CN107856858A - A kind of unmanned plane for being used to search and rescue based on ultrasonic listening - Google Patents
A kind of unmanned plane for being used to search and rescue based on ultrasonic listening Download PDFInfo
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- CN107856858A CN107856858A CN201711096782.3A CN201711096782A CN107856858A CN 107856858 A CN107856858 A CN 107856858A CN 201711096782 A CN201711096782 A CN 201711096782A CN 107856858 A CN107856858 A CN 107856858A
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- 238000012806 monitoring device Methods 0.000 claims abstract description 29
- 230000001681 protective effect Effects 0.000 claims abstract description 9
- 238000009434 installation Methods 0.000 claims description 65
- 238000006243 chemical reaction Methods 0.000 claims description 26
- 230000000737 periodic effect Effects 0.000 claims description 10
- 238000012544 monitoring process Methods 0.000 abstract description 23
- 238000013461 design Methods 0.000 abstract description 8
- 239000011435 rock Substances 0.000 abstract description 6
- 238000010276 construction Methods 0.000 abstract description 5
- 230000009286 beneficial effect Effects 0.000 abstract description 4
- 208000032825 Ring chromosome 2 syndrome Diseases 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 238000006424 Flood reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000005236 sound signal Effects 0.000 description 1
- 238000002604 ultrasonography Methods 0.000 description 1
Classifications
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- 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
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/18—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast
- H04N7/183—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source
- H04N7/185—Closed-circuit television [CCTV] systems, i.e. systems in which the video signal is not broadcast for receiving images from a single remote source from a mobile camera, e.g. for remote control
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- 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)
- Multimedia (AREA)
- Signal Processing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses a kind of unmanned plane for being used to search and rescue based on ultrasonic listening, its structure includes wing, rotation ring, fuselage, protective plate, folder thing device, high-definition monitoring device, wing is v-shaped structure, folder thing device, high-definition monitoring device are separately mounted to fuselage and wing bottom, wing and fuselage composition ARROW structure, folder thing device is located at the stitching portion of wing and fuselage, and high-definition monitoring device is located at the middle part of wing.Present invention good appearance cost simple in construction is low, and stability of the unmanned plane in flight is added using three rotation rings and V-arrangement wing design；Press from both sides thing device to design using double fastener, after being gripped, side plate carries out secondary gripping and reinforced again, and fastness is strong, more stablizes and is not easy to drop and rocks；High-definition monitoring device can carry out 360 rotations and monitoring, monitoring image refresh repeatedly in real time, beneficial to monitoring and arranges.
Description
Technical field
The present invention is a kind of unmanned plane for being used to search and rescue based on ultrasonic listening, belongs to unmanned plane field.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel are tracked to it, positioned, being remotely controlled, remote measurement and Digital Transmission by equipment such as radars.Can be in radio
Take off as conventional airplane or launched with booster rocket under remote control, can also take aerial launch to by machine tool and fly.Recovery
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be reclaimed by remote control parachute or block.Can
It is reused several times.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..It is that unmanned plane is earliest to investigate monitoring
One of purposes, scounting aeroplane can go deep into one or two hundred kilometers of position forward position and enemy's rear area, or even farther distance, and it is by dress
The equipment such as visible light camera, film camera, standard or low-light level television camera, infrared scanner and radar on machine,
Various scouting and monitoring tasks are completed, in general, a frame unmanned plane can carry one or more of reconnaissance equipments, by predetermined journey
Sequence or surface instruction are operated, and the information obtained and image are finally sent back into ground at any time, are used for relevant department；
All information records of acquisition can be got off, once be taken when unmanned plane reclaims.With the development and application of new and high technology,
Equipment performance on unmanned plane is also improving constantly, while also add some new equipments, and application further expands.Such as
After equipping global positioning system, unmanned plane can be used cooperatively with reconnaissance satellite and manned reconnaissance plane, form high, medium and low sky,
At many levels, multi-faceted three-dimensional aerial reconnaissance monitoring net, makes obtained information more accurately and reliably.
