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CN111301679A - Platform type unmanned aerial vehicle working system - Google Patents

Platform type unmanned aerial vehicle working system Download PDF

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Publication number
CN111301679A
CN111301679A CN202010238690.XA CN202010238690A CN111301679A CN 111301679 A CN111301679 A CN 111301679A CN 202010238690 A CN202010238690 A CN 202010238690A CN 111301679 A CN111301679 A CN 111301679A
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Prior art keywords
aerial vehicle
unmanned aerial
main body
platform
uav
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Chinese (zh)
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苑高伟
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Shandong Huayuan Cable Co ltd
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Shandong Huayuan Cable Co ltd
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Priority to CN202010238690.XA priority Critical patent/CN111301679A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/022Tethered aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/16Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F3/00Ground installations specially adapted for captive aircraft
    • B64F3/02Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls
    • B64U2201/202Remote controls using tethers for connecting to ground station

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Electric Cable Installation (AREA)

Abstract

本发明涉及无人机设备技术领域,公开了一种平台式无人机工作系统包括:无人机移动平台和无人机,移动平台的底部固定在运载设备上,移动平台上对称设置有两个起降支架、脐带缆绞盘和控制台,脐带缆顶部连接至无人机的电缆接头上;移动平台上还设有发电设备、大功率电源,脐带缆内部的电源线用于为无人机供电;光纤用于实现无人机与控制平台之间的数据通信。无人机,包括主体和机翼,机翼对称设置与主体两侧,主体内部设有无人机动力机构和控制电路板,主体底部设有用于与所述脐带缆连接的电缆接头。本发明能够配合运载设备使用,移动灵活,无人机通过脐带缆供电和通信,实时信号传输更加清晰,无人机的负载能力大,续航时间长。

Figure 202010238690

The invention relates to the technical field of unmanned aerial vehicle equipment, and discloses a platform-type unmanned aerial vehicle working system, comprising: an unmanned aerial vehicle mobile platform and an unmanned aerial vehicle. The bottom of the mobile platform is fixed on the carrying equipment, and two symmetrically arranged A take-off and landing bracket, umbilical cable winch and console, the top of the umbilical cable is connected to the cable joint of the drone; the mobile platform is also equipped with power generation equipment and high-power power supply, and the power line inside the umbilical cable is used for the drone. Power supply; optical fiber is used to realize data communication between the drone and the control platform. The drone includes a main body and wings, the wings are symmetrically arranged on both sides of the main body, the drone power mechanism and a control circuit board are arranged inside the main body, and a cable joint for connecting with the umbilical cable is arranged at the bottom of the main body. The present invention can be used with carrying equipment and is flexible in movement. The UAV is powered and communicated through the umbilical cable, the real-time signal transmission is clearer, the UAV has a large load capacity and a long battery life.

Figure 202010238690

Description

一种平台式无人机工作系统A platform type unmanned aerial vehicle working system

技术领域technical field

本发明涉及无人机及其辅助设备技术领域,特别是指一种平台式无人机工作系统。The invention relates to the technical field of unmanned aerial vehicles and their auxiliary equipment, in particular to a platform-type unmanned aerial vehicle working system.

背景技术Background technique

无人机是近年来出现的空中飞行器,它可以替代人类,在人类无法到达的区域,执行一些高空高难度的或危险的任务。UAV is an aerial vehicle that has appeared in recent years. It can replace humans and perform some high-altitude difficult or dangerous tasks in areas that humans cannot reach.

但是现有的无人机,所携带的电源容量所限,即不能长时间的在空中工作,又不能搭载大重量负载,所以执行任务能力受到一定的限制。现有技术中为解决上述问题,通过脐带缆将地面可移动设备与空中无人机进行连接,使地面可移动设备大功率电源通过脐带缆将电力源源不断地、稳定可靠地传送给无人机,使其在长时间内可以获得足够的动能。与此同时信号线组传送从地面控制台发出的信号,遥控飞行器完成各种工作;用于通讯的光电信号也通过脐带缆中的光纤高保真地得以传输,实时监控飞行环境,使悬飞的无人机安全、平稳地得以控制。However, the existing UAVs have limited power supply capacity, that is, they cannot work in the air for a long time, nor can they carry heavy loads, so the ability to perform tasks is limited to a certain extent. In order to solve the above problems in the prior art, the ground movable equipment is connected with the aerial drone through the umbilical cable, so that the high-power power supply of the ground movable equipment can continuously, stably and reliably transmit the power to the drone through the umbilical cable. , so that it can obtain sufficient kinetic energy for a long time. At the same time, the signal line group transmits the signals sent from the ground console, and the remote control aircraft completes various tasks; the photoelectric signals used for communication are also transmitted with high fidelity through the optical fiber in the umbilical cable, and the flight environment is monitored in real time. The drone is safely and smoothly controlled.

