TW201912226A - Unmanned vehicle with vertical lifting and fast horizontal flying functions capable of reducing requirement of processor system and making flying more stable - Google Patents
Unmanned vehicle with vertical lifting and fast horizontal flying functions capable of reducing requirement of processor system and making flying more stable Download PDFInfo
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本發明係關於一種無人載具，特別是關於一種具垂直升降及快速水平飛行功能之無人載具。The present invention relates to an unmanned vehicle, and more particularly to an unmanned vehicle having a vertical lift and a fast horizontal flight function.
由於科技的進步快速，在材料科技、微機電技術以及GPS結合陀螺儀的定位技術等各項技術整合，無人載具的樣貌也快速改變，大型的載人載具的各項科技得以微小化應用於遙控的無人載具，垂直升降技術應用於小型無人載具也日益成熟，例如：遙控直升機，但直升機受限於垂直旋翼的先天構造限制，無法進行水平方向的速度提升。Due to the rapid advancement of technology, the integration of various technologies such as materials technology, MEMS technology and GPS and gyro positioning technology has rapidly changed the appearance of unmanned vehicles, and the technologies of large-scale manned vehicles have been miniaturized. For unmanned vehicles used in remote control, vertical lifting technology is also becoming more and more mature for small unmanned vehicles, such as RC helicopters, but helicopters are limited by the innate structural limitations of vertical rotors and cannot be upgraded horizontally.
另一種垂直升降機型，例如：由美國貝爾直升機公司和波音直升機公司共同研製的V-22「魚鷹」飛機，能改變旋翼旋轉軸的方向使其能垂直升降還能於升空後快速的水平飛行，但由於無人載具的馬力重量比遠大於真實的載人飛機，若將載人飛機的構造直接應用於體積與重量縮小很多的遙控無人載具，該種對稱雙軸的旋翼構造在重量較輕無人機很容易產生偏擺失去平衡，可能需要更快速的陀螺儀及運算處理器才能滿足其運算速度，製造的成本與重量也會增加。Another type of vertical lift, such as the V-22 "Osprey" aircraft developed by Bell Helicopter and Boeing Helicopter, can change the direction of the rotor's rotating shaft so that it can be vertically lifted and can also fly quickly after the lift. However, since the horsepower weight ratio of the unmanned vehicle is much larger than that of the real manned aircraft, if the structure of the manned aircraft is directly applied to the remote unmanned vehicle with a much smaller volume and weight, the symmetrical biaxial rotor structure is weighted. Light drones are prone to yaw imbalance, and may require faster gyroscopes and arithmetic processors to meet their computing speeds, and the cost and weight of manufacturing will increase.
因此有必要研發新的無人載具以克服上述問題。It is therefore necessary to develop new unmanned vehicles to overcome the above problems.
﹝發明所欲解決之問題﹞[The problem that the invention wants to solve]
本發明之一目的在提供一種具垂直升降及快速水平飛行功能之無人載具，能降低處理器系統的需求且能使飛行更平穩。It is an object of the present invention to provide an unmanned vehicle having vertical lift and fast horizontal flight functions that reduces the need for a processor system and enables a smoother flight.
本發明之另一目的在提供一種具垂直升降及快速水平飛行功能之無人載具，可提供多維度的翻滾及作各式花式動作的表演。Another object of the present invention is to provide an unmanned vehicle having vertical lifting and fast horizontal flying functions, which can provide multi-dimensional tumbling and performance for various fancy actions.
