TWI810715B - Drone charging device - Google Patents

Drone charging device Download PDF

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TWI810715B
TWI810715B TW110143225A TW110143225A TWI810715B TW I810715 B TWI810715 B TW I810715B TW 110143225 A TW110143225 A TW 110143225A TW 110143225 A TW110143225 A TW 110143225A TW I810715 B TWI810715 B TW I810715B
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charging
units
unit
drone
charging device
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TW110143225A
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TW202321113A (en
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陳楊正光
葉崇偉
翁志遠
江志煌
翁瑞侑
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空軍航空技術學院
葉崇偉
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本發明提供一種無人機充電裝置,係組設於具複數飛行軸桿之一無人機,其主要包含有一充電支架模組及具一可撓充電導線之一電池模組,而該充電支架模組具有一主支架單元、由主支架單元凸設之複數第一次支架單元與複數第二次支架單元、設於該等第一次支架單元之複數第一結合單元及設於該等第二次支架單元另端之複數第二結合單元,而該電池模組相對該可撓充電導線之另側設有複數第三結合單元,該等第三結合單元組設於該等第二結合單元,藉此,使該無人機充電裝置組設於具複數飛行軸桿之無人機,並由該可撓充電導線對待充電之無人機進行充電。The present invention provides an unmanned aerial vehicle charging device, which is assembled on an unmanned aerial vehicle with a plurality of flying shafts, which mainly includes a charging bracket module and a battery module with a flexible charging wire, and the charging bracket module It has a main support unit, a plurality of first support units and a plurality of second support units protruding from the main support unit, a plurality of first combination units arranged on the first support units, and a plurality of first combination units arranged on the second support units. A plurality of second combination units at the other end of the bracket unit, and the battery module is provided with a plurality of third combination units on the other side of the flexible charging wire, and the third combination units are set on the second combination units, by Therefore, the UAV charging device is assembled on the UAV with multiple flying shafts, and the UAV to be charged is charged by the flexible charging wire.

Description

無人機充電裝置Drone charging device

本發明有關於一種充電裝置,尤指一種裝設於無人機之複數飛行軸桿上並用以對另一無人機進行充電之一種無人機充電裝置。The invention relates to a charging device, in particular to a charging device for an unmanned aerial vehicle installed on a plurality of flying shafts of an unmanned aerial vehicle and used for charging another unmanned aerial vehicle.

按,無人機在現在環境的應用層面非常的廣泛,包含有環境數據的檢測、特定區域的偵查與急難搜救等,特別是一些困難環境,不僅無須人員直接前往,而是派遣無人機即可獲取所需位置的即時影像資料,做為偵查與判斷的依據,如此,不僅降低人員的前往因難環境偵查時可能產生的風險因素,同時可以先利用無人機進行特定區域的偵查,縮短人員前往搜查的時間,因此,無人機對於急難搜救等行動無疑是一大利器。By the way, UAVs are widely used in the current environment, including detection of environmental data, investigation of specific areas and emergency search and rescue, etc., especially in some difficult environments, not only do not need personnel to go directly, but can be obtained by dispatching UAVs The real-time image data of the required location is used as the basis for investigation and judgment. In this way, it not only reduces the risk factors that may arise when personnel go to the difficult environment for investigation, but also can use drones to conduct investigations in specific areas first, shortening personnel to search Therefore, drones are undoubtedly a great weapon for emergency search and rescue operations.

然而,無人機雖然方便飛行至所需地點進行偵查,但由於無人機之動力來源係由電池所提供所需電力為主,因此,無人機的飛行時間係為有限,再者,有些人會改裝無人機之電池藉由電池容量的提升而延長其飛行時間,但電池容量的增加也代表者重量的增加,因此,也考驗著無人機的載重能力。是以,如何結合一充電裝置於無人機上,並使無人機可以透過一外接充電電池的方式進行充電,實為業界亟欲克服之問題。However, although the UAV is convenient to fly to the desired location for reconnaissance, since the power source of the UAV is mainly provided by the battery, the flight time of the UAV is limited. Moreover, some people will refit The drone's battery can prolong its flight time by increasing the battery capacity, but the increase in battery capacity also means an increase in weight, so it also tests the drone's load capacity. Therefore, how to combine a charging device on the drone so that the drone can be charged through an external rechargeable battery is a problem that the industry is eager to overcome.

