WO2017166716A1 - 飞行器 - Google Patents

飞行器 Download PDF

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Publication number
WO2017166716A1
WO2017166716A1 PCT/CN2016/097933 CN2016097933W WO2017166716A1 WO 2017166716 A1 WO2017166716 A1 WO 2017166716A1 CN 2016097933 W CN2016097933 W CN 2016097933W WO 2017166716 A1 WO2017166716 A1 WO 2017166716A1
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WO
WIPO (PCT)
Prior art keywords
light
light source
side optical
aircraft
optical fiber
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PCT/CN2016/097933
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English (en)
French (fr)
Inventor
杨震
李大龙
Original Assignee
乐视控股（北京）有限公司
乐视体育文化产业发展（北京）有限公司
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Application filed by 乐视控股（北京）有限公司, 乐视体育文化产业发展（北京）有限公司 filed Critical 乐视控股（北京）有限公司
Publication of WO2017166716A1 publication Critical patent/WO2017166716A1/zh

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/02—Arrangements or adaptations of signal or lighting devices
    • B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls

Definitions

  • Embodiments of the present application relate to the field of flight equipment technology, for example, to an aircraft.
  • the drone referred to as the "unmanned aerial vehicle" is a non-manned aircraft operated by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control devices are installed. The ground, the ship or the remote control station personnel can control the drone through radar, remote control and other equipment.
  • the drone can take off like a normal airplane under a remote control or launch it with a booster rocket. It can also be carried by the parent aircraft into the air.
  • the shape design of the drone is too simple, not cool enough, and can not satisfy the visual feeling of some consumers on the appearance of the drone.
  • the present application provides an aircraft that can solve the problem that the outer shape design of the aircraft in the prior art is too simple to improve the visual enjoyment of the user.
  • An embodiment of the present application provides an aircraft, including:
  • the illuminator is disposed on the drone, and the illuminating portion of the illuminator is exposed to the outside of the aircraft.
  • the illuminator comprises a light source and a side optical fiber, and the side optical fiber serves as a illuminating portion of the illuminant;
  • the light input end of the side optical fiber corresponds to the light source, and the side optical fiber receives light emitted by the light source through the light input end.
  • the side optical fiber is disposed on a side surface of the drone.
  • the number of the side optical fibers and the light source are equal and multiple, and the optical input ends of the plurality of side optical fibers are in one-to-one correspondence with the plurality of the light sources.
  • a plurality of the side optical fibers are sequentially arranged in parallel.
  • any two of the light sources emit different colors of light.
  • the light source is a laser light or an LED light, and the light emitted by the light source is red, green, yellow, blue or purple;
  • the light source is an LED color changing lamp.
  • it also includes:
  • control unit disposed on the drone, the output end of the control unit being electrically connected to the controlled end of the light source;
  • a signal receiving unit disposed on the drone, the output end of the signal receiving unit being electrically connected to an input end of the control unit;
  • a remote controller comprising an input unit and a signal transmitting unit, the output end of the input unit being electrically connected to an input end of the signal transmitting unit; the signal transmitting unit configured to cooperate with the signal receiving unit to The signal receiving unit transmits a signal.
  • a groove is disposed on a side surface of the drone, and the groove extends along a first trajectory on a side surface of the drone;
  • the side optical fiber is embedded in the trench along a first track.
  • the optical input end of the side optical fiber has a groove
  • the light emitting end of the light source extends into the recess.
  • the illuminant since the illuminant is disposed on the drone, the illuminating portion of the illuminator is exposed outside the aircraft, and when the illuminating portion of the illuminator emits light, the aircraft of the present invention has the effect of emitting light, which is in use. Especially at night, the aircraft is more visually cool and enhances the user's visual enjoyment.
  • the illuminating portion of the illuminator emits light, which enables the user to accurately capture the position of the aircraft through the naked eye, and facilitates the user to perform the flight trajectory of the aircraft. Control to prevent the aircraft of the present invention from colliding with other objects in the night sky.
  • FIG. 1 is a schematic structural view of an aircraft provided by an embodiment of the present application.
  • FIG. 2 is a schematic structural view of another aircraft provided by an embodiment of the present application.