﹝解決問題之技術手段﹞[Technical means to solve the problem]
為達成上述目的，本發明之具垂直升降及快速水平飛行功能之無人載具在一個實施例中包含：一主機體，該主機體界定一中央縱向面及一前進方向；一主機翼，該主機翼交叉結合於該主機體，該主機翼於該中央縱向面兩側形成對稱設置；偶數個第一動力組，該偶數個第一動力組於該中央縱向面兩側對稱的設置於該主機翼，該每一第一動力組包含一方向變換馬達及一螺旋槳馬達，該方向變換馬達固定於該主機翼，該螺旋槳馬達固定於一螺旋槳馬達座，該螺旋槳馬達座可樞轉的結合於該方向變換馬達，該螺旋槳馬達結合一螺旋槳，該螺旋槳的第一旋轉軸可以改變方向；一第二動力組，該第二動力組包含一螺旋槳馬達，該螺旋槳馬達結合一螺旋槳，該第二動力組固定於該主機體之中央縱向面，該第二動力組之螺旋槳之第二旋轉軸與所述前進方向形成60至90度角設置。In order to achieve the above object, the unmanned vehicle with vertical lifting and fast horizontal flying functions of the present invention comprises, in one embodiment, a main body defining a central longitudinal plane and a forward direction; a main wing, the mainframe a wing cross is coupled to the main body, the main wing is symmetrically disposed on both sides of the central longitudinal surface; an even number of first power groups, the even number of first power groups are symmetrically disposed on the main wing on both sides of the central longitudinal surface Each of the first power units includes a direction changing motor and a propeller motor, and the direction changing motor is fixed to the main wing. The propeller motor is fixed to a propeller motor seat, and the propeller motor base is pivotally coupled in the direction. Transforming a motor, the propeller motor is combined with a propeller, the first rotating shaft of the propeller can change direction; a second power group, the second power group comprises a propeller motor, the propeller motor is combined with a propeller, and the second power group is fixed a second rotating shaft of the propeller of the second power group forms a 60 to 90 with the advancing direction on a central longitudinal plane of the main body Degree angle setting.
在一些實施例中，其中該第一動力組數量為2個，該2個第一動力組與該第二動力組形成等腰三角形設置。In some embodiments, wherein the number of the first power groups is two, the two first power groups and the second power group form an isosceles triangle.
在一些實施例中，其中該主機體設有控制套件，該控制套件能透過一遙控器無線控制該方向變換馬達作動及控制該螺旋槳馬達的轉速。In some embodiments, the main body is provided with a control kit, and the control kit can wirelessly control the direction changing motor to operate and control the rotation speed of the propeller motor through a remote controller.
在一些實施例中，其中該主機體另包含一垂直尾翼及一水平尾翼，該垂直尾翼設有一方向舵，該水平尾翼設有一升降舵，該控制套件透過該遙控器無線控制該方向舵及該升降舵作動，該控制套件另包含電池、無線接收裝置、GPS定位裝置及陀螺儀裝置。In some embodiments, the main body further includes a vertical tail and a horizontal tail. The vertical tail is provided with a rudder. The horizontal tail is provided with an elevator. The control kit wirelessly controls the rudder and the elevator through the remote controller. The control kit also includes a battery, a wireless receiving device, a GPS positioning device, and a gyroscope device.
在一些實施例中，其中該第一動力組或第二動力組之螺旋槳葉片上方或下方皆可設有數個LED燈裝置，該主機體設有旋轉輪顯示控制器並且電性連接至該數個LED燈，當該螺旋槳旋轉時利用人眼視覺暫留效果可顯示文字或圖案。In some embodiments, a plurality of LED lamp devices may be disposed above or below the propeller blades of the first power group or the second power group, and the main body is provided with a rotating wheel display controller and electrically connected to the plurality of The LED lamp can display characters or patterns by using the human eye persistence effect when the propeller rotates.
在一些實施例中，其中第二動力組之螺旋槳之第二旋轉軸與所述前進方向形成90度角設置。In some embodiments, the second axis of rotation of the propeller of the second power pack forms a 90 degree angle with the advancement direction.
在一些實施例中，其中該方向變換馬達透過一延伸座固定於該主機翼。In some embodiments, the direction changing motor is secured to the main wing by an extension.
在一些實施例中，其中該螺旋槳馬達座相對該方向變換馬達樞轉的樞轉面平行於該中央縱向面。In some embodiments, a pivoting surface of the propeller motor mount that pivots relative to the direction change motor is parallel to the central longitudinal plane.
在一些實施例中，其中該第一動力組之螺旋槳之第一旋轉軸可從該前進方向旋轉至向上90度。In some embodiments, the first axis of rotation of the propeller of the first power pack is rotatable from the advancement direction to an upward 90 degrees.
在一些實施例中，其中該第一動力組之螺旋槳之第一旋轉軸更可以從該前進方向旋轉至向下90度。In some embodiments, the first axis of rotation of the propeller of the first power pack is more rotatable from the forward direction to the next 90 degrees.