本發明之目的,在於提供一種可結合充電裝置於無人機上,藉以提供無人機充電電源之一種無人機充電裝置。The purpose of the present invention is to provide a charging device for a drone that can be combined with a charging device on a drone to provide a charging power source for the drone.

為達上述目的,本發明提供一種無人機充電裝置,係組設於具複數飛行軸桿之一無人機,其主要包含有一充電支架模組及一電池模組,而該充電支架模組具有一主支架單元、複數第一次支架單元、複數第二次支架單元、複數第一結合單元及複數第二結合單元,其中,該等第一次支架單元與該等第二次支架單元係自該主支架單元凸設形成,而該等第一次支架單元相對該主支架單元的另端係各樞設有一該第一結合單元,該等第二次支架單元相對該主支架單元之另端各設有一該第二結合單元;該電池模組具有一控制單元、複數電池單元、一可撓充電導線及複數第三結合單元,其中,該控制單元係電性連接該等電池單元及該可撓充電導線,而該可撓充電導線設有與該控制單元電性連接之二第一磁性導片,該等第一磁性導片之磁極性彼此不同;其中,至少一該第二次支架單元設於兩該等第一次支架單元之間,且該等第三結合單元係各組設一該第二結合單元。In order to achieve the above purpose, the present invention provides a charging device for an unmanned aerial vehicle, which is assembled on an unmanned aerial vehicle with a plurality of flying shafts. It mainly includes a charging bracket module and a battery module, and the charging bracket module has a The main support unit, the plurality of first support units, the plurality of second support units, the plurality of first combination units and the plurality of second combination units, wherein, the first support units and the second support units are from the The main support unit is protrudingly formed, and the other ends of the first support units relative to the main support unit are each pivotally provided with a first coupling unit, and the other ends of the second support units relative to the main support unit are each pivoted. There is a second combination unit; the battery module has a control unit, a plurality of battery units, a flexible charging wire and a plurality of third combination units, wherein the control unit is electrically connected to the battery units and the flexible charging wire, and the flexible charging wire is provided with two first magnetic guides electrically connected to the control unit, and the magnetic polarities of the first magnetic guides are different from each other; wherein, at least one of the second support units is provided Between the two first support units, and each of the third combination units is provided with a second combination unit.

進一步地,該主支架單元並組設有一充電連接模組,該充電連接模組內設有一充電中繼單元及電性連接該充電中繼單元之二第二磁性導片,該等第二磁性導片之磁極性彼此不同。Further, the main bracket unit is also equipped with a charging connection module, and the charging connection module is provided with a charging relay unit and two second magnetic guides electrically connected to the charging relay unit, and the second magnetic The magnetic polarities of the guide pieces are different from each other.

進一步地,該充電中繼單元為一無線充電器。Further, the charging relay unit is a wireless charger.

進一步地,該充電中繼單元為一有線充電器,且該充電中繼單元並電性連接一充電連接線。Further, the charging relay unit is a wired charger, and the charging relay unit is electrically connected to a charging connection wire.

進一步地,該電池模組更設有與該控制單元電性連接之一控制按鍵、一電量指示器及一充電座。Furthermore, the battery module is further provided with a control button electrically connected to the control unit, a power indicator and a charging stand.

進一步地,該可撓充電導線一端並設有一組合罩體,該等第一磁性導片設於該組合罩體內。Furthermore, one end of the flexible charging wire is provided with a combined cover, and the first magnetic guide pieces are arranged in the combined cover.

進一步地,該等第一結合單元進一步包含有一第一扣件,該等第一扣件各具有一鋸齒部。Further, the first combining units further include a first fastener, and each of the first fasteners has a sawtooth portion.

