TWI821744B - Tail drive system for unmanned helicopters - Google Patents

Tail drive system for unmanned helicopters Download PDF

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Publication number
TWI821744B
TWI821744B TW110133455A TW110133455A TWI821744B TW I821744 B TWI821744 B TW I821744B TW 110133455 A TW110133455 A TW 110133455A TW 110133455 A TW110133455 A TW 110133455A TW I821744 B TWI821744 B TW I821744B
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Taiwan
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tail
tail boom
boom
transmission system
brushless motor
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TW110133455A
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Chinese (zh)
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TW202311116A (en
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許仕儒
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經緯航太科技股份有限公司
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Abstract

一種用於無人直升機的尾翼傳動系統,包含:一主尾桿;一驅動部,連接該主尾桿,該驅動部包含:一無刷馬達裝置;以及一尾旋翼部,連接該無刷馬達裝置;其中該無刷馬達裝置驅動該尾旋翼部,以使該尾旋翼部繞著該無刷馬達裝置的一軸向方向旋轉。 A tail transmission system for an unmanned helicopter, including: a main tail rod; a driving part connected to the main tail rod, the driving part including: a brushless motor device; and a tail rotor part connected to the brushless motor device ; wherein the brushless motor device drives the tail rotor portion so that the tail rotor portion rotates around an axial direction of the brushless motor device.

Description

用於無人直升機的尾翼傳動系統 Tail drive system for unmanned helicopters

本發明係關於一種用於無人直升機的尾翼傳動系統,特別係關於一種可減少或避免砂石及粉塵傷害的用於無人直升機的尾翼傳動系統。 The present invention relates to a tail transmission system for an unmanned helicopter, and in particular to a tail transmission system for an unmanned helicopter that can reduce or avoid damage by sand, gravel and dust.

傳統的無人直升機的尾翼傳動系統均係使用傳動式尾旋翼,此傳動式尾旋翼係以機械式的機制帶動尾旋翼,其機構複雜,且具有相當多的零件。因此,當傳統無人直升機在砂石、粉塵較多的環境下執行飛航任務時,環境中的砂石或粉塵容易進入尾翼傳動系統中,並磨耗或阻塞尾翼傳動系統的各個零件,長期下來將導致尾翼傳動系統的使用壽命大幅縮短,而讓使用者必須時常更換或清潔尾翼傳動系統的相關零件,此將致使無人直升機的零件更換成本以及維修時間成本大幅提高。有鑑於此,將需要一種可減少或避免砂石及粉塵傷害的用於無人直升機的尾翼傳動系統。 The tail drive system of traditional unmanned helicopters all use transmission tail rotors. This transmission tail rotor uses a mechanical mechanism to drive the tail rotor. Its mechanism is complex and has a considerable number of parts. Therefore, when a traditional unmanned helicopter performs flight missions in an environment with a lot of sand, gravel and dust, the sand, gravel or dust in the environment can easily enter the tail transmission system and wear or block various parts of the tail transmission system. In the long run, it will As a result, the service life of the tail transmission system is greatly shortened, and users must frequently replace or clean related parts of the tail transmission system. This will significantly increase the cost of parts replacement and maintenance time of the unmanned helicopter. In view of this, there will be a need for a tail drive system for unmanned helicopters that can reduce or avoid damage from sand, gravel and dust.

為了解決上述問題,本發明之一構想在於提供一種可減少或避免砂石及粉塵傷害的用於無人直升機的尾翼傳動系統。 In order to solve the above problems, one idea of the present invention is to provide a tail transmission system for an unmanned helicopter that can reduce or avoid damage from sand, gravel and dust.

基於前揭構想,本發明提供一種用於無人直升機的尾翼傳動系統,包含:一主尾桿;一驅動部,連接該主尾桿,該驅動部包含:一無刷馬達裝置;以及一尾旋翼部,連接該無刷馬達 裝置;其中該無刷馬達裝置驅動該尾旋翼部,以使該尾旋翼部繞著該無刷馬達裝置的一軸向方向旋轉。 Based on the foregoing concept, the present invention provides a tail transmission system for an unmanned helicopter, including: a main tail rod; a driving part connected to the main tail rod, the driving part including: a brushless motor device; and a tail rotor part, connect the brushless motor Device; wherein the brushless motor device drives the tail rotor portion so that the tail rotor portion rotates around an axial direction of the brushless motor device.

