CN207060413U - One kind is taken photo by plane unmanned plane - Google Patents
One kind is taken photo by plane unmanned plane Download PDFInfo
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- CN207060413U CN207060413U CN201720851797.5U CN201720851797U CN207060413U CN 207060413 U CN207060413 U CN 207060413U CN 201720851797 U CN201720851797 U CN 201720851797U CN 207060413 U CN207060413 U CN 207060413U
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- unmanned plane
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Abstract
Taken photo by plane unmanned plane the utility model discloses one kind, solve unmanned plane to break down when taking photo by plane, the problem of loss is difficult to give for change, its drip irrigation device is to include frame, be fixedly installed in frame and be used to provide the electrical source of power of power, and stand-by power supply component is also installed with frame, is fixedly installed in the standby GPS transmitting chips can be positioned and launch positioning signal in frame；Also include detecting the electricity of electrical source of power with export the electric quantity detection apparatus of detection signal, be coupled to electric quantity detection apparatus and in response to detection signal with the control device of output control signal, be coupled to control device and in response to control signal to enable standby GPS transmitting chips to carry out the positioner of positioning signal transmitting, one kind of the present utility model is taken photo by plane unmanned plane, can be when flight failure causes unmanned plane to fall, it is easy to look for unmanned plane, avoids unmanned plane from losing and cause damage.
Description
Technical field
It the utility model is related to aircraft, more particularly to one kind is taken photo by plane unmanned plane.
Background technology
With the development of science and technology, aerophotography technology is gradually emerging, wherein, unmanned plane technology is due to the more manned boat of its cost
Bat is lower and safer, gradually obtains the favor of photographer.Unmanned plane work generally use aircraft carrying video camera,
The filming apparatus such as camera are shot.
But unmanned plane can be because failure or out of hand more than controlled stroke when flight is taken photo by plane, this
When generally require after unmanned plane is automatically judged according to the program of setting and make a return voyage, but the process maked a return voyage can be each by other
The judgement of mistake even occurs in the interference of kind environmental factor, the unmanned plane of failure, deviates the track of setting, with nobody
The lasting power consumption of machine can then cause the power-off of machine, and positioning signal is lost while power-off, it is difficult to looks for, is looked for user
Seek and bring certain difficulty, the space that could be improved.
Utility model content
The purpose of this utility model is to provide one kind and taken photo by plane unmanned plane, in flight failure unmanned plane can be caused to fall
When be easy to look for unmanned plane, avoid unmanned plane lose cause damage.
Above-mentioned technical purpose of the present utility model technical scheme is that：
One kind is taken photo by plane unmanned plane, including frame, is fixedly installed in and is used for the electrical source of power for providing power, the machine in frame
Stand-by power supply component is also installed with frame, is fixedly installed in frame can be positioned and launched positioning signal standby
With GPS transmitting chips；Also include being arranged in the current supply circuit of stand-by power supply component and be used to examine the electricity of electrical source of power
Survey to export the electric quantity detection apparatus of detection signal, be coupled to electric quantity detection apparatus and believed in response to detection signal with output control
Number control device, be coupled to control device and in response to control signal to enable standby GPS transmitting chips to be positioned
The positioner of signal transmitting；The electric quantity detection apparatus is set with a low battery threshold signal, when the detection signal detected
During less than low battery threshold signal, the stand-by power supply assembly power supply with cause the control device start positioner pass through it is standby
Launch positioning signal with GPS transmitting chips.
Using such scheme, by stand-by power supply component is installed and standby GPS transmitting chips can realize it is independent
Power supply and positioning, are detected by electric quantity detection apparatus to the electricity of electrical source of power so that failure fails normally to make a return voyage
Unmanned plane can be detected by electric quantity detection apparatus when cause low battery after lasting power consumption, and pass through stand-by power supply
Component, which is powered, enables standby GPS transmitting chips timely to realize positioning under control of the control means, and utilization is standby
Power supply module and standby GPS transmitting chips, work independently not by the electric energy loss of other components so that power supply continues
Time can be more permanent, also more stable in the positioning for unmanned plane, is convenient for people to look for unmanned plane.
Preferably, the control device include be used for control positioner open and close relay, in addition to be parallel to after
The fly-wheel diode of the coil of electrical equipment.
Using such scheme, the relay of control device can realize the keying control to positioner, be parallel to relay
The setting of the fly-wheel diode of the coil of device is protected to the component in circuit, avoids induced electricity of the coil in power on/off
Gesture damages driver or other elements.