但是,地面控制台与无人机的降落点是独立的,还没有一种能够将无人机的控制、无人机起降以及脐带缆的收放控制结合为一体的平台,为无人机工作提供全面的服务,基于上述原因,研制了一种平台式无人机工作系统。However, the ground console and the landing point of the UAV are independent, and there is no platform that can integrate the control of the UAV, the take-off and landing of the UAV, and the retraction and release control of the umbilical cable. The work provides a comprehensive service, and based on the above reasons, a platform-based UAV work system has been developed.

发明内容SUMMARY OF THE INVENTION

本发明提出一种平台式无人机工作系统,将无人机的控制、起降平台和脐带缆的收放结合为一体。The invention proposes a platform-type unmanned aerial vehicle working system, which integrates the control of the unmanned aerial vehicle, the take-off and landing platform and the retraction and release of the umbilical cable.

本发明的技术方案是这样实现的:一种平台式无人机工作系统,包括:The technical scheme of the present invention is realized as follows: a platform-type unmanned aerial vehicle working system, comprising:

无人机移动平台,所述移动平台的底部通过紧定件固定在运载设备上,所述移动平台上对称设置有两个用于支撑无人机的起降支架、无人机脐带缆绞盘和无人机控制台,所述绞盘上缠绕有无人机脐带缆,所述脐带缆的顶部连接至无人机的电缆接头上;所述移动平台上还设有发电设备、市电连接端口和/或大功率电源,所述脐带缆内部设有电源线和光纤,所述发电设备、市电连接接口和/或大功率电源与所述电源线电连接,用于为无人机供电;所述光纤通过光电耦合器与所述控制台的通信端电连接,用于实现无人机与控制平台之间的数据通信。UAV mobile platform, the bottom of the mobile platform is fixed on the carrying equipment through the fastener, and two take-off and landing brackets for supporting the UAV, the UAV umbilical cable winch and the UAV umbilical cable winch are symmetrically arranged on the mobile platform UAV console, the winch is wound with UAV umbilical cable, and the top of the umbilical cable is connected to the cable joint of the UAV; the mobile platform is also provided with power generation equipment, mains connection port and /or a high-power power supply, a power cord and an optical fiber are provided inside the umbilical cable, and the power generation equipment, the mains connection interface and/or the high-power power supply are electrically connected to the power cord for supplying power to the drone; The optical fiber is electrically connected to the communication terminal of the console through a photoelectric coupler, so as to realize data communication between the drone and the control platform.

无人机,包括主体和机翼,所述机翼对称设置与所述主体两侧,所述主体内部设有无人机动力机构和控制电路板,所述主体底部设有用于与所述脐带缆连接的电缆接头。The drone includes a main body and wings, the wings are symmetrically arranged on both sides of the main body, the main body is provided with a drone power mechanism and a control circuit board, and the bottom of the main body is provided with the umbilical cord the cable gland for the cable connection.

作为优选的技术方案,所述绞盘位于两个起降支架之间且所述绞盘的高度低于所述起降支架的高度。As a preferred technical solution, the winch is located between two take-off and landing supports, and the height of the winch is lower than the height of the take-off and landing support.

作为优选的技术方案,所述绞盘与控制电机传动连接,所述控制电机驱动所述绞盘转动以收放脐带缆且精确控制所述脐带缆的收放长度。As a preferred technical solution, the winch is drivingly connected to a control motor, and the control motor drives the winch to rotate to retract the umbilical cable and precisely control the retraction and retraction length of the umbilical cable.

作为优选的技术方案,所述控制电机是步进电机或伺服电机,所述控制电机的电源端与所述发电设备、市电连接接口和/或大功率电源电连接,所述控制电机的控制端电连接至所述控制台,接收所述控制台发送的控制信号。As a preferred technical solution, the control motor is a stepping motor or a servo motor, and the power supply end of the control motor is electrically connected to the power generation equipment, the mains connection interface and/or the high-power power supply, and the control motor controls The terminal is electrically connected to the console, and receives the control signal sent by the console.

