CN205738120U - It is a kind of that unmanned plane is out of control falls rear location position device - Google Patents
It is a kind of that unmanned plane is out of control falls rear location position device Download PDFInfo
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- CN205738120U CN205738120U CN201620619546.XU CN201620619546U CN205738120U CN 205738120 U CN205738120 U CN 205738120U CN 201620619546 U CN201620619546 U CN 201620619546U CN 205738120 U CN205738120 U CN 205738120U
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Abstract
The utility model discloses that a kind of unmanned plane is out of control falls rear location position device, including wireless signal transmitter and radio receiver, therebetween without any physical connection, wherein, wireless signal transmitter is installed on unmanned plane, including: the first signal processing unit and be respectively connecting to the Vibration induction unit of the first signal processing unit, humidity inductive unit, the first radio receiving transmitting module, voice guard and lighting unit；Radio receiver is hand-held device, including: secondary signal processing unit and the second radio receiving transmitting module of the first radio receiving transmitting module adaptation and display unit, the second radio receiving transmitting module and display unit are respectively connecting to secondary signal processing unit.This utility model simple in construction, effect are notable, can unmanned plane is out of control fall after guide people to give unmanned plane quickly and accurately for change by the display content on sound, light and display unit, it is to avoid unnecessary economic loss.
Description
Technical field
This utility model relates to a kind of positioner, particularly relates to that a kind of unmanned plane is out of control falls rear location position device.
Background technology
Existing unmanned plane is often at outside work, but manually is being inconvenient to arrive frequently by Remote flight
Place, in the occasion that some are more complicated, drops if as the most out of control in mountain forest, gully, waters etc., owing to its scale of construction is less, and can
Can be difficult to give for change.
Utility model content
For the deficiency in structure in prior art, this utility model provides that a kind of unmanned plane is out of control falls rear location positioning
Device, it is ensured that give unmanned plane quickly and accurately for change.
The technical scheme that this utility model solves above-mentioned technical problem is as follows: a kind of unmanned plane is out of control falls rear location positioning
Device, including wireless signal transmitter and radio receiver, nothing between described wireless signal transmitter and described radio receiver
Any physical connection, wherein, described wireless signal transmitter is installed on described unmanned plane, including: the first signal processing unit, shake
Dynamic sensing unit, humidity inductive unit, the first radio receiving transmitting module, voice guard and lighting unit, wherein, described vibrations
Sensing unit, described humidity inductive unit, described first radio receiving transmitting module, described voice guard and described lighting unit
It is respectively connecting to described first signal processing unit；Described radio receiver is hand-held device, including: secondary signal processes single
Unit and adaptive the second radio receiving transmitting module of described first radio receiving transmitting module and display unit, wherein, described second wireless
Transceiver module and described display unit are respectively connecting to described secondary signal processing unit.
On the basis of technique scheme, this utility model can also do following improvement.
Further, described Vibration induction unit includes: hollow housing；Spring, its first end is located at described hollow housing
Surface, the second end extends to the inside of described hollow housing；Metal ball, it is connected to the second end of described spring；Negative pole, its
It is located at the outside of described hollow housing, is electrically connected to the first end of described spring；Positive pole, it is also located at outside described hollow housing
Portion, is positioned at the not homonymy of described negative pole；Described positive pole does not contacts with described metal ball when unmanned plane is properly functioning, and falls
When falling, spring generation elastic deformation, metal ball strikes positive pole, connects circuit.
Further, described radio receiver also includes the trigger button being connected to described secondary signal processing unit.
Further, described first signal processing unit is single-chip microcomputer.
Further, described secondary signal processing unit is single-chip microcomputer.
Further, described display unit is liquid crystal display or LED display.
Further, described humidity inductive unit is humidity sensor.
Further, described voice guard is speaker or buzzer.
Further, described lighting unit is LED.
The beneficial effects of the utility model are: simple in construction, effect are notable, can unmanned plane is out of control fall after pass through sound
Display content on sound, light and display unit guides people finally to give unmanned plane for change, it is to avoid unnecessary economic loss.
Accompanying drawing explanation
Fig. 1 is the unmanned plane of the present utility model structural representation falling rear location position device out of control；
Fig. 2 is the structural representation of Vibration induction unit of the present utility model；
In the accompanying drawings, the list of designations represented by each label is as follows:
100 wireless signal transmitters
101 first signal processing units
102 Vibration induction unit
1021 hollow housings
1022 springs
1023 metal ball
1024 negative poles
1025 positive poles
103 humidity inductive unit
104 first radio receiving transmitting modules
105 voice guards
106 lighting units
200 radio receivers
201 secondary signal processing units
202 second radio receiving transmitting modules
203 display units
204 trigger buttons
Detailed description of the invention
Being described principle of the present utility model and feature below in conjunction with accompanying drawing, example is served only for explaining this practicality
Novel, it is not intended to limit scope of the present utility model.
