CN208125162U - Device for retrieving and aircraft assembly for aircraft - Google Patents
Device for retrieving and aircraft assembly for aircraft Download PDFInfo
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- CN208125162U CN208125162U CN201820691766.2U CN201820691766U CN208125162U CN 208125162 U CN208125162 U CN 208125162U CN 201820691766 U CN201820691766 U CN 201820691766U CN 208125162 U CN208125162 U CN 208125162U
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- aircraft
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Abstract
The utility model relates to the device for retrieving and aircraft assembly for aircraft.The device for retrieving setting on board the aircraft, and works independently of the aircraft, and the device for retrieving includes：Guiding module, for giving signal for change to user's sending or the aircraft being directed to predetermined position；Trigger module, for triggering the guiding module；Controller, for controlling the guiding module and the trigger module；And power module, for powering for the guiding module, the trigger module and the controller.
Description
Technical field
The utility model relates to the fields of aircraft especially unmanned plane.Particularly, the utility model relates to one kind to be used for
The device for retrieving of aircraft is especially used for the device for retrieving of unmanned plane.In addition, the utility model is also related to including the aircraft
With the aircraft assembly of the device for retrieving.
Background technique
Currently, aircraft especially unmanned plane is widely used in various fields, such as high-altitude is taken pictures, forest monitoring, goods and materials
Deliver etc..The unmanned plane however, application of unmanned plane usually will receive the limitation of environment, such as in-flight breaks down, nothing
It is man-machine in the high wind or remaining capacity is too low and may crash at any time, the flight time of unmanned plane is too long or temperature is excessively high or
It is too low and may damage that component or the distance between unmanned plane and user therein are excessive and may lost control, etc.
Deng.In these cases, recall as early as possible unmanned plane can yet be regarded as one well selection.
In other cases, unmanned plane may be out of touch with user due to break down or meeting with barrier.
These barriers are for instance it can be possible that trees, building, massif, electric wire etc..It is used when under complex landform or complicated weather condition
When unmanned plane, such case is especially prominent.In addition, this of loss unmanned plane also often occurs when new hand uses unmanned plane
Kind situation.Therefore, there is an urgent need to the device for retrieving that one kind can actively or passively give unmanned plane for change.
Utility model content
The purpose of this utility model is that drawings is in the device for retrieving and method for retrieving of aircraft, it can be actively or passively
It gives aircraft for change, reduces the economic loss of user.
In one aspect, the utility model provides a kind of device for retrieving for aircraft, which is characterized in that described to look for
Return device is arranged on board the aircraft, and works independently of the aircraft, and the device for retrieving includes：Guiding module, for
User issues and gives signal for change or the aircraft is directed to predetermined position；Trigger module, for triggering the guidance mould
Block；Controller, for controlling the guiding module and the trigger module；And power module, for for the guiding module,
The trigger module and controller power supply.
In one embodiment, mode of operation and operating environment of the controller based on the aircraft make the touching
It sends out module and triggers the guiding module.In this case, aircraft is not based on the instruction of user, but is based on giving dress for change
The autonomous judgement set initiatively is retrieved.
Preferably, the device for retrieving further comprises sensing module, and the sensing module detects the behaviour of the aircraft
Make state and operating environment, to make the trigger module trigger the guiding module in the case where there：The aircraft hair
Raw failure；The remaining capacity of the aircraft is lower than predetermined threshold；The flight time of the aircraft is more than predetermined threshold；It is described
The flying height of aircraft is more than predetermined threshold；The temperature of environment is higher than predetermined threshold where the aircraft；The aircraft
The temperature of place environment is lower than predetermined threshold；The distance between the aircraft and user are greater than predetermined threshold；The flight
Device is in high wind；Or the aircraft encounter barrier.
In other words, device for retrieving can actively give aircraft for change when meeting above-mentioned condition.Correspondingly, sensing module can
To be the respective sensor for judging whether above-mentioned condition is true, such as aircraft flight data collection and analytical equipment, electricity inspection
Survey device, timer, height sensor, temperature sensor, GPS, big-dipper satellite locating module, airspeedometer etc..
After mode is given in starting for change, the guiding module can be triggered module triggering and the aircraft is directed to pre-
Positioning is set.The predetermined position can be user position, or by the predefined position of user.For example, user exists
Position at that time can be defined as predetermined position when letting aircraft fly away, then device for retrieving will in the case where above-mentioned condition meets
Aircraft can be made to fly back the position to where when initially letting fly away.At this point, the guiding module can have locating module, to winged
Row device navigates.
In another advantageous scheme, the device for retrieving further comprises wireless communication module, and the controller passes through
The wireless communication module is received to be issued by user and be instructed, and triggers the guidance by the trigger module based on described instruction
Module.In this case, the instruction based on user is passively retrieved by aircraft.