作为优选的技术方案,所述无人机的主体四周设有多个用于采集各方位图像的摄像头,以及多个用于避障的红外测距传感器;所述主体的上方还设有灭火球发射装置。As a preferred technical solution, the main body of the UAV is provided with a plurality of cameras for collecting images in various directions, and a plurality of infrared ranging sensors for obstacle avoidance; a fire extinguishing ball is also provided above the main body launcher.

作为优选的技术方案,所述无人机的机翼安装在所述主体两侧,所述机翼为可折叠机翼,所述机翼在展开状态时位于所述主体的两侧,处于折叠状态时,折叠在主体下方;所述机翼上安装有若干个涵道风扇。As a preferred technical solution, the wings of the UAV are installed on both sides of the main body, the wings are foldable wings, and the wings are located on both sides of the main body in the unfolded state, and are folded In the state, it is folded under the main body; several ducted fans are installed on the wing.

作为优选的技术方案,所述无人机控制台的顶部设有显示屏和操控面板,所述人机控制台的内部设有操控电盘,与所述光纤连接的所述光电耦合器和通信端均设置在所述操控电盘上。As a preferred technical solution, the top of the drone console is provided with a display screen and a control panel, the interior of the man-machine console is provided with a control panel, the photoelectric coupler connected with the optical fiber and the communication The terminals are all arranged on the control panel.

作为优选的技术方案,所述显示屏和操控面板是显示和输入一体的触摸屏。As a preferred technical solution, the display screen and the control panel are touch screens integrating display and input.

本发明的有益效果在于:本发明能够配合运载设备使用,可以任意场合移动,移动灵活且活动范围广,使得无人机的工作更加专业、高效和安全;无人机飞行范围受脐带缆的长度制约,实时信号传输更加清晰,操控信号更稳定,通过脐带缆供电,使无人机的负载能力更大,续航时间更长,可控性更高。The beneficial effects of the present invention are as follows: the present invention can be used with carrying equipment, can be moved in any occasion, is flexible and has a wide range of activities, so that the work of the unmanned aerial vehicle is more professional, efficient and safe; the flying range of the unmanned aerial vehicle is affected by the length of the umbilical cable The real-time signal transmission is clearer, the control signal is more stable, and the power is supplied through the umbilical cable, so that the UAV has a larger load capacity, longer battery life and higher controllability.

运载设备包括燃油汽车、电动汽车、油电混合动力汽车等自行驱动的移动车辆,也可用于船上、潜艇等有运载能力的设备。The delivery equipment includes self-propelled mobile vehicles such as fuel vehicles, electric vehicles, and gasoline-electric hybrid vehicles, and can also be used for equipment with carrying capacity such as ships and submarines.

移动平台上配有无人机飞行控制台、电源、发电机,可以向悬浮的无人机输送稳定的大功率电能,无人机脐带缆的信号传输采用单模光纤,对光信号通过光电转换部件进行传输,使控制信号不失真、稳定可靠,速度快。The mobile platform is equipped with a UAV flight console, power supply, and generator, which can deliver stable high-power electrical energy to the suspended UAV. The signal transmission of the UAV umbilical cable adopts single-mode optical fiber, and the optical signal is converted by photoelectricity. The components are transmitted, so that the control signal is undistorted, stable and reliable, and the speed is fast.

无人机搭载于运载设备上运输至工作地点,使用无人机时,脐带缆根据无人机工作范围,通过绞盘收放脐带缆控制无人机的飞行高度和范围。脐带缆的重量轻、拉力大、信号传输全部采用单模光纤,不受电磁的干扰,可以反复收放使用,工作十分可靠,紧急情况下可以通过脐带缆强行回收工作无人机。The UAV is carried on the carrier equipment and transported to the work site. When using the UAV, the umbilical cable controls the flight height and range of the UAV through the winch retracting and retracting the umbilical cable according to the working range of the UAV. The umbilical cable is light in weight, large in tension, and uses single-mode optical fiber for signal transmission, which is not subject to electromagnetic interference, and can be used repeatedly.