  • FIG. 3 is a partial cross-sectional view showing an assembly of an edge optical fiber and a light source of an aircraft according to an embodiment of the present application;
  • FIG. 4 is a partial cross-sectional view showing a side optical fiber of an aircraft embedded in a trench of a drone according to an embodiment of the present application;
  • FIG. 5 is a structural block diagram of a remote controller and an unmanned aerial vehicle of an aircraft according to an embodiment of the present application.
  • an aircraft 10 includes a drone 1 and an illuminator 2.
  • the illuminator 2 is disposed on the drone 1 and the illuminating portion of the illuminator 2 is exposed outside the aircraft 10.
  • the above-described drone 1 is a non-manned aircraft operated by a radio remote control device and a self-contained program control device.
  • the aircraft 10 of the present application when the light-emitting portion of the illuminator 2 emits light, the aircraft 10 of the present application has an effect of illuminating, for example, when flying at night, the aircraft 10 is visually more cool, improving the visual enjoyment of the user.
  • the aircraft 10 of the present application flies at night, the illuminating portion of the illuminant 2 emits light, enabling the user to accurately capture the position of the aircraft 10 through the naked eye, facilitating the user to control the flight trajectory of the aircraft 10, and preventing the aircraft 10 of the present application from being protected. Hit other objects in the night sky.
  • the illuminant 2 includes a light source 21 and a side optical fiber. twenty two. Both the light source 21 and the side optical fiber 22 are disposed on the unmanned aerial vehicle 1, and the side optical fiber 22 is exposed as the light emitting portion of the illuminant 2 to the outside of the aircraft 10 of the present invention.
  • the side optical fiber 22 has a light input end (not shown), and the light input end of the side light fiber 22 corresponds to the light source 21, and the side light fiber 22 receives the light emitted by the light source 21 through the light input end.
  • the side optical fiber 22, also called a whole body light emitting fiber, is usually a step type polymer fiber, and the refractive index of the core material is higher than the refractive index of the skin material.
  • the core material is mostly made of transparent polymer or transparent organic matter. Since the side optical fiber 22 is mostly used in lighting and decorative decoration, in order to ensure its excellent mechanical properties and aging resistance, the leather material is usually made of a fluoroplastic such as polytetrafluoroethylene.
  • a side of the side optical fiber 22 is coated with a transparent material which is resistant to aging, ultraviolet rays and weather resistance, such as transparent polyvinyl chloride.
  • the light input end of the side optical fiber 22 corresponds to the light source 21
  • the light emitted by the light source 21 can be input into the side optical fiber 22 through the optical input end, thereby causing the side optical fiber 22 to emit light through the body.
  • the light source 21 described above may be an LED lamp or a laser lamp or the like.
  • the color of the light emitted by the light source can be common green, yellow, blue or purple.
  • the light source described above can also be an LED color change lamp that can emit an adjustable plurality of colors of light.
  • the aforementioned drone 1 has a power module (not shown), and the light source 21 is electrically connected to the power module of the drone 1 to supply the light source 21 through the power module of the drone 1 power ups.
  • the aforementioned light source 21 may also not use the power module of the drone 1 .
  • the drone 1 carries an external power source, and the light source 21 is electrically connected to the external power source to supply power to the light source 21 through the external power source.
  • the aforementioned light source 21 includes a power module and a light, and the light is a led light or a tungsten light.
  • the light is electrically connected to the power module.
  • the light source 21 is a light source having a power module and has its own power supply function.
  • the light input end of the side optical fiber 22 has a recess 221.
  • the light emitting end 211 of the light source 21 extends into the recess 221 to reduce leakage of light.
  • an end of the light source 21 opposite to the light emitting end 211 blocks the opening of the recess 221, and has the technical effect of further reducing light leakage, so that the light source 21 is provided.
  • the emitted light can all be conducted to the interior of the side optical fiber 22 via the light input end of the side optical fiber 22.
  • the aforementioned side optical fiber 22 is wound around the side surface of the drone 1 with the entire circumference of the side surface of the drone 1 being illuminated.
  • the position of the position of the side optical fiber 22 can be set according to actual needs of the user.
