CN208325667U - A kind of multifunction anti-collision is tethered at unmanned plane - Google Patents
A kind of multifunction anti-collision is tethered at unmanned plane Download PDFInfo
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- CN208325667U CN208325667U CN201820699017.4U CN201820699017U CN208325667U CN 208325667 U CN208325667 U CN 208325667U CN 201820699017 U CN201820699017 U CN 201820699017U CN 208325667 U CN208325667 U CN 208325667U
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- unmanned plane
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Abstract
The utility model provides a kind of multifunction anti-collision and is tethered at unmanned plane, including body, Anti-bumping protection, control system, multifunctional platform, undercarriage, Ground Support case, earth station, optoelectrical cable；Anti-bumping protection, control system are incorporated in multifunctional platform；Multifunctional platform is installed on body middle and lower part position, frame is fallen to be located at below body and coupled, Ground Support case is connected with the optoelectrical cable other end, it includes power supply unit, automatic deploying and retracting line capstan winch, ground fixing device, independent to insure power supply, the automatic deploying and retracting line capstan winch is used for the folding and unfolding of optoelectrical cable；The earth station includes ground platform and signal receiving and transmitting system, and the signal receiving and transmitting system and data receiving-transmitting system, image transmission/reception system carry out the interaction process of signal.The apparatus structure is simplified, vdiverse in function, quickly carry sand-blasting machine, spraying equipment, searchlight, high-pitched speaker, high-definition camera etc. can realize a tractor serves several purposes.
Description
Technical field
The utility model relates to unmanned plane applied technical fields, and in particular to a kind of multifunction anti-collision is tethered at unmanned plane.
Background technique
Being tethered at unmanned plane is by unmanned plane and to be tethered at the UAV system that comprehensive cable knot realizes altogether, is tethered at unmanned plane
Electric energy is transmitted by photoelectric comprehensive hawser, so that unmanned plane is not limited by electric energy and is stopped in the sky for a long time, gets rid of biography
System unmanned plane receives the predicament of energy limitation greatly, thus can be applicable in the various civilian long-time high altitude operation of various industries such as military
In dangerous scene, play a multiplier effect.
Summary of the invention
The utility model is intended to provide a kind of multifunction anti-collision and is tethered at unmanned plane, can overcome the above problem, provides structure essence
Letter, it is vdiverse in function, it can be achieved that a tractor serves several purposes unmanned plane.
The technical solution of the utility model is as follows:
A kind of multifunction anti-collision is tethered at unmanned plane, including body, multifunctional platform, undercarriage, Ground Support case, ground
It stands, optoelectrical cable；
The multifunctional platform is installed on the middle and lower part position of body, including Anti-bumping protection, control system, Navigation of Pilotless Aircraft fly
Control system, electrical system, photoelectric comprehensive cable connector box, data receiving-transmitting system, image transmission/reception system；
The photoelectric comprehensive cable connector box with respectively with Anti-bumping protection, control system, Navigation of Pilotless Aircraft flight control system, number
It is electrically connected according to receive-transmit system, image transmission/reception system；The photoelectric comprehensive cable connector box passes through optoelectrical cable and Ground Support
Case connection；The Ground Support case is electrically connected with earth station；
The image transmission/reception system is electrically connected with camera, is received the image of camera and is transmitted by optoelectrical cable
To earth station；
The data receiving-transmitting system is electrically connected with body, Navigation of Pilotless Aircraft flight control system respectively, receives Navigation of Pilotless Aircraft
Flight control system information, and body information is transmitted to earth station, and satellite receiver controls information, it is transmitted to Navigation of Pilotless Aircraft and flies control
The flight of system control machine body；
The Anti-bumping protection, control system are set to multifunctional platform front end, for detecting barrier and alarming；
The electrical system is electrically connected by photoelectric comprehensive cable connector box, optoelectrical cable with Ground Support case, is obtained
Electric energy, at the same electrical system respectively with Anti-bumping protection, control system, Navigation of Pilotless Aircraft flight control system, data receiving-transmitting system, image
Receive-transmit system electrical connection, to these module for power supply.
The camera is installed on multifunctional platform front by tilt-top
The Anti-bumping protection, control system include sensor, control device；The sensor is electrically connected with control device
Connect, the control device respectively with Navigation of Pilotless Aircraft flight control system, alarm system and earth station, when sensor detect front
When having barrier in set distance, for transmission signal to control device, control device transmission halts signal to Navigation of Pilotless Aircraft
Flight control system, Navigation of Pilotless Aircraft flight control system controls body hovering, while control device also transmits obstacle signal to earth station.