進一步地,該等第一扣件各設有一第一鎖固件。Further, each of the first fasteners is provided with a first locking piece.

進一步地,該等第三結合單元各設有一第二鎖固件鎖設於該第二次支架單元。Further, each of the third combination units is provided with a second locking member locked to the second support unit.

本發明之一種無人機充電裝置,其具有下述優點:An unmanned aerial vehicle charging device of the present invention has the following advantages:

本發明之無人機充電裝置利用該充電支架模組而組設具複數飛行軸桿的無人機,其中,該充電支架模組可以依需求來增加該等第一次支架單元、該等第一結合單元、該等第二次支架單元及該等第二結合單元之數量,使該等第一次支架單元藉由該等第一結合單元而穩固地組設於無人機之該等飛行軸桿上,其次、再將該電池模組的該等第三結合單元再分別與該等第二次支架單元上之該等第二結合單元相組設,並依需求將該可撓充電導線彎折為所需形狀,藉此,使用者將設有該電池模組之無人機飛至要待充電之另一無人機之位置時,可以透過該可撓充電導線直接對待充電之另一無人機採有線充電或無線充電之方式進行充電,節省無人機執行任務時返航更換電池所耗時間,也增加操作的便利性。The drone charging device of the present invention uses the charging bracket module to assemble a drone with a plurality of flying shafts, wherein, the charging bracket module can increase the first bracket units and the first combinations according to requirements Units, the second support units and the number of the second combination units, so that the first support units are firmly assembled on the flight shafts of the drone through the first combination units , secondly, the third combining units of the battery module are respectively assembled with the second combining units on the second support unit, and the flexible charging wire is bent into The required shape, so that when the user flies the drone equipped with the battery module to the position of another drone to be charged, the other drone that is charged can be directly charged through the flexible charging wire. Charging or wireless charging saves the time spent on returning to the drone to replace the battery when performing missions, and also increases the convenience of operation.

茲就本申請案的技術特徵暨操作方式舉數個較佳實施態樣,並配合圖示說明謹述於后,俾提供審查參閱。再者,本發明中之圖式,為便於說明其比例未必按實際比例繪製,圖式中之比例並不用以限制本發明所欲請求保護之範圍。 Several preferred implementations of the technical features and operation methods of this application are hereby given, and will be described later in conjunction with illustrations, so as to provide reference for examination. Furthermore, the proportions of the drawings in the present invention may not be drawn according to the actual scale for the convenience of explanation, and the proportions in the drawings are not intended to limit the scope of protection claimed by the present invention.