  • the foregoing side optical fiber 22 can be wound into different shapes as needed to perform different pattern display, for example, being circled, Round, heart shaped, etc.
  • the side surface of the unmanned aerial vehicle 1 is provided with a groove 11 on the side surface of the drone 1 Extending along the first trajectory.
  • the side optical fiber 22 is embedded in the trench 11 along the first track.
  • the side optical fiber 22 is coated with glue at a position corresponding to the groove wall of the groove 11.
  • a portion of the cylindrical surface of the side optical fiber 22 is embedded in the groove 11, and other portions protrude from the outer surface of the drone 1.
  • one half of the cylindrical surface of the side optical fiber 22 is embedded in the groove 11, and the other half protrudes from the outer surface of the drone 1.
  • the foregoing number of the side optical fibers 22 and the light source 21 are equal and multiple.
  • the light input ends of the plurality of side optical fibers 22 are in one-to-one correspondence with the plurality of light sources 21, and when the different light sources 21 emit light, the corresponding side optical fibers 22 can be caused to emit light.
  • the colors of the lights emitted by any two of the light sources 21 are different, so that the colors of the lights emitted by the plurality of side optical fibers 22 are different, and the plurality of different light colors are different.
  • the side optical fiber 22 emits light at the same time, it can give the user a more intense visual impact.
  • the colors of the light emitted by the plurality of light sources 21 may be the same, and may be set according to actual needs of the user.
  • the plurality of side optical fibers 22 may be arranged in parallel in sequence, or may be arranged in other shapes according to user requirements, and may be set according to actual needs of the user.
  • the aforementioned aircraft 10 further includes a control unit 3, a signal receiving unit 4, and a remote controller 5. Both the control unit 3 and the signal receiving unit 4 are disposed on the drone 1.
  • the output of the control unit 3 is electrically connected to the controlled end of the light source 21.
  • the output of the signal receiving unit 4 is electrically connected to the input of the control unit 3.
  • the remote controller 5 includes an input unit 51 and a signal transmitting unit 52.
  • the output of the input unit 51 is electrically connected to the input of the signal transmitting unit 52.
  • the signal transmitting unit 52 is for cooperating with the signal receiving unit 4 to transmit a signal to the signal receiving unit 4.
  • the user can input a control command through the input unit 51, and the signal transmitting unit 52 on the remote controller 5 transmits the control command to the control unit 3 through the signal receiving unit 4 on the aircraft 10.
  • the control unit 3 receives the control instruction, and sends a corresponding instruction to the controlled end of the light source 21 according to the set rule to control the light source 21, such as controlling the light source 21 to be turned on or off, or controlling The light source 21 blinks or the like.
  • control unit 3 can be a single chip microcomputer or a microprocessor.
  • the aforementioned input unit 51 may be a keyboard or a touch pad or the like.
  • the foregoing signal receiving unit 4 may be a Bluetooth module, a radio frequency module, or a WIFI module.
  • the foregoing signal sending unit 52 is also a Bluetooth module, a radio frequency module or a WIFI module.
  • the control unit 3 of the aircraft 10 may be electrically connected to the controlled ends of the plurality of light sources 21 to the plurality of light sources 21
  • the illumination state is controlled such that the aircraft 10 of the present invention has different illumination effects.
  • a part of the plurality of light sources 21 can be controlled to be constantly lit, another part of the light source 21 is blinking; or all of the light sources 21 can be controlled to be constantly lit; or all of the light sources 21 can be controlled to blink, wherein the control can be specifically performed according to the actual preference of the user.
  • the utility model is enabled.
  • the aircraft 10 has the effect of illuminating, and in use, especially at night, the aircraft 10 is visually more cool, improving the user's visual enjoyment.
  • the aircraft 10 of the embodiment of the present application flies at night, the illuminating portion of the illuminant 2 emits light, which enables the user to accurately capture the position of the aircraft 10 through the naked eye, thereby facilitating the user to control the flight trajectory of the aircraft 10, thereby preventing the utility.
  • the new aircraft 10 hits other objects in the night sky.
  • the utility model provides an aircraft, which can solve the problem that the outer shape design of the aircraft in the prior art is too simple, so as to improve the visual enjoyment of the user.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Circuit Arrangement For Electric Light Sources In General (AREA)
  • Non-Portable Lighting Devices Or Systems Thereof (AREA)