於本發明之一較佳實施例中,該主尾桿包含:一第一尾桿部;一尾桿連接部,連接該第一尾桿部;以及一第二尾桿部,連接該尾桿連接部以及該驅動部;其中該第二尾桿部藉由該尾桿連接部,以可相對於該第一尾桿部樞轉的方式連接該第一尾桿部。 In a preferred embodiment of the present invention, the main tail boom includes: a first tail boom part; a tail boom connecting part connected to the first tail boom part; and a second tail boom part connected to the tail boom The connecting part and the driving part; wherein the second tail rod part is connected to the first tail rod part in a pivotable manner relative to the first tail rod part through the tail rod connecting part.

於本發明之一較佳實施例中,該尾桿連接部包含:一第一連接部,連接該第一尾桿部;一第二連接部,連接該第二尾桿部;以及一樞轉部,連接該第一連接部以及該第二連接部;其中該第二連接部藉由該樞轉部,以可相對於該第一連接部樞轉的方式連接該第一連接部。 In a preferred embodiment of the present invention, the tail boom connection part includes: a first connection part connected to the first tail boom part; a second connection part connected to the second tail boom part; and a pivot. part, connecting the first connecting part and the second connecting part; wherein the second connecting part is connected to the first connecting part in a pivotable manner relative to the first connecting part through the pivoting part.

於本發明之一較佳實施例中,該尾桿連接部包含:一固定部,連接該第一連接部,並以可分離的方式連接該第二連接部;其中該固定部使該第二連接部相對於該第一連接部而固定,並使該第二尾桿部的一第二軸向固定在該第一尾桿部的一第一軸向上。 In a preferred embodiment of the present invention, the tail rod connecting part includes: a fixing part connected to the first connecting part and detachably connected to the second connecting part; wherein the fixing part makes the second connecting part The connecting part is fixed relative to the first connecting part, and fixes a second axial direction of the second tail boom part in a first axial direction of the first tail boom part.

於本發明之一較佳實施例中,該樞轉部設置於該尾桿連接部的一第一側,該固定部設置於該尾桿連接部上與該第一側相對的一第二側。 In a preferred embodiment of the present invention, the pivoting part is provided on a first side of the tail boom connection part, and the fixing part is provided on a second side of the tail boom connection part opposite to the first side. .

於本發明之一較佳實施例中,該尾桿連接部包含:一固定部,連接該第二連接部,並以可分離的方式連接該第一連接部;其中該固定部使該第二連接部相對於該第一連接部而固定,並使該第二尾桿部的一第二軸向固定在該第一尾桿部的一第一軸向上。 In a preferred embodiment of the present invention, the tail rod connecting part includes: a fixing part connected to the second connecting part and detachably connected to the first connecting part; wherein the fixing part makes the second connecting part The connecting part is fixed relative to the first connecting part, and fixes a second axial direction of the second tail boom part in a first axial direction of the first tail boom part.

於本發明之一較佳實施例中,該樞轉部設置於該尾桿連接部的一第一側,該固定部設置於該尾桿連接部上與該第一側相對的一第二側。 In a preferred embodiment of the present invention, the pivoting part is provided on a first side of the tail boom connection part, and the fixing part is provided on a second side of the tail boom connection part opposite to the first side. .

於本發明之一較佳實施例中,該驅動部包含一連接裝置,該連接裝置連接該無刷馬達裝置,且該主尾桿延伸固定於該連接裝置內。 In a preferred embodiment of the present invention, the driving part includes a connecting device connected to the brushless motor device, and the main and tail rods are extended and fixed in the connecting device.

於本發明之一較佳實施例中,該尾翼傳動系統進一步包含:一控制裝置;以及一控制電線,連接該控制裝置以及該無刷馬達裝置;其中該控制裝置藉由該控制電線以控制該無刷馬達裝置對該尾旋翼部的一驅動速度。 In a preferred embodiment of the present invention, the tail transmission system further includes: a control device; and a control wire connecting the control device and the brushless motor device; wherein the control device controls the control wire through the control wire. A driving speed of the brushless motor device for the tail rotor portion.

