limiting groove -1602, extension spring -1603, shock start switch -1604, hit triggering
Ball -1605 hits shutdown switch -1606, supersonic generator fixed plate -1701, supersonic generator -1702.
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
As Figure 1-Figure 5, the present invention provides a kind of monitoring based on thermal image analysis and drives the skill of alarm unmanned plane
Art scheme:
A kind of monitoring based on thermal image analysis and alarm unmanned plane is driven, structure includes urgent protection thermal image analysis
Fixing device 1, thermal image analysis camera 2, fixed foot prop 3, unmanned plane motor 4, rotation blade 5, unmanned plane wing 6,
Unmanned plane body 7, comprehensive adjuster 8, the urgent protection thermal image analysis fixing device 1 are taken the photograph set on thermal image analysis
It is connected as first 2 upper end and by way of fixed installation, the fixed foot prop 3 is set to 7 lower end of unmanned plane body and leads to
It crosses movable mode to be connected, the unmanned plane motor 4 is set to rotation 5 lower end of blade and is connected by way of rotation
, the unmanned plane motor 4 be set to 6 upper end of unmanned plane wing and insertion installation by way of be connected, the unmanned plane
Wing 6 is set to 7 left end of unmanned plane body and is connected by welding, and the unmanned plane body 7 is set to comprehensive tune
It saves 8 upper end of device and is connected by way of fixed installation, the comprehensive adjuster 8 is set to urgent protection thermal image analysis
1 upper end of fixing device and it is connected by way of nested, the urgent protection thermal image analysis fixing device 1
Including balance trigger mechanism 11, fixed limiting mechanism 12, fixed installation sector 13, safe come mechanism 14, GPS positioning mechanism
15, trigger mechanism 16, supersonic wave bird driving mechanism 17 are gone up and down, the balance trigger mechanism 11 is used with fixed limiting mechanism 12 and is electrically connected
It connects, the fixed limiting mechanism 12 is set to 13 lower end of fixed installation sector and is connected by way of insertion installation, described
The mechanism 14 that comes safely is connected set on 13 lower end of fixed installation sector and by way of transmission cooperation, the GPS positioning
Mechanism 15 is set to 16 lower section of lifting trigger mechanism, and the lifting trigger mechanism 16 is used with supersonic wave bird driving mechanism 17 and is electrically connected,
The balance trigger mechanism 11 includes trigger switch 1101, steel ball loose collar 1102, loose collar fixed block 1103, balance steel ball
1104, crust of the device 1105, terminal control unit 1106, connecting cable 1107, the trigger switch 1101 and terminal control unit
1106 using electrical connection, and the trigger switch 1101 is set to 1102 inside of steel ball loose collar and the phase by way of fixed installation
Connection, the loose collar fixed block 1103 is set to 1102 right end of steel ball loose collar and is connected by welding, described
Balance steel ball 1104 is set to 1102 inside of steel ball loose collar and is connected by movable mode, the terminal control unit 1106
It is connected set on 1105 inside of crust of the device and by way of fixed installation, the connecting cable 1107 and terminal control unit
1106 are used with fixed limiting mechanism 12 and are electrically connected using electrical connection, the connecting cable 1107, the fixed limiting mechanism 12
Including fixed limiting mechanism shell 1201, strong electromagnet 1202, spring card slot 1203, sliding groove 1204, linking spring 1205,
It is connected movable plate 1206, the strong electromagnet 1202 is set to fixed 1201 inside of limiting mechanism shell and passes through fixed installation
Mode be connected, the spring card slot 1203 is set to linking and 1206 right end of movable plate and is integrated, the linking
Movable plate 1206 is set to 1204 upper end of sliding groove and is connected by way of sliding, and the sliding groove 1204 is set to fixed limit
It inside mechanism shell 1201 processed and is integrated, the linking spring 1205 is set to 1203 right end of spring card slot and leads to
The mode for crossing transmission cooperation is connected, and the linking spring 1205 is set to fixed 1201 inside of limiting mechanism shell and passes through weldering
The mode connect is connected, and the fixed installation sector 13 includes insertion fixed block 1301, block 1302, limitation kelly is fixedly mounted