Prior art discloses Application No.：201720126416.7 become more meticulous inspection for power network conveying circuit shaft tower
Unmanned plane, including carrier aircraft platform and navigation camera lens, connecting plate is installed on carrier aircraft platform, electric rotating machine is fixed on connection
On plate, the activity of pole upper end is connected after running through connecting plate with the output end of electric rotating machine, is provided with camera in pole stage casing, is being propped up
The be hinged supporter for being provided with prism, annular being provided with pole outer wall in bar hypomere end, shock bracket are provided with spacing ring,
The groove to match with supporter is provided with spacing ring inner peripheral wall.Inventor is by the use of unmanned plane as carrier, by flying hand
Precise manipulation, while the mode coordinated using prism with camera lens, are carried out shooting record to shaft tower point position respectively, solved existing
The point position of shaft tower can only use the defects of telephoto lens shooting in unmanned plane power network routine inspection mode, and reduce shooting time point position
Limitation, to ensure the stability in use of grid power transmission circuit.But prior art construction complexity cost is high and profile unsightly,
Using twin designs, stability is poor during flight；Grip article when, article easily slides, and fastness is poor, it is unstable and easily drop and
Rock, easily cause loss and security is low；Monitor can not carry out 360 rotations, and monitoring image can not repeatedly refresh, be unfavorable for
Monitoring and arrangement.
The content of the invention
In view of the deficienciess of the prior art, it is used for what is searched and rescued based on ultrasonic listening it is an object of the present invention to provide a kind of
Unmanned plane, with solve that complicated cost is high and profile unsightly, using twin designs, stability is poor during flight；Grip article
When, article easily slides, and fastness is poor, unstable and easily drop and rock, and easily causes loss and security is low；Monitor without
Method carries out 360 rotations, and monitoring image can not refresh repeatedly, the problem of being unfavorable for monitoring and arrange.
To achieve these goals, the present invention is to realize by the following technical solutions：One kind is based on ultrasonic listening
The unmanned plane for being used to search and rescue, its structure includes wing, rotation ring, fuselage, protective plate, folder thing device, high-definition monitoring device, the machine
The wing is v-shaped structure, and the folder thing device, high-definition monitoring device are separately mounted to fuselage and wing bottom, the wing and fuselage group
Into ARROW structure, the folder thing device is located at the stitching portion of wing and fuselage, and the high-definition monitoring device is located at the middle part of wing, institute
State folder thing device and be in same axis with high-definition monitoring device, the protective plate is engaged in body upper, and described is circular configuration
Rotation, which is equipped with, separately constitutes triangular structure, described to set round-meshed front fuselage embedded with rotation ring, described to set round-meshed machine
For wing afterbody embedded with a pair of rotation rings, the rotation ring includes a rotation ring, two rotation rings, three rotation rings, the rotation ring, two rotations
Ring, three rotation ring structures are identical, and the rotation ring, two rotation rings, three rotation ring groups are described to press from both sides thing device into triangular structure
It is made up of installation jam plate, installation poppet, train wheel bridge, side clamping plate, hinge lock, jig arm, the installation jam plate is respectively H with installation poppet
Shape structure, the installation jam plate are locked with installation poppet by hinge, and the installation jam plate is located above installation poppet, and the two
Parallel, the train wheel bridge is mesh word structure, and the installation poppet is welded in above train wheel bridge, the installation poppet and train wheel bridge group
Into cross structure, the train wheel bridge is with side clamping plate by cutting with scissors lock locking, the train wheel bridge and side clamping plate composition inverted U-shaped, institute
State jig arm and be fixedly connected on train wheel bridge bottom, the hinge lock is made up of convergence hole, portable plate, locking bolt, hinge ring, fixed column, described
Hinge ring is welded to each other with fixed column, and the portable plate is flexibly connected with hinge ring by locking bolt, and the portable plate is located at the outer of hinge ring
Side, the portable plate are provided with convergence hole, and the convergence hole is in same level position with locking bolt, and the jig arm is by left part jig arm, branch
Bar, right part jig arm composition, the left part jig arm and right part jig arm are symmetrical, and the pole is through left part jig arm and right part jig arm, institute
State that left part jig arm is identical with right part arm clamping structure, the pole be provided with more than a jack, the left part jig arm and a right part jig arm
Plug is respectively equipped with, the jack coordinates with plug, and the high-definition monitoring device is by mounting cup, nested frame, camera, shooting eye group
Into, the mounting cup bottom is flexibly connected with nested frame upper surface, and the mounting cup is vertical with nested frame, the mounting cup with it is embedding
Stock gap coordinates, and the camera both sides are movably connected on the inside of nested frame, and the nested frame excessively coordinates with camera, institute
State camera and be provided with shooting eye, the camera is connected with conversion with shooting eye composition integral structure, the high-definition monitoring device
High definition system, the conversion high definition system are made up of periodic refreshing device, single conversion module, data processor, data link,
The periodic refreshing device electrically connects with single conversion module, and the single conversion module is connected with data processor, the data
Processor is connected with data link power information, and the installation jam plate, mounting cup are separately mounted to fuselage and wing bottom.