於本發明之一較佳實施例中,該控制電線延伸設置於該主尾桿內。 In a preferred embodiment of the present invention, the control wire extends into the main and tail boom.

本發明前述各方面及其它方面依據下述的非限制性具體實施例詳細說明以及參照附隨的圖式將更趨於明瞭。 The foregoing aspects and other aspects of the present invention will become more apparent based on the following detailed description of non-limiting specific embodiments and with reference to the accompanying drawings.

100:尾翼傳動系統 100: Tail transmission system

110:主尾桿 110: Main and tail rod

112:第一尾桿部 112:First tail rod part

114:尾桿連接部 114: Tail rod connection part

116:第二尾桿部 116:Second tail rod part

120:驅動部 120:Drive Department

122:連接裝置 122:Connection device

124:無刷馬達裝置 124: Brushless motor device

126:轉軸部 126:Rotating shaft part

200:主尾桿 200: Main and tail rod

220:第一尾桿部 220:First tail rod part

222:第一軸向 222: First axis

240:尾桿連接部 240: Tail rod connection part

242:第一連接部 242:First connection part

244:樞轉部 244: Pivot part

246:第二連接部 246: Second connection part

248:固定部 248:Fixed part

260:第二尾桿部 260:Second tail rod part

262:第二軸向 262: Second axis

300:驅動部 300:Drive Department

320:連接裝置 320:Connection device

322:通道 322:Channel

324:通道 324:Channel

340:無刷馬達裝置 340: Brushless motor device

342:轉軸部 342:Rotating shaft part

360:尾旋翼部 360: Tail rotor section

802~808:鎖固元件 802~808: Locking components

922~926:鎖固元件 922~926: Locking components

962~968:鎖固元件 962~968: Locking components

第一圖為本發明尾翼傳動系統一具體實施例的架構圖。 The first figure is a structural diagram of a specific embodiment of the tail transmission system of the present invention.

第二圖為主尾桿一具體實施例的架構圖。 The second figure is a structural diagram of a specific embodiment of the main tail boom.

第三圖為驅動部一具體實施例的架構圖。 The third figure is an architectural diagram of a specific embodiment of the driving unit.

請參閱第一圖,其例示說明了本發明尾翼傳動系統一具體實施例的架構圖。如第一圖所示實施例,用於無人直升機的尾翼傳動系統100包含主尾桿110以及驅動部120,且驅動部120連接主尾桿110。主尾桿110包含第一尾桿部112、尾桿連接部114 以及第二尾桿部116。其中,尾桿連接部114連接第一尾桿部112以及第二尾桿部116,且第二尾桿部116連接驅動部120。第二尾桿部116係藉由尾桿連接部114,以可相對於第一尾桿部112而樞轉的方式連接第二尾桿部116。亦即,第二尾桿部116可藉由尾桿連接部114而相對於第一尾桿部112樞轉。驅動部120包含連接裝置122、無刷馬達裝置124以及尾旋翼部(圖未示)。連接裝置122連接主尾桿110的第二尾桿部116,無刷馬達裝置124連接(或裝設於)連接裝置122,尾旋翼部連接(或裝設於)無刷馬達裝置124的轉軸部126上。較佳地,主尾桿110的第二尾桿部116可延伸固定於連接裝置122內。在第一圖所示實施例中,無刷馬達裝置124可驅動尾旋翼部繞著無刷馬達裝置124的一軸向(即轉軸部126的軸向)方向旋轉,藉以調整無人直升機的飛行方向或調整機身所面對的方向。 Please refer to the first figure, which illustrates a structural diagram of a specific embodiment of the tail transmission system of the present invention. As shown in the first figure, the tail transmission system 100 for an unmanned helicopter includes a main tail boom 110 and a driving part 120 , and the driving part 120 is connected to the main tail boom 110 . The main tail boom 110 includes a first tail boom part 112 and a tail boom connecting part 114 and a second tail boom portion 116 . The tail boom connecting part 114 connects the first tail boom part 112 and the second tail boom part 116 , and the second tail boom part 116 connects to the driving part 120 . The second tail boom part 116 is pivotally connected to the first tail boom part 112 through the tail boom connecting part 114 . That is, the second tail boom portion 116 can pivot relative to the first tail boom portion 112 through the tail boom connection portion 114 . The driving part 120 includes a connection device 122, a brushless motor device 124 and a tail rotor part (not shown). The connecting device 122 is connected to the second tail boom portion 116 of the main tail boom 110 , the brushless motor device 124 is connected to (or installed on) the connecting device 122 , and the tail rotor portion is connected to (or installed on) the rotating shaft portion of the brushless motor device 124 126 on. Preferably, the second tail rod portion 116 of the main tail rod 110 can be extended and fixed in the connecting device 122 . In the embodiment shown in the first figure, the brushless motor device 124 can drive the tail rotor portion to rotate around an axial direction of the brushless motor device 124 (ie, the axial direction of the rotating shaft portion 126), thereby adjusting the flight direction of the unmanned helicopter. Or adjust the direction the fuselage is facing.

在一具體實施例中,尾翼傳動系統100進一步包含控制裝置以及控制電線。控制電線連接控制裝置以及無刷馬達裝置124,且控制裝置可藉由控制電線以控制無刷馬達裝置124對尾旋翼部的驅動速度。較佳地,控制電線可延伸設置於主尾桿110內。然應了解,控制電線亦可視需求而設置於主尾桿110的外部。在一具體實施例中,控制裝置係透過控制電線以調控輸入至無刷馬達裝置124的電流,進而控制無刷馬達裝置124的驅動速度。在一具體實施例中,控制電線包含三條電纜線,控制裝置係透過此三條電纜線以調控輸入至無刷馬達裝置124的電流。 In a specific embodiment, the tail drive system 100 further includes a control device and control wires. The control wire connects the control device and the brushless motor device 124, and the control device can control the driving speed of the brushless motor device 124 on the tail rotor part through the control wire. Preferably, the control wires can be extended and disposed inside the main tail rod 110 . However, it should be understood that the control wires may also be disposed outside the main and tail rods 110 as required. In a specific embodiment, the control device regulates the current input to the brushless motor device 124 through the control wire, thereby controlling the driving speed of the brushless motor device 124 . In a specific embodiment, the control wires include three cable lines, and the control device controls the current input to the brushless motor device 124 through these three cable lines.

在一具體實施例中,驅動部120為一模組化的組件,因此當驅動部120的任一部分損壞時,使用者可直接更換整組驅動部 120,而無須僅更換或維修驅動部120中的單一元件。此種模組化的做法可大幅減少更換時間,進而可避免延誤到無人直升機執行後續的飛航任務。此外,此種模組化的做法其更換作業較為簡單,而可由一般使用者獨立進行。在一具體實施例中,尾翼傳動系統100為一模組化的組件(此模組化的組件是否須包含控制裝置,可視需求而決定),因此當尾翼傳動系統100的任一部分損壞時,使用者可直接更換整組尾翼傳動系統100,而無須僅更換或維修尾翼傳動系統100中的單一元件。此種模組化的做法可大幅減少更換時間,進而可避免延誤到無人直升機執行後續的飛航任務。此外,此種模組化的做法其更換作業較為簡單,而可由一般使用者獨立進行(應了解,若僅更換單一元件,則除了更換手續較為複雜外,尚需另外執行零件調整作業,此些流程須經由無人直升機的維修技師方可執行)。在一具體實施例中,控制裝置可不包含在模組化的尾翼傳動系統中,而係可將控制裝置設置在無人直升機的機體上。如此,使用者在更換模組化的尾翼傳動系統時,僅需將此尾翼傳動系統固定於機體上,並將控制電線連接至控制裝置即可。 In a specific embodiment, the driving part 120 is a modular component, so when any part of the driving part 120 is damaged, the user can directly replace the entire set of driving parts. 120 without having to replace or repair only a single component in the driving part 120. This modular approach can significantly reduce replacement time, thereby avoiding delays in the unmanned helicopter's subsequent flight missions. In addition, this modular approach makes the replacement operation relatively simple and can be performed independently by ordinary users. In a specific embodiment, the tail transmission system 100 is a modular component (whether this modular component must include a control device depends on the requirements), so when any part of the tail transmission system 100 is damaged, use The user can directly replace the entire tail transmission system 100 without having to replace or repair only a single component in the tail transmission system 100 . This modular approach can significantly reduce replacement time, thereby avoiding delays in the unmanned helicopter's subsequent flight missions. In addition, the replacement operation of this modular approach is relatively simple and can be performed independently by ordinary users (it should be understood that if only a single component is replaced, in addition to the more complicated replacement procedures, additional parts adjustment operations are required. These The process must be performed by the maintenance technician of the unmanned helicopter). In a specific embodiment, the control device may not be included in the modular tail transmission system, but the control device may be provided on the body of the unmanned helicopter. In this way, when the user replaces the modular tail drive system, he only needs to fix the tail drive system to the body and connect the control wires to the control device.