關於本發明之技術,請參照第1圖至第6圖所示,本發明提供一種無人機充電裝置100,一無人機200係具有複數飛行軸桿210,而該無人機充電裝置100會與無人機200相組設,使該無人機200載送該無人機充電裝置100至待充電之另一無人機200處進行充電,該無人機充電裝置100主要包含有一充電支架模組10及一電池模組20,其中:該充電支架模組10,具有一主支架單元11、複數第一次支架單元12、複數第二次支架單元13、複數第一結合單元121、複數第二結合單元131及一充電連接模組14,請再參閱第1與第2圖所示,其中,該等第一次支架單元12與該等第二次支架單元13係自該主支架單元11朝外側方向凸設形成,而該等第一次支架單元12相對該主支架單元11的另端係各樞設有一該第一結合單元121,該等第二次支架單元13相對該等主支架單元11之另端各設有一該第二結合單元131,請再參閱第4-1圖所示,而該等第一結合單元121進一步包含有一第一扣件122,該等第一扣件122各具有一鋸齒部123,該等第一扣件122各設有一第一鎖固件124將每一該第一扣件122各鎖設於對應之該飛行軸桿,而該充電連接模組14係被組設於該主支架單元11上;該電池模組20,具有一控制單元21、複數電池單元22、一可撓充電導線23、複數第三結合單元24、一控制按鍵25、一電量指示器26及一充電座27,其中,該控制單元21係電性連接該等電池單元22、該可撓充電導線23、該控制按鍵25、該電量指示器26及該充電座27,該控制單元21接收到該控制按鍵25之訊號後會使該電量指示器26顯示該等電池單元22可提供之電量,而該控制單元21並可控制外部電源自該充電座27對該等電池單元22充電,並可由該電量指示器26顯示該等電池單元22的充電狀態,而該電池模組20所凸設連接之該可撓充電導線23其一端並設有一組合罩體231,並於該組合罩體231內設有與該控制單元21電性連接之二第一磁性導片232,該等第一磁性導片232之磁極性彼此不同;Regarding the technology of the present invention, please refer to Figures 1 to 6. The present invention provides a charging device 100 for a drone. A drone 200 has a plurality of flying shafts 210, and the charging device 100 for the drone will communicate with no one. The drone 200 is assembled so that the drone 200 carries the drone charging device 100 to another drone 200 to be charged for charging. The drone charging device 100 mainly includes a charging stand module 10 and a battery module. Group 20, wherein: the charging stand module 10 has a main stand unit 11, a plurality of first stand units 12, a plurality of second stand units 13, a plurality of first combination units 121, a plurality of second combination units 131 and a For the charging connection module 14, please refer to Figures 1 and 2 again, wherein the primary support units 12 and the secondary support units 13 are formed by protruding outward from the main support unit 11 , and the other ends of the primary support units 12 relative to the main support unit 11 are each pivotally provided with a first coupling unit 121, and the other ends of the secondary support units 13 relative to the main support units 11 are respectively There is a second coupling unit 131, please refer to Fig. 4-1 again, and the first coupling units 121 further include a first fastener 122, and each of the first fasteners 122 has a serration 123 Each of the first fasteners 122 is provided with a first locking member 124 to lock each of the first fasteners 122 on the corresponding flight shaft, and the charging connection module 14 is assembled on the main On the bracket unit 11; the battery module 20 has a control unit 21, a plurality of battery units 22, a flexible charging wire 23, a plurality of third coupling units 24, a control button 25, a power indicator 26 and a charging stand 27, wherein, the control unit 21 is electrically connected to the battery units 22, the flexible charging wire 23, the control button 25, the power indicator 26 and the charging stand 27, and the control unit 21 receives the control button 25 will make the power indicator 26 display the power that these battery units 22 can provide, and the control unit 21 can also control the external power supply to charge the battery units 22 from the charging stand 27, and can be indicated by the power The device 26 displays the charging status of the battery units 22, and one end of the flexible charging wire 23 protrudingly connected to the battery module 20 is provided with a combination cover 231, and a combination cover 231 is provided inside the combination cover 231. The control unit 21 is electrically connected to two first magnetic guide pieces 232, and the magnetic polarities of the first magnetic guide pieces 232 are different from each other;

其中,該等第二次支架單元13至少其中之一者係設於兩該等第一次支架單元12之間,而該等第三結合單元24係各組設一該第二結合單元131,且該等第三結合單元24各設有一第二鎖固件241使該等第三結合單元24鎖設於對應之一該第二次支架單元13;Wherein, at least one of the second support units 13 is arranged between the two first support units 12, and each of the third combination units 24 is provided with a second combination unit 131, And each of the third combination units 24 is provided with a second locking member 241 so that the third combination units 24 are locked to the corresponding one of the second support units 13;

其中,請參閱第1圖、第3-1圖及第3-2圖所示,該充電連接模組14內設有一充電中繼單元141及電性連接該充電中繼單元141之二第二磁性導片142,該等第二磁性導片142之磁極性彼此不同,請參閱第1圖與第2圖所示,該充電中繼單元141可以依需求為一無線充電器,請再參閱第6圖所示,或者該充電中繼單元141可以依需求為一有線充電器及與其電性連接之一充電連接線143。Wherein, as shown in Fig. 1, Fig. 3-1 and Fig. 3-2, the charging connection module 14 is provided with a charging relay unit 141 and two second charging relay units electrically connected to the charging relay unit 141. Magnetic guides 142, the magnetic polarities of the second magnetic guides 142 are different from each other, please refer to Figure 1 and Figure 2, the charging relay unit 141 can be a wireless charger according to requirements, please refer to the first 6, or the charging relay unit 141 can be a wired charger and a charging connection line 143 electrically connected thereto as required.

再者,請參閱第1圖與第2圖所示,使用者將該充電支架模組10與無人機200之飛行軸桿210相結合,也就是將該等第一次支架單元12之該等第一結合單元121的每一該第一扣件122組設於對應之飛行軸桿210,本實施例係將4個該等第一結合單元121之該等第一扣件122組設於具6個飛行軸桿210之無人機其前、後各兩個飛行軸桿210上,請再參閱第4-1圖所示,並藉由該等第一扣件122之該等鋸齒部123而咬合抵緊所對應之飛行軸桿210,使該等第一扣件122可以適用於不同尺寸之飛行軸桿210,此時,該等第一次支架單元12係使該主支架單元11大致位於無人機200的中心軸線上,接者再由該電池模組20之該等第三結合單元24組設於對應之該等第二結合單元131,再者,為增加無人機200組設該無人機充電裝置100時之安全性,請參閱第4-1圖與第4-2圖所示,該等第一扣件122並各設有一該第一鎖固件124而鎖設於對應之飛行軸桿210,該等第三結合單元24亦將該等第二鎖固件241鎖設於該等第二次支架單元13之該等第二結合單元131,藉此,使用者讓該充電支架模組10依無人機200之飛行軸桿210的數量,而增加該等第一次支架單元12及該等第一結合單元121之該等第一扣件122的數量,而讓使用者可依飛行軸桿210的數量來進行該等第一次支架單元12、該等第二次支架單元13其位置與數量之調整。Furthermore, please refer to FIG. 1 and FIG. 2, the user combines the charging bracket module 10 with the flying shaft 210 of the drone 200, that is, the first bracket unit 12 of the Each of the first fasteners 122 of the first combination unit 121 is assembled on the corresponding flight shaft 210. In this embodiment, the first fasteners 122 of the four first combination units 121 are assembled on the corresponding flight shaft 210. The drone with 6 flying shafts 210 has two flying shafts 210 at the front and rear respectively, please refer to Fig. Bite against the corresponding flight shafts 210 so that the first fasteners 122 can be adapted to flight shafts 210 of different sizes. At this time, the first support units 12 make the main support unit 11 approximately On the central axis of the unmanned aerial vehicle 200, the third combination units 24 of the battery module 20 are connected to the corresponding second combination units 131; Please refer to Figure 4-1 and Figure 4-2 for the safety of the charging device 100. The first fasteners 122 are each provided with a first locking member 124 which is locked on the corresponding flight shaft. Rod 210, the third combination units 24 also lock the second locking pieces 241 on the second combination units 131 of the second bracket units 13, whereby the user allows the charging bracket module 10 According to the number of flying shafts 210 of the drone 200, increase the number of the first bracket units 12 and the first fasteners 122 of the first coupling units 121, so that the user can The number of rods 210 is used to adjust the position and quantity of the first support units 12 and the second support units 13 .