Advantageously, the wireless communication module is wifi module, zigbee communication module, bluetooth module, 2G module, 3G mould
One of block, 4G module are a variety of.
In a preferred approach, power supply of the power module independently of the aircraft.Alternatively, the power module is
A part of the power supply of the aircraft.
In a preferred approach, the signal of giving for change includes optical signal, voice signal, smoke signal, olfactory signal, image letter
Number and one of positioning signal or a variety of, wherein described image signal includes the image information of environment where the aircraft,
The positioning signal includes the location information of the aircraft position.Optical signal can be the LED light hair by device for retrieving
Colourama and/or flash of light out, it is especially beneficial that this gives aircraft for change to night.
Advantageously, described image signal or the positioning signal, which can be sent on the terminal device of user, looks into
It sees.When aircraft surprisingly crashes or by the camera of aircraft carrying when being blocked by barrier or in addition picture signal can be
Picture around aircraft captured by camera, user can according to these pictures speculate aircraft be in where.
Positioning signal for example can be the longitude and latitude of aircraft position.Above-mentioned image information and location information for example can be by
It is sent on the mobile phone of user and checks.
In second aspect, the utility model further relates to a kind of aircraft assembly comprising aircraft and according to this is practical
Novel device for retrieving.
Preferably, the aircraft is unmanned plane.
In the third aspect, the utility model provides a kind of method for retrieving for aircraft, wherein the aircraft band
There is device for retrieving, the device for retrieving is arranged on the aircraft, and works independently of the aircraft, the device for retrieving
Including guiding module, trigger module, controller and power module, which is characterized in that the method for retrieving includes：Determine that starting is looked for
The mode of returning；The guiding module is triggered by trigger module；And from the guiding module to user issue give for change signal or
The aircraft is directed to predetermined position.
In one embodiment, determine that the step of mode is given in starting for change includes：The flight is based on by the controller
The mode of operation of device or operating environment determine whether to give mode for change described in starting.
Preferably, determine that the step of mode is given in starting for change includes：Detect the mode of operation or operating environment of the aircraft；
And determined whether to give mode for change described in starting based on the mode of operation or the operating environment by the controller.
In another advantageous scheme, determine that the step of mode is given in starting for change includes：Receive user's sending gives finger for change
It enables, and determines and give mode for change described in starting.
In a preferred approach, issuing the step of giving signal for change includes：Optical signal is issued, signal is made a sound, issues smog
Signal, scent of signal, sends picture signal to user, and/or send positioning signal to user.
Detailed description of the invention
Fig. 1 is the block diagram according to the first embodiment of the device for retrieving of the utility model；
Fig. 2 is the block diagram according to the modification of the first embodiment of the device for retrieving of the utility model；
Fig. 3 is the block diagram according to the second embodiment of the device for retrieving of the utility model；
Fig. 4 is the block diagram according to the modification of the second embodiment of the device for retrieving of the utility model；
Fig. 5 is the flow chart according to the method for retrieving of the utility model；And
Fig. 6 is the flow chart according to the modification of the method for retrieving of the utility model.
Specific embodiment
The utility model is more fully retouched below with reference to relevant drawings for the ease of understanding the utility model,
It states.The better embodiment of the utility model is given in attached drawing.But the utility model can come in many different forms
It realizes, however it is not limited to embodiments described herein.On the contrary, the purpose of providing these embodiments is that in order to more comprehensively
Thoroughly understand the disclosure of the utility model.
First embodiment according to the present utility model provides a kind of device for retrieving operated with active mode.Such as Fig. 1
Shown, which includes controller, sensing module, trigger module, guiding module and power module.Sensing module detection with
The relevant parameter of mode of operation or operating environment of aircraft, for example, flying quality, remaining capacity, the flight time, flying height,
Environment temperature, position, wind speed etc., and these parameters are sent to controller.Controller analyzes various parameters,
And it determines whether to starting and gives mode for change.Under mode of giving for change, controller controls trigger module and starts guiding module.Guide mould
Block then issues and gives signal for change.In addition, power module is other all module for power supply.
Controller gives mode for change in the lower starting of one or more of following situation based on the signal that sensing module senses：
Aircraft breaks down, and the remaining capacity of aircraft is lower than predetermined threshold, and the flight time of aircraft is more than predetermined threshold, flight
The flying height of device is more than predetermined threshold, and the temperature of environment where aircraft is higher than predetermined threshold, the temperature of environment where aircraft
Degree is lower than predetermined threshold, and the distance between aircraft and user are greater than predetermined threshold, and aircraft is in high wind, and aircraft meets with
Meet barrier.