1303, shifting chute 1304, the insertion fixed block 1301, which is set to, to be fixedly mounted 1302 lower end of block and is integrated, described
Limitation kelly 1303 is set to insertion 1301 left end of fixed block and is connected by way of insertion installation, the limitation kelly
1303 are set to the inside of shifting chute 1304 and are connected by way of sliding, and the safety mechanism 14 that comes includes chute pack
Positioning ring 1401, mechanical spring 1402, chute pack 1403, effect push plate 1404, linking rope 1405, rope locating piece
1406, rope storage tray 1407, centralized positioning axis 1408, the chute pack positioning ring 1401 are located at same with chute pack 1403
One axle center and use transition fit, the mechanical spring 1402 be set to effect 1404 upper end of push plate and by transmission cooperation
Mode is connected, and the effect push plate 1404 is set to 1403 lower end of chute pack and is connected by way of fitting, described
Linking rope 1405 is connected through 1406 center of rope locating piece and by movable mode, the rope locating piece
1406 are set to 1407 upper end of rope storage tray and are connected by welding, and the rope storage tray 1407 and center are fixed
Position axis 1408 is located at same axle center and is connected by way of rotation, and the GPS positioning mechanism 15 includes SIM card fixing groove
1501, SIM card 1502, fixed pasting board 1503, the SIM card 1502 are set to 1501 inside of SIM card fixing groove and pass through insertion
The mode of installation is connected, and the fixed pasting board 1503 is set to 1502 front end face of SIM card and is connected by way of fitting,
The lifting trigger mechanism 16 includes lifting trigger mechanism shell 1601, spring limiting groove 1602, extension spring 1603, hits and open
Dynamic switch 1604 hits trigger ball 1605, hits shutdown switch 1606, and the spring limiting groove 1602 is set to lifting trigger mechanism
It inside shell 1601 and is integrated, the spring limiting groove 1602 is set to 1603 left end of extension spring and passes through biography
The mode of dynamic cooperation is connected, and the extension spring 1603, which is set to, hits 1605 left end of trigger ball and by welding phase
Connection, the shock start switch 1604 and are set to lifting 1601 inner wall of trigger mechanism shell and the phase by way of fixed installation
Connection, the shock, which starts switch 1604 and is located at, hits immediately below shutdown switch 1606, the shocks shutdown switch 1606 with surpass
Using electrical connection, the supersonic wave bird driving mechanism 17 includes supersonic generator fixed plate 1701, ultrasound for sound wave bird repellent mechanism 17
Wave producer 1702, the supersonic generator fixed plate 1701 are set to 1702 left end of supersonic generator and by fixed peaces
The mode of dress is connected.
A kind of monitoring based on thermal image analysis of the invention and alarm unmanned plane is driven, its working principle is that: when nobody
Machine is by force majeure and when breaking down, and unmanned plane disequilibrium is inverted, the balance steel ball in steel ball loose collar 1102
1104 are rolled, and are in contact during scrolling with trigger switch 1101, so that terminal control unit 1106 induces current into
Strong electromagnet 1202, strong electromagnet 1202 generates adsorption capacity to the linking movable plate 1206 of metal material, so that linking moves
Movable plate 1206 is mobile to drive limitation kelly 1303 to release the limitation to insertion fixed block 1301,2 moment of thermal image analysis camera
It is detached from unmanned plane body 7, during disengaging, limitation of the releasing of block 1302 to chute pack 1403 is fixedly mounted, compresses shape
The mechanical spring 1402 of state releases elastic force limitation, is sprung back, and induced effect push plate 1404 is by 1403 device for ejecting of chute pack
Outside shell 1105, the small-sized parachute in chute pack 1403 is opened, so that thermal image analysis camera 2 gently lands in ground
Face, staff can carry out recycling thermal image analysis camera 2 by the positioning to SIM card 1502, when unmanned plane body 7 takes off
When, it hits trigger ball 1605 and is generated by moment overweight, moved down, start switch 1604 with shock and be in contact, so that
Supersonic generator 1702 is started to work, and is expelled to aerial birds, when unmanned plane body 7 lands, hits trigger ball
1605 weightlessness by moment generation is moved up, and is in contact with shutdown switch 1606 is hit, supersonic generator 1702 stops
Only work.