Refer to shown in Fig. 1, it is the unmanned plane of the present utility model structural representation falling rear location position device out of control
Figure.Described positioner includes: wireless signal transmitter 100 and radio receiver 200, described wireless signal transmitter 100 and institute
State without any physical connection between radio receiver 200, wherein,
Described wireless signal transmitter 100 is installed on described unmanned plane, comprising: the first signal processing unit 101, vibrations
Sensing unit 102, humidity inductive unit the 103, first radio receiving transmitting module 104, voice guard 105 and lighting unit 106,
Wherein,
Described first signal processing unit 101 can be such as single-chip microcomputer, but is not limited；
Described Vibration induction unit 102 is connected to described first signal processing unit 101, and its structure will be carried out in detail below
Thin description；
Described humidity inductive unit 103 is connected to described first signal processing unit 101, described humidity inductive unit 103
Can be such as humidity sensor, but be not limited；
Described first radio receiving transmitting module 104 is connected to described first signal processing unit 101, and it is existing common nothing
Line transceiver module, can wireless receiving and dispatching information, it is achieved the high speed data transfer in certain distance；
Described voice guard 105 and described lighting unit 106 are respectively connecting to described first signal processing unit 101,
Described voice guard 105 can be such as speaker or buzzer, and described lighting unit 106 can be such as LED, described sound
Alarm 105 and described lighting unit 106 by sound and the falling position of light prompting unmanned plane, guide people to look for respectively
Arrive；
Thus, if unmanned plane falls ground, Vibration induction unit is triggered, and the first signal processing unit sends signal and refers to
Order, is on the one hand spread out of information by the first radio receiving transmitting module, on the other hand sends sound or light；Or, unmanned plane falls
Drop down onto in water, shake inconspicuous, and humidity inductive unit is triggered, also can spread out of information and send sound or light.
Described radio receiver 200 is hand-held device, comprising: secondary signal processing unit 201 and described first nothing
Second radio receiving transmitting module 202 of line transceiver module 104 adaptation and display unit 203, wherein,
Described secondary signal processing unit 201 can be such as single-chip microcomputer, but is not limited；
Described second radio receiving transmitting module 202 is connected to described secondary signal processing unit 201, and it is existing common nothing
Line transceiver module, can wireless receiving and dispatching information, it is achieved the high speed data transfer in certain distance；
Described display unit 203 is connected to described secondary signal processing unit 201, and it can be liquid crystal display or be LED
Display screen, for showing direction, place and the approximate distance of unmanned plane；
Thus, the second radio receiving transmitting module receives the information from the first radio receiving transmitting module, processes through secondary signal
After unit carries out data analysis, direction, place and the approximate distance of unmanned plane are presented on display unit, guide people to find；
Preferably, also to include that trigger button 204, described trigger button 204 are connected to described for described radio receiver 200
Secondary signal processing unit 201, its can by send one trigger signal to described secondary signal processing unit 201, described the
Two radio receiving transmitting modules 202, described first radio receiving transmitting module 104, described first signal processing unit 101, so that institute
State voice guard 105 and send sound and/or described lighting unit 106 sends light, guide people to eventually find unmanned plane and fall
The accurate location fallen.
In this utility model, described radio receiver can be commercially available channels watcher, and it is mainly used in short distance
From direction-finding station campaign, receiving frequency is 3.5～3.6MHz, can be not less than 300m by H.D, but be not limited.
It follows that referring again to shown in Fig. 2, it is the structural representation of Vibration induction unit of the present utility model；Described
Vibration induction unit 102 includes:
Hollow housing 1021；
Spring 1022, its first end is located at described hollow housing 1021 surface, and the second end extends to described hollow housing
1021 is internal；
Metal ball 1023, it is connected to the second end of described spring 1022；
Negative pole 1024, it is outside that it is located at described hollow housing 1021, is electrically connected to the first end of described spring 1022；
Positive pole 1025, it is outside that it is also located at described hollow housing 1021, is positioned at the not homonymy of described negative pole 1024；Need into
Row explanation: about the position of positive pole, with unmanned plane properly functioning time do not contact with described metal ball, and when falling,
Due to spring generation elastic deformation, cause metal ball to strike positive pole, connect circuit and be as the criterion.
Thus, when unmanned plane falls, spring generation elastic deformation, metal ball strikes positive pole, connects circuit, Vibration induction
Unit is triggered, and triggers signal and sends to the first signal processing unit.
Unmanned plane of the present utility model is out of control falls rear location position device simple in construction, effect significantly, can be at unmanned plane
Out of control fall after guide people finally to give unmanned plane for change by the display content on sound, light and display unit, it is to avoid
Unnecessary economic loss.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model, all in this practicality
Within novel spirit and principle, any modification, equivalent substitution and improvement etc. made, should be included in guarantor of the present utility model
Within the scope of protecting.