Further, the rotation ring includes capel, rotating vane, turncap.
Further, the turncap is provided with the rotating vane of more than 3, and the capel coordinates with rotating vane, the capel and rotation
Cap is in concentric circles, and the turncap is located at capel center.
Further, the installation jam plate includes installation jam plate body, installation jam plate lockhole, described to install in jam plate body
Installation jam plate lockhole is provided with the heart.
Further, the side clamping plate includes side clamping plate plate, side clamping plate brake pad.
Further, the side clamping plate brake pad is provided with more than 3 pieces, and the side clamping plate brake pad is welded in side clamping plate plate
Medial surface bottom.
Further, the fuselage bottom middle is provided with ultrasonic detector, and the ultrasonic detector includes solid
Determine mounting head, signal conditioner, ultrasonic detector body, ultrasonic receiver, infrared transmitter, amplifier.
Further, the fuselage is fixedly connected with ultrasonic detector body by fixed mounting head, the ultrasonic wave
Detector body is separately installed with signal conditioner, infrared transmitter, amplifier, and the signal conditioner is provided with individual and composition three
Angular structure, positioned at ultrasonic detector body prism, the infrared transmitter is adjacent with amplifier and is in same axis,
The infrared transmitter is located at ultrasonic detector body ring side with amplifier, and the ultrasonic detector body is provided with ultrasound
Ripple receiver, the ultrasonic receiver are located at ultrasonic detector body bottom portion.
Beneficial effect
A kind of unmanned plane for being used to search and rescue based on ultrasonic listening of the present invention, carrying out in use, rotation ring is rotated
Drive the flight of complete machine；When carrying out gripping article, object is fixed on left part jig arm and the right side by adjustment left part jig arm with right part jig arm
Between portion's jig arm, after the completion of cut with scissors lock strap move side clamping plate secondary clamping, high-definition monitoring device be used in real time monitor, mounting cup with it is nested
Frame coordinates the lateral rotation of drive shooting eye, while nested frame coordinates the vertical rotating for realizing camera, conversion height with camera
Clear system repeatedly refreshes monitoring image, is easy to monitor and arranges, and becomes apparent from camera image when rotating.
Present invention good appearance cost simple in construction is low, is added unmanned plane using three rotation rings and V-arrangement wing design and is existed
Stability during flight；Press from both sides thing device to design using double fastener, after being gripped, side plate carries out secondary gripping and reinforced again, fastness
By force, more stablize and be not easy to drop and rock；High-definition monitoring device can carry out 360 rotations and monitoring, monitoring image are brushed repeatedly in real time
Newly, beneficial to monitoring and arrangement.
Brief description of the drawings
The detailed description made by reading with reference to the following drawings to non-limiting example, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural representation of the unmanned plane for being used to search and rescue based on ultrasonic listening of the present invention.
Fig. 2 is the structural representation of present invention folder thing device.
Fig. 3 is the structural representation of present invention folder thing device mirror image.
Fig. 4 is the structural representation of present invention hinge lock.
Fig. 5 is the structural representation of jig arm of the present invention.
Fig. 6 is the structural representation of high-definition monitoring device of the present invention.
Fig. 7 is the structural representation of present invention conversion high definition system.
Fig. 8 is the structural representation of ultrasonic detector of the present invention
Fig. 9 is the structural representation that ultrasonic detector of the present invention rotates 45 degree.
In figure：- 6, wing -1, rotation ring -2, fuselage -3, protective plate -4, folder thing device -5, high-definition monitoring device rotation rings -
20th, two rotation rings -21, three rotation rings -22, installation jam plate -50, installation poppet -51, train wheel bridge -52, side clamping plate -53, hinge lock -
54th, jig arm -55, convergence hole -540, portable plate -541, locking bolt -542, hinge ring -543, fixed column -544, left part jig arm -550, branch
Bar -551, right part jig arm -552, mounting cup -60, nested frame -61, camera -62, shooting eye -63, periodic refreshing device -70, list
Secondary modular converter -71, data processor -72, data link -73, capel -200, rotating vane -201, turncap -202, installation jam plate
Body -500, installation jam plate lockhole -501, side clamping plate plate -530, side clamping plate brake pad -531, ultrasonic detector -8, fixation
Mounting head -80, signal conditioner -81, ultrasonic detector body -82, ultrasonic receiver -83, infrared transmitter -84, put
Big device -85, jack -5510, plug -5520, conversion high definition system -7.