Abstract

一种飞行器（10），包括无人机（1）和发光体（2），发光体（2）设置在无人机（1）上，发光体（2）的发光部显露于飞行器（10）的外部；发光体（2）包括光源（21）和侧光光纤（22），侧光光纤（22）作为发光体（2）的发光部；以及侧光光纤（22）的光输入端与光源（21）相对应，侧光光纤（22）通过光输入端接收光源（21）发出的光。该飞行器（10）在夜间更为醒目，视觉上更加炫酷，提高了用户的视觉享受。

Description

飞行器
本申请要求在2016年3月30日提交中国专利局、申请号为2016202551319、发明名称为“飞行器”的中国专利申请的优先权，其全部内容通过引用结合在本申请中。
技术领域
本申请实施例涉及飞行设备技术领域，例如涉及一种飞行器。
背景技术
无人驾驶飞机简称“无人机”，是利用无线电遥控设备和自备的程序控制装置操纵的不载人飞机。机上无驾驶舱，但安装有自动驾驶仪、程序控制装置等设备。地面、舰艇上或母机遥控站人员可以通过雷达、遥控器等设备对该无人机进行控制。无人机可在遥控下像普通飞机一样起飞或用助推火箭发射升空，也可以由母机带到空中投放飞行。
相关技术中的无人机在实际应用过程中，发明人发现至少存在如下问题：无人机的外形设计过于简单，不够炫酷，无法满足部分消费者对无人机外形上的视觉感受。
发明内容
本申请提供一种飞行器，可以解决现有技术中飞行器的外形设计过于简单的问题，以提高用户的视觉享受。
本申请实施例提供一种飞行器，包括：
无人机；以及
发光体，设置在所述无人机上，所述发光体的发光部显露于所述飞行器的外部。
可选的，所述发光体包括光源和侧光光纤，所述侧光光纤作为所述发光体的发光部；以及
所述侧光光纤的光输入端与所述光源相对应，所述侧光光纤通过所述光输入端接收所述光源发出的光。
可选的，所述侧光光纤绕设在所述无人机的侧表面上。
可选的，所述侧光光纤和所述光源的数量相等且均为多个，多个所述侧光光纤的光输入端与多个所述光源一一对应。
可选的，多个所述侧光光纤依次平行排布。
可选的，任意两个所述光源发出的光的颜色不同。
可选的，所述光源为激光灯或LED灯，所述光源发出的光的颜色为红色、绿色、黄色、蓝色或紫色；
或，所述光源为LED变色灯。
可选的，还包括：
控制单元，设置在所述无人机上，所述控制单元的输出端与所述光源的受控端电连接；
信号接收单元，设置在所述无人机上，所述信号接收单元的输出端与所述控制单元的输入端电连接；以及
遥控器，其包括输入单元和信号发送单元，所述输入单元的输出端与所述信号发送单元的输入端电连接；所述信号发送单元用于与所述信号接收单元配合，以向所述信号接收单元发送信号。
可选的，所述无人机的侧表面上设有沟槽，所述沟槽在所述无人机的侧表面上沿第一轨迹延伸；以及
所述侧光光纤沿第一轨迹嵌设在所述沟槽内。
可选的，所述侧光光纤的光输入端具有凹槽；以及
所述光源的发光端伸入所述凹槽内。
本申请实施例的技术方案，由于在无人机上设置有发光体，发光体的发光部显露在飞行器的外部，发光体的发光部发光时，使本实用新型飞行器具有发光的效果，其在使用时尤其在夜晚，飞行器在视觉上会更加炫酷，提高了用户的视觉享受。
另外，当本实用新型的飞行器在夜晚飞行时，发光体的发光部发光，能够让用户通过肉眼准确捕捉到飞行器的位置，方便用户对飞行器的飞行轨迹进行 控制，防止本实用新型飞行器在夜空撞击到其它物体。
附图说明
一个或多个实施例通过与之对应的附图中的图片进行示例性说明，这些示例性说明并不构成对实施例的限定，附图中具有相同参考数字标号的元件表示为类似的元件，除非有特别申明，附图中的图不构成比例限制。
图1是本申请的一实施例提供的一种飞行器的结构示意图；
图2是本申请的一实施例提供的另一种飞行器的结构示意图；