另,請再參閱第2圖與第5圖所示,使用者操作無人機前往目的地對另一無人機200進行充電任務前,使用者可以先調整該可撓充電導線23的彎折方向,使該組合罩體231內之該等第一磁性導片232可以朝向需充電之另一無人機200上所設置之另一該充電連接模組14之該等第二磁性導片142所設置之方向,待使用者操作組設有該無人機充電裝置100之無人機200至待充電之另一無人機200位置時,使用者透過設有該無人機充電裝置100之無人機200所提供之影像來進行操作,請參閱第3-2圖所示,使該電池模組20所設置之該可撓充電導線23之該等第一磁性導片232可以磁吸住待充電之另一無人機200之該等第二磁性導片142,待該等第一磁性導片232與該等第二磁性導片142彼此連接後,該電池模組20內該等電池單元22之電力會由該可撓充電導線23之該等第一磁性導片232,將電力透過待充電之無人機200之該等第二磁性導片142而傳至其連接之另一該充電中繼單元141,待充電之另一無人機200之該充電中繼單元141再依其狀態而決定係採無線充電方式或者是採有線充電方式來進行充電。In addition, please refer to FIG. 2 and FIG. 5 again. Before the user operates the drone to go to the destination to charge another drone 200, the user can first adjust the bending direction of the flexible charging wire 23, The first magnetic guides 232 in the combined cover 231 can face the second magnetic guides 142 of the charging connection module 14 on another unmanned aerial vehicle 200 to be charged. Direction, when the user operates the UAV 200 equipped with the UAV charging device 100 to the position of another UAV 200 to be charged, the image provided by the user through the UAV 200 equipped with the UAV charging device 100 To operate, please refer to Figure 3-2, so that the first magnetic guide pieces 232 of the flexible charging wire 23 provided on the battery module 20 can magnetically attract another unmanned aerial vehicle 200 to be charged The second magnetic guide pieces 142, after the first magnetic guide pieces 232 and the second magnetic guide pieces 142 are connected to each other, the power of the battery units 22 in the battery module 20 will be generated by the flexible The first magnetic guides 232 of the charging wire 23 pass the power through the second magnetic guides 142 of the unmanned aerial vehicle 200 to be charged to the other charging relay unit 141 connected to it, and the other charging relay unit 141 to be charged The charging relay unit 141 of an unmanned aerial vehicle 200 then decides whether to adopt a wireless charging method or a wired charging method for charging according to its state.

綜上所述,本發明之該無人機充電裝置100利用該充電支架模組10而組設具複數飛行軸桿210的無人機200上,該充電支架模組10可以依需求來增加該等第一次支架單元12、該等第二次支架單元13,該等第一結合單元121、該等第二結合單元131及該等第三結合單元24的數量,當設有該充電支架模組10之無人機200係用以進行充電任務時,則再將該電池模組20的該等第三結合單元24分別與一該第二結合單元131相組設,再依需求將該可撓充電導線23彎折為所需形狀,藉此,使用者將設有該電池模組20之無人機200飛至待充電之另一無人機200之位置時,已彎折為所需形狀之該可撓充電導線23使該該組合罩體231內之該等第一磁性導片232磁吸於待充電之另一無人機200之該充電連接模組14的該等第二磁性導片142,並透過該可撓充電導線23直接對待充電之另一無人機200採有線方式或無線方式來進行充電,節省無人機返航更換電池所耗時間,增加操作的便利性。In summary, the UAV charging device 100 of the present invention utilizes the charging stand module 10 to assemble the UAV 200 with a plurality of flying shafts 210, and the charging stand module 10 can add the second The number of the primary support unit 12, the secondary support units 13, the first combination units 121, the second combination units 131 and the third combination units 24, when the charging stand module 10 is provided When the UAV 200 is used for charging tasks, then the third combination units 24 of the battery module 20 are combined with the second combination unit 131 respectively, and then the flexible charging wire is used as required 23 is bent into the desired shape, whereby when the user flies the unmanned aerial vehicle 200 equipped with the battery module 20 to the position of another unmanned aerial vehicle 200 to be charged, the flexible battery that has been bent into the desired shape The charging wire 23 makes the first magnetic guide pieces 232 in the combined cover 231 magnetically attract the second magnetic guide pieces 142 of the charging connection module 14 of another unmanned aerial vehicle 200 to be charged, and passes through The flexible charging wire 23 directly charges another UAV 200 to be charged in a wired or wireless manner, which saves the time spent in replacing the battery when the UAV returns to the voyage, and increases the convenience of operation.