Guiding module can issue one of optical signal, voice signal, smoke signal, picture signal and positioning signal or
It is a variety of.For example, guiding module can be LED light, to issue white light or colored optical signal, these optical signals when being triggered
It can be flashing.Guiding module can be sound generator, to beep when being triggered or music.Guiding module
It can be aerosol producer, to issue smog when being triggered.Guiding module can be signal generator, thus being triggered
When issue the recognizable signal of human or animal.Guiding module can be camera, thus when being triggered to aircraft around
Environment is taken pictures, and sends the pictures to user.Guiding module is also possible to GPS, to record aircraft when being triggered
The location information at place, and the location information is sent to user.In the case where above-mentioned picture signal and positioning signal,
Device for retrieving should also contain wireless communication module, to send image or position signal to user.
In all the above cases, device for retrieving actively issues and gives signal for change, and user needs to follow these flashes of light, sound
Sound, smog, smell find aircraft, or judge based on image, position the physical location of aircraft and find aircraft.?
It is actively triggered that is, giving mode for change, but aircraft needs are passively given for change by user.
Fig. 2 provides a kind of modification of first embodiment, wherein guiding module do not issue give signal for change but voluntarily
Aircraft is guided.That is, trigger module triggers guiding module, the aircraft is directed to predetermined by subsequent guiding module
Position.The predetermined position can be user position, be also possible to by the predefined position of user.For example, user
Position at that time can be defined as predetermined position when letting aircraft fly away, then device for retrieving is in the case where above-mentioned condition meets
Aircraft will be made to fly back the position to where when initially letting fly away.
This mode is highly beneficial when aircraft is with the work of autonomous cruise mode.For example, user let fly away it is winged
It can be set flight duration to 1 hour before row device, and aircraft is made to fly under cruise mode.In this way, winged letting fly away
After row device, user can go to carry out other work there is no need to control aircraft in real time.It is small in aircraft flight 1
When after, actively mode is given in triggering for change to device for retrieving, and aircraft is directed to predetermined position by guiding module.User can
To check aircraft recorded data afterwards.
In this case, device for retrieving actively issues and gives signal for change, while aircraft is initiatively given for change.In this process
In do not need the participation of user.In addition, guiding module needs to be equipped with GPS module, to record flight path or to navigate to
Predetermined position.
Second embodiment according to the present utility model provides a kind of device for retrieving passively operated.With Fig. 1
Shown in first embodiment compare, which further comprises wireless communication module, as shown in Figure 3.In this scenario,
User actively gives instruction for change to device for retrieving sending, and the wireless communication module of device for retrieving receives the instruction, and instruction is passed
Controller is sent to start the mode of giving for change.Under mode of giving for change, controller controls trigger module and starts guiding module.Guiding module
It then issues and gives signal for change.Wireless communication module can be the various skills for being suitble to be communicated with the handheld terminal that user is held
Art, such as wifi module, zigbee communication module, bluetooth module, 2G module, 3G module, 4G module.
It is identical as first embodiment shown in FIG. 1, the guiding module in scheme shown in Fig. 3 can also issue optical signal,
One of voice signal, smoke signal, picture signal and positioning signal are a variety of.User can follow these signals and find
Aircraft.It is passively triggered that is, giving mode for change, aircraft is also required to passively be given for change by user.
Fig. 4 provides a kind of modification of second embodiment, similar to modification shown in Fig. 2.That is, device for retrieving base
Passively start mode of giving for change in the instruction of user, but aircraft is initiatively given for change.User, which only needs to issue, gives finger for change
It enables, later taking part in there is no need to user.
According to the utility model, recovery module is set on board the aircraft, user passively receives looking for for recovery module sending
Letter in reply number, or actively instruction is given for change to recovery module transmission, allow user to give aircraft for change in time, to improve
A possibility that aircraft is given for change reduces the economic loss of user.
In addition, the recovery module can also initiatively fly back to designated place, to save the time of user and mention
The convenience used for aircraft.
The utility model is also related to the method for retrieving for aircraft.As shown in figure 5, the process of this method is as follows.In step
At rapid 101, what controller determined whether to receive user's sending gives instruction for change；Instruction is given for change if received, in step
At 104, starting gives mode for change and triggers guiding module by trigger module；Then it at step 105, is looked for by guiding module sending
Letter in reply number.
In addition, this method also can be implemented it is as follows.At step 102, by the mode of operation of sensing module sense aircraft
And operating environment；Then at step 103, determine whether that mode is given in starting for change by controller；If it is determined that mode is given in starting for change,
Then at step 104, guiding module is triggered by trigger module；Then at step 105, signal is given for change by guiding module sending.
Fig. 6 shows the modification of method for retrieving according to the present utility model.At step 201, controller determines whether to connect
Receive user's sending gives instruction for change；Give instruction for change if received, at step 204, starting give for change mode and by
Trigger module triggers guiding module；Then at step 205, aircraft is directed to predetermined position by guiding module.