Preferably, the control device, which is additionally provided with, is controlled by relay to form self-locking so that control device is persistently carried out
The latching circuit of control signal output.
Using such scheme, the latching circuit in control device is controlled by relay so that is detected in electric quantity detection apparatus
Lasting control can be realized when having arrived the situation of low battery to realize lasting location control so that the control after detection is more
Stabilization.
Preferably, the electric quantity detection apparatus is coupled in the loop of electrical source of power with to the electricity in loop including base stage
Amount detect the PNP type triode of judgement.
Using such scheme, base stage is coupled to three of the positive-negative-positive in the current supply circuit of electrical source of power in electric quantity detection apparatus
Pole pipe can be detected in the voltage x current size in the current supply circuit according to electrical source of power, and the conducting threshold of triode itself
Value realizes the conducting control to subsequent control device, only when electricity is low, the magnitude of voltage of the base stage of the triode of positive-negative-positive
Reduce and then enable triode to turn on the transmission for realizing detection signal.
Preferably, the upper surface of the frame offers the mounting groove for installing stand-by power supply component, the installation
The installation lid for being covered with and being sealed to mounting groove is hinged on groove.
Using such scheme, mounting groove that the upper surface of frame opens up is easy to the installing/dismounting of stand-by power supply component just
Victory, and the setting for the installation lid being hinged on mounting groove make it that installation is stable, firm stable during use.
Preferably, the upper surface of the installation lid is installed with the battery by opto-electronic conversion to stand-by power supply component
The solar panel of charging.
Using such scheme, installing the solar panel of the upper surface fixed installation of lid can realize opto-electronic conversion with reality
The operation that now battery of the stand-by power supply component to being installed in mounting groove is charged so that when unmanned plane is difficult to look for
Wait, the solar panel that can be covered by installing realizes the charging to reserve battery component, and then causes the standby of positioner
With GPS transmitting chips can obtain long lasting for power supply positioned, and then cause on the time for look for unmanned plane more
What is added is abundant.
Preferably, the electricity for connecting solar panel and stand-by power supply component is installed with the mounting groove
Pond is conductively connected block, and the installation covers to be installed with and is connected to solar panel and extends in mounting groove to abut
In the connector for being conductively connected block side.
Using such scheme, the connector reality for being conductively connected block and installation and covering fixed installation of fixed installation in mounting groove
It is existing affixed, and then to realize connection between solar panel and the battery of stand-by power supply component.
Preferably, the connector is the elastic metallic buckle of the side protrusion away from installation lid hinged place, it is described to lead
The side wall of electric connection block offers the neck for elastic metal buckle inlay card.
Using such scheme, connector is that elastic metallic buckle can be realized smoothly between solar panel and battery
Loop conducting, then by being engaged with the neck that mounting groove opens up on block is conductively connected, realize snapping, and then cause installation
The installation that covers of lid is stablized, firmly.
In summary, the utility model has the advantages that：
By installing stand-by power supply component and standby GPS transmitting chips in frame, it can break down what is lost
When realize unmanned plane is looked for, the setting of electric quantity detection apparatus is matched with control device and can realized to be difficult to look in unmanned plane
Seek and can be realized by electric quantity detection apparatus when main power source gradually uses up and stand-by power supply component is enabled so that be standby
GPS transmitting chips can avoid causing the waste of the electricity of stand-by power supply component while timely transmission signal.
Brief description of the drawings
Fig. 1 is the structural representation of unmanned plane；
Fig. 2 is the top view of unmanned plane；
Fig. 3 is A-A phantoms in Fig. 2；
Fig. 4 is circuit theory diagrams.
In figure：1st, frame；11st, mounting groove；2nd, stand-by power supply component；21st, installation lid；22nd, solar panel；23rd, lead
Electric connection block；231st, neck；24th, connector；3rd, electric quantity detection apparatus；4th, control device；41st, latching circuit；5th, positioner；
51st, standby GPS transmitting chips.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
One kind disclosed in the present embodiment is taken photo by plane unmanned plane, as shown in figure 1, including organic frame 1 and being arranged at the four of frame 1
It is used for the rotor for driving unmanned plane during flying on individual corner, the electrical source of power for control is then mainly installed in frame 1.And nothing
It is man-machine to be typically provided a controller gripped by operator, realize the reception and transmitting of all kinds of control signals.
