CN212980561U - Unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle Download PDFInfo
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- CN212980561U CN212980561U CN202021320141.9U CN202021320141U CN212980561U CN 212980561 U CN212980561 U CN 212980561U CN 202021320141 U CN202021320141 U CN 202021320141U CN 212980561 U CN212980561 U CN 212980561U
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Abstract
The utility model provides an unmanned aerial vehicle light assembly and unmanned aerial vehicle, unmanned aerial vehicle light assembly include control panel, lamp plate and set up the light assembly that seafares on the lamp plate, the light assembly that seafares sets up respectively at unmanned aerial vehicle aircraft nose position or tail position at least, and the colour of setting at the light assembly that seafares of different positions is different, the control panel provides control signal for the lamp plate, set up the electronic switch who is used for receiving control signal on the lamp plate, set up the constant current module on the electronic switch control circuit, the current output end at constant current module is connected to the light assembly electricity that seafares. The utility model discloses a set up the pilot lamp in unmanned aerial vehicle's aircraft nose or tail or both wings position, perhaps a plurality of positions all set up, and different positions set up to different light colours, to controlling of unmanned aerial vehicle, orientation and position that can audio-visual instruction unmanned aerial vehicle improve unmanned aerial vehicle and control the security, reduce and control the error rate, reduce and cause the damage to unmanned aerial vehicle.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle correlation technique field, specific theory relates to an unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle.
Background
The statements in this section merely provide background information related to the present disclosure and may not necessarily constitute prior art.
Along with the development of science and technology, unmanned aerial vehicle technique is utilized in many fields, and unmanned aerial vehicle is from a new life thing of strange, more and more accepted by masses, and many people begin to learn the unmanned aerial vehicle operation, in unmanned aerial vehicle operation process, because the reason of distance or light for control personnel often can meet the problem of unable recognition unmanned aerial vehicle aircraft nose and unmanned aerial vehicle flight state, thereby appear chaotic to controlling of unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve above-mentioned problem, provided an unmanned aerial vehicle suitable for navigation lamp and unmanned aerial vehicle, set up the pilot lamp of different light colours through the both wings at aircraft nose, tail or stationary vane, realize aircraft nose, tail or unmanned aerial vehicle flight state's instruction, improve unmanned aerial vehicle's maneuverability.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an unmanned aerial vehicle light assembly that seafares, includes control panel, lamp plate and sets up the pilot lamp that seafares on the lamp plate, the pilot lamp that seafares sets up respectively at unmanned aerial vehicle aircraft nose position or tail position or/and sets up at unmanned aerial vehicle's both wings at least, and the color of the pilot lamp that seafares of setting in different positions is different, the control panel provides control signal for the lamp plate, set up the electronic switch who is used for receiving control signal on the lamp plate, set up the constant current module on the electronic switch control circuit, the pilot lamp electricity is connected at the current output of constant current module.
The utility model provides an unmanned aerial vehicle adopts foretell unmanned aerial vehicle light subassembly, the pilot lamp that seafares sets up in unmanned aerial vehicle's aircraft nose or/and tail or/and both wings department.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses a set up the pilot lamp in unmanned aerial vehicle's aircraft nose or tail or both wings position, perhaps a plurality of positions all set up, if the fixed wing aircraft can set up at the both wings, many rotor unmanned aerial vehicle can set up at aircraft nose and tail, different positions set up to different light colours, to controlling of unmanned aerial vehicle, orientation and position that can audio-visual instruction unmanned aerial vehicle, improve unmanned aerial vehicle nature controlled and control the security, reduce and control the error rate, the reduction causes the damage to unmanned aerial vehicle. The utility model discloses modular component structure, the position and the colour that set up the light of navigating can self-defined setting, have improved the flexibility of device.
Drawings
The accompanying drawings, which form a part of the specification, are provided to provide a further understanding of the invention, and are included to explain the illustrative embodiments and the description of the invention, and not to constitute a limitation of the invention.
Fig. 1 is a circuit diagram of an airworthiness lamp assembly of embodiment 1 of the present disclosure;
fig. 2 is a circuit diagram of the lamp panel of embodiment 1 of the present disclosure provided with three airworthiness indicator lamps.
The specific implementation mode is as follows:
the present invention will be further explained with reference to the accompanying drawings and examples.
It should be noted that the following detailed description is exemplary and is intended to provide further explanation of the invention. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments in accordance with the invention. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.
Example 1
In the technical solutions disclosed in one or more embodiments, as shown in fig. 1, an unmanned aerial vehicle seaworthiness lamp assembly includes a control panel, a lamp panel, and seaworthiness indicator lamps disposed on the lamp panel, wherein the seaworthiness indicator lamps are disposed at a nose position or/and a tail position of the unmanned aerial vehicle or/and disposed at two wings of the unmanned aerial vehicle, respectively, colors of the seaworthiness indicator lamps disposed at different positions are different, the control panel provides a control signal for the lamp panel, an electronic switch for receiving the control signal is disposed on the lamp panel, a constant current module is disposed on a control circuit of the electronic switch, and the seaworthiness indicator lamps are electrically connected to a current output end of the constant current module.