Claims (9)
1. a unmanned plane is out of control falls rear location position device, it is characterised in that include wireless signal transmitter and wireless receiving
Device, without any physical connection between described wireless signal transmitter and described radio receiver, wherein,
Described wireless signal transmitter is installed on described unmanned plane, comprising: the first signal processing unit, Vibration induction unit,
Humidity inductive unit, the first radio receiving transmitting module, voice guard and lighting unit, wherein, described Vibration induction unit, institute
State humidity inductive unit, described first radio receiving transmitting module, described voice guard and described lighting unit to be respectively connecting to
Described first signal processing unit；
Described radio receiver is hand-held device, comprising: secondary signal processing unit and described first radio receiving transmitting module
The second adaptive radio receiving transmitting module and display unit, wherein, described second radio receiving transmitting module divides with described display unit
It is not connected to described secondary signal processing unit.
Positioner the most according to claim 1, it is characterised in that described Vibration induction unit includes:
Hollow housing；
Spring, its first end is located at the surface of described hollow housing, and the second end extends to the inside of described hollow housing；
Metal ball, it is connected to the second end of described spring；
Negative pole, it is located at the outside of described hollow housing, is electrically connected to the first end of described spring；
Positive pole, it is also located at the outside of described hollow housing, is positioned at the not homonymy of described negative pole；Described positive pole is normal at unmanned plane
Do not contact with described metal ball during operation, and when falling, spring generation elastic deformation, metal ball strikes positive pole, connects
Circuit.
Positioner the most according to claim 1 and 2, it is characterised in that described radio receiver also includes being connected to
The trigger button of described secondary signal processing unit.
Positioner the most according to claim 1 and 2, it is characterised in that described first signal processing unit is single-chip microcomputer.
Positioner the most according to claim 1 and 2, it is characterised in that described secondary signal processing unit is single-chip microcomputer.
Positioner the most according to claim 1 and 2, it is characterised in that described display unit is liquid crystal display or LED
Display screen.
Positioner the most according to claim 1 and 2, it is characterised in that described humidity inductive unit is humidity sensor.
Positioner the most according to claim 1 and 2, it is characterised in that described voice guard is speaker or buzzing
Device.
Positioner the most according to claim 1 and 2, it is characterised in that described lighting unit is LED.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620619546.XU CN205738120U (en) | 2016-06-21 | 2016-06-21 | It is a kind of that unmanned plane is out of control falls rear location position device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620619546.XU CN205738120U (en) | 2016-06-21 | 2016-06-21 | It is a kind of that unmanned plane is out of control falls rear location position device |
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| CN205738120U true CN205738120U (en) | 2016-11-30 |
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| CN201620619546.XU Expired - Fee Related CN205738120U (en) | 2016-06-21 | 2016-06-21 | It is a kind of that unmanned plane is out of control falls rear location position device |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108288334A (en) * | 2018-01-31 | 2018-07-17 | 广东容祺智能科技有限公司 | A kind of unmanned plane burglary-resisting system |
| CN108700884A (en) * | 2017-09-19 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Unmanned plane localization method, device and electric tune, dynamical system, UAV system |
| WO2018196494A1 (en) * | 2017-04-26 | 2018-11-01 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method and device, and unmanned aerial vehicle |
| CN109383831A (en) * | 2018-09-30 | 2019-02-26 | 安徽煜丰农业机械制造有限公司 | A kind of plant protection drone for automatic positioning of falling |
| CN109573028A (en) * | 2018-12-12 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane |
| CN111752307A (en) * | 2019-12-19 | 2020-10-09 | 广州极飞科技有限公司 | Position marking device, unmanned aerial vehicle and position marking method |
-
2016
- 2016-06-21 CN CN201620619546.XU patent/CN205738120U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018196494A1 (en) * | 2017-04-26 | 2018-11-01 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle control method and device, and unmanned aerial vehicle |
| CN108803650A (en) * | 2017-04-26 | 2018-11-13 | 深圳市道通智能航空技术有限公司 | The control method and device of unmanned plane, unmanned plane |
| US11501649B2 (en) | 2017-04-26 | 2022-11-15 | Autel Robotics Co., Ltd. | Drone control method and device and drone |
| CN108700884A (en) * | 2017-09-19 | 2018-10-23 | 深圳市大疆创新科技有限公司 | Unmanned plane localization method, device and electric tune, dynamical system, UAV system |
| WO2019056181A1 (en) * | 2017-09-19 | 2019-03-28 | 深圳市大疆创新科技有限公司 | Method and device for positioning unmanned aerial vehicle, and electric adjustment and power system, and unmanned aerial vehicle system |
| CN108288334A (en) * | 2018-01-31 | 2018-07-17 | 广东容祺智能科技有限公司 | A kind of unmanned plane burglary-resisting system |
| CN109383831A (en) * | 2018-09-30 | 2019-02-26 | 安徽煜丰农业机械制造有限公司 | A kind of plant protection drone for automatic positioning of falling |
| CN109573028A (en) * | 2018-12-12 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane |
| CN111752307A (en) * | 2019-12-19 | 2020-10-09 | 广州极飞科技有限公司 | Position marking device, unmanned aerial vehicle and position marking method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Wu Haoru Inventor after: Feng Tao Inventor before: Li Die Inventor before: Li Chunbo |
|
| COR | Change of bibliographic data | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161130 Termination date: 20210621 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |