CN114537210A - Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicle - Google Patents
Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicleDownload PDFInfo
- Publication number
- CN114537210A CN114537210ACN202210355235.7ACN202210355235ACN114537210ACN 114537210 ACN114537210 ACN 114537210ACN 202210355235 ACN202210355235 ACN 202210355235ACN 114537210 ACN114537210 ACN 114537210A
- Authority
- CN
- China
- Prior art keywords
- battery
- unmanned aerial
- aerial vehicle
- battery jar
- jar
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000009434installationMethods0.000titleclaimsdescription3
- 230000005611electricityEffects0.000claimsdescription6
- 210000001503jointAnatomy0.000claims1
- 210000000078clawAnatomy0.000abstractdescription6
- 238000013461designMethods0.000abstractdescription4
- 238000012423maintenanceMethods0.000abstractdescription4
- 238000004519manufacturing processMethods0.000abstractdescription3
- 238000000034methodMethods0.000description9
- 238000010586diagramMethods0.000description6
- 238000003032molecular dockingMethods0.000description6
- 238000010276constructionMethods0.000description2
- 238000011161developmentMethods0.000description2
- 239000000446fuelSubstances0.000description2
- 230000001681protective effectEffects0.000description2
- 230000009286beneficial effectEffects0.000description1
- 238000004891communicationMethods0.000description1
- 230000008602contractionEffects0.000description1
- 238000005516engineering processMethods0.000description1
- 238000006467substitution reactionMethods0.000description1
Images
Classifications
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/80—Exchanging energy storage elements, e.g. removable batteries
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
Description
Translated fromChinese技术领域technical field
本发明涉及无人机技术领域，尤其涉及一种无人机换电装置、换电平台及无人机。The invention relates to the technical field of unmanned aerial vehicles, in particular to a power exchange device for unmanned aerial vehicles, a power exchange platform and unmanned aerial vehicles.
背景技术Background technique
当今社会，无人机作为新兴的科技产业被应用于各个行业。尽管无人机发展的势头很大，由于所携带电池的容量有限，电量损耗较快，需要频繁的更换电池，所以，无人机续航问题在很大程度上限制了无人机的推广应用。若要促进无人机市场持久的良性发展，解决无人机的续航问题迫在眉睫。目前，主流的方式是在无人机电池更换装置上设置机械爪，通过机械爪的抓取来实现无人机电池的拆卸更换。然而，机械爪不仅在工程设计上比较复杂，造价成本高，并且安装后不易调整，维修成本高。In today's society, drones are used in various industries as an emerging technology industry. Although the development momentum of UAV is great, due to the limited capacity of the battery carried, the power consumption is fast, and the battery needs to be replaced frequently. Therefore, the problem of UAV battery life limits the promotion and application of UAV to a large extent. In order to promote the sustainable and healthy development of the UAV market, it is urgent to solve the problem of UAV battery life. At present, the mainstream method is to set a mechanical claw on the UAV battery replacement device, and realize the disassembly and replacement of the UAV battery by grasping the mechanical claw. However, the mechanical claws are not only complicated in engineering design, but also high in cost, difficult to adjust after installation, and high in maintenance costs.
发明内容SUMMARY OF THE INVENTION
有鉴于此，本发明的目的在于提供一种无人机换电装置、换电装置及无人机，用以克服了现有技术中机械爪在工程设计上比较复杂，造价和维修成本高，不易调整等技术问题。In view of this, the purpose of the present invention is to provide an unmanned aerial vehicle power exchange device, power exchange device and unmanned aerial vehicle, in order to overcome the complex engineering design of the mechanical claw in the prior art, and the high cost of construction and maintenance, Not easy to adjust and other technical problems.
为了实现上述目的，本发明实施例采用的技术方案如下：In order to achieve the above purpose, the technical solutions adopted in the embodiments of the present invention are as follows:
第一方面，提供了一种无人机换电装置，包括：滑轨、推送部、第一电池槽及第二电池槽；In a first aspect, a power exchange device for a drone is provided, including: a slide rail, a push portion, a first battery slot, and a second battery slot;
所述第一电池槽和所述第二电池槽均通过连接部与所述滑轨连接，所述第一电池槽和所述第二电池槽均用于放置无人机电池；The first battery slot and the second battery slot are both connected to the slide rail through a connecting portion, and both the first battery slot and the second battery slot are used for placing drone batteries;
所述推送部，用于沿所述滑轨滑动以在第一电池槽或第二电池槽中推送所述无人机电池。The pushing part is used for sliding along the sliding rail to push the drone battery in the first battery slot or the second battery slot.
在一种可选的实施方式中，所述推送部包括连接臂、推送块和滑块，所述推送部的一端通过所述滑块与所述滑轨滑动连接，所述推送部的另一端与所述推送块连接。In an optional implementation manner, the push portion includes a connecting arm, a push block and a slider, one end of the push portion is slidably connected to the slide rail through the slider, and the other end of the push portion is slidably connected to the slide rail. Connect with the push block.
在一种可选的实施方式中，所述连接臂包括第一连接杆和第二连接杆，所述第一连接杆与所述滑块连接，所述第二连接杆与所述推送块连接，所述第一连接杆绕所述第二连接杆旋转。In an optional implementation manner, the connecting arm includes a first connecting rod and a second connecting rod, the first connecting rod is connected with the slider, and the second connecting rod is connected with the pushing block , the first connecting rod rotates around the second connecting rod.
在一种可选的实施方式中，所述第一电池槽靠近所述第二电池槽的一端和所述第二电池槽靠近所述第一电池槽的一端均设置有斜坡。In an optional implementation manner, slopes are provided at the end of the first battery slot close to the second battery slot and the end of the second battery slot close to the first battery slot.
在一种可选的实施方式中，所述连接部包括升降架，所述升降架用于调整所述推送部在第一方向的位置，所述滑轨与所述升降架滑动连接，所述滑轨用于调整所述推送部在第二方向的位置。In an optional implementation manner, the connecting portion includes a lifting frame, and the lifting frame is used to adjust the position of the pushing portion in the first direction, the sliding rail is slidably connected to the lifting frame, and the lifting frame is slidably connected. The slide rail is used to adjust the position of the push portion in the second direction.
在一种可选的实施方式中，所述第一电池槽与所述第二电池槽一体设置，所述第一电池槽和/或所述第二电池槽配置有充电部，所述充电部用于对所述无人机电池进行充电。In an optional implementation manner, the first battery well and the second battery well are integrally provided, the first battery well and/or the second battery well are provided with a charging part, and the charging part for charging the drone battery.
第二方面，提供一种换电平台，所述换电平台包括底座以及所述提供的无人机换电装置，所述无人机换电装置设置于所述底座，所述底座开设有换电口，所述换电口位于第一电池槽与第二电池槽之间。In a second aspect, a power exchange platform is provided, the power exchange platform includes a base and the provided UAV power exchange device, the UAV power exchange device is arranged on the base, and the base is provided with a power exchange device. The power port is located between the first battery slot and the second battery slot.
在一种可选的实施方式中，所述换电平台的底部设置有第一轨道，所述第一轨道位于所述换电口的两侧，所述第一轨道与所述第一电池槽、所述第二电池槽均构成异面垂直，所述第一轨道用于对接无人机。In an optional implementation manner, the bottom of the power exchange platform is provided with first rails, the first rails are located on both sides of the power exchange port, and the first rails are connected to the first battery slot. , The second battery slots are all formed in different planes and vertical, and the first track is used for docking the drone.
第三方面，提供一种无人机，所述无人机包括电池仓，所述电池仓内部设置弹性部件，所述弹性部件用于将电池自动弹出。In a third aspect, an unmanned aerial vehicle is provided, the unmanned aerial vehicle includes a battery compartment, and an elastic component is arranged inside the battery compartment, and the elastic component is used to automatically eject the battery.
在一种可选的实施方式中，所述电池仓顶部的两侧设置有第二轨道，所述第二轨道用于与无人机换电平台的第一轨道进行对接。In an optional implementation manner, second rails are provided on both sides of the top of the battery compartment, and the second rails are used for docking with the first rails of the UAV power exchange platform.