請參閱第二圖,其例示說明了主尾桿一具體實施例的架構圖。如第二圖所示實施例,主尾桿200包含第一尾桿部220、尾桿連接部240以及第二尾桿部260。尾桿連接部240連接第一尾桿部220以及第二尾桿部260,且第二尾桿部260可藉由尾桿連接部240,以可相對於第一尾桿部220樞轉的方式連接第一尾桿部220。尾桿連接部240包含第一連接部242、樞轉部244、第二連接部246以及固定部248。第一尾桿部220可連接第一連接 部242,並可藉由鎖固元件922、924、926以將第一尾桿部220鎖固至第一連接部242。第二尾桿部260可連接第二連接部246,並可藉由鎖固元件962、964、966、968以將第二尾桿部260鎖固至第二連接部246。樞轉部244連接第一連接部242以及第二連接部246,且第二連接部246可藉由樞轉部244,以可相對於第一連接部242樞轉的方式連接第一連接部242。亦即,第二連接部246可藉由樞轉部244而相對於第一連接部242樞轉。 Please refer to the second figure, which illustrates an architectural diagram of a specific embodiment of the main and tail booms. As shown in the second figure, the main tail boom 200 includes a first tail boom part 220 , a tail boom connecting part 240 and a second tail boom part 260 . The tail boom connecting part 240 connects the first tail boom part 220 and the second tail boom part 260 , and the second tail boom part 260 can be pivoted relative to the first tail boom part 220 through the tail boom connecting part 240 Connect the first tail rod part 220. The tail boom connection part 240 includes a first connection part 242 , a pivot part 244 , a second connection part 246 and a fixed part 248 . The first tail rod part 220 can be connected to the first connection part 242, and the first tail rod part 220 can be locked to the first connecting part 242 through the locking elements 922, 924, and 926. The second tail rod part 260 can be connected to the second connecting part 246, and the second tail rod part 260 can be locked to the second connecting part 246 through the locking elements 962, 964, 966, 968. The pivoting part 244 connects the first connecting part 242 and the second connecting part 246 , and the second connecting part 246 can be connected to the first connecting part 242 in a pivotable manner relative to the first connecting part 242 through the pivoting part 244 . That is, the second connecting part 246 can pivot relative to the first connecting part 242 through the pivoting part 244 .

在第二圖所示實施例中,固定部248係連接(或裝設於)第二連接部246,且固定部248以可分離的方式連接(或鎖固於)第一連接部242。當固定部248未鎖固於第一連接部242時,第二連接部246即可藉由樞轉部244而相對於第一連接部242樞轉。而當固定部248鎖固於第一連接部242時,第二連接部246即無法藉由樞轉部244而相對於第一連接部242樞轉。此時,固定部248使第二連接部246相對於第一連接部242而固定,並使第二尾桿部260的第二軸向262固定在第一尾桿部220的第一軸向222上。如此,第二軸向262即實質上與第一軸向222平行。較佳地,尾桿連接部240的樞轉部244係設置於尾桿連接部240的一第一側,而固定部248係設置於尾桿連接部240上與該第一側相對的一第二側,如第二圖中所示。 In the embodiment shown in the second figure, the fixing part 248 is connected to (or installed on) the second connecting part 246 , and the fixing part 248 is detachably connected to (or locked on) the first connecting part 242 . When the fixing part 248 is not locked to the first connecting part 242, the second connecting part 246 can pivot relative to the first connecting part 242 through the pivoting part 244. When the fixing part 248 is locked to the first connecting part 242, the second connecting part 246 cannot pivot relative to the first connecting part 242 through the pivoting part 244. At this time, the fixing part 248 fixes the second connecting part 246 relative to the first connecting part 242 and fixes the second axial direction 262 of the second tail rod part 260 to the first axial direction 222 of the first tail rod part 220 superior. In this way, the second axial direction 262 is substantially parallel to the first axial direction 222 . Preferably, the pivoting portion 244 of the tail boom connecting portion 240 is disposed on a first side of the tail boom connecting portion 240 , and the fixing portion 248 is disposed on a first side of the tail boom connecting portion 240 opposite to the first side. Two sides, as shown in the second picture.