Embodiment
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, the present invention is expanded on further.
Embodiment 1：
Fig. 1-Fig. 7 is referred to, the present invention provides a kind of unmanned plane for being used to search and rescue based on ultrasonic listening：Its structure bag
Include wing 1, rotation ring 2, fuselage 3, protective plate 4, folder thing device 5, high-definition monitoring device 6, the wing 1 is v-shaped structure, the folder thing
Device 5, high-definition monitoring device 6 are separately mounted to fuselage 3 and the bottom of wing 1, and the wing 1 forms ARROW structure with fuselage 3, described
Thing device 5 is pressed from both sides positioned at the stitching portion of wing 1 and fuselage 3, the high-definition monitoring device 6 is located at the middle part of wing 1, the folder thing device
5 are in same axis with high-definition monitoring device 6, and the protective plate 4 is engaged in the top of fuselage 3, described to be set for the rotation ring 2 of circular configuration
There are 3 to separately constitute triangular structure, it is described to set the round-meshed front end of fuselage 3 embedded with rotation ring 2, it is described to set round-meshed wing 1
For afterbody embedded with a pair of rotation rings 2, the rotation ring 2 includes 20, two, rotation ring, 21, three, a rotation ring rotation ring 22, the rotation ring
20th, two rotation rings, 21, three rotation structures of ring 22 are identical, and 20, two, rotation ring, 21, three, the rotation ring rotation ring 22 forms triangle
Shape structure, the folder thing device 5 is by installation jam plate 50, installation poppet 51, train wheel bridge 52, side clamping plate 53, hinge lock 54,55 groups of jig arm
Into the installation jam plate 50 is respectively H-shaped structure with installation poppet 51, and the installation jam plate 50 passes through hinge with installation poppet 51
Locking, the installation jam plate 50 is positioned at the top of installation poppet 51, and the two is parallel, and the train wheel bridge 52 is mesh word structure, described
Installation poppet 51 is welded in the top of train wheel bridge 52, and the installation poppet 51 forms cross structure, the train wheel bridge with train wheel bridge 52
52 form inverted U-shaped by cutting with scissors the locking of lock 54, the train wheel bridge 52 with side clamping plate 53 with side clamping plate 53, and the jig arm 55 is fixed
The bottom of train wheel bridge 52 is connected to, the hinge lock 54 is by convergence hole 540, portable plate 541, locking bolt 542, hinge ring 543, fixed column 544
Composition, the hinge ring 543 are welded to each other with fixed column 544, and the portable plate 541 is connected with hinge ring 543 by the activity of locking bolt 542
Connect, the portable plate 541 is located at the outside of hinge ring 543, and the portable plate 541 is provided with convergence hole 540, the convergence hole 540 with
Locking bolt 542 is in same level position, and the jig arm 55 is made up of left part jig arm 550, pole 551, right part jig arm 552, the left side
Portion's jig arm 550 is symmetrical with right part jig arm 552, and the pole 551 is through left part jig arm 550 and right part jig arm 552, the left part folder
Arm 550 is identical with the structure of right part jig arm 552, and the pole 551 is provided with the jack 5510 of more than 3, the left part jig arm 550 and
Right part jig arm 552 is respectively equipped with plug 5520, and the jack 5510 coordinates with plug 5520, and the high-definition monitoring device 6 is by installing
Cover 60, nested frame 61, camera 62, shooting eye 63 are formed, and the bottom of mounting cup 60 is flexibly connected with the nested upper surface of frame 61,
The mounting cup 60 is vertical with nested frame 61, and the mounting cup 60 coordinates with the nested gap of frame 61, and the both sides of camera 62 are lived
Dynamic to be connected to the nested inner side of frame 61, the nested frame 61 excessively coordinates with camera 62, and the camera 62 is provided with shooting eye 63,
The camera 62 forms integral structure with shooting eye 63, and the high-definition monitoring device 6 is connected with conversion high definition system 7, described
Conversion high definition system 7 is made up of periodic refreshing device 70, single conversion module 71, data processor 72, data link 73, described
Periodic refreshing device 70 electrically connects with single conversion module 71, and the single conversion module 71 is connected with data processor 72, described
Data processor 72 is connected with the power information of data link 73, installation jam plate 50, the mounting cup 60 be separately mounted to fuselage 3 with
The bottom of wing 1, the rotation ring 20 include capel 200, rotating vane 201, turncap 202, and the turncap 202 is provided with more than 3
Rotating vane 201, the capel 200 coordinates with rotating vane 201, and the capel 200 is in concentric circles, the turncap 202 with turncap 202
At the center of capel 200, the installation jam plate 50 includes installation jam plate body 500, installation jam plate lockhole 501, the installation
Installation jam plate lockhole 501 is provided with the center of jam plate body 500, the side clamping plate 53 includes side clamping plate plate 530, side clamping plate friction
Block 531, the side clamping plate brake pad 531 are provided with more than 3 pieces, and the side clamping plate brake pad 531 is welded in side clamping plate plate 530
Side bottom.