﹝發明之效果、相較先前技術之功效﹞[Effect of the invention, compared to the efficacy of the prior art]
藉由上述揭示，本發明之具垂直升降及快速水平飛行功能之無人載具能降低處理器系統的需求且能使飛行更平穩，以及可提供多維度的翻滾及作各式花式動作的表演，且因為能降低系統需求又能使飛行更穩定快速，因此具有省電的效果。By the above disclosure, the unmanned vehicle with vertical lifting and fast horizontal flying function of the invention can reduce the demand of the processor system and make the flight more stable, and can provide multi-dimensional rollover and various fancy action performances. And because it can reduce the system requirements and make the flight more stable and fast, it has the effect of saving electricity.
以下將詳細說明參考附圖中的代表性實施例，其中相似或相同的元件使用相同的編號。以下描述之實施例預期涵蓋如所附申請專利範圍定義的實施例之精神及範疇內的替代實施例、修改或等效的替換。應理解，本發明所提到的方向用語僅是參考附圖的方向說明本發明，非用以限制本發明。另外，以下說明將一特徵、元件或手段描述於一實施例時，熟習此項技藝者運用其知識將該特徵、元件或手段實施於未描述的其他實施例當視為等效；在一些單獨實施例中描述的某些特徵，也可以在其他實施例中單獨或組合實現；相反的，在多個實施例的上下文中描述的各種特徵也可以分開地或以任何合適的子組合在其他單獨或多個實施例中實現。Representative embodiments in the drawings will be described in detail below, wherein like or identical elements have the same number. The embodiments described below are intended to cover alternative embodiments, modifications, or equivalent substitutions within the spirit and scope of the embodiments as defined by the appended claims. It is to be understood that the invention is not intended to limit the invention. In addition, the following descriptions of a feature, element, or means are described in an embodiment, and those skilled in the art will use the knowledge to implement the feature, element or means in other embodiments not described as equivalent; Some of the features described in the embodiments can also be implemented in other embodiments, alone or in combination; conversely, the various features described in the context of the various embodiments can also be separately or in any suitable sub-combination in other separate Implemented in multiple embodiments.
本發明說明書內容可能使用“第一”、“第二”等序數用語來描述元件，可以理解的是，這些序數用語僅用於區別一個元件或一個特徵與另一個元件或另一個特徵，而非用以限制元件之間的順序關係。本文中使用的單數形式“一個”、“一件”等數量用語亦包含複數形式的意義，除非上下文以其它方式清楚地指出該特徵不包含複數的數量。The content of the present specification may be used to describe elements using the ordinal terms such as "first" and "second", and it is understood that these ordinal terms are used only to distinguish one element or one feature from another or another feature, rather than Used to limit the order relationship between components. The singular forms "a", "an", "the", "
請同時參照圖1至圖3，圖1係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的立體組合圖，圖2係本實施例的組合前視圖，圖3係本實施例的第一動力組立體圖；本發明之無人載具10在本實施例中較佳係包含一主機體11、一主機翼12、偶數個第一動力組20及一第二動力組30。1 to FIG. 3, FIG. 1 is a perspective assembled view of an embodiment of the unmanned vehicle with vertical lifting and fast horizontal flying functions of the present invention, and FIG. 2 is a combined front view of the embodiment, and FIG. 3 is a In the present embodiment, the unmanned vehicle 10 of the present invention preferably includes a main body 11, a main wing 12, an even number of first power units 20, and a second power unit 30.
該主機體11界定一中央縱向面A及一前進方向D；該主機體11為一飛行載具之機身，由於飛行載具的型態多樣，本實施例揭示一種較常見的飛行載具但不以此為限，為了使飛行穩定不會偏移，主機體11通常為左右對稱的設計以使獲得左右平衡的空氣阻力，該左右對稱的分介面於本發明界定為一中央縱向面A，而該主機體11於水平飛行時的主要飛行方向界定為一前進方向D。The main body 11 defines a central longitudinal plane A and a forward direction D. The main body 11 is a fuselage of a flying vehicle. Due to various types of flying vehicles, the present embodiment discloses a more common flying carrier. Without limitation, in order to make the flight stability not shift, the main body 11 is generally designed to be bilaterally symmetrical so as to obtain a right and left balanced air resistance, which is defined as a central longitudinal plane A in the present invention. The main flight direction of the main body 11 when flying horizontally is defined as a forward direction D.