As shown in Figures 2 and 3, the upper surface of frame 1 offers mounting groove 11, and fixed placement has standby electricity in mounting groove 11
Source component 2, stand-by power supply component 2 include chargeable compact battery, and installation lid 21 is covered with mounting groove 11, installation lid
21 sides are articulated with the side side wall of mounting groove 11, in opposite side by there is connector 24 to achieve a fixed connection.Lid 21 is installed
Upper surface is installed with solar panel 22, and connector 24 is fixedly connected on installation lid 21, and one end is fixedly connected on the sun
Can cell panel 22 and the other end extend to the side of mounting groove 11.In mounting groove 11 peace is fixed close to the side side wall of connector 24
Equipped with block 23 is conductively connected, connector 24 is elastic metallic buckle, and is offered on the side wall of block 23 is conductively connected for elasticity
The neck 231 of metal buckle snapping, consolidating to installation lid 21 is realized by the cooperation inlay card of elastic metallic buckle and neck 231
It is fixed, while elastic metallic buckle abuts the conducting connection realized between solar panel 22 and battery with being conductively connected block 23,
Realize that charging of the solar panel 22 to the battery of stand-by power supply component 2 is set.
As shown in figure 4, include the electric quantity detection apparatus 3 detected to the electricity of electrical source of power, be coupled to electricity inspection
Survey the control device 4 of device 3 and enable the standby positioner 5 to work to standby GPS transmitting chips 51.Electric power detection
Device 3, control device 4 and positioner 5 are powered by stand-by power supply component 2, are realized between electrical source of power only
It is vertical to separate.
Electric quantity detection apparatus 3 includes PNP type triode Q1 of the base series in the current supply circuit of electrical source of power, three poles
Manage preferred model S9012.Power drive assem is in series with the current supply circuit of electrical source of power, is being coupled at earth terminal GND
Small-sized divider resistance R1 is in series with, triode Q1 base stage is coupled between resistance R1 and the node of power drive assem, three poles
The colelctor electrode of pipe is coupled to the positive pole of the direct current supply battery of stand-by power supply component 2, and emitter stage is coupled to negative pole, works as electrical source of power
In electricity gradually consumption cause the voltage of resistance R1 partial pressures to be gradually reduced, and then cause triode Q1 base stages one end voltage
Less than conduction threshold, the low battery threshold signal that electric quantity detection apparatus 3 is set is to be controlled using triode Q1 threshold value, with electricity
The reduction of amount causes the voltage of triode Q1 base terminals to reduce, and when reaching threshold value, triode Q1 could be switched on, output inspection
Survey signal.
Control device 4 then includes the relay KM1 between the positive pole and negative pole of the battery for being series at stand-by power supply component 2
Coil, relay KM1 coils from parallel connection of coils has fly-wheel diode, and fly-wheel diode is reversal connection in the current supply circuit of control device 4
In diode D1.Control device 4 is additionally provided with the latching circuit 41 to form self-locking, and latching circuit 41 is to be coupled to triode Q1's
The normally opened contact of relay KM1 between emitter stage and colelctor electrode, when relay KM1 coil obtains electric, i.e. electric quantity detection apparatus 3
During so that the conducting of control device 4 being controlled, the normally opened contact closure of latching circuit 41 realizes self-locking so that control device 4 is protected
Lasting path and then lasting export control signal realizes control.
Positioner 5 is equally series between the positive pole and negative pole of the battery of stand-by power supply component 2, real with control device 4
Existing parallel connection, the feeder ear of standby GPS transmitting chips 51 are series between the positive pole and negative pole of the battery of stand-by power supply component 2, and
The normally opened contact for the relay KM1 coils for being controlled by control device 4 is in series with the current supply circuit of positioner 5 so that
Positioner 5 is controlled to carry out the transmitting of positioning signal during 4 path of control device.
Solar panel 22 charges to the battery of stand-by power supply component 2, the power supply inside solar panel 22
The positive and negative electrode that SP output end is respectively coupled to battery realizes charging, and solar panel 22 and stand-by power supply component 2 it
Between be in series with switch K1, switch K1 be connection sheet and connector 24 contact, circuit is realized by the connection between two contacts
Conducting.
When unmanned plane breaks down or dropped, electrical source of power consumption, electric quantity detection apparatus 3 is detected in real time, and
When the detection signal for detecting electricity is less than low battery threshold signal, control device 4, which turns on and forms self-locking, carries out lasting control
System, by the power supply of stand-by power supply component 2, positioner 5 is controlled by control device 4 so that standby GPS transmitting chips 51 are launched
Positional information realizes the reposition after unmanned plane failure, electrical source of power consumption, is easy to look for controller.