与现有技术相比，本发明的有益效果：Compared with the prior art, the beneficial effects of the present invention:
本发明实施例的一种无人机换电装置、换电平台及无人机，该换电装置包括：滑轨、推送部、第一电池槽及第二电池槽；第一电池槽和第二电池槽均用于放置无人机电池；推送部用于沿滑轨滑动以将无人机旧电池推送至第一电池槽或第二电池槽中，并将第一电池槽或第二电池槽中的新电池推送至无人机中，以此完成无人机的新旧电池更换过程。解决了现有技术中无人机换电装置使用的机械爪结构复杂，高价成本高，操作繁琐等问题，本装置结构简单、轻便，更易安装调整，在减少了繁琐的结构设计的同时，还有效的降低了制作和维修成本。A UAV power exchange device, a power exchange platform and a drone according to an embodiment of the present invention, the power exchange device includes: a slide rail, a push portion, a first battery slot and a second battery slot; the first battery slot and the first battery slot The two battery slots are both used to place the drone battery; the push part is used to slide along the slide rail to push the old drone battery into the first battery slot or the second battery slot, and the first battery slot or the second battery slot. The new battery in the slot is pushed into the drone, thus completing the process of replacing the old and new battery of the drone. It solves the problems of complex structure, high price, high cost, and complicated operation of the mechanical claw used in the UAV power exchange device in the prior art. The device has a simple and lightweight structure, and is easier to install and adjust. Effectively reduce production and maintenance costs.
附图说明Description of drawings
为了更清楚地说明本发明的技术方案，下面将对实施例中所需要使用的附图作简单地介绍，应当理解，以下附图仅示出了本发明的某些实施例，因此不应被看作是对本发明保护范围的限定。在各个附图中，类似的构成部分采用类似的编号。In order to illustrate the technical solutions of the present invention more clearly, the accompanying drawings required in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of the present invention, and therefore should not be It is regarded as the limitation of the protection scope of the present invention. In the various figures, similar components are numbered similarly.
图1示出了本发明实施例提供的一种换电装置的结构示意图；FIG. 1 shows a schematic structural diagram of a power exchange device provided by an embodiment of the present invention;
图2示出了本发明实施例提供的一种换电装置的正视图；FIG. 2 shows a front view of a power exchange device provided by an embodiment of the present invention;
图3示出了本发明实施例提供的另一种换电装置的结构示意图；FIG. 3 shows a schematic structural diagram of another power exchange device provided by an embodiment of the present invention;
图4示出了本发明实施例提供的一种换电过程的示意图；FIG. 4 shows a schematic diagram of a power exchange process provided by an embodiment of the present invention;
图5示出了本发明实施例提供的一种换电平台的结构示意图；FIG. 5 shows a schematic structural diagram of a power exchange platform provided by an embodiment of the present invention;
图6示出了本发明实施例提供的一种换电平台的正视图；6 shows a front view of a power exchange platform provided by an embodiment of the present invention;
图7示出了本发明实施例提供的一种换电平台的侧视图；7 shows a side view of a power exchange platform provided by an embodiment of the present invention;
图8示出了本发明实施例提供的一种无人机的结构示意图；8 shows a schematic structural diagram of an unmanned aerial vehicle provided by an embodiment of the present invention;
图9示出了本发明实施例提供的一种无人机中电池仓的结构示意图；FIG. 9 shows a schematic structural diagram of a battery compartment in an unmanned aerial vehicle provided by an embodiment of the present invention;
图10示出了本发明实施例提供的一种无人机中电池仓的透视图。FIG. 10 shows a perspective view of a battery compartment in an unmanned aerial vehicle provided by an embodiment of the present invention.
主要元件符号说明：Description of main component symbols:
1-无人机换电装置；11-滑轨；12-推送部；13-第一电池槽；14-第二电池槽；1-UAV power exchange device; 11-Slide rail; 12-Pushing part; 13-First battery slot; 14-Second battery slot;
121-连接臂；122-推送块；123-滑块；121-connecting arm; 122-push block; 123-slider;
1211-第一连接杆；1212-第二连接杆；1211 - the first connecting rod; 1212 - the second connecting rod;
15-连接部；151-升降架；15-connecting part; 151-lifting frame;
131-充电部；131 - charging department;
2-换电平台；21-底座；22-第一轨道；2- power exchange platform; 21- base; 22- first track;
211-换电口；211 - power change port;
3-无人机；31-电池仓；3-UAV; 31-Battery compartment;
311-弹性部件；312-第二轨道；313-电池仓门。311-elastic part; 312-second rail; 313-battery compartment door.
具体实施方式Detailed ways
下面将结合本发明实施例中附图，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。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, but not all of the embodiments.