於本實施例中，該主機體11為了有較佳的操控穩定性及操控方便性，其較佳但非必要另包含一垂直尾翼111及一水平尾翼113，該垂直尾翼111設有一方向舵112，該水平尾翼113設有一升降舵114，該主機體11內部設有一控制套件13，該控制套件13透過一遙控器(未繪示)無線控制該方向舵112及該升降舵114作動，該垂直尾翼111、一水平尾翼113、方向舵112、升降舵114及該控制套件13均屬該無線遙控無人載具之習知技術，於此不再予以詳述；該控制套件13另包含電池、無線接收裝置、GPS定位裝置、陀螺儀裝置及微處理器等元件，甚至可包含攝影裝置以形成一空拍機，此亦屬於習知技術於此不予詳述。In the present embodiment, the main body 11 preferably has a vertical tail 111 and a horizontal tail 113 for better steering stability and handling convenience. The vertical tail 111 is provided with a rudder 112. The horizontal tail 113 is provided with an elevator 114. The main body 11 is internally provided with a control kit 13. The control unit 13 wirelessly controls the rudder 112 and the elevator 114 via a remote controller (not shown). The vertical tail 111 and the vertical tail 111 The horizontal tail 113, the rudder 112, the elevator 114, and the control kit 13 are all known technologies of the wireless remote control unmanned vehicle, and will not be described in detail herein; the control kit 13 further includes a battery, a wireless receiving device, and a GPS positioning device. The components such as the gyroscope device and the microprocessor may even include a photographing device to form an air paparator, which is also a conventional technique and will not be described in detail herein.
該主機翼12交叉結合於該主機體11，該主機翼12於該中央縱向面A兩側形成對稱設置；該主機翼12於本實施例中略成V形，但其可以是平直的水平機翼或是形成後掠翼，該主機翼12可以另設有副翼121以增加該無人載具10的操控性能，唯該副翼121非必要設置。The main wing 12 is cross-coupled to the main body 11. The main wing 12 is symmetrically disposed on both sides of the central longitudinal plane A. The main wing 12 is slightly V-shaped in this embodiment, but it may be a flat horizontal machine. The wing or the swept wing is formed. The main wing 12 may be further provided with an aileron 121 to increase the handling performance of the unmanned vehicle 10, except that the aileron 121 is not necessarily provided.
該偶數個第一動力組20於本實施例中之數量為2個，該2個第一動力組20於該中央縱向面A兩側對稱的設置於該主機翼12，該每一第一動力組20包含一方向變換馬達21及一螺旋槳馬達22，該方向變換馬達21固定於該主機翼12，該螺旋槳馬達22固定於一螺旋槳馬達座23，該螺旋槳馬達座23可樞轉的結合於該方向變換馬達21，該螺旋槳馬達22結合一螺旋槳24，使該螺旋槳24之一第一旋轉軸X可以改變方向；該方向變換馬達21可以直接固定於該主機翼12之前翼緣，或者可以如圖所示將該方向變換馬達21透過一延伸座212固定於該主機翼12，如此使該螺旋槳24可以較遠離該主機翼12，避免螺旋槳24打到主機翼12。The number of the first plurality of power units 20 in the present embodiment is two, and the two first power units 20 are symmetrically disposed on the main wing 12 on both sides of the central longitudinal plane A, and each of the first powers The set 20 includes a direction changing motor 21 and a propeller motor 22, and the direction changing motor 21 is fixed to the main wing 12. The propeller motor 22 is fixed to a propeller motor base 23, and the propeller motor base 23 is pivotally coupled thereto. a direction changing motor 21, the propeller motor 22 is combined with a propeller 24, such that the first rotating shaft X of the propeller 24 can change direction; the direction changing motor 21 can be directly fixed to the front flange of the main wing 12, or can be as shown in the figure The direction change motor 21 is shown secured to the main wing 12 by an extension seat 212 such that the propeller 24 can be remote from the main wing 12 to prevent the propeller 24 from hitting the main wing 12.
該偶數個第一動力組20如果數量為4個，則於該中央縱向面A兩側分別各設置2個第一動力組20，對稱的設置於該主機翼12兩側。If the number of the first plurality of first power groups 20 is four, two first power groups 20 are respectively disposed on two sides of the central longitudinal surface A, and are symmetrically disposed on both sides of the main wing 12.