This embodiment sets up the airworthiness pilot lamp through aircraft nose at unmanned aerial vehicle or tail position, perhaps two positions all set up, and different positions set up to different light colours, to unmanned aerial vehicle's controlling, orientation and position that can audio-visually instruct unmanned aerial vehicle improve unmanned aerial vehicle nature controlled and control the security, reduce and control the error rate, cause the damage to unmanned aerial vehicle.
Specifically, the electronic switch of this embodiment can adopt 8205A, and 8205A is the MOS transistor, controls the on-off of LED, and the input is provided with current-limiting resistor R1, protects driver chip's control pin. The constant current module can adopt AMC7135 to keep the current constant at 350mA and provide stable input current for the indicator lamp, thereby ensuring the service life of the airworthiness indicator lamp.
In some embodiments, as shown in fig. 1, the control board includes a main control chip circuit, a mode selection circuit and an output interface circuit, the main control chip circuit is configured to send a control signal, the mode selection circuit is configured to select a set working mode, and the output interface circuit is configured to electrically connect the control board and the lamp panel and transmit the control signal to the input terminal of the electronic switch.
In this embodiment, a plurality of output interface circuits J3-J7 may be provided, and each interface circuit may independently control one lamp panel. Realizable, can set up the pilot lamp into the same colour on the same lamp plate, set up the pilot lamp on same lamp plate in unmanned aerial vehicle's same position, if can all set up arrange in unmanned aerial vehicle aircraft nose department and set up in left the place ahead, right front, top or aircraft nose below, the mode of setting up of tail department can adopt the same mode of setting up with the aircraft nose position, locate to set up a plurality of pilot lamps of seaworthiness in same position, avoid the fuselage to shelter from the pilot lamp, make operating personnel can't judge unmanned aerial vehicle's orientation.
Can set up to the pilot lamp of different colours on the same lamp plate, the pilot lamp of different colours sets up respectively in unmanned aerial vehicle's different positions, if can set up red pilot lamp at tail, green pilot lamp at the aircraft nose, two pilot lamps light simultaneously and can instruct simultaneously, and wing department can set up another kind of colour, can instruct simultaneously in a plurality of positions, improves the accuracy of instructing, improves the accuracy of controlling.
It can be realized that the airworthiness indicator lamps arranged at the output end of the electronic switch can be connected in parallel, as shown in fig. 1 and 2, two indicator lamps L1 and L2 are arranged in fig. 1, a can increase the number of indicator lamps on the lamp panel according to needs, as shown in fig. 2, three indicator lamps are L1, L2 and L3 respectively. This setting can improve the suitability of airworthiness banks spare, can be applicable to various unmanned aerial vehicles.
The main control chip circuit can adopt a single chip microcomputer, specifically, can be STC15 series single chip microcomputer, and the specific model that this embodiment adopted can be STC15W204, and this single chip microcomputer, operating voltage are: 2.4V-5.5V, and is suitable for the extreme environment of unmanned aerial vehicle work.
Specifically, the mode selection circuit may include a key and a current limiting resistor R2 connected in series, and a connection end of the key and the current limiting resistor is connected to the signal input end of the main control chip.
The working mode can be set in the memory, and the main control chip switches the working mode according to the combined signal of the keys. The working modes comprise a light normally-on working mode and a controllable working mode; the controllable working mode is that the turn-on and turn-off of the navigation lights arranged on the surface of the unmanned aerial vehicle shell are controlled according to the output signal of the control chip; the normally-on working mode may specifically be: under unmanned aerial vehicle operating condition, the light of airworthiness is in the state of lighting all the time. The mode selection circuit is arranged, so that the control flexibility of the airworthiness lamp can be improved.
Further, for improving the stability of light work that is suitable for navigation, still include power supply converting circuit and power indicator circuit, power supply converting circuit can adopt the step-down voltage module, can adopt LM-MINI360 model aeroplane and model ship step-down module, and the input voltage scope is 6-28V, is fit for the unmanned aerial vehicle of 2S-6S power, connects power supply through setting up interface circuit in this embodiment, carries out the step-down transform and obtains the power that is fit for the voltage level, if can export 5V voltage, 3A electric current, can satisfy the work needs of singlechip and light that is suitable for navigation.
The power supply indicating circuit is used for indicating whether a power supply is switched on or not, and comprises a resistor R3 and a light emitting diode D1 which are connected in series, wherein two ends of the power supply indicating circuit are respectively grounded and connected with the anode of the power supply through a current limiting resistor.