移动平台上载有控制台,控制台可以通过无人机上监视器实时监控飞行器周围情况,控制台通过光纤实现对无人机的指令传输。There is a console on the mobile platform, the console can monitor the situation around the aircraft in real time through the monitor on the drone, and the console can transmit instructions to the drone through optical fiber.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动性的前提下,还可以根据这些附图获得其他的附图。In order to explain the embodiments of the present invention or the technical solutions in the prior art more clearly, the following briefly introduces the accompanying drawings that need to be used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description are only These are some embodiments of the present invention, and for those of ordinary skill in the art, other drawings can also be obtained from these drawings without any creative effort.

图1为移动平台的结构示意图;Fig. 1 is the structural representation of the mobile platform;

图2为无人机的结构示意图;Figure 2 is a schematic structural diagram of an unmanned aerial vehicle;

图中,1-无人机移动平台;11-起降支架;12-绞盘;13-控制台;14-发电设备;15-大功率电源;16-触摸屏;2-无人机;21-主体;22-机翼;23-涵道风扇;24-灭火球发射装置;25-摄像头;26-红外测距传感器;3-脐带缆。In the figure, 1- UAV mobile platform; 11- take-off and landing bracket; 12- winch; 13- console; 14- power generation equipment; 15- high-power power supply; 16- touch screen; 2- drone; 21- main body ; 22-wing; 23-ducted fan; 24-fire ball launcher; 25-camera; 26-infrared ranging sensor; 3-umbilical cable.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例,对于这些实施方式的说明用于帮助理解本发明,但并不构成对本发明的限定。基于本发明中的实施例,本领域普通技术人员在没有作出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. The description of these embodiments is used to help the understanding of the present invention, but does not constitute a limitation of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

其中,在本申请实施例的描述中,除非另有说明,“/”表示或的意思,例如,A/B可以表示A或B;本文中的“和/或”仅仅是一种描述关联对象的关联关系,表示可以存在三种关系,例如,A和/或B,可以表示:单独存在A,同时存在A和B,单独存在B这三种情况。另外,在本申请实施例的描述中,“多个”是指两个或多于两个。Wherein, in the description of the embodiments of the present application, unless otherwise stated, “/” means or means, for example, A/B can mean A or B; “and/or” in this document is only a description of the associated object The association relationship of , indicates that there can be three kinds of relationships, for example, A and/or B, can indicate that A exists alone, A and B exist at the same time, and B exists alone. In addition, in the description of the embodiments of the present application, "plurality" refers to two or more than two.

以下,术语“第一”、“第二”仅用于描述目的,而不能理解为指示或暗示相对重要性或者隐含指明所指示的技术特征的数量。由此,限定有“第一”、“第二”的特征可以明示或者隐含地包括一个或者更多个该特征。在本申请实施例的描述中,除非另有说明,“多个”的含义是两个或两个以上。Hereinafter, the terms "first" and "second" are only used for descriptive purposes, and should not be construed as indicating or implying relative importance or implicitly indicating the number of indicated technical features. Thus, a feature defined as "first" or "second" may expressly or implicitly include one or more of that feature. In the description of the embodiments of the present application, unless otherwise specified, "plurality" means two or more.

如图1和图2所示,一种平台式无人机工作系统,包括无人机移动平台1和无人机2。As shown in Figure 1 and Figure 2, a platform-type UAV working system includes a UAV mobile platform 1 and an UAV 2.

移动平台1的底部通过紧定件固定在运载设备上,移动平台1上对称设置有两个用于支撑无人机的起降支架11、无人机脐带缆绞盘12和无人机控制台13,绞盘12上缠绕有无人机脐带缆3,脐带缆3的顶部连接至无人机2的电缆接头上;移动平台1上还设有发电设备14、市电连接端口(图中未示出)和大功率电源15,脐带缆3内部设有电源线和光纤,发电设备14、市电连接接口和大功率电源15与电源线电连接,用于为无人机2供电;光纤通过光电耦合器与控制台13的通信端电连接,用于实现无人机2与控制平台之间的数据通信。The bottom of the mobile platform 1 is fixed on the carrying equipment through the fasteners, and two take-off and landing brackets 11 for supporting the drone, the drone umbilical cable winch 12 and the drone console 13 are symmetrically arranged on the mobile platform 1 , the winch 12 is wound with an unmanned aerial vehicle umbilical cable 3, and the top of the umbilical cable 3 is connected to the cable joint of the unmanned aerial vehicle 2; the mobile platform 1 is also provided with a power generating device 14, a mains connection port (not shown in the figure) ) and a high-power power supply 15, the umbilical cable 3 is provided with a power supply line and an optical fiber inside, and the power generation equipment 14, the mains connection interface and the high-power power supply 15 are electrically connected with the power supply line for supplying power to the drone 2; The device is electrically connected to the communication terminal of the console 13 for realizing data communication between the UAV 2 and the control platform.