該方向變換馬達21較佳但不限於係為伺服馬達，伺服馬達內部通常已經包含直流馬達及減速機構，其經常被使用作為遙控模型的舵機馬達；較佳地，該方向變換馬達21具有一旋轉盤211，螺旋槳馬達座23形成C字形由其二端結合於該旋轉盤211，該螺旋槳馬達22固定於該螺旋槳馬達座23，因此當方向變換馬達21作動時可帶動螺旋槳馬達22改變方向，進而改變螺旋槳24的第一旋轉軸X的方向。The direction change motor 21 is preferably, but not limited to, a servo motor. The servo motor usually includes a DC motor and a speed reduction mechanism, which is often used as a steering motor of a remote control model; preferably, the direction change motor 21 has a The rotary disk 211, the propeller motor base 23 is formed in a C shape, and the two ends thereof are coupled to the rotary disk 211. The propeller motor 22 is fixed to the propeller motor base 23, so that when the direction changing motor 21 is actuated, the propeller motor 22 can be driven to change direction. The direction of the first axis of rotation X of the propeller 24 is then changed.
該第二動力組30包含一螺旋槳馬達31，該螺旋槳馬達31結合一螺旋槳32，該第二動力組30固定設置於該主機體11之中央縱向面A上，該第二動力組30之螺旋槳32之一第二旋轉軸Y與所述前進方向D大約形成60至90度角設置；較佳地，該第二動力組30之螺旋槳32之第二旋轉軸Y與所述前進方向D形成90度直角設置。The second power unit 30 includes a propeller motor 31. The propeller motor 31 is coupled to a propeller 32. The second power unit 30 is fixedly disposed on the central longitudinal surface A of the main body 11. The propeller 32 of the second power unit 30 One of the second rotation axes Y and the advancing direction D are formed at an angle of about 60 to 90 degrees; preferably, the second rotation axis Y of the propeller 32 of the second power group 30 forms 90 degrees with the advancing direction D. Right angle setting.
於本實施例中，該第二動力組30係安裝於該主機體11之下方，其亦可安裝於主機體11上方，只需位於該中央縱面A，該2個第一動力組20與該第二動力組30就可以形成等腰三角形設置，如此三個動力組構成一三角形，當其中一角的施力方向改變就可能使另一個角形成支點而容易進行翻轉，如此使操控更靈活同時具有較佳的穩定性。In this embodiment, the second power unit 30 is mounted under the main body 11, and can also be mounted on the main body 11, only in the central longitudinal plane A, and the two first power units 20 and The second power group 30 can form an isosceles triangle arrangement, such that the three power groups form a triangle, and when the direction of the force applied to one of the corners changes, the other angle may form a fulcrum and is easily flipped, thereby making the manipulation more flexible. Has better stability.
參照圖4，係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的組合側視圖；如圖所示，該第一動力組20之螺旋槳24之第一旋轉軸X已從該前進方向D旋轉至向上90度，同時該第二動力組30之螺旋槳32之第二旋轉軸Y與所述前進方向D固定形成大約90度直角設置，於此狀態啟動該無人載具10，該第一動力組20之螺旋槳24以及該第二動力組30之螺旋槳32旋轉時都會把空氣帶動朝下方吹送，而產生一向上的反作用力將無人載具10帶離地面垂直升空。Referring to Figure 4, there is shown a combined side view of an embodiment of the unmanned vehicle having vertical lift and fast horizontal flight functions of the present invention; as shown, the first axis of rotation X of the propeller 24 of the first power pack 20 has been The forward direction D is rotated to an upward 90 degrees, and the second rotation axis Y of the propeller 32 of the second power group 30 is fixed to the forward direction D to form a right angle setting of about 90 degrees. In this state, the unmanned vehicle 10 is activated. When the propeller 24 of the first power unit 20 and the propeller 32 of the second power unit 30 rotate, the air is driven to be driven downward, and an upward reaction force is generated to bring the unmanned vehicle 10 vertically off the ground.