In addition, this method also can be implemented it is as follows.At step 202, by the mode of operation of sensing module sense aircraft
And operating environment；Then at step 203, determine whether that mode is given in starting for change by controller；If it is determined that mode is given in starting for change,
Then at step 204, guiding module is triggered by trigger module；Then at step 205, aircraft is directed to by guiding module
Predetermined position.
Each technical characteristic of embodiment described above can be combined arbitrarily, for simplicity of description, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, all should be considered as described in this specification.
Embodiment described above only expresses the several embodiments of the utility model, and description is more specific and detailed
Carefully, but it should not be understood as limiting the scope of the patent of the utility model.It should be pointed out that for the general of this field
For logical technical staff, without departing from the concept of the premise utility, various modifications and improvements can be made, these are all
Belong to the protection scope of the utility model.Therefore, the scope of protection shall be subject to the appended claims for the utility model patent.
Claims (10)
1. a kind of device for retrieving for aircraft, which is characterized in that the device for retrieving is arranged on board the aircraft, and independently of
The aircraft work, the device for retrieving include：
Guiding module, for giving signal for change to user's sending or the aircraft being directed to predetermined position；
Trigger module, for triggering the guiding module；
Controller, for controlling the guiding module and the trigger module；And
Power module, for powering for the guiding module, the trigger module and the controller.
2. the device for retrieving according to claim 1 for aircraft, which is characterized in that the controller is based on described fly
The mode of operation and operating environment of row device make trigger module trigger the guiding module.
3. the device for retrieving according to claim 2 for aircraft, which is characterized in that the device for retrieving further wraps
Sensing module is included, the sensing module detects the mode of operation and operating environment of the aircraft, to make the trigger module
The guiding module is triggered in the case where there：
The aircraft breaks down；
The remaining capacity of the aircraft is lower than predetermined threshold；
The flight time of the aircraft is more than predetermined threshold；
The flying height of the aircraft is more than predetermined threshold；
The temperature of environment is higher than predetermined threshold where the aircraft；
The temperature of environment is lower than predetermined threshold where the aircraft；
The distance between the aircraft and user are greater than predetermined threshold；
The aircraft is in high wind；Or
The aircraft encounter barrier.
4. the device for retrieving according to claim 1 for aircraft, which is characterized in that the device for retrieving further wraps
Wireless communication module is included, the controller is received to be issued by user by the wireless communication module and be instructed, and based on described
Instruction triggers the guiding module by the trigger module.
5. the device for retrieving according to claim 4 for aircraft, which is characterized in that the wireless communication module is
One of wifi module, zigbee communication module, bluetooth module, 2G module, 3G module, 4G module are a variety of.
6. the device for retrieving according to claim 1 for aircraft, which is characterized in that the power module is independently of institute
State the power supply of aircraft, or a part of the power supply for the aircraft.
7. the device for retrieving according to any one of claim 1 to 6 for aircraft, which is characterized in that described to give for change
Signal includes one of optical signal, voice signal, smoke signal, olfactory signal, picture signal and positioning signal or a variety of,
In, described image signal includes the image information of environment where the aircraft, and the positioning signal includes the aircraft institute
Location information in position.
8. the device for retrieving according to claim 7 for aircraft, which is characterized in that described image signal is described fixed
Position signal, which can be sent on the terminal device of user, to be checked.
9. a kind of aircraft assembly, which is characterized in that including：
Aircraft；And
Device for retrieving according to any one of claim 1 to 8 for aircraft.
10. aircraft assembly according to claim 9, which is characterized in that the aircraft is unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820691766.2U CN208125162U (en) | 2018-04-28 | 2018-04-28 | Device for retrieving and aircraft assembly for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820691766.2U CN208125162U (en) | 2018-04-28 | 2018-04-28 | Device for retrieving and aircraft assembly for aircraft |
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| Publication Number | Publication Date |
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| CN208125162U true CN208125162U (en) | 2018-11-20 |
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| CN201820691766.2U Expired - Fee Related CN208125162U (en) | 2018-04-28 | 2018-04-28 | Device for retrieving and aircraft assembly for aircraft |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN110510138A (en) * | 2019-09-03 | 2019-11-29 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method, device and aircraft |
| 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 |
-
2018
- 2018-04-28 CN CN201820691766.2U patent/CN208125162U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| WO2020119720A1 (en) * | 2018-12-12 | 2020-06-18 | 深圳市道通智能航空技术有限公司 | Auxiliary unmanned aerial vehicle finding method and apparatus, and unmanned aerial vehicle |
| CN110510138A (en) * | 2019-09-03 | 2019-11-29 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method, device and aircraft |
| 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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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181120 Termination date: 20190428 |