應了解,固定部248的設置方式亦可與第二圖中所示不同。在一具體實施例中,固定部248連接(或裝設於)第一連接部242,且固定部248以可分離的方式連接(或鎖固於)第二連接部246。當固定部248未鎖固於第二連接部246時,第二連接部246即可藉由樞轉部244而相對於第一連接部242樞轉。而當固定部248鎖固於 第二連接部246時,第二連接部246即無法藉由樞轉部244而相對於第一連接部242樞轉。此時,固定部248使第二連接部246相對於第一連接部242而固定,並使第二尾桿部260的第二軸向262固定在第一尾桿部220的第一軸向222上。如此,第二軸向262即實質上與第一軸向222平行。較佳地,尾桿連接部240的樞轉部244係設置於尾桿連接部240的一第一側,而固定部248係設置於尾桿連接部240上與該第一側相對的一第二側。 It should be understood that the arrangement of the fixing portion 248 may also be different from that shown in the second figure. In a specific embodiment, the fixing part 248 is connected to (or installed on) the first connecting part 242 , and the fixing part 248 is detachably connected to (or locked on) the second connecting part 246 . When the fixing part 248 is not locked to the second connecting part 246, the second connecting part 246 can pivot relative to the first connecting part 242 through the pivoting part 244. And when the fixed part 248 is locked on When the second connecting portion 246 is configured, the second connecting portion 246 cannot pivot relative to the first connecting portion 242 through the pivoting portion 244 . At this time, the fixing part 248 fixes the second connecting part 246 relative to the first connecting part 242 and fixes the second axial direction 262 of the second tail rod part 260 to the first axial direction 222 of the first tail rod part 220 superior. In this way, the second axial direction 262 is substantially parallel to the first axial direction 222 . Preferably, the pivoting portion 244 of the tail boom connecting portion 240 is disposed on a first side of the tail boom connecting portion 240 , and the fixing portion 248 is disposed on a first side of the tail boom connecting portion 240 opposite to the first side. Two sides.

請參閱第三圖,其例示說明了驅動部一具體實施例的架構圖。如第三圖所示實施例,驅動部300包含連接裝置320、無刷馬達裝置340以及尾旋翼部360。無刷馬達裝置340可藉由鎖固元件802、804、806、808以鎖固於連接裝置320上。尾旋翼部360可連接於無刷馬達裝置340的轉軸部342上,且無刷馬達裝置340可驅動尾旋翼部360,以使尾旋翼部360繞著無刷馬達裝置340的一軸向方向旋轉。連接裝置320具有通道322、324,尾翼傳動系統的主尾桿可延伸穿過通道322、324,以連接並固定(或鎖固)於連接裝置320內。 Please refer to the third figure, which illustrates the architecture diagram of a specific embodiment of the driving unit. As shown in the third embodiment, the driving part 300 includes a connecting device 320, a brushless motor device 340 and a tail rotor part 360. The brushless motor device 340 can be locked on the connection device 320 through the locking components 802, 804, 806, and 808. The tail rotor portion 360 can be connected to the rotating shaft portion 342 of the brushless motor device 340 , and the brushless motor device 340 can drive the tail rotor portion 360 so that the tail rotor portion 360 rotates around an axial direction of the brushless motor device 340 . The connecting device 320 has channels 322 and 324, and the main tail rod of the tail drive system can extend through the channels 322 and 324 to be connected and fixed (or locked) in the connecting device 320.

應了解,傳統的尾翼傳動系統係使用傳動馬達,並係以機械機制控制尾旋翼,此種控制方式使尾翼傳動系統必須具有極其複雜的機械架構,且必須具備數量極多的機械元件。而在砂石、粉塵較多的環境中,過多的機械元件將導致各元件之間容易受到砂石、粉塵的磨損,進而大幅縮短尾翼傳動系統的使用壽命。相較於此,本發明之尾翼傳動系統係使用無刷馬達裝置(無刷馬達具備防塵特性及防水特性為業界所知),且本發明之尾翼傳動系統係透過電控制的方式控制無刷馬達裝置以驅動尾旋翼部,因而無 需過多的機械元件。本發明之尾翼傳動系統的此種設置方式將令無人直升機可適用於砂石、粉塵較多的環境,而不會因環境中的砂石、粉塵而大幅縮短尾翼傳動系統的使用壽命。在一具體實施例中,本發明之尾翼傳動系統係用於單旋翼的無人直升機。 It should be understood that the traditional tail drive system uses a transmission motor and uses a mechanical mechanism to control the tail rotor. This control method requires the tail drive system to have an extremely complex mechanical structure and must have an extremely large number of mechanical components. In an environment with a lot of sand, gravel, and dust, too many mechanical components will cause the components to be easily worn by sand, gravel, and dust, which will greatly shorten the service life of the tail transmission system. In comparison, the tail drive system of the present invention uses a brushless motor device (brushless motors are known in the industry to have dust-proof and waterproof properties), and the tail drive system of the present invention controls the brushless motor through electrical control. device to drive the tail rotor section, so there is no Requires too many mechanical components. This arrangement of the tail transmission system of the present invention will make the unmanned helicopter suitable for environments with a lot of sand, gravel and dust, and will not significantly shorten the service life of the tail transmission system due to sand, gravel and dust in the environment. In a specific embodiment, the tail transmission system of the present invention is used for a single-rotor unmanned helicopter.

至此,本發明之用於無人直升機的尾翼傳動系統已經由上述說明及圖式加以說明。然應了解,本發明的各個具體實施例僅是做為說明之用,在不脫離本發明申請專利範圍與精神下可進行各種改變,且均應包含於本發明之專利範圍中。因此,本說明書所描述的各具體實施例並非用以限制本發明,本發明之真實範圍與精神揭示於以下申請專利範圍。 So far, the tail transmission system of the present invention for an unmanned helicopter has been explained based on the above description and drawings. However, it should be understood that each specific embodiment of the present invention is for illustration only, and various changes can be made without departing from the patent scope and spirit of the present invention, and all should be included in the patent scope of the present invention. Therefore, the specific embodiments described in this specification are not intended to limit the invention, and the true scope and spirit of the invention are disclosed in the following patent applications.

100:尾翼傳動系統 100: Tail transmission system

110:主尾桿 110: Main and tail rod

112:第一尾桿部 112:First tail rod part

114:尾桿連接部 114: Tail rod connection part

116:第二尾桿部 116:Second tail rod part

120:驅動部 120:Drive Department

122:連接裝置 122:Connection device

124:無刷馬達裝置 124: Brushless motor device

126:轉軸部 126:Rotating shaft part

Claims (8)