The earth station is equipped with warning device and sounds an alarm when receiving obstacle signal.
The sensor is 4, is divided into the four direction positioned at multifunctional platform bottom.
The undercarriage is set to the lower section of body, including platform support, carrier, carrier locking bolt, connector, pitching dress
It sets, fixing clamp；The platform support is connect with underpart；The carrier is located at below platform support, and carrier is
Half-headed square body, is respectively equipped with locking bolt on 4 vertical edges of multi-functional carrier, and the bottom plate of carrier is equipped with cross
Connector, elevation mount is equipped on the leading flank of multi-functional carrier, the trailing flank of multi-functional carrier is equipped with fixing clamp.
The carrier is made of high strength composite or carbon fibre material, is connect by three axis holders with body, can
The operation modules such as sandblasted with Fast Installation, painted.
The electrical system and photoelectric comprehensive cable connector box connecting place are equipped with non-slip groove.
The multifunctional platform further includes functional interface, the functional interface include multiple Universal Serial Bus Interface,
Power interface and RJ45 interface.
It further include shield (8), the shield (8) is circular foam rubber circle.
The utility model use process is as follows:
The multifunction anti-collision is tethered at unmanned plane and is connected by photoelectric comprehensive cable with floor power supply device, holds to reach
Long stagnant sky.It is tethered at unmanned plane middle and lower part and multifunctional platform is installed, surrounding is mounted with Anti-bumping protection, control system, multi-functional
Data receiving-transmitting system, image transmission/reception system in platform are used to interact place with what the signal receiving and transmitting system of earth station carried out signal
Reason, undercarriage as reserved accommodation space for carry derust, spray, propagandaing directed to communicate, illuminating, each generic task such as signal relay station is set
It is standby.
The utility model advantage is as follows:
1. high universalizable, convenience, structure is simple, maintenance cost is low, reliable performance.
2. multiple-task equipment can be carried, such as derusts, sprays, propagandaing directed to communicate, illuminating, signal relay station, skyscraper glass curtain
Wall cleaning etc. realizes that one is multi-purpose.3. transmit electric energy by photoelectric comprehensive hawser, allow unmanned plane do not limited by electric energy and
It stops for a long time and gets rid of traditional unmanned plane in the sky and receive the predicament of energy limitation greatly, thus can be applicable in various civilian military etc.
In the dangerous scene of the long-time high altitude operation of various industries, play a multiplier effect.
Detailed description of the invention
Fig. 1 is that multifunction anti-collision provided by the utility model is tethered at unmanned plane overall structure diagram.
Fig. 2 is that multifunction anti-collision provided by the utility model is tethered at unmanned plane Anti-bumping protection, control system and Multifunctional flat
Platform structural schematic diagram.
Fig. 3 is that multifunction anti-collision provided by the utility model is tethered at unmanned plane landing gear structure schematic diagram.
Fig. 4 is that multifunction anti-collision provided by the utility model is tethered at unmanned plane top view.
Each section title and serial number are as follows in figure:
1- body, 2- Anti-bumping protection, control system, 3- multifunctional platform, 4- undercarriage, 5- Ground Support case, the ground 6-
It stands, 7- optoelectrical cable, 8- protective cover, 21- sensor, 31- Navigation of Pilotless Aircraft flight control system, 32- electrical system, 33- photoelectricity
Comprehensive cable connector box, 34- functional interface, 35- tilt-top, 36- data receiving-transmitting system, 37- image transmission/reception system, 41- platform
Bracket, 42- carrier, 43- carrier locking bolt, 44- connector, 45- elevation mount, 46- fixing clamp, 51- power supply unit, 52-
Automatic deploying and retracting line capstan winch, 53- ground fixing device, 54 independent insurance power supplys.
Specific embodiment
The utility model is illustrated with reference to the accompanying drawings and examples.