图3是本申请的一实施例提供的一种飞行器的侧光光纤与光源两者组装时的部分剖面视图；
图4是本申请的一实施例提供的一种飞行器的侧光光纤嵌设在无人机的沟槽内的部分剖面视图；
图5是本申请的一实施例提供的一种飞行器的遥控器与无人机两者配合使用的结构框图。
实施方式
为使本申请实施例的目的、技术方案和优点更加清楚，下面将结合本申请实施例中的附图，对本申请实施例中的技术方案进行相关描述，显然，所描述的实施例是本申请一部分实施例，而不是全部的实施例。
如图1所示，本申请的一个实施例提出的一种飞行器10，包括无人机1和发光体2。发光体2设置在无人机1上，发光体2的发光部显露在飞行器10的外部。
上述的无人机1是利用无线电遥控设备和自备的程序控制装置操作的不载人飞机。
在上述提供的技术方案中，发光体2的发光部发光时，使本申请飞行器10具有发光的效果，例如夜晚飞行时，飞行器10在视觉上会更加炫酷，提高了用户的视觉享受。另外，当本申请的飞行器10在夜晚飞行时，发光体2的发光部发光，能够让用户通过肉眼准确捕捉到飞行器10的位置，方便用户对飞行器10的飞行轨迹进行控制，防止本申请飞行器10在夜空撞击到其它物体。
在一个可选的应用示例中，如图2所示，发光体2包括光源21和侧光光纤 22。光源21和侧光光纤22均设置在无人机1上，侧光光纤22作为前述发光体2的发光部显露在本实用新型飞行器10的外部。侧光光纤22具有光输入端(图中未标示)，侧光光纤22的光输入端与光源21相对应，侧光光纤22通过光输入端接收光源21发出的光。
侧光光纤22，也叫通体发光光纤，通常为阶跃型聚合物光纤，芯材的折射率高于皮材折射率。芯材多采用透明聚合物或透明有机物。由于侧光光纤22多用于照明、装饰装璜中，为保证其具有优异的机械性能和耐老化性能，皮材通常采用氟塑料，如聚四氟乙烯。为延长侧光光纤22的使用寿命，多在侧光光纤22外包覆一层抗老化、抗紫外线及耐候性好的透明材料，如透明聚氯乙烯。
由于侧光光纤22的光输入端与光源21相对应，使得光源21发出的光能够通过光输入端输入到侧光光纤22内，进而使侧光光纤22通体发光。
上述的光源21可以为LED灯或激光灯等。光源发出的光的颜色可以为常见的绿色、黄色、蓝色或紫色等。然而，在一个替代的实施例中，上述的光源也可以为LED变色灯，LED变色灯可以发出可调的多种颜色的光。
在一个可选的应用示例中，前述的无人机1具有电源模块(图中未标示)，光源21与无人机1的电源模块电连接，以通过无人机1的电源模块给光源21通电。
在一个替代的实施例中，前述的光源21也可以不使用无人机1的电源模块。在使用时，无人机1携带外部电源，光源21与该外部电源电连接，以通过该外部电源给光源21供电。
在另一个替代的实施例中，前述的光源21包括电源模块和发光灯，该发光灯为led灯或钨丝灯等。发光灯与电源模块电连接。在该示例中，光源21为具有电源模块的光源，自身具有供电功能。
为了提高前述光源21对侧光光纤22的光输入效率，如图3所示，前述侧光光纤22的光输入端具有凹槽221。光源21的发光端211伸入凹槽221内，以减少光线的泄露。可选的，前述光源21的发光端211伸入凹槽221后，光源21的与发光端211相背的一端封堵凹槽221的开口，带有进一步减少光线泄露的技术效果，使光源21发出的光能够全部经由侧光光纤22的光输入端传导至侧光光纤22的内部。
在一个可选的应用示例中，如图2所示，前述的侧光光纤22绕设在无人机1的侧表面上，带有使无人机1的侧表面上整圈都能发光的技术效果。
当然，前述侧光光纤22位置的设置可以根据用户的实际需求进行设置，前述的侧光光纤22可以根据需要被绕设成不同的形状，以进行不同的图案显示，比如被绕设成三角形、圆形、心形等。