通常在此处附图中描述和示出的本发明实施例的组件可以以各种不同的配置来布置和设计。因此，以下对在附图中提供的本发明的实施例的详细描述并非旨在限制要求保护的本发明的范围，而是仅仅表示本发明的选定实施例。基于本发明的实施例，本领域技术人员在没有做出创造性劳动的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 components of the embodiments of the invention generally described and illustrated in the drawings herein may be arranged and designed in a variety of different configurations. Thus, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the invention as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative work fall within the protection scope of the present invention.
在下文中，可在本发明的各种实施例中使用的术语“包括”、“具有”及其同源词仅意在表示特定特征、数字、步骤、操作、元件、组件或前述项的组合，并且不应被理解为首先排除一个或更多个其它特征、数字、步骤、操作、元件、组件或前述项的组合的存在或增加一个或更多个特征、数字、步骤、操作、元件、组件或前述项的组合的可能性。Hereinafter, the terms "comprising", "having" and their cognates, which may be used in various embodiments of the present invention, are only intended to denote particular features, numbers, steps, operations, elements, components, or combinations of the foregoing, and should not be construed as first excluding the presence or addition of one or more other features, numbers, steps, operations, elements, components or combinations of the foregoing or the possibility of a combination of the foregoing.
在本发明的描述中，需要说明的是，术语“中心”、“上”、“下”、“左”、“右”、“竖直”、“水平”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系，仅是为了便于描述本发明和简化描述，而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作，因此不能理解为对本发明的限制。此外，术语“第一”、“第二”、“第三”仅用于描述目的，而不能理解为指示或暗示相对重要性。In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the indicated device or element must have a specific orientation or a specific orientation. construction and operation, and therefore should not be construed as limiting the invention. Furthermore, the terms "first", "second", and "third" are used for descriptive purposes only and should not be construed to indicate or imply relative importance.
在本发明的描述中，需要说明的是，除非另有明确的规定和限定，术语“安装”、“相连”、“连接”应做广义理解，例如，可以是固定连接，也可以是可拆卸连接，或一体地连接；可以是机械连接，也可以是电连接；可以是直接相连，也可以通过中间媒介间接相连，可以是两个元件内部的连通。对于本领域的普通技术人员而言，可以具体情况理解上述术语在本发明中的具体含义。In the description of the present invention, it should be noted that the terms "installed", "connected" and "connected" should be understood in a broad sense, unless otherwise expressly specified and limited, for example, it may be a fixed connection or a detachable connection Connection, or integral connection; can be mechanical connection, can also be electrical connection; can be directly connected, can also be indirectly connected through an intermediate medium, can be internal communication between two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood in specific situations.
除非另有限定，否则在这里使用的所有术语(包括技术术语和科学术语)具有与本发明的各种实施例所属领域普通技术人员通常理解的含义相同的含义。所述术语(诸如在一般使用的词典中限定的术语)将被解释为具有与在相关技术领域中的语境含义相同的含义并且将不被解释为具有理想化的含义或过于正式的含义，除非在本发明的各种实施例中被清楚地限定。Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which various embodiments of this invention belong. The terms (such as those defined in commonly used dictionaries) will be interpreted as having the same meaning as the contextual meaning in the relevant technical field and will not be interpreted as having an idealized or overly formal meaning, unless explicitly defined in the various embodiments of the present invention.
下面结合附图并通过具体实施方式来进一步说明本发明的技术方案。The technical solutions of the present invention are further described below with reference to the accompanying drawings and through specific embodiments.