以上已詳細說明本發明之內容,惟以上所述者,僅為本發明之較佳實施例而已,當不能以此限定本發明實施之範圍,即凡依本發明申請專利範圍所作之均等變化與修飾,皆應仍屬本發明之專利涵蓋範圍內。The content of the present invention has been described in detail above, but the above is only a preferred embodiment of the present invention, and should not limit the scope of the present invention with this, that is, all equivalent changes made according to the patent scope of the present invention and Modifications should still fall within the scope of the patent of the present invention.

100:無人機充電裝置 10:充電支架模組 11:主支架單元 12:第一次支架單元 121:第一結合單元 122:第一扣件 123:鋸齒部 124:第一鎖固件 13:第二次支架單元 131:第二結合單元 14:充電連接模組 141:充電中繼單元 142:第二磁性導片 143:充電連接線 20:電池模組 21:控制單元 22:電池單元 23:可撓充電導線 231:組合罩體 232:第一磁性導片 24:第三結合單元 241:第二鎖固件 25:控制按鍵 26:電量指示器 27:充電座 200:無人機 210:飛行軸桿 100: Drone charging device 10: Charging stand module 11: Main bracket unit 12: The first bracket unit 121: first binding unit 122: The first fastener 123: Sawtooth 124: The first locking piece 13: The second bracket unit 131: Second binding unit 14: Charging connection module 141: Charging relay unit 142: The second magnetic guide 143: Charging cable 20: Battery module 21: Control unit 22: battery unit 23: Flexible charging wire 231: combined cover 232: The first magnetic guide 24: The third binding unit 241: Second locking piece 25: Control buttons 26: Battery indicator 27: Charging stand 200: Drone 210: Flight Shaft

第1圖:為本發明之無人機充電裝置之立體部份分解示意圖。 第2圖:為本發明之無人機充電裝置之對採無線方式進行充電之無人機之動作示意圖。 第3-1圖:為第2圖圈選處之局部放大圖。 第3-2圖:為第3-1圖沿A-A剖線之剖面示意圖。 第4-1圖:為第1圖沿B-B剖線之剖面示意圖。 第4-2圖:為第1圖沿C-C剖線之剖面示意圖。 第5圖:為本發明之無人機充電裝置完成充電狀態之動作示意圖。 第6圖:為本發明之無人機充電裝置對採有線方式充電之無人機充電之動作示意圖。 Figure 1: An exploded schematic diagram of the three-dimensional part of the drone charging device of the present invention. Figure 2: It is a schematic diagram of the action of the drone charging device of the present invention charging the drone wirelessly. Figure 3-1: A partially enlarged view of the area circled in Figure 2. Figure 3-2: It is a schematic cross-sectional view along the line A-A in Figure 3-1. Figure 4-1: It is a schematic cross-sectional view along the line B-B in Figure 1. Figure 4-2: It is a schematic cross-sectional view along the line C-C in Figure 1. Figure 5: It is a schematic diagram of the operation of the drone charging device of the present invention to complete the charging state. Figure 6: It is a schematic diagram of the operation of the UAV charging device of the present invention charging the UAV that adopts wired charging.

100:無人機充電裝置 10:充電支架模組 11:主支架單元 12:第一次支架單元 121:第一結合單元 122:第一扣件 13:第二次支架單元 131:第二結合單元 14:充電連接模組 20:電池模組 21:控制單元 22:電池單元 23:可撓充電導線 231:組合罩體 24:第三結合單元 25:控制按鍵 26:電量指示器 27:充電座 200:無人機 210:飛行軸桿 100: Drone charging device 10: Charging stand module 11: Main bracket unit 12: The first bracket unit 121: first binding unit 122: The first fastener 13: The second bracket unit 131: Second binding unit 14: Charging connection module 20: Battery module 21: Control unit 22: battery unit 23: Flexible charging wire 231: combined cover 24: The third binding unit 25: Control buttons 26: Battery indicator 27: Charging stand 200: Drone 210: Flight Shaft

Claims (9)

一種無人機充電裝置,係組設於具複數飛行軸桿之一無人機,其主要包含有: 一充電支架模組,具有一主支架單元、複數第一次支架單元、複數第二次支架單元、複數第一結合單元及複數第二結合單元,其中,該等第一次支架單元與該等第二次支架單元係自該主支架單元凸設形成,而該等第一次支架單元相對該主支架單元的另端係各樞設有一該第一結合單元,該等第二次支架單元相對該主支架單元之另端各設有一該第二結合單元;以及 一電池模組,具有一控制單元、複數電池單元、一可撓充電導線及複數第三結合單元,其中,該控制單元係電性連接該等電池單元及該可撓充電導線,而該可撓充電導線設有與該控制單元電性連接之二第一磁性導片,該等第一磁性導片之磁極性彼此不同; 其中,至少一該第二次支架單元設於兩該等第一次支架單元之間; 其中,該等第三結合單元係各組設一該第二結合單元。 A charging device for an unmanned aerial vehicle is assembled on an unmanned aerial vehicle with a plurality of flying shafts, which mainly includes: A charging stand module has a main stand unit, a plurality of first stand units, a plurality of second stand units, a plurality of first combination units and a plurality of second combination units, wherein the first stand units and the The second support unit is formed by protruding from the main support unit, and the other ends of the first support units opposite to the main support unit are each pivotally provided with a first coupling unit, and the second support units are opposite to each other. The other end of the main support unit is respectively provided with a second combination unit; and A battery module has a control unit, a plurality of battery units, a flexible charging wire and a plurality of third connecting units, wherein the control unit is electrically connected to the battery units and the flexible charging wire, and the flexible The charging wire is provided with two first magnetic guide pieces electrically connected to the control unit, and the magnetic polarities of the first magnetic guide pieces are different from each other; Wherein, at least one of the second support units is arranged between two of the first support units; Wherein, each of the third combination units is provided with one second combination unit. 如請求項1所述之無人機充電裝置,進一步地,該主支架單元並組設有一充電連接模組,該充電連接模組內設有一充電中繼單元及電性連接該充電中繼單元之二第二磁性導片,該等第二磁性導片之磁極性彼此不同。As for the UAV charging device described in claim 1, further, the main bracket unit is also equipped with a charging connection module, and the charging connection module is provided with a charging relay unit and electrically connected to the charging relay unit. Two second magnetic guide pieces, the magnetic polarities of these second magnetic guide pieces are different from each other. 如請求項2所述之無人機充電裝置,其中,該充電中繼單元為一無線充電器。The drone charging device according to claim 2, wherein the charging relay unit is a wireless charger. 如請求項2所述之無人機充電裝置,其中,該充電中繼單元為一有線充電器,且該充電中繼單元並電性連接一充電連接線。The drone charging device according to claim 2, wherein the charging relay unit is a wired charger, and the charging relay unit is electrically connected to a charging cable. 如請求項1所述之無人機充電裝置,進一步地,該電池模組更設有與該控制單元電性連接之一控制按鍵、一電量指示器及一充電座。As for the drone charging device described in claim 1, further, the battery module is further provided with a control button electrically connected to the control unit, a power indicator and a charging stand. 如請求項1所述之無人機充電裝置,其中,該可撓充電導線一端並設有一組合罩體,該等第一磁性導片設於該組合罩體內。The drone charging device as described in claim 1, wherein one end of the flexible charging wire is provided with a combined cover, and the first magnetic guide pieces are arranged in the combined cover. 如請求項1所述之無人機充電裝置,其中,該等第一結合單元進一步包含有一第一扣件,該等第一扣件各具有一鋸齒部。The drone charging device according to claim 1, wherein the first coupling units further include a first fastener, and each of the first fasteners has a sawtooth portion. 如請求項7所述之無人機充電裝置,其中,該等第一扣件各設有一第一鎖固件。The drone charging device according to claim 7, wherein each of the first fasteners is provided with a first locking member. 如請求項1所述之無人機充電裝置,其中,該等第三結合單元各設有一第二鎖固件鎖設於該第二次支架單元。The drone charging device as described in claim 1, wherein each of the third combining units is provided with a second locking piece locked to the second bracket unit.
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