无人机2控制台13的顶部设有显示屏和操控面板,人机控制台13的内部设有操控电盘,与光纤连接的光电耦合器和通信端均设置在操控电盘上。The top of the console 13 of the UAV 2 is provided with a display screen and a control panel, and the interior of the man-machine console 13 is provided with a control panel.

优选的,显示屏和操控面板是显示和输入一体的触摸屏16。Preferably, the display screen and the control panel are a touch screen 16 that integrates display and input.

移动平台1上还有多个功能区域,用于其他工具和设备的存放。There are also several functional areas on the mobile platform 1 for the storage of other tools and equipment.

为便于无人机起降,绞盘12位于两个起降支架11之间且绞盘12的高度低于起降支架11的高度。In order to facilitate the take-off and landing of the drone, the winch 12 is located between the two take-off and landing brackets 11 and the height of the winch 12 is lower than the height of the take-off and landing bracket 11 .

绞盘12与控制电机传动连接,控制电机驱动绞盘12转动以收放脐带缆3且精确控制脐带缆3的收放长度。The winch 12 is drivingly connected with the control motor, and the control motor drives the winch 12 to rotate to retract the umbilical cable 3 and precisely control the retraction and retraction length of the umbilical cable 3 .

控制电机是步进电机或伺服电机,控制电机的电源端与发电设备14、市电连接接口和/或大功率电源15电连接,控制电机的控制端电连接至控制台13,接收控制台13发送的控制信号。The control motor is a stepper motor or a servo motor, the power supply end of the control motor is electrically connected to the power generating equipment 14, the mains connection interface and/or the high-power power supply 15, and the control end of the control motor is electrically connected to the console 13, which receives the console 13. control signal sent.

无人机2,包括主体21和机翼22,机翼22对称设置与主体21两侧,主体21内部设有无人机动力机构和控制电路板,主体21底部设有用于与脐带缆3连接的电缆接头。The drone 2 includes a main body 21 and wings 22, the wings 22 are symmetrically arranged on both sides of the main body 21, the main body 21 is provided with a power mechanism of the drone and a control circuit board, and the bottom of the main body 21 is provided with an umbilical cable 3 for connection cable connector.

无人机主体21四周设有多个用于采集各方位图像的摄像头25,以及多个用于避障的红外测距传感器26;主体21的上方还设有灭火球发射装置24。A plurality of cameras 25 for collecting images from all directions and a plurality of infrared ranging sensors 26 for obstacle avoidance are arranged around the main body 21 of the drone; a fire ball launching device 24 is also arranged above the main body 21 .

无人机2的机翼22安装在主体21两侧,机翼22为可折叠机翼22,机翼22在展开状态时位于主体21的两侧,处于折叠状态时,折叠在主体21下方;机翼22上安装有若干个涵道风扇23。The wings 22 of the drone 2 are installed on both sides of the main body 21, and the wings 22 are foldable wings 22. The wings 22 are located on both sides of the main body 21 in the unfolded state, and are folded below the main body 21 when in the folded state; Several ducted fans 23 are installed on the wing 22 .

本发明的原理和功能如下:移动平台通过运载设备运输到工作现场,本发明中尤其适用于火警救援现场。The principles and functions of the present invention are as follows: the mobile platform is transported to the work site by carrying equipment, and the present invention is especially suitable for fire rescue sites.