參照圖5，係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的動作示意圖；當無人載具10升空後，例用遙控器操作改變形進方向，則該該第一動力組20之螺旋槳24之第一旋轉軸X從向上90度的方向改為與該前進方向D平行的方向，同時該第二動力組30由於係固定於主機體11，其螺旋槳32之第二旋轉軸Y仍保持朝下方向使無人載具10保持具有一抬昇力，該第一動力組20的水平方向前進的力量加上該第二動力組30輔助該無人載具10浮升，使該無人載具10於此狀態可以保持快速水平飛行。5 is a schematic diagram of the operation of an embodiment of the unmanned vehicle with vertical lifting and fast horizontal flying functions of the present invention; when the unmanned vehicle 10 is lifted off, and the remote control is used to change the direction of the forming, the first The first rotation axis X of the propeller 24 of a power pack 20 is changed from a direction of upward 90 degrees to a direction parallel to the forward direction D, and the second power group 30 is fixed to the main body 11 by the propeller 32 The rotation axis Y remains in the downward direction to maintain the unmanned vehicle 10 with a lifting force, and the force of the first power group 20 in the horizontal direction plus the second power group 30 assists the unmanned vehicle 10 to rise. The unmanned vehicle 10 can maintain a fast horizontal flight in this state.
參照圖4至圖6，該螺旋槳馬達座23相對該方向變換馬達21樞轉的樞轉面，較佳地，係平行於該中央縱向面A。Referring to Figures 4-6, the pivoting surface of the propeller motor mount 23 relative to the direction changing motor 21 is preferably parallel to the central longitudinal plane A.
由本發明上述揭示之構造可以理解，該第一動力組20之螺旋槳24之第一旋轉軸X也可以從該前進方向D旋轉至向下90度(如圖6所示)，甚至設定各項控制參數使該二第一動力組20可以分開控制進行不同方向的調整，如此可以進行複雜的方向操作，例如可以完成螺旋路線的飛行或多方向的滾轉與翻滾。熟悉本發明領域之一般技術者可以瞭解，透過本發明揭示的結構可以使無人載具10達成垂直起降及快速水平飛行的目的，甚至可以進行複雜的飛行控制，而複雜的飛行控制可以透過現今的陀螺儀與微處理器的協同控制技術達成。該主機體11設有控制套件13，該控制套件13能透過一遙控器無線控制該方向變換馬達21作動及控制該螺旋槳馬達22的轉速，通過上述說明可以理解，本發明藉由特殊的三角設置的動力組來達成使無人載具可以垂直升降又可以快速改變狀態進行水平飛行，並且可以靈活的進行翻滾等飛行動作，係具有進步性。It can be understood from the above-discussed configuration of the present invention that the first rotation axis X of the propeller 24 of the first power unit 20 can also be rotated from the forward direction D to the next 90 degrees (as shown in FIG. 6), and even the various controls are set. The parameters enable the two first power units 20 to be separately controlled for adjustment in different directions, so that complicated direction operations can be performed, for example, flight of a spiral path or rolling and tumbling of multiple directions can be completed. Those of ordinary skill in the art will appreciate that the structure disclosed by the present invention allows the unmanned vehicle 10 to achieve vertical takeoff and landing and rapid horizontal flight, and even for complex flight control, while complex flight control can be achieved today. The gyroscope and the microprocessor's cooperative control technology are achieved. The main body 11 is provided with a control kit 13 which can wirelessly control the direction change motor 21 to operate and control the rotation speed of the propeller motor 22 through a remote controller. It can be understood from the above description that the present invention has a special triangular setting. The power group is made to make the unmanned vehicle can be vertically lifted and can quickly change the state for horizontal flight, and can flexibly perform tumbling and other flight actions, which is progressive.
該第一動力組20或第二動力組30之螺旋槳24、32可以進一步設有數個LED燈，該主機體11設有旋轉輪顯示控制器(未繪示，其為習知技術)，並且電性連接至該數個LED燈，當該螺旋槳旋轉時利用人眼視覺暫留效果可顯示文字或圖案，透過該LED的設置可以是本發明之具垂直升降及快速水平飛行功能之無人載具應用於天空的飛行廣告載具。The propellers 24, 32 of the first power unit 20 or the second power unit 30 may further be provided with a plurality of LED lamps, and the main body 11 is provided with a rotating wheel display controller (not shown, which is a conventional technique), and is electrically Sexually connected to the plurality of LED lights, when the propeller rotates, the human eye visual persistence effect can display text or a pattern, and the setting of the LED can be the unmanned vehicle application of the present invention with vertical lifting and fast horizontal flying functions. Flying advertising vehicle in the sky.
