M290065 八、新型說明： 【新型所屬之技術領域】 本創作係有關一種飛行器，尤指一種結構簡單而得以小型 化的微型飛行裝置。 【先前技術】 昆蟲的飛行運動，是一門深奥的學問。 以常見的果蠅為例，它們的飛行運動，包含了快速起飛、 > 盤旋、俯衝、急轉彎等等。這些高超的飛行技巧，讓果蠅得以 輕而易舉地進攻食物，並同時躲避人們的追殺。 它們是怎麼做到的？昆蟲輕薄的翅翼顯然與鳥類的大翅膀 作用不同。動物、航太、流體力學專家們，一直對自然界的生 物特別疋此触的飛行運動有莫大的興趣。不過這項運動還沒 有得到充分而完整的認識。 困難之處在於人們很難對三維空間的氣流活動做出精確的 | ^述，尤其H蟲翅翼周圍的氣體流動現象。H的翅翼特別 地小，動的特別地快，也特別的複雜。 早期的科學家是以分析（穩態空氣動力學） 和計算 jNavie卜St〇kes方程式）的方式來探究昆蟲飛行的機制，但 〜這兩種方式依舊幾法解釋昆蟲起飛或停滯於空中的行為，也無 法^整的描緣昆蟲的飛行。到了 1980年代，研究人員改以直接 測里的方式進行，將昆蟲的運動模式予以量化，才逐漸揭開昆 蟲飛行運動神秘面紗的一角。 5 M290065 關於昆蟲飛行的原理，如今已有許多論文進行討論研究， 而有了初步的認識。大體來說，翅翼的擺動方向與角度的不同， 將會產生疋的幵力。剞緣渴流（Leading-edge vortex)、延 缓失速（delayed stall)、旋轉昇力（r〇tati〇nHft)與尾波 捕獲（wake capture)等，由科學家自昆蟲飛行運動中所發現 的氣體流動現象，如今已有部分的應用。 雖然有許多原理已被科學家研究出來，但不代表可以就此 產出小型飛行器。在實際應用層面上，還是有許多技術問題尚 待克服。基於已知的氣體流動原理，美國專利公 2〇_55145舰揭露了_的飛行裝置。此案主要是在翅翼 =-端連設具有第-觀部與第二槽止部的凸輪，並利用驅動 =牽動驅動盤使其產生旋轉，進而帶動凸輪與翅翼產生運