High-definition monitoring device 6 described in this patent is the exsertile monitoring software of circular hole, inputs the IP of other side and controls close
Code just can real remote monitoring, software penetrates Intranet using udp protocol, port mapping that it goes without doing, and user just can at any one
Far-end computer is all connected with the computer of online, carries out telecommuting and remote management.Monitoring system is generally used for commercial civilian
Increasingly popularization, CCTV camera is widely used in every field, escort for social security.Monitor, which refers to utilize, to be taken the photograph
The general name that video, audio signal are included and stored as storage device.
Carrying out in use, rotation ring carries out rotating the flight for driving complete machine；When carrying out gripping article, adjustment left part jig arm with
Object is fixed between left part jig arm and right part jig arm by right part jig arm, after the completion of cut with scissors the secondary clamping that lock strap moves side clamping plate, it is high
Clear monitor is used to monitor in real time, and mounting cup coordinates the lateral rotation for driving shooting eye, while nested frame and shooting with nested frame
Head coordinates the vertical rotating for realizing camera, and conversion high definition system repeatedly refreshes monitoring image, is easy to monitor and arranges, make shooting
Head image when rotating becomes apparent from.When having disaster generation, some places are rescue personnels in the very first time basic nothing
What method reached, either fire, disaster caused by a windstorm, floods or earthquake, as rescue spot using the unmanned plane very first time obtain scene or
The situation data in disaster area, understand field condition.
Embodiment 2：
Fig. 1 and Fig. 8, Fig. 9 are referred to, the bottom middle of fuselage 3 is provided with ultrasonic detector 8, the ultrasonic wave
Detector 8 includes fixed mounting head 80, signal conditioner 81, ultrasonic detector body 82, ultrasonic receiver 83, infrared hair
Emitter 84, amplifier 85, the fuselage 3 are fixedly connected with ultrasonic detector body 82 by fixed mounting head 80, described super
Acoustic detector body 82 is separately installed with signal conditioner 81, infrared transmitter 84, amplifier 85, the signal conditioner 81
Provided with 3 and triangular structure is formed, positioned at the prism of ultrasonic detector body 82, the infrared transmitter 84 and amplifier
85 is adjacent and be in same axis, and the infrared transmitter 84 is located at the ring side of ultrasonic detector body 82 with amplifier 85,
The ultrasonic detector body 82 is provided with ultrasonic receiver 83, and the ultrasonic receiver 83 is located at ultrasonic detector sheet
The bottom of body 82.
With reference to embodiment 1 and operation instruction, the fuselage 3 is solid by fixed mounting head 80 with ultrasonic detector body 82
Fixed connection, ultrasonic detector 8 carry out coordinate detection, fixed mounting head 80 are connected into installation with fuselage 3, rotation ring carries out rotational band
After the flight of dynamic complete machine, signal conditioner 81 carries out signal and receives and feed back, and ultrasonic receiver 83 receives for ultrasonic wave, red
External transmitter 84 is used for auxiliary positioning, and amplifier 85 realizes signal conditioner 81, ultrasonic receiver 83, infrared transmitter 84
Signal is strengthened.
6, wing 1 of the present invention, rotation ring 2, fuselage 3, protective plate 4, folder thing device 5, high-definition monitoring device 20, two, rings of rotation
Revolve 21, three rotation rings 22 of ring, installation jam plate 50, installation poppet 51, train wheel bridge 52, side clamping plate 53, hinge lock 54, jig arm 55, linking
Hole 540, portable plate 541, locking bolt 542, hinge ring 543, fixed column 544, left part jig arm 550, pole 551, right part jig arm 552, peace
Dress cover 60, nested frame 61, camera 62, shooting eye 63, periodic refreshing device 70, single conversion module 71, data processor 72, number
According to transmitter 73, capel 200, rotating vane 201, turncap 202, installation jam plate body 500, installation jam plate lockhole 501, side clamping plate plate
530th, side clamping plate brake pad 531, ultrasonic detector 8, fixed mounting head 80, signal conditioner 81, ultrasonic detector body
82nd, ultrasonic receiver 83, infrared transmitter 84, amplifier 85, jack 5510, plug 5520, conversion high definition system 7, part
It is universal standard part or part that those skilled in the art know, its structure and principle all can pass through skill for this technology personnel
Art handbook learns or known by normal experiment method that the present invention solves the problems, such as prior art construction complexity cost height and profile
Unsightly, using twin designs, stability is poor during flight；Grip article when, article easily slides, and fastness is poor, it is unstable and
Easily drop and rock, easily cause loss and security is low；Monitor can not carry out 360 rotations, and monitoring image can not be brushed repeatedly
Newly, it is unfavorable for monitoring and arranging, being combined with each other by above-mentioned part of the invention, good appearance cost simple in construction can be reached
It is low, add stability of the unmanned plane in flight using three rotation rings and V-arrangement wing design；Folder thing device is set using double fastener
Meter, after being gripped, side plate carries out secondary gripping and reinforced again, and fastness is strong, more stablizes and is not easy to drop and rocks；High definition is supervised
Control device can carry out 360 rotations and monitoring, monitoring image refresh repeatedly in real time, beneficial to monitoring and arranges, described in detail below:
The rotation ring 2 includes 20, two, rotation ring, 21, three, a rotation ring rotation ring 22, described 20, two rotation rings of rotation ring
21st, three rotation structures of ring 22 are identical, and 20, two, rotation ring, 21, three, the rotation ring rotation ring 22 forms triangular structure, described
Folder thing device 5 is made up of installation jam plate 50, installation poppet 51, train wheel bridge 52, side clamping plate 53, hinge lock 54, jig arm 55, the installation
Jam plate 50 is respectively H-shaped structure with installation poppet 51, and the installation jam plate 50 is locked with installation poppet 51 by hinge, the peace
Jam plate 50 is filled positioned at the top of installation poppet 51, and the two is parallel, the train wheel bridge 52 is mesh word structure, and the installation poppet 51 welds
The top of train wheel bridge 52 is connected to, the installation poppet 51 forms cross structure, the train wheel bridge 52 and side clamping plate 53 with train wheel bridge 52
By cutting with scissors the locking of lock 54, the train wheel bridge 52 forms inverted U-shaped with side clamping plate 53, and the jig arm 55 is fixedly connected on train wheel bridge
52 bottoms, the hinge lock 54 are made up of convergence hole 540, portable plate 541, locking bolt 542, hinge ring 543, fixed column 544, the hinge ring
543 are welded to each other with fixed column 544, and the portable plate 541 is flexibly connected with hinge ring 543 by locking bolt 542, the portable plate
541 are located at the outside of hinge ring 543, and the portable plate 541 is provided with convergence hole 540, and the convergence hole 540 is in same with locking bolt 542
One horizontal position, the jig arm 55 are made up of left part jig arm 550, pole 551, right part jig arm 552, the left part jig arm 550 and the right side
Portion's jig arm 552 is symmetrical, and the pole 551 is pressed from both sides through left part jig arm 550 and right part jig arm 552, the left part jig arm 550 with right part
The structure of arm 552 is identical, and the pole 551 is provided with the jack 5510 of more than 3, and the left part jig arm 550 is divided with right part jig arm 552
Not She You plug 5520, the jack 5510 coordinates with plug 5520, the high-definition monitoring device 6 by mounting cup 60, nested frame 61,
Camera 62, shooting eye 63 form, the bottom of mounting cup 60 is flexibly connected with the nested upper surface of frame 61, the mounting cup 60 and
Nested frame 61 is vertical, and the mounting cup 60 coordinates with the nested gap of frame 61, and the both sides of camera 62 are movably connected on nested frame
61 inner sides, the nested frame 61 excessively coordinates with camera 62, and the camera 62 is provided with shooting eye 63, the camera 62 and
Image eye 63 and form integral structure, the high-definition monitoring device 6 is connected with conversion high definition system 7, the conversion high definition system 7 by
Periodic refreshing device 70, single conversion module 71, data processor 72, data link 73 form, the periodic refreshing device 70 with
Single conversion module 71 electrically connects, and the single conversion module 71 is connected with data processor 72, the data processor 72 with
The power information of data link 73 connects, and the installation jam plate 50, mounting cup 60 are separately mounted to fuselage 3 and the bottom of wing 1.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above, for this area skill
For art personnel, it is clear that the invention is not restricted to the details of above-mentioned one exemplary embodiment, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Which point therefore, no matter from the point of view of, all should incite somebody to action
Embodiment regards exemplary as, and be it is nonrestrictive, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that all changes fallen in the implication and scope of the equivalency of claim are included in the present invention
It is interior.Any reference in claim should not be considered as to the involved claim of limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (6)
1. it is a kind of based on ultrasonic listening be used for search and rescue unmanned plane, its structure include wing (1), rotation ring (2), fuselage (3),
Protective plate (4), folder thing device (5), high-definition monitoring device (6), the wing (1) is v-shaped structure, the folder thing device (5), high definition
Monitor (6) is separately mounted to fuselage (3) and wing (1) bottom, the wing (1) and fuselage (3) composition ARROW structure, described
Folder thing device (5) is located at the stitching portion of wing (1) and fuselage (3), and the high-definition monitoring device (6) is located at the middle part of wing (1), institute
State folder thing device (5) and be in same axis with high-definition monitoring device (6), the protective plate (4) is engaged in above fuselage (3), described
Triangular structure is separately constituted provided with 3 for the rotation ring (2) of circular configuration, described round-meshed fuselage (3) front end that sets is embedded with rotation
Ring (2), described round-meshed wing (1) afterbody that sets is embedded with a pair of rotation rings (2), it is characterised in that：
The rotation ring (2) includes a rotation ring (20), two rotation rings (21), three rotation rings (22), rotation ring (20), two
Position rotation ring (21), three rotation ring (22) structures are identical, a rotation ring (20), two rotation rings (21), three rotation ring (22) groups
Into triangular structure；
The folder thing device (5) is locked by installation jam plate (50), installation poppet (51), train wheel bridge (52), side clamping plate (53), hinge
(54), jig arm (55) forms, and the installation jam plate (50) and installation poppet (51) are respectively H-shaped structure, the installation jam plate
(50) locked with installation poppet (51) by hinge, the installation jam plate (50) is above installation poppet (51), and the two is flat
OK, the train wheel bridge (52) is mesh word structure, and the installation poppet (51) is welded in above train wheel bridge (52), the installation poppet
(51) with train wheel bridge (52) composition cross structure, the train wheel bridge (52) is locked with side clamping plate (53) by cutting with scissors lock (54), described
Train wheel bridge (52) and side clamping plate (53) composition inverted U-shaped, the jig arm (55) is fixedly connected on train wheel bridge (52) bottom, described
Hinge lock (54) is made up of convergence hole (540), portable plate (541), locking bolt (542), hinge ring (543), fixed column (544), the hinge
Ring (543) is welded to each other with fixed column (544), and the portable plate (541) is flexibly connected with hinge ring (543) by locking bolt (542),
The portable plate (541) is located at the outside of hinge ring (543), and the portable plate (541) is provided with convergence hole (540), the convergence hole
(540) same level position is in locking bolt (542), the jig arm (55) is by left part jig arm (550), pole (551), right part jig arm
(552) form, with right part jig arm (552) symmetrically, the pole (551) runs through left part jig arm (550) to the left part jig arm (550)
With right part jig arm (552), the left part jig arm (550) is identical with right part jig arm (552) structure, and the pole (551) is provided with 3
Jack (5510) above, the left part jig arm (550) are respectively equipped with plug (5520), the jack with right part jig arm (552)
(5510) coordinate with plug (5520)；
The high-definition monitoring device (6) is made up of mounting cup (60), nested frame (61), camera (62), shooting eye (63), the peace
Dress cover (60) bottom is flexibly connected with nested frame (61) upper surface, and the mounting cup (60) is vertical with nested frame (61), the peace
Dress cover (60) coordinates with nested frame (61) gap, and camera (62) both sides are movably connected on the inside of nested frame (61), described
Nested frame (61) and camera (62) excessively coordinate, and the camera (62) is provided with shooting eye (63), the camera (62) with
Eye (63) composition integral structure is imaged, the high-definition monitoring device (6) is connected with conversion high definition system (7), the conversion high definition
System (7) is made up of periodic refreshing device (70), single conversion module (71), data processor (72), data link (73), institute
State periodic refreshing device (70) to electrically connect with single conversion module (71), the single conversion module (71) is connected with data processor
(72), the data processor (72) is connected with data link (73) power information, the installation jam plate (50), mounting cup (60)
It is separately mounted to fuselage (3) and wing (1) bottom.
A kind of 2. unmanned plane for being used to search and rescue based on ultrasonic listening according to claim 1, it is characterised in that：It is described
One rotation ring (20) includes capel (200), rotating vane (201), turncap (202).
A kind of 3. unmanned plane for being used to search and rescue based on ultrasonic listening according to claim 2, it is characterised in that：It is described
Turncap (202) is provided with the rotating vane (201) of more than 3, and the capel (200) coordinates with rotating vane (201), the capel (200)
Concentric circles is in turncap (202), the turncap (202) is located at capel (200) center.
A kind of 4. unmanned plane for being used to search and rescue based on ultrasonic listening according to claim 1, it is characterised in that：It is described
Installing jam plate (50) includes installation jam plate body (500), installation jam plate lockhole (501), described installation jam plate body (500) center
Place is provided with installation jam plate lockhole (501).
A kind of 5. unmanned plane for being used to search and rescue based on ultrasonic listening according to claim 1, it is characterised in that：It is described
Side clamping plate (53) includes side clamping plate plate (530), side clamping plate brake pad (531).
A kind of 6. unmanned plane for being used to search and rescue based on ultrasonic listening according to claim 5, it is characterised in that：It is described
Side clamping plate brake pad (531) is provided with more than 3 pieces, and the side clamping plate brake pad (531) is welded in side clamping plate plate (530) medial surface
Bottom.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711096782.3A CN107856858B (en) | 2017-11-09 | 2017-11-09 | Unmanned aerial vehicle for search and rescue based on ultrasonic detection |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711096782.3A CN107856858B (en) | 2017-11-09 | 2017-11-09 | Unmanned aerial vehicle for search and rescue based on ultrasonic detection |
Publications (2)
| Publication Number | Publication Date |
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| CN107856858A true CN107856858A (en) | 2018-03-30 |
| CN107856858B CN107856858B (en) | 2021-07-27 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202011472U (en) * | 2011-02-28 | 2011-10-19 | 南昌航空大学 | Tilting duct unmanned aerial vehicle |
| CN105163064A (en) * | 2015-07-23 | 2015-12-16 | 安徽师范大学 | Embedded network video data acquisition transmission system and method |
| CN105799935A (en) * | 2016-04-18 | 2016-07-27 | 南京航空航天大学 | Flight carrier system of unmanned aerial vehicle |
| US20160286135A1 (en) * | 2015-03-26 | 2016-09-29 | Eslam Abbas Baseuny | Surveillance and Tracking Device |
| CN106864766A (en) * | 2017-03-16 | 2017-06-20 | 山东大学 | It is applied to unmanned plane independently the battery clamp device of continuation of the journey and replacing device and method |
-
2017
- 2017-11-09 CN CN201711096782.3A patent/CN107856858B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202011472U (en) * | 2011-02-28 | 2011-10-19 | 南昌航空大学 | Tilting duct unmanned aerial vehicle |
| US20160286135A1 (en) * | 2015-03-26 | 2016-09-29 | Eslam Abbas Baseuny | Surveillance and Tracking Device |
| CN105163064A (en) * | 2015-07-23 | 2015-12-16 | 安徽师范大学 | Embedded network video data acquisition transmission system and method |
| CN105799935A (en) * | 2016-04-18 | 2016-07-27 | 南京航空航天大学 | Flight carrier system of unmanned aerial vehicle |
| CN106864766A (en) * | 2017-03-16 | 2017-06-20 | 山东大学 | It is applied to unmanned plane independently the battery clamp device of continuation of the journey and replacing device and method |
Non-Patent Citations (1)
| Title |
|---|
| 喻建华等: "《建筑弱电应用技术》", 31 August 2009 * |
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| CN107856858B (en) | 2021-07-27 |
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