This specific embodiment is only that it is not to limitation of the present utility model, ability to explanation of the present utility model
Field technique personnel can make the modification of no creative contribution to the present embodiment as needed after this specification is read, but
As long as all protected in right of the present utility model by Patent Law.
Claims (8)
- The unmanned plane 1. one kind is taken photo by plane, including frame (1), be fixedly installed in frame (1) and be used to provide the electrical source of power of power, its It is characterized in：Stand-by power supply component (2) is also installed with the frame (1), is fixedly installed in frame (1) that can be determined Position and the standby GPS transmitting chips (51) for launching positioning signal；Also include the current supply circuit for being arranged at stand-by power supply component (2) In be used to detect to export the electric quantity detection apparatus of detection signal (3), be coupled to electric power detection the electricity of electrical source of power Device (3) and in response to detection signal with the control device (4) of output control signal, be coupled to control device (4) and in response to Control signal is to cause standby GPS transmitting chips (51) to carry out the positioner (5) of positioning signal transmitting；The electricity inspection Survey device (3) and be set with a low battery threshold signal, it is described standby when the detection signal detected is less than low battery threshold signal Powered with power supply module (2) to cause the control device (4) starts positioner (5) to pass through standby GPS transmitting chips (51) Launch positioning signal.
- 2. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：The control device (4) includes being used to control positioning The relay that device (5) opens and closes, in addition to it is parallel to the fly-wheel diode of the coil of relay.
- 3. unmanned plane according to claim 2 of taking photo by plane, it is characterized in that：The control device (4), which is additionally provided with, is controlled by relay Device is to form self-locking so that control device (4) is persistently controlled the latching circuit (41) of signal output.
- 4. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：The electric quantity detection apparatus (3) includes base stage string coupling It is connected in the loop of electrical source of power to the electricity in loop detect the PNP type triode of judgement.
- 5. unmanned plane according to claim 1 of taking photo by plane, it is characterized in that：The upper surface of the frame (1) is offered for pacifying The mounting groove (11) with power supply module (2) is equipped, be hinged be covered with seals to mounting groove (11) on the mounting groove (11) Installation lid (21).
- 6. unmanned plane according to claim 5 of taking photo by plane, it is characterized in that：The upper surface of the installation lid (21) is installed with The solar panel (22) to be charged by opto-electronic conversion to the battery of stand-by power supply component (2).
- 7. unmanned plane according to claim 6 of taking photo by plane, it is characterized in that：It is installed with the mounting groove (11) for connecting Connect the battery of solar panel (22) and stand-by power supply component (2) is conductively connected block (23), and the installation is covered solid on (21) Dingan County is equipped with to be connected to solar panel (22) and extend in mounting groove (11) is conductively connected block (23) side to be connected to Connector (24).
- 8. unmanned plane according to claim 7 of taking photo by plane, it is characterized in that：The connector (24) is to cover (21) hinge away from installation The elastic metallic buckle of the side protrusion at place is connect, the side wall for being conductively connected block (23) is offered for elastic metal buckle inlay card Neck (231).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720851797.5U CN207060413U (en) | 2017-07-13 | 2017-07-13 | One kind is taken photo by plane unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720851797.5U CN207060413U (en) | 2017-07-13 | 2017-07-13 | One kind is taken photo by plane unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207060413U true CN207060413U (en) | 2018-03-02 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720851797.5U Active CN207060413U (en) | 2017-07-13 | 2017-07-13 | One kind is taken photo by plane unmanned plane |
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| Country | Link |
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| CN (1) | CN207060413U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110621579A (en) * | 2018-03-30 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Multi-battery power supply control method and device and unmanned aerial vehicle |
| CN117465712A (en) * | 2023-12-26 | 2024-01-30 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
-
2017
- 2017-07-13 CN CN201720851797.5U patent/CN207060413U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110621579A (en) * | 2018-03-30 | 2019-12-27 | 深圳市大疆创新科技有限公司 | Multi-battery power supply control method and device and unmanned aerial vehicle |
| CN117465712A (en) * | 2023-12-26 | 2024-01-30 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
| CN117465712B (en) * | 2023-12-26 | 2024-03-15 | 成都金支点科技有限公司 | Locking structure with tongue-shaped elastic sheet for unmanned aerial vehicle, load cabin and unmanned aerial vehicle |
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