一種用於無人直升機的尾翼傳動系統,包含:一主尾桿;一驅動部,連接該主尾桿,該驅動部包含:一無刷馬達裝置;以及一尾旋翼部,連接該無刷馬達裝置;其中該無刷馬達裝置驅動該尾旋翼部,以使該尾旋翼部繞著該無刷馬達裝置的一軸向方向旋轉;其中該尾翼傳動系統進一步包含:一控制裝置;以及一控制電線,連接該控制裝置以及該無刷馬達裝置;其中該控制裝置藉由該控制電線以控制該無刷馬達裝置對該尾旋翼部的一驅動速度;其中該控制電線延伸設置於該主尾桿內。 A tail transmission system for an unmanned helicopter, including: a main tail rod; a driving part connected to the main tail rod, the driving part including: a brushless motor device; and a tail rotor part connected to the brushless motor device ; wherein the brushless motor device drives the tail rotor portion so that the tail rotor portion rotates around an axial direction of the brushless motor device; wherein the tail rotor transmission system further includes: a control device; and a control wire, The control device and the brushless motor device are connected; wherein the control device controls a driving speed of the brushless motor device to the tail rotor portion through the control wire; wherein the control wire extends and is provided in the main tail boom. 如請求項1之尾翼傳動系統,其中該主尾桿包含:一第一尾桿部;一尾桿連接部,連接該第一尾桿部;以及一第二尾桿部,連接該尾桿連接部以及該驅動部;其中該第二尾桿部藉由該尾桿連接部,以可相對於該第一尾桿部樞轉的方式連接該第一尾桿部。 The tail wing transmission system of claim 1, wherein the main tail boom includes: a first tail boom part; a tail boom connecting part connected to the first tail boom part; and a second tail boom part connected to the tail boom connection part and the driving part; wherein the second tail rod part is connected to the first tail rod part in a pivotable manner relative to the first tail rod part through the tail rod connecting part. 如請求項2之尾翼傳動系統,其中該尾桿連接部包含:一第一連接部,連接該第一尾桿部;一第二連接部,連接該第二尾桿部;以及一樞轉部,連接該第一連接部以及該第二連接部; 其中該第二連接部藉由該樞轉部,以可相對於該第一連接部樞轉的方式連接該第一連接部。 The tail wing transmission system of claim 2, wherein the tail boom connection part includes: a first connection part connected to the first tail boom part; a second connection part connected to the second tail boom part; and a pivot part , connect the first connecting part and the second connecting part; The second connecting part is connected to the first connecting part in a pivotable manner relative to the first connecting part through the pivoting part. 如請求項3之尾翼傳動系統,其中該尾桿連接部包含:一固定部,連接該第一連接部,並以可分離的方式連接該第二連接部;其中該固定部使該第二連接部相對於該第一連接部而固定,並使該第二尾桿部的一第二軸向固定在該第一尾桿部的一第一軸向上。 The tail wing transmission system of claim 3, wherein the tail boom connecting part includes: a fixing part connected to the first connecting part and detachably connected to the second connecting part; wherein the fixing part makes the second connecting part The part is fixed relative to the first connecting part, and a second axial direction of the second tail boom part is fixed in a first axial direction of the first tail boom part. 如請求項4之尾翼傳動系統,其中該樞轉部設置於該尾桿連接部的一第一側,該固定部設置於該尾桿連接部上與該第一側相對的一第二側。 The tail wing transmission system of claim 4, wherein the pivot part is provided on a first side of the tail boom connection part, and the fixing part is provided on a second side of the tail boom connection part opposite to the first side. 如請求項3之尾翼傳動系統,其中該尾桿連接部包含:一固定部,連接該第二連接部,並以可分離的方式連接該第一連接部;其中該固定部使該第二連接部相對於該第一連接部而固定,並使該第二尾桿部的一第二軸向固定在該第一尾桿部的一第一軸向上。 The tail wing transmission system of claim 3, wherein the tail boom connection part includes: a fixed part connected to the second connecting part and detachably connected to the first connecting part; wherein the fixed part makes the second connecting part The part is fixed relative to the first connecting part, and a second axial direction of the second tail boom part is fixed in a first axial direction of the first tail boom part. 如請求項6之尾翼傳動系統,其中該樞轉部設置於該尾桿連接部的一第一側,該固定部設置於該尾桿連接部上與該第一側相對的一第二側。 The tail wing transmission system of claim 6, wherein the pivoting part is provided on a first side of the tail boom connection part, and the fixing part is provided on a second side of the tail boom connection part opposite to the first side. 如請求項1之尾翼傳動系統,其中該驅動部包含一連接裝置,該連接裝置連接該無刷馬達裝置,且該主尾桿延伸固定於該連接裝置內。 The tail wing transmission system of claim 1, wherein the driving part includes a connecting device, the connecting device is connected to the brushless motor device, and the main tail rod is extended and fixed in the connecting device.
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TWM584706U (en) * 2018-12-13 2019-10-11 龍華科技大學 Triple blades-tail rotor assembly
CN112896497A (en) * 2021-03-23 2021-06-04 珠海紫燕无人飞行器有限公司 Unmanned helicopter

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WO2016187310A2 (en) * 2015-05-19 2016-11-24 Alion Science And Technology Corporation Helicopter blade folding apparatus
CN108974348A (en) * 2017-05-31 2018-12-11 贝尔直升机德事隆公司 The rotor braking effect for making main rotor slow down using electric distributed reaction torque generator and reversed electric motor thrust
CN107310717A (en) * 2017-07-03 2017-11-03 雷虎飞行器有限公司 Depopulated helicopter
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