为了将侧光光纤22稳定地固设到无人机1上，如图4所示，前述无人机1的侧表面上设有沟槽11，沟槽11在无人机1的侧表面上沿第一轨迹延伸。侧光光纤22沿第一轨迹嵌设在沟槽11内。为了加强稳固效果，侧光光纤22与沟槽11的槽壁相对应的位置涂覆有胶水。
在一个可选的应用示例中，如图4所示，前述侧光光纤22的圆柱面的一部分嵌设在沟槽11内，其它部分凸出于无人机1的外侧表面。比如侧光光纤22的圆柱面的一半嵌设在沟槽11内，另一半凸出无人机1的外侧表面。
可选的，如图2所示，前述的侧光光纤22和光源21的数量相等且均为多个。多个侧光光纤22的光输入端与多个光源21一一对应，不同的光源21发光时，可以使相应的侧光光纤22发光。
为了提高本申请实施例的飞行器10的炫酷效果，前述任意两个光源21发出的光的颜色不同，从而多个侧光光纤22发出的光的颜色均不相同，给多个具有不同发光颜色的侧光光纤22同时发光时，能够给予用户更为强烈的视觉冲击。当然，在一个替代的实施例中，前述多个光源21发出的光的颜色也可以相同，具体可以根据用户的实际需求设置。
在一个可选的应用示例中，如图2所示，前述多个侧光光纤22可以依次平行排布，也可以按照用户的需求排列成其它形状，可以根据用户的实际需求设置。
如图5所示，前述的飞行器10还包括控制单元3、信号接收单元4和遥控器5。控制单元3和信号接收单元4均设置在无人机1上。控制单元3的输出端与光源21的受控端电连接。信号接收单元4的输出端与控制单元3的输入端电连接。遥控器5包括输入单元51和信号发送单元52。输入单元51的输出端与信号发送单元52的输入端电连接。信号发送单元52用于与信号接收单元4配合，以向信号接收单元4发送信号。
在上述实施例中，用户可以通过输入单元51输入控制指令，遥控器5上的信号发送单元52将该控制指令通过飞行器10上的信号接收单元4发送给控制单元3。控制单元3接收到该控制指令，根据设定的规则向光源21的受控端发送相应的指令，以对光源21进行控制，比如控制光源21开启或关闭，或控制 光源21闪烁等。
这里需要说明的是：前述的控制单元3可以为单片机或微处理器等。前述的输入单元51可以为键盘或触控板等。前述的信号接收单元4可以为蓝牙模块、无线射频模块或WIFI模块等，相应的，前述的信号发送单元52也为蓝牙模块、无线射频模块或WIFI模块等。
在上述光源21和侧光光纤22的数量相等且均为多个的技术方案中，上述飞行器10的控制单元3可以与上述多个光源21的受控端电连接，以对多个光源21的发光状态进行控制，使本实用新型飞行器10具有不同的发光效果。比如可以控制多个光源21中的一部分光源21恒亮，另一部分光源21闪烁；或控制所有的光源21恒亮；或控制所有的光源21均闪烁，其中具体可以根据用户的实际喜好进行控制。
在本申请实施例提供的技术方案中，由于在无人机1上设置有发光体2，发光体2的发光部显露在飞行器10的外部，发光体2的发光部发光时，使本实用新型飞行器10具有发光的效果，其在使用时尤其在夜晚，飞行器10在视觉上会更加炫酷，提高了用户的视觉享受。另外，当本申请实施例的飞行器10在夜晚飞行时，发光体2的发光部发光，能够让用户通过肉眼准确捕捉到飞行器10的位置，方便用户对飞行器10的飞行轨迹进行控制，防止本实用新型飞行器10在夜空撞击到其它物体。
注意，上述仅为本申请的可选实施例及所运用技术原理。本领域技术人员会理解，本申请不限于这里所述的特定实施例。此外在不冲突的情况下，本申请实施例中的多种特征可以相互任意组合，组合之后的技术方案仍落入本申请的保护范围。
工业实用性
本申请实用新型提供了一种飞行器，可以解决现有技术中飞行器的外形设计过于简单的问题，以提高用户的视觉享受。