无人机由起降支架上起飞,通过摄像头和红外测距传感器检测火灾位置,最终飞行高度控制在接近火灾现场的位置,无人机的侧面具有多个摄像头和红外测距传感器,摄像头能够采集多方位的图像,以便于火灾现场的观察,红外测距传感器检测建筑物或其他物体的距离,避免无人机碰撞。控制台根据火灾现场的位置控制绞盘收放脐带缆,通过灭火球发射装置将灭火球投射进入火灾现象。The drone takes off from the take-off and landing bracket, detects the fire position through the camera and infrared ranging sensor, and controls the final flight height close to the fire scene. There are multiple cameras and infrared ranging sensors on the side of the drone. The camera can collect Multi-directional images to facilitate the observation of the fire scene, the infrared ranging sensor detects the distance of buildings or other objects, and avoids the collision of drones. The console controls the winch to retract the umbilical cable according to the position of the fire scene, and projects the fire ball into the fire phenomenon through the fire ball launch device.

其中绞盘收放电缆的速度和长度由控制电机控制,通过预先计算,设置电机的转速比,以控制电机转速和转动圈数,以实现精确控制电缆的收放长度。The speed and length of the winch retracting and unwinding cables are controlled by the control motor. Through pre-calculation, the speed ratio of the motor is set to control the motor speed and the number of turns, so as to accurately control the length of the cable.

本发明中,无人机和控制电机的控制,以及大功率电源和发电设备的电源转换均是现有技术。In the present invention, the control of the unmanned aerial vehicle and the control motor, and the power conversion of the high-power power supply and the power generation equipment are all in the prior art.

此外,现有技术中的摄像头等图像采集设备、测距传感器和灭火球发射装置均可应用于本发明。In addition, image acquisition devices such as cameras, ranging sensors and fire-extinguishing ball launching devices in the prior art can all be applied to the present invention.

以上仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention. within.

Claims (8)