实施例1Example 1
请参照图1和图2，本实施例提出一种无人机换电装置1，包括：滑轨11、推送部12、第一电池槽13及第二电池槽14；Please refer to FIGS. 1 and 2 , the present embodiment provides a
第一电池槽13和第二电池槽14均通过连接部15与滑轨11连接，第一电池槽13和第二电池槽14均用于放置无人机电池；The
推送部12用于沿滑轨11滑动，以在第一电池槽13或第二电池槽14中推送无人机电池。The pushing
本申请实施例提供的一种无人机换电装置1，通过推送部12来实现无人机电池的推进推出，简化了繁琐的结构设计，可见，该无人机换电装置1结构简单、轻便，更易安装调整，有效的降低了制作成本。The UAV
在本发明实施例中，第一电池槽13靠近第二电池槽14和第二电池槽14靠近第一电池槽13的一端设置有斜坡，便于推送部12在推送第一电池槽13或第二电池槽14中电池的过程中，更加省力且快捷，提高了换电效率。可选地，斜坡与电池槽底部的夹角为30°-45°。In the embodiment of the present invention, slopes are provided at one end of the
请参照图3，在本发明的另一实施例中，第一电池槽13和第二电池槽14一体设置，第一电池槽13和/或第二电池槽14设置有充电部131，充电部131用于对无人机电池进行充电。Referring to FIG. 3 , in another embodiment of the present invention, the
在本发明实施例中，充电部131位于第一电池槽13和/或第二电池槽14的槽内，将电池推到与充电部131对应的位置，以使充电部131对电池充电。In the embodiment of the present invention, the charging
在本发明实施例中，推送部12包括连接臂121、推送块122和滑块123，推送部12的一端通过滑块123与滑轨11滑动连接，推送部12的另一端与推送块122连接。In the embodiment of the present invention, the
进一步地，推送部12的一端通过滑块123与滑轨11滑动连接，通过滑块123的在滑轨11上滑动，实现带动连接臂121在滑轨11上滑动，连接臂121也可以绕滑块123旋转，推送块122也可以绕连接臂121进行旋转，从而更加准确地调整推送块122的位置；Further, one end of the
在本发明实施例中，连接臂121包括第一连接杆1211和第二连接杆1212，第一连接杆1211与滑块123连接，第二连接杆1212与推送块122连接，第一连接杆1211绕第二连接杆1212旋转，以使连接臂121更加灵活。In the embodiment of the present invention, the connecting
进一步地，第一连接杆1211也可以绕滑块123旋转，以使在推送电池过程中推送部12能够调整到最佳推送电池的位置。Further, the first connecting
在本发明实施例中，连接部15包括升降架151，升降架151用于调整推送部12在第一方向的位置，滑轨11与升降架151滑动连接，用于调整推送部12在第二方向的位置。In the embodiment of the present invention, the connecting portion 15 includes a
进一步地，升降架151位于在第一电池槽13远离第二电池槽14和第二电池槽14远离第一电池槽13两端的上方，通过升降架151的伸缩来改变滑轨11的高度，从而调整推送部12的高度位置，从而实现将电池压入无人机内，提高了空间利用率，节约了成本。Further, the
进一步地，升降架151位于滑轨11两端的下方，并且升降架151还能在滑轨11上进水平移动，从而能够调整推送部12的水平位置。Further, the
请参照图4，当无人机进行换电时，无人机换电装置1通过连接臂121绕滑块123旋转，推送块122绕连接臂121进行旋转，调整推送部12的位置，同时推送部12在滑块123的带动下沿着滑轨11滑到无人机电池的旁侧，滑块123左移，带动推送部12同时向左移动，将无人机电池推进第一电池槽内。升降架151上升，滑块123右移，带动推送部12滑到第一电池槽13中新电池的旁侧，升降架151下降，同时滑块123向左滑动，并带动推送部12向左移动，将第一电池槽13中的新电池推进无人机，以此，完成了无人机的换电过程。Please refer to FIG. 4 , when the UAV is changing power, the UAV
实施例2Example 2
请参照图5、图6和图7，本发明实施例2提供一种换电平台2，包括底座21以及实施例1的无人机换电装置1，无人机换电装置1设置于底座21上，底座21开设有换电口211，换电口211位于第一电池槽13与第二电池槽14之间。Please refer to FIG. 5 , FIG. 6 and FIG. 7 ,
在本发明实施例中，电池从无人机弹出后，电池位于换电口211处，换电口211除了用于让电池从换电平台2上通过，还起到了对位的作用。In the embodiment of the present invention, after the battery is ejected from the drone, the battery is located at the
进一步地，换电口211可以设置磁吸定位设备，用于扩大无人机的定位范围，保证了无人机与换电口211进行精准对接。Further, the
请参照图6和图7，在本发明实施例中，换电平台2的底部设置有第一轨道22，第一轨道22位于换电口211的两侧，第一轨道22与第一电池槽13、第二电池槽14均构成异面垂直，第一轨道22用于对接无人机，并当无人机对接成功处于预设位置时能够固定无人机。6 and 7, in the embodiment of the present invention, the bottom of the
在本发明实施例中，换电平台2上还可以配置多个无人机换电装置1，对应配置相应数量的换电口211，便能够实现同时对多台无人机进行换电操作。In the embodiment of the present invention, a plurality of UAV
在本发明实施例中，为保证无人机换电装置1适时启动，换电平台2还装载有燃油，通过燃油转化为电力来为无人机换电装置1提供动力。In the embodiment of the present invention, in order to ensure that the drone
实施例3Example 3
请参照图8、图9和图10，本发明实施例3提供一种无人机3，该无人机3包括电池仓31，电池仓31位于无人机的顶部，在电池仓31的内部设置有弹性部件311，所述弹性部件311用于将电池自动弹出。8 , 9 and 10 ,
可以理解的是，电池仓31还设置有电池仓门313，电池仓31内设置有电池时，电池夹设于电池仓门313与弹性部件311之间。It can be understood that the
在本发明实施例中，当无人机3与第一轨道22完成对接到达预设位置并固定时，电池仓门313打开，借助弹性部件311的弹力，实现电池的自动弹出。In the embodiment of the present invention, when the
示范性地，上述弹性部件311可以是弹簧，在电池仓31内部中，将有预设数量的弹簧设置在电池的下方，通过计算设置弹簧的型变量长度、型变量系数从而控制弹力的大小，实现电池弹起并快速达到平衡状态。可选地，所述预设数量为四个。可以理解的是，弹簧的数量可以根据实际需求设置，本发明实施例对此不作限定。Exemplarily, the above-mentioned