Claims (10)

  1. 一种飞行器，包括：
    无人机；以及
    发光体，设置在所述无人机上，所述发光体的发光部显露于所述飞行器的外部。
  2. 根据权利要求1所述的飞行器，其中，
    所述发光体包括光源和侧光光纤，所述侧光光纤作为所述发光体的发光部；以及
    所述侧光光纤的光输入端与所述光源相对应，所述侧光光纤通过所述光输入端接收所述光源发出的光。
  3. 根据权利要求2所述的飞行器，其中，
    所述侧光光纤绕设在所述无人机的侧表面上。
  4. 根据权利要求2所述的飞行器，其中，
    所述侧光光纤和所述光源的数量相等且均为多个，多个所述侧光光纤的光输入端与多个所述光源一一对应。
  5. 根据权利要求2-4任一项所述的飞行器，其中，
    多个所述侧光光纤依次平行排布。
  6. 根据权利要求2-4任一项所述的飞行器，其中，
    任意两个所述光源发出的光的颜色不同。
  7. 根据权利要求6所述的飞行器，其中，
    所述光源为激光灯或LED灯，所述光源发出的光的颜色为红色、绿色、黄色、蓝色或紫色；
    或，所述光源为LED变色灯。
  8. 根据权利要求2-7任一项所述的飞行器，还包括：
    控制单元，设置在所述无人机上，所述控制单元的输出端与所述光源的受控端电连接；
    信号接收单元，设置在所述无人机上，所述信号接收单元的输出端与所述控制单元的输入端电连接；以及
    遥控器，其包括输入单元和信号发送单元，所述输入单元的输出端与所述信号发送单元的输入端电连接；所述信号发送单元用于与所述信号接收单元配合，以向所述信号接收单元发送信号。
  9. 根据权利要求2-8任一项所述的飞行器，其中，
    所述无人机的侧表面上设有沟槽，所述沟槽在所述无人机的侧表面上沿第一轨迹延伸；以及
    所述侧光光纤沿第一轨迹嵌设在所述沟槽内。
  10. 根据权利要求2-9任一项所述的飞行器，其中，
    所述侧光光纤的光输入端具有凹槽；以及
    所述光源的发光端伸入所述凹槽内。
PCT/CN2016/097933 2016-03-30 2016-09-02 飞行器 WO2017166716A1 (zh)

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CN205524986U (zh) * 2016-03-30 2016-08-31 乐视控股（北京）有限公司 飞行器
CN111309047B (zh) * 2020-02-21 2020-12-22 北京京东乾石科技有限公司 无人机的控制方法、装置、设备及存储介质

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CN205060034U (zh) * 2015-10-27 2016-03-02 杨珊珊 一种便于观察的无人飞行器
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CN103616811A (zh) * 2013-11-28 2014-03-05 胡启宽 一种光纤侧光在黑暗中照射盘面周边的石英钟
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