Embodiment 1
As shown in Figure 1-3, the technical solution of the utility model provided in this embodiment is as follows:
A kind of multifunction anti-collision is tethered at unmanned plane, including body 1, multifunctional platform 3, undercarriage 4, Ground Support case 5,
Face station 6, optoelectrical cable 7；
The multifunctional platform 3 is installed on the middle and lower part position of body 1, including Anti-bumping protection, control system 2, unmanned plane are led
Boat flight control system 31, electrical system 32, photoelectric comprehensive cable connector box 33, data receiving-transmitting system 36, image transmission/reception system 37；
The photoelectric comprehensive cable connector box 33 with respectively with Anti-bumping protection, control system 2, Navigation of Pilotless Aircraft flight control system
31, data receiving-transmitting system 36, image transmission/reception system 37 are electrically connected；The photoelectric comprehensive cable connector box 33 passes through optoelectrical cable
7 connect with Ground Support case 5；The Ground Support case 5 is electrically connected with earth station 6；
The image transmission/reception system 37 is electrically connected with camera, receives the image of camera and by optoelectrical cable 7
It is transmitted to earth station 6；
The data receiving-transmitting system 36 is electrically connected with body 1, Navigation of Pilotless Aircraft flight control system 31 respectively, receives unmanned plane
31 information of navigation flight control system, and 1 information of body is transmitted to earth station 6, and satellite receiver 6 controls information, is transmitted to nobody
Machine navigation flight control system 31 controls body 1 and flies；
The Anti-bumping protection, control system 2 are set to 3 front end of multifunctional platform, for detecting barrier and alarming；
The electrical system 32 is electrically connected by photoelectric comprehensive cable connector box 33, optoelectrical cable 7 with Ground Support case 5
Connect, obtain electric energy, while electrical system 32 respectively with Anti-bumping protection, control system 2, Navigation of Pilotless Aircraft flight control system 31, data
Receive-transmit system 36, image transmission/reception system 37 are electrically connected, to these module for power supply.
The camera is installed on 3 front of multifunctional platform by tilt-top 35
The Anti-bumping protection, control system 2 include sensor 21, control device；The sensor 21 and control device
Electrical connection, the control device respectively with Navigation of Pilotless Aircraft flight control system 31, alarm system and earth station 6, when sensor 21
Detect that transmission signal to control device, control device transmission halts signal extremely when having barrier in the set distance of front
Navigation of Pilotless Aircraft flight control system 31, Navigation of Pilotless Aircraft flight control system 31 controls body 1 and hovers, while control device also transmits obstacle
Object signal is to earth station 6.
The earth station is equipped with warning device and sounds an alarm when receiving obstacle signal.
The sensor 21 is 4, is divided into the four direction positioned at 3 bottom of multifunctional platform.
The undercarriage 4 is set to the lower section of body 1, including platform support 41, carrier 42, carrier locking bolt 43, connection
Part 44, elevation mount 45, fixing clamp 46；The platform support 41 is connect with 1 lower part of body；The carrier 42 is located at
41 lower section of platform support, carrier 42 is half-headed square body, is respectively equipped with lock on 4 vertical edges of multi-functional carrier 42
The bottom plate of bolt 43, carrier 42 is equipped with criss-cross connector 44, and pitching is equipped on the leading flank of multi-functional carrier 42
The trailing flank of device 45, multi-functional carrier 42 is equipped with fixing clamp 46.
The carrier 42 is made of high strength composite or carbon fibre material, is connect by three axis holders with body 1,
The operation modules such as can be sandblasted with Fast Installation, be painted.
The electrical system 32 is equipped with non-slip groove with 33 connecting place of photoelectric comprehensive cable connector box.
The multifunctional platform 3 further includes functional interface 34, and the functional interface 34 includes multiple universal serial bus
Interface, power interface and RJ45 interface.
Further include shield), the shield 8 is circular foam rubber circle.
The present embodiment use process is as follows:
The multifunction anti-collision is tethered at unmanned plane and is connected by photoelectric comprehensive cable 7 with floor power supply device 51, to reach
To lasting stagnant sky.It being tethered at unmanned plane middle and lower part and multifunctional platform 3 is installed, surrounding is mounted with Anti-bumping protection, control system 2,
Data receiving-transmitting system 36, image transmission/reception system 37 in multifunctional platform 3 are used to carry out with the signal receiving and transmitting system 62 of earth station 6
The interaction process of signal, undercarriage 4 as reserved accommodation space for carry derust, spray, propagandaing directed to communicate, illuminating, signal relay station
Etc. all kinds of task devices.
Claims (10)
1. a kind of multifunction anti-collision is tethered at unmanned plane, including body (1), multifunctional platform (3), undercarriage (4), Ground Support case
(5), earth station (6), optoelectrical cable (7)；It is characterized by:
The multifunctional platform (3) is installed on the middle and lower part position of body (1), including Anti-bumping protection, control system (2), unmanned plane
Navigation flight control system (31), electrical system (32), photoelectric comprehensive cable connector box (33), data receiving-transmitting system (36), image transmission/reception
System (37)；
The photoelectric comprehensive cable connector box (33) with respectively with Anti-bumping protection, control system (2), Navigation of Pilotless Aircraft flight control system
(31), data receiving-transmitting system (36), image transmission/reception system (37) electrical connection；The photoelectric comprehensive cable connector box (33) passes through light
Electric comprehensive cable (7) connect with Ground Support case (5)；The Ground Support case (5) is electrically connected with earth station (6)；
The image transmission/reception system (37) is electrically connected with camera, receives the image of camera and by optoelectrical cable (7)
It is transmitted to earth station (6)；
The data receiving-transmitting system (36) is electrically connected with body (1), Navigation of Pilotless Aircraft flight control system (31) respectively, receives nobody
Machine navigation flight control system (31) information, and body (1) information is transmitted to earth station (6), and satellite receiver (6) controls information,
It is transmitted to Navigation of Pilotless Aircraft flight control system (31) control body (1) flight；
The Anti-bumping protection, control system (2) are set to multifunctional platform (3) front end, for detecting barrier and alarming；
The electrical system (32) is by photoelectric comprehensive cable connector box (33), optoelectrical cable (7) and Ground Support case (5) electricity
Connection, obtain electric energy, while electrical system (32) respectively with Anti-bumping protection, control system (2), Navigation of Pilotless Aircraft flight control system
(31), data receiving-transmitting system (36), image transmission/reception system (37) electrical connection, to these module for power supply.
2. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: the camera passes through pitching
Holder (35) is installed on multifunctional platform (3) front.
3. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: the Anti-bumping protection, control system
System (2) includes sensor (21), control device；The sensor (21) is electrically connected with control device, the control device
Respectively with Navigation of Pilotless Aircraft flight control system (31), alarm system and earth station (6), when sensor (21) detect front setting away from
From it is interior have barrier when, for transmission signal to control device, control device transmission signal to the Navigation of Pilotless Aircraft that halts flies control system
It unites (31), Navigation of Pilotless Aircraft flight control system (31) controls body (1) hovering, while control device also transmits obstacle signal to ground
Face station (6).
4. multifunction anti-collision according to claim 3 is tethered at unmanned plane, it is characterised in that: the earth station is equipped with alarm
Device is sounded an alarm when receiving obstacle signal.
5. multifunction anti-collision according to claim 3 is tethered at unmanned plane, it is characterised in that: the sensor (21) is 4
It is a, it is divided into the four direction positioned at multifunctional platform (3) bottom.
6. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: the undercarriage (4) is set to machine
The lower section of body (1), including platform support (41), carrier (42), carrier locking bolt (43), connector (44), elevation mount
(45), fixing clamp (46)；The platform support (41) is connect with body (1) lower part；The carrier (42) is located at platform
Below bracket (41), carrier (42) is half-headed square body, is respectively equipped on 4 vertical edges of multi-functional carrier (42)
The bottom plate of locking bolt (43), carrier (42) is equipped with criss-cross connector (44), the leading flank in multi-functional carrier (42)
It is equipped with elevation mount (45), the trailing flank of multi-functional carrier (42) is equipped with fixing clamp (46).
7. multifunction anti-collision according to claim 6 is tethered at unmanned plane, it is characterised in that: the carrier (42) is by high-strength
Degree composite material or carbon fibre material are made, and are connect by three axis holders with body (1), can be sandblasted, be painted with Fast Installation
Operation module.
8. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: the electrical system (32) and light
Comprehensive cable connector box (33) connecting place of electricity is equipped with non-slip groove.
9. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: the multifunctional platform (3)
It further include functional interface (34), the functional interface (34) includes that multiple Universal Serial Bus Interface, power interface and RJ45 connect
Mouthful.
10. multifunction anti-collision according to claim 1 is tethered at unmanned plane, it is characterised in that: further include shield (8), institute
Stating shield (8) is circular foam rubber circle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820699017.4U CN208325667U (en) | 2018-05-11 | 2018-05-11 | A kind of multifunction anti-collision is tethered at unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820699017.4U CN208325667U (en) | 2018-05-11 | 2018-05-11 | A kind of multifunction anti-collision is tethered at unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208325667U true CN208325667U (en) | 2019-01-04 |
Family
ID=64776894
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820699017.4U Active CN208325667U (en) | 2018-05-11 | 2018-05-11 | A kind of multifunction anti-collision is tethered at unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208325667U (en) |
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2018
- 2018-05-11 CN CN201820699017.4U patent/CN208325667U/en active Active
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