In other embodiments, for the validity that improves the light indication of seaworthiness, still include elastic connecting rod, the light indication of seaworthiness can set up on unmanned aerial vehicle through elastic connecting rod, the inside sinle silk that sets up pilot lamp and lamp plate and be connected of elastic connecting rod.
As a further improvement, the elastic connecting rod can be arranged in a telescopic structure and can be arranged in a plurality of nested sleeves.
Optionally, a base is further provided, the base can also be provided, the base is movably connected with the elastic connecting rod, and a cavity for retracting the connecting rod is arranged in the base.
The distance between the adaptive light and the unmanned aerial vehicle base body can be adjusted according to the adaptive environment by an operator. If in the environment that the surrounding objects are dense, the long elastic connecting rod can cause hanging and lapping, damage to the unmanned plane and appropriate shortening of the length of the elastic connecting rod; such as the elastic connecting rod can be properly elongated under the open environment. The flexibility of the device use is greatly improved.
Example 2
This embodiment provides an unmanned aerial vehicle, this unmanned aerial vehicle adopt embodiment 1 an unmanned aerial vehicle airworthiness banks spare, the airworthiness pilot lamp sets up in unmanned aerial vehicle's aircraft nose or/and tail or/and both wings department.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Although the present invention has been described with reference to the accompanying drawings, it is not intended to limit the scope of the present invention, and those skilled in the art should understand that various modifications or variations that can be made by those skilled in the art without inventive work are still within the scope of the present invention.
Claims (10)
1. The utility model provides an unmanned aerial vehicle light assembly that seaworthiness, characterized by: the unmanned aerial vehicle is characterized by comprising a control panel, a lamp panel and airworthiness indicating lamps arranged on the lamp panel, wherein the airworthiness indicating lamps are arranged at the head position or/and the tail position of the unmanned aerial vehicle or/and are arranged on two wings of the unmanned aerial vehicle respectively at least, colors of the airworthiness indicating lamps arranged at different positions are different, the control panel provides control signals for the lamp panel, an electronic switch used for receiving the control signals is further arranged on the lamp panel, a constant current module is arranged on an electronic switch control circuit, and the airworthiness indicating lamps are electrically connected to the current output end of the constant current module.
2. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: set up to the pilot lamp of same colour on the same lamp plate, set up the pilot lamp on the same lamp plate in unmanned aerial vehicle's same position.
3. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: set up to the pilot lamp of different colours on the same lamp plate, the pilot lamp of different colours sets up respectively in unmanned aerial vehicle's different positions.
4. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: the control panel includes main control chip circuit, mode selection circuit and output interface circuit, main control chip circuit is used for sending control signal, and mode selection circuit is used for selecting the good mode of setting for, output interface circuit is used for connecting control panel and lamp plate for the control signal transmission to electronic switch's input with main control chip circuit on the control panel.
5. The unmanned aerial vehicle airworthiness light assembly of claim 4, wherein: the output interface circuits are multiple, and each output interface circuit is connected with one lamp panel;
or the mode selection circuit comprises a key and a current-limiting resistor which are connected in series, and the connecting end of the key and the current-limiting resistor is connected with the signal input end of the main control chip circuit.
6. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: the power supply circuit can adopt a voltage reduction module.
7. The unmanned aerial vehicle airworthiness light assembly of claim 6, wherein: the power supply indicating circuit comprises a resistor and a light emitting diode which are connected in series, one end of the power supply indicating circuit is connected with the anode of the power supply, and the other end of the power supply indicating circuit is grounded.
8. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: still include elastic connecting rod, the pilot lamp passes through elastic connecting rod and sets up on unmanned aerial vehicle.
9. The unmanned aerial vehicle airworthiness light assembly of claim 1, wherein: the elastic connecting rod is of a telescopic structure which is provided with a plurality of nested sleeves;
or the base is movably connected with the elastic connecting rod, and a cavity for retracting the connecting rod is arranged in the base.
10. An unmanned aerial vehicle, characterized by: the unmanned aerial vehicle airworthiness lamp assembly of any one of claims 1-9, wherein the airworthiness indicator lamp is arranged at the nose or/and the tail or/and the wings of the unmanned aerial vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021320141.9U CN212980561U (en) | 2020-07-07 | 2020-07-07 | Unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021320141.9U CN212980561U (en) | 2020-07-07 | 2020-07-07 | Unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
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| CN212980561U true CN212980561U (en) | 2021-04-16 |
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| CN202021320141.9U Active CN212980561U (en) | 2020-07-07 | 2020-07-07 | Unmanned aerial vehicle airworthiness banks spare and unmanned aerial vehicle |
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| CN (1) | CN212980561U (en) |
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- 2020-07-07 CN CN202021320141.9U patent/CN212980561U/en active Active
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