1.一种平台式无人机工作系统,其特征在于,包括:1. a platform type unmanned aerial vehicle working system, is characterized in that, comprises: 无人机移动平台,所述移动平台的底部通过紧定件固定在运载设备上,所述移动平台上对称设置有两个用于支撑无人机的起降支架、无人机脐带缆绞盘和无人机控制台,所述绞盘上缠绕有无人机脐带缆,所述脐带缆的顶部连接至无人机的电缆接头上;所述移动平台上还设有发电设备、市电连接端口和/或大功率电源,所述脐带缆内部设有电源线和光纤,所述发电设备、市电连接接口和/或大功率电源与所述电源线电连接,用于为无人机供电;所述光纤通过光电耦合器与所述控制台的通信端电连接,用于实现无人机与控制平台之间的数据通信。UAV mobile platform, the bottom of the mobile platform is fixed on the carrying equipment through the fastener, and two take-off and landing brackets for supporting the UAV, the UAV umbilical cable winch and the UAV umbilical cable winch are symmetrically arranged on the mobile platform UAV console, the winch is wound with UAV umbilical cable, and the top of the umbilical cable is connected to the cable joint of the UAV; the mobile platform is also provided with power generation equipment, mains connection port and /or a high-power power supply, a power cord and an optical fiber are provided inside the umbilical cable, and the power generation equipment, the mains connection interface and/or the high-power power supply are electrically connected to the power cord for supplying power to the drone; The optical fiber is electrically connected to the communication terminal of the console through a photoelectric coupler, so as to realize data communication between the drone and the control platform. 无人机,包括主体和机翼,所述机翼对称设置与所述主体两侧,所述主体内部设有无人机动力机构和控制电路板,所述主体底部设有用于与所述脐带缆连接的电缆接头。The drone includes a main body and wings, the wings are symmetrically arranged on both sides of the main body, the main body is provided with a drone power mechanism and a control circuit board, and the bottom of the main body is provided with the umbilical cord the cable gland for the cable connection. 2.如权利要求1所述的一种平台式无人机工作系统,其特征在于:所述绞盘位于两个起降支架之间且所述绞盘的高度低于所述起降支架的高度。2 . The platform-type unmanned aerial vehicle working system according to claim 1 , wherein the winch is located between two take-off and landing brackets and the height of the winch is lower than the height of the take-off and landing bracket. 3 . 3.如权利要求1所述的一种平台式无人机工作系统,其特征在于:所述绞盘与控制电机传动连接,所述控制电机驱动所述绞盘转动以收放脐带缆且精确控制所述脐带缆的收放长度。3. A platform-type unmanned aerial vehicle working system according to claim 1, characterized in that: the winch is connected to a control motor in a transmission, and the control motor drives the winch to rotate to retract the umbilical cable and precisely control the umbilical cable. the retractable length of the umbilical. 4.如权利要求3所述的一种平台式无人机工作系统,其特征在于:所述控制电机是步进电机或伺服电机,所述控制电机的电源端与所述发电设备、市电连接接口和/或大功率电源电连接,所述控制电机的控制端电连接至所述控制台,接收所述控制台发送的控制信号。4. A platform-type unmanned aerial vehicle working system as claimed in claim 3, characterized in that: the control motor is a stepping motor or a servo motor, and the power supply end of the control motor is connected to the power generation equipment, the mains The connection interface and/or the high-power power supply are electrically connected, and the control end of the control motor is electrically connected to the console, and receives the control signal sent by the console. 5.如权利要求1所述的一种平台式无人机工作系统,其特征在于:所述无人机的主体四周设有多个用于采集各方位图像的摄像头,以及多个用于避障的红外测距传感器;所述主体的上方还设有灭火球发射装置。5. A platform-type unmanned aerial vehicle working system according to claim 1, characterized in that: the main body of the unmanned aerial vehicle is provided with a plurality of cameras around the main body for collecting images of various directions, and a plurality of cameras for avoiding The infrared ranging sensor of the obstacle is provided; a fire-extinguishing ball launching device is also arranged above the main body. 6.如权利要求1所述的一种平台式无人机工作系统,其特征在于:所述无人机的机翼安装在所述主体两侧,所述机翼为可折叠机翼,所述机翼在展开状态时位于所述主体的两侧,处于折叠状态时,折叠在主体下方;所述机翼上安装有若干个涵道风扇。6. A platform-type unmanned aerial vehicle working system as claimed in claim 1, characterized in that: the wings of the unmanned aerial vehicle are installed on both sides of the main body, and the wings are foldable wings, so The wings are located on both sides of the main body in the unfolded state, and are folded under the main body when in the folded state; a number of ducted fans are installed on the airfoil. 7.如权利要求1所述的一种平台式无人机工作系统,其特征在于:所述无人机控制台的顶部设有显示屏和操控面板,所述人机控制台的内部设有操控电盘,与所述光纤连接的所述光电耦合器和通信端均设置在所述操控电盘上。7. A platform-type unmanned aerial vehicle working system as claimed in claim 1, wherein the top of the unmanned aerial vehicle console is provided with a display screen and a control panel, and the interior of the man-machine console is provided with a display screen and a control panel. A control panel, the photoelectric coupler and the communication terminal connected with the optical fiber are all arranged on the control panel. 8.如权利要求7所述的一种平台式无人机工作系统,其特征在于:所述显示屏和操控面板是显示和输入一体的触摸屏。8 . The platform-type unmanned aerial vehicle working system according to claim 7 , wherein the display screen and the control panel are touch screens integrating display and input. 9 .
CN202010238690.XA 2020-03-30 2020-03-30 Platform type unmanned aerial vehicle working system Pending CN111301679A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113252689A (en) * 2021-05-14 2021-08-13 南京市特种设备安全监督检验研究院 Nondestructive testing device for large steel structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101645309B1 (en) * 2015-07-10 2016-08-04 (주)엔정보기술 Apparatus for disaster observation of knapsack type using unmanned air vehicle
CN108528753A (en) * 2018-07-09 2018-09-14 公安部上海消防研究所 A kind of captive fire-fighting Air Surveillance Platform
CN110282048A (en) * 2019-07-05 2019-09-27 中电莱斯信息系统有限公司 A kind of multi-purpose unmanned aerial vehicle acting trailer system
CN212290334U (en) * 2020-03-30 2021-01-05 山东华苑电缆有限公司 Platform type unmanned aerial vehicle working system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101645309B1 (en) * 2015-07-10 2016-08-04 (주)엔정보기술 Apparatus for disaster observation of knapsack type using unmanned air vehicle
CN108528753A (en) * 2018-07-09 2018-09-14 公安部上海消防研究所 A kind of captive fire-fighting Air Surveillance Platform
CN110282048A (en) * 2019-07-05 2019-09-27 中电莱斯信息系统有限公司 A kind of multi-purpose unmanned aerial vehicle acting trailer system
CN212290334U (en) * 2020-03-30 2021-01-05 山东华苑电缆有限公司 Platform type unmanned aerial vehicle working system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113252689A (en) * 2021-05-14 2021-08-13 南京市特种设备安全监督检验研究院 Nondestructive testing device for large steel structure

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