Problems solved by the invention is during the unmanned plane of the prior art works in the sky, when by force majeure
When interference, unmanned plane breaks down, since unmanned plane during flying is higher from the ground, when falling, and the thermal imaging installed on unmanned plane
Analysis camera can generate damage, cause the data in thermal image analysis camera to be lost, impact to monitoring work,
Meanwhile unmanned plane is before take-off, needs to manually start scarecrow device, is easy to forget to start because of carelessness, and unmanned plane is caused to fly
It during row, is hit with birds, the present invention is combined with each other by above-mentioned component, is equipped with when unmanned plane is in flight course
When breaking down, the equipment for having data automatically disengage and the structure of safe falling, helps to prevent data in equipment from sending out
It is raw to lose, monitoring work is impacted, meanwhile, equipped with the bird repellent structure started automatically by gravity, effectively prevent because dredging
Sometimes forget to start, cause unmanned plane in flight course, hit with birds.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (8)
1. a kind of monitoring based on thermal image analysis and driving alarm unmanned plane, structure includes that urgent protection thermal image analysis is set
Standby fixed device (1), thermal image analysis camera (2), fixed foot prop (3), unmanned plane motor (4), rotation blade (5), nobody
Machine wing (6), unmanned plane body (7), comprehensive adjuster (8), it is characterised in that:
The urgent protection thermal image analysis fixing device (1) is set to thermal image analysis camera (2) upper end and passes through
The mode of fixed installation is connected, and the fixed foot prop (3) is set to unmanned plane body (7) lower end and passes through movable mode phase
Connection, the unmanned plane motor (4) are set to rotation and blade (5) lower end and are connected by way of rotation, it is described nobody
Machine motor (4) is set to unmanned plane wing (6) upper end and is connected by way of insertion installation, the unmanned plane wing (6)
It is connected set on unmanned plane body (7) left end and by welding, the unmanned plane body (7) is set to comprehensive adjusting
Device (8) upper end and it is connected by way of fixed installation, the comprehensive adjuster (8) is set to urgent protection thermal imaging point
Desorption device fixes device (1) upper end and is connected by way of nested；
The urgent protection thermal image analysis fixing device (1) includes balance trigger mechanism (11), fixed limiting mechanism
(12), fixed installation sector (13), the safe mechanism (14) that comes, GPS positioning mechanism (15), lifting trigger mechanism (16), ultrasound
Wave bird repellent mechanism (17), with fixed limiting mechanism (12) using being electrically connected, the fixation limits the balance trigger mechanism (11)
Mechanism (12) is set to fixed installation sector (13) lower end and is connected by way of insertion installation, and the safety comes mechanism
(14) it is set to fixed installation sector (13) lower end and is connected by way of transmission cooperation, the GPS positioning mechanism (15)
Below lifting trigger mechanism (16), the lifting trigger mechanism (16) uses with supersonic wave bird driving mechanism (17) and is electrically connected.
2. a kind of monitoring based on thermal image analysis according to claim 1 and driving alarm unmanned plane, it is characterised in that:
The balance trigger mechanism (11) includes trigger switch (1101), steel ball loose collar (1102), loose collar fixed block (1103), puts down
Weighing apparatus steel ball (1104), crust of the device (1105), terminal control unit (1106), connecting cable (1107), the trigger switch
(1101) with terminal control unit (1106) using being electrically connected, it is internal that the trigger switch (1101) is set to steel ball loose collar (1102)
And it is connected by way of fixed installation, the loose collar fixed block (1103) is set to steel ball loose collar (1102) right end simultaneously
And be connected by welding, the balance steel ball (1104) is set to steel ball loose collar (1102) inside and passes through activity
Mode be connected, it is internal and by way of fixed installation that the terminal control unit (1106) is set to crust of the device (1105)
Be connected, the connecting cable (1107) and terminal control unit (1106) using be electrically connected, the connecting cable (1107) with consolidate
Definite limitation mechanism (12) is using electrical connection.
3. a kind of monitoring based on thermal image analysis according to claim 1 or 2 and driving alarm unmanned plane, feature exists
In: the fixed limiting mechanism (12) includes fixed limiting mechanism shell (1201), strong electromagnet (1202), spring card slot
(1203), sliding groove (1204), linking spring (1205), linking movable plate (1206), the strong electromagnet (1202) are set to
Fixed limiting mechanism shell (1201) are internal and are connected by way of fixed installation, and the spring card slot (1203) is set to
It is connected movable plate (1206) right end and is integrated, the linking movable plate (1206) is set to sliding groove (1204) upper end
And it is connected by way of sliding, the sliding groove (1204) is set to fixed limiting mechanism shell (1201) inside and is
Integral structure, the linking spring (1205) are set to spring card slot (1203) right end and are connected by way of transmission cooperation
It connects, the linking spring (1205) is set to fixed limiting mechanism shell (1201) inside and is connected by welding.
4. a kind of monitoring based on thermal image analysis according to claim 1 and driving alarm unmanned plane, it is characterised in that:
The fixed installation sector (13) includes insertion fixed block (1301), block (1302), limitation kelly (1303), movement is fixedly mounted
Slot (1304), the insertion fixed block (1301), which is set to, to be fixedly mounted block (1302) lower end and is integrated, the limit
Fabrication bar (1303) is set to insertion fixed block (1301) left end and is connected by way of insertion installation, the limitation kelly
(1303) it is set to shifting chute (1304) inside and is connected by way of sliding.
5. a kind of monitoring based on thermal image analysis according to claim 1 and driving alarm unmanned plane, it is characterised in that:
The safety come mechanism (14) include chute pack positioning ring (1401), mechanical spring (1402), chute pack (1403), make
With push plate (1404), linking rope (1405), rope locating piece (1406), rope storage tray (1407), centralized positioning axis
(1408), the chute pack positioning ring (1401) and chute pack (1403) are located at same axle center and use transition fit,
The mechanical spring (1402) is set to effect push plate (1404) upper end and is connected by way of transmission cooperation, the effect
Push plate (1404) is set to chute pack (1403) lower end and is connected by way of fitting, and the linking rope (1405) is passed through
It is through at rope locating piece (1406) center and is connected by movable mode, the rope locating piece (1406) is set to rope
Storage tray (1407) upper end and it is connected by welding, the rope storage tray (1407) and centralized positioning axis
(1408) it is located at same axle center and is connected by way of rotation.
6. a kind of monitoring based on thermal image analysis according to claim 1 and driving alarm unmanned plane, it is characterised in that:
The GPS positioning mechanism (15) includes SIM card fixing groove (1501), SIM card (1502), fixed pasting board (1503), the SIM card
(1502) it is set to SIM card fixing groove (1501) inside and is connected by way of insertion installation, the fixed pasting board
(1503) it is set to SIM card (1502) front end face and is connected by way of fitting.
7. a kind of monitoring based on thermal image analysis according to claim 1 and driving alarm unmanned plane, it is characterised in that:
The lifting trigger mechanism (16) includes lifting trigger mechanism shell (1601), spring limiting groove (1602), extension spring
(1603), it hits and starts switch (1604), hit trigger ball (1605), hit shutdown switch (1606), the spring limiting groove
(1602) it is set to lifting trigger mechanism shell (1601) inside and is integrated, the spring limiting groove (1602) is set to
Extension spring (1603) left end and transmission cooperation by way of be connected, the extension spring (1603) be set to hit triggering
Ball (1605) left end and it is connected by welding, the shock starts switch (1604) and is set to outside lifting trigger mechanism
Shell (1601) inner wall and it is connected by way of fixed installation, the shock, which starts switch (1604) and is located to hit, to stop opening
It closes immediately below (1606), the shock shutdown switch (1606) uses with supersonic wave bird driving mechanism (17) and is electrically connected.
8. a kind of monitoring based on thermal image analysis according to claim 1 or claim 7 and driving alarm unmanned plane, feature exists
In: the supersonic wave bird driving mechanism (17) include supersonic generator fixed plate (1701), supersonic generator (1702), it is described
Supersonic generator fixed plate (1701) is set to supersonic generator (1702) left end and is connected by way of fixed installation
It connects.
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| CN201910254599.4A CN109911208A (en) | 2019-03-31 | 2019-03-31 | A kind of monitoring based on thermal image analysis and drive alarm unmanned plane |
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| CN201910254599.4A CN109911208A (en) | 2019-03-31 | 2019-03-31 | A kind of monitoring based on thermal image analysis and drive alarm unmanned plane |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702998A (en) * | 2019-11-09 | 2020-01-17 | 重庆市辐射技术服务中心有限公司 | Electromagnetic radiation monitoring system based on mobile terminal and monitoring method thereof |
| CN112373699A (en) * | 2020-10-22 | 2021-02-19 | 刘占波 | Unmanned aerial vehicle anti-falling device |
| CN112799394A (en) * | 2020-12-15 | 2021-05-14 | 广州极飞科技股份有限公司 | Unmanned operation equipment control method, device, equipment and storage medium |
| CN113816232A (en) * | 2021-09-30 | 2021-12-21 | 本溪市特种设备监督检验所 | Monitoring device for special equipment inspection and use method thereof |
-
2019
- 2019-03-31 CN CN201910254599.4A patent/CN109911208A/en not_active Withdrawn
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110702998A (en) * | 2019-11-09 | 2020-01-17 | 重庆市辐射技术服务中心有限公司 | Electromagnetic radiation monitoring system based on mobile terminal and monitoring method thereof |
| CN112373699A (en) * | 2020-10-22 | 2021-02-19 | 刘占波 | Unmanned aerial vehicle anti-falling device |
| CN112373699B (en) * | 2020-10-22 | 2022-12-30 | 刘占波 | Unmanned aerial vehicle anti-falling device |
| CN112799394A (en) * | 2020-12-15 | 2021-05-14 | 广州极飞科技股份有限公司 | Unmanned operation equipment control method, device, equipment and storage medium |
| CN112799394B (en) * | 2020-12-15 | 2022-09-13 | 广州极飞科技股份有限公司 | Unmanned operation equipment control method, device, equipment and storage medium |
| CN113816232A (en) * | 2021-09-30 | 2021-12-21 | 本溪市特种设备监督检验所 | Monitoring device for special equipment inspection and use method thereof |
| CN113816232B (en) * | 2021-09-30 | 2023-02-21 | 本溪市特种设备监督检验所 | Monitoring device for special equipment inspection and use method thereof |
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Application publication date: 20190621 |