以上所述之實施例僅係為說明本發明之技術思想及特徵，其目的在使熟習此項技藝之人士均能了解本發明之內容並據以實施，當不能以此限定本發明之專利範圍，凡依本發明之精神及說明書內容所作之均等變化或修飾，皆應涵蓋於本發明專利範圍內。The embodiments described above are merely illustrative of the technical spirit and characteristics of the present invention, and the objects of the present invention can be understood by those skilled in the art and can be implemented according to the present invention. Equivalent changes or modifications made in accordance with the spirit of the invention and the contents of the specification are intended to be included within the scope of the invention.
10‧‧‧無人載具10‧‧‧No-man vehicle
11‧‧‧主機體11‧‧‧Host body
111‧‧‧垂直尾翼111‧‧‧Vertical tail
112‧‧‧方向舵112‧‧ rudder
113‧‧‧水平尾翼113‧‧‧Horizontal tail
114‧‧‧水平舵114‧‧‧ horizontal rudder
12‧‧‧主機翼12‧‧‧ main wing
121‧‧‧副翼121‧‧‧Aileron
13‧‧‧控制套件13‧‧‧Control kit
20‧‧‧第一動力組20‧‧‧First Power Group
21‧‧‧方向變換馬達21‧‧‧ Directional change motor
211‧‧‧旋轉盤211‧‧‧ rotating disk
212‧‧‧延伸座212‧‧‧Extension seat
22‧‧‧螺旋槳馬達22‧‧‧propeller motor
23‧‧‧螺旋槳馬達座23‧‧‧propeller motor seat
24‧‧‧螺旋槳24‧‧‧propeller
30‧‧‧第二動力組30‧‧‧Second Power Group
31‧‧‧螺旋槳馬達31‧‧‧propeller motor
311‧‧‧固定座311‧‧‧ Fixed seat
32‧‧‧螺旋槳32‧‧‧propeller
A‧‧‧中央縱向面A‧‧‧Central longitudinal face
D‧‧‧前進方向D‧‧‧ Forward direction
X‧‧‧第一旋轉軸X‧‧‧first rotating shaft
Y‧‧‧第二旋轉軸Y‧‧‧second rotating shaft
圖1係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的立體組合圖； 圖2係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的組合前視圖； 圖3係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的第一動力組立體圖； 圖4係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的組合側視圖； 圖5係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的動作示意圖； 圖6係本發明之具垂直升降及快速水平飛行功能之無人載具一實施例的動作示意前視圖。1 is a perspective assembled view of an embodiment of an unmanned vehicle having vertical lifting and fast horizontal flying functions of the present invention; FIG. 2 is a combination of an embodiment of the unmanned vehicle having vertical lifting and fast horizontal flying functions of the present invention. 3 is a perspective view of a first power pack of an embodiment of the unmanned vehicle with vertical lift and fast horizontal flight functions of the present invention; FIG. 4 is an implementation of the unmanned vehicle with vertical lift and fast horizontal flight functions of the present invention. FIG. 5 is a schematic view showing the operation of an unmanned vehicle with vertical lifting and fast horizontal flying functions according to the present invention; FIG. 6 is an unmanned vehicle having a vertical lifting and fast horizontal flying function according to the present invention. The action of the embodiment is a front view.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW106130255A TW201912226A (en) | 2017-09-05 | 2017-09-05 | Unmanned vehicle with vertical lifting and fast horizontal flying functions capable of reducing requirement of processor system and making flying more stable |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW106130255A TW201912226A (en) | 2017-09-05 | 2017-09-05 | Unmanned vehicle with vertical lifting and fast horizontal flying functions capable of reducing requirement of processor system and making flying more stable |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| TW201912226A true TW201912226A (en) | 2019-04-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| TW106130255A TW201912226A (en) | 2017-09-05 | 2017-09-05 | Unmanned vehicle with vertical lifting and fast horizontal flying functions capable of reducing requirement of processor system and making flying more stable |
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| TW (1) | TW201912226A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021134541A1 (en) * | 2019-12-31 | 2021-07-08 | 李庆远 | Intersecting multi-rotor display |
-
2017
- 2017-09-05 TW TW106130255A patent/TW201912226A/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021134541A1 (en) * | 2019-12-31 | 2021-07-08 | 李庆远 | Intersecting multi-rotor display |
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