在本发明实施例中，电池仓31顶部的两侧设置有第二轨道312，第二轨道312从电池仓31顶部两侧延伸，第二轨道312长度可以和电池仓31仓身等长，用于实现与换电平台2的第一轨道22进行对接。In the embodiment of the present invention,
进一步地，在第二轨道312之间还设置有保护装置，在电池弹起过程中起防护作用。Further, a protection device is also provided between the
示范性地，上述的保护装置可以是约为电池高度一半的挡板，前后挡板不影响无人机与换电平台2的对接，并能够防止电池在弹起过程中滑落。Exemplarily, the above-mentioned protective device may be a baffle with a height of about half of the battery, the front and rear baffles do not affect the docking of the drone with the
在无人机更换电池的过程中，无人机电池仓31的第二轨道312与换电平台2的第一轨道22进行对接，当第二轨道312到达预设位置时，将并第二轨道312固定在第一轨道22上，实现无人机与换电平台的位置对齐，此时，电池仓门313打开，弹性部件311将电池弹出。During the battery replacement process of the drone, the
以上所述，仅为本发明的具体实施方式，但本发明的保护范围并不局限于此，任何熟悉本技术领域的技术人员在本发明揭露的技术范围内，可轻易想到变化或替换，都应涵盖在本发明的保护范围之内。The above are only specific embodiments of the present invention, but the protection scope of the present invention is not limited to this. Any person skilled in the art can easily think of changes or substitutions within the technical scope disclosed by the present invention. should be included within the protection scope of the present invention.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210355235.7ACN114537210B (en) | 2022-04-06 | 2022-04-06 | Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210355235.7ACN114537210B (en) | 2022-04-06 | 2022-04-06 | Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN114537210Atrue CN114537210A (en) | 2022-05-27 |
| CN114537210B CN114537210B (en) | 2024-01-19 |
Family
ID=81666576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210355235.7AActiveCN114537210B (en) | 2022-04-06 | 2022-04-06 | Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114537210B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115185213A (en)* | 2022-06-28 | 2022-10-14 | 广东国地规划科技股份有限公司 | Unmanned aerial vehicle battery replacement control method, device and system |
Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170129352A1 (en)* | 2014-07-31 | 2017-05-11 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle dock and battery replacement device thereof |
| US20170129464A1 (en)* | 2014-07-31 | 2017-05-11 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle base station system and method |
| US20170334581A1 (en)* | 2016-05-20 | 2017-11-23 | Michael White | Aerial Vehicle Refueling System incorporating a Universal Refueling Interface |
| JP2018100088A (en)* | 2018-02-02 | 2018-06-28 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Method of supplying energy to uav, and uav |
| CN208149603U (en)* | 2018-04-19 | 2018-11-27 | 南通科技职业学院 | A kind of plant protection drone |
| US20200017342A1 (en)* | 2018-07-11 | 2020-01-16 | Nio Nextev Limited | Conveying device and battery swap station |
| CN111891374A (en)* | 2020-07-30 | 2020-11-06 | 上海海洋大学 | A kind of unmanned aerial vehicle field endurance system and method thereof |
| WO2020239034A1 (en)* | 2019-05-28 | 2020-12-03 | 深圳市道通智能航空技术有限公司 | Battery management method, battery management apparatus and aircraft |
| CN112208775A (en)* | 2020-10-22 | 2021-01-12 | 台州汇金国际贸易有限公司 | Unmanned plane |
| CN112874776A (en)* | 2021-04-12 | 2021-06-01 | 西华大学 | Unmanned aerial vehicle platform and unmanned aerial vehicle group |
| CN213861926U (en)* | 2020-12-08 | 2021-08-03 | 泰昌科技(杭州)有限公司 | Unmanned aerial vehicle is with arm that can realize quick replacement battery |
| CN113212235A (en)* | 2021-06-11 | 2021-08-06 | 西安冰果智能航空科技有限公司 | Arm that unmanned aerial vehicle changed battery usefulness |
| CN113492716A (en)* | 2020-04-03 | 2021-10-12 | 奥动新能源汽车科技有限公司 | Battery replacing equipment, battery replacing station and battery replacing method |
| CN113548192A (en)* | 2021-08-31 | 2021-10-26 | 浙江工业大学 | A device that is used for many rotor unmanned aerial vehicle auto-control handling goods and trades electric unmanned station |
| CN215245598U (en)* | 2021-08-11 | 2021-12-21 | 西华大学 | A UAV charging platform and UAV group |
| CN113815879A (en)* | 2021-11-04 | 2021-12-21 | 广东电网有限责任公司 | Unmanned aerial vehicle battery replacing device |
| US20210408632A1 (en)* | 2020-06-29 | 2021-12-30 | Coretronic Intelligent Robotics Corporation | Battery replacement mechanism, battery replacement system, and battery replacement method |
| CN113859041A (en)* | 2021-10-27 | 2021-12-31 | 中苏科技股份有限公司 | Unmanned aerial vehicle battery replacing system and method |
| CN216186134U (en)* | 2021-09-16 | 2022-04-05 | 星逻人工智能技术(上海)有限公司 | Unmanned aerial vehicle fills and trades motor storehouse |
- 2022
- 2022-04-06CNCN202210355235.7Apatent/CN114537210B/enactiveActive
Patent Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170129464A1 (en)* | 2014-07-31 | 2017-05-11 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle base station system and method |
| US20170129352A1 (en)* | 2014-07-31 | 2017-05-11 | SZ DJI Technology Co., Ltd. | Unmanned aerial vehicle dock and battery replacement device thereof |
| US20170334581A1 (en)* | 2016-05-20 | 2017-11-23 | Michael White | Aerial Vehicle Refueling System incorporating a Universal Refueling Interface |
| JP2018100088A (en)* | 2018-02-02 | 2018-06-28 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Method of supplying energy to uav, and uav |
| CN208149603U (en)* | 2018-04-19 | 2018-11-27 | 南通科技职业学院 | A kind of plant protection drone |
| US20200017342A1 (en)* | 2018-07-11 | 2020-01-16 | Nio Nextev Limited | Conveying device and battery swap station |
| WO2020239034A1 (en)* | 2019-05-28 | 2020-12-03 | 深圳市道通智能航空技术有限公司 | Battery management method, battery management apparatus and aircraft |
| CN113492716A (en)* | 2020-04-03 | 2021-10-12 | 奥动新能源汽车科技有限公司 | Battery replacing equipment, battery replacing station and battery replacing method |
| US20210408632A1 (en)* | 2020-06-29 | 2021-12-30 | Coretronic Intelligent Robotics Corporation | Battery replacement mechanism, battery replacement system, and battery replacement method |
| CN111891374A (en)* | 2020-07-30 | 2020-11-06 | 上海海洋大学 | A kind of unmanned aerial vehicle field endurance system and method thereof |
| CN112208775A (en)* | 2020-10-22 | 2021-01-12 | 台州汇金国际贸易有限公司 | Unmanned plane |
| CN213861926U (en)* | 2020-12-08 | 2021-08-03 | 泰昌科技(杭州)有限公司 | Unmanned aerial vehicle is with arm that can realize quick replacement battery |
| CN112874776A (en)* | 2021-04-12 | 2021-06-01 | 西华大学 | Unmanned aerial vehicle platform and unmanned aerial vehicle group |
| CN113212235A (en)* | 2021-06-11 | 2021-08-06 | 西安冰果智能航空科技有限公司 | Arm that unmanned aerial vehicle changed battery usefulness |
| CN215245598U (en)* | 2021-08-11 | 2021-12-21 | 西华大学 | A UAV charging platform and UAV group |
| CN113548192A (en)* | 2021-08-31 | 2021-10-26 | 浙江工业大学 | A device that is used for many rotor unmanned aerial vehicle auto-control handling goods and trades electric unmanned station |
| CN216186134U (en)* | 2021-09-16 | 2022-04-05 | 星逻人工智能技术(上海)有限公司 | Unmanned aerial vehicle fills and trades motor storehouse |
| CN113859041A (en)* | 2021-10-27 | 2021-12-31 | 中苏科技股份有限公司 | Unmanned aerial vehicle battery replacing system and method |
| CN113815879A (en)* | 2021-11-04 | 2021-12-21 | 广东电网有限责任公司 | Unmanned aerial vehicle battery replacing device |
Non-Patent Citations (5)
| Title |
|---|
| 康张琦: "三维机器人主动嗅觉仿真平台设计", 中国优秀硕士学位论文全文数据库 (信息科技辑), pages 140 - 314* |
| 张帆等: "基于5G输电线路无人机多源定位的智慧换电平台", 通信电源技术, pages 224 - 226* |
| 王博等: "任务管理计算机电池盒结构的设计与实现", 通信电源技术, vol. 35, no. 4, pages 116 - 120* |
| 程怀俊等: "基于视觉感受野的无人机目标检测", 现代计算机, pages 108 - 111* |
| 韩航迪等: "基于视觉自动换电池无人机自主着陆方法研究", 机械制造与自动化, pages 153 - 155* |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115185213A (en)* | 2022-06-28 | 2022-10-14 | 广东国地规划科技股份有限公司 | Unmanned aerial vehicle battery replacement control method, device and system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN114537210B (en) | 2024-01-19 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104425838B (en) | It is horizontal to stack the battery with prism case at a high speed | |
| CN107503531B (en) | Container battery replacement station and installation method thereof | |
| CN109515395B (en) | Swap actuator | |
| CN110893790B (en) | Electric vehicle automatic charging and replacing system and electric vehicle automatic charging and replacing method | |
| CN109094809B (en) | Electromagnetic launch slide for fixed-wing unmanned aerial vehicle launch and launch method thereof | |
| CN110696782A (en) | Power conversion device with floating function | |
| US20240413379A1 (en) | Cell module stacking device and cell module stacking method | |
| CN113492698B (en) | Charging devices, charging assemblies and battery swap stations | |
| CN219904312U (en) | Battery replacement device and battery replacement station | |
| WO2023024375A1 (en) | Battery charging and swapping station | |
| CN217808524U (en) | Trade lifting device and trade power station of power station | |
| CN114537210A (en) | Unmanned aerial vehicle trades electric installation, trades electric platform and unmanned aerial vehicle | |
| CN116374590A (en) | Circulation conveying device and cell coating production system | |
| CN113635810A (en) | High-modularization combined battery replacing station | |
| CN209526250U (en) | Push-pull structure, battery carrier and electric charging station | |
| CN108791226B (en) | Transporter docking device, battery exchange transporter and docking method | |
| CN116352337A (en) | Positioning device and welding equipment | |
| CN220220694U (en) | A power exchange system | |
| CN117864728A (en) | A transmission device for electric traction used for automatic control | |
| CN118343333A (en) | Vehicle-mounted unmanned aerial vehicle's shut down platform, vehicle-mounted unmanned aerial vehicle cabin and vehicle | |
| CN220009717U (en) | Battery tray mechanism and battery replacing device | |
| CN216915593U (en) | Power conversion station | |
| CN114619914B (en) | Mechanical unlocking mechanism, battery pack power conversion device and power conversion station | |
| CN112311026B (en) | Battery charging mechanism | |
| CN115489384A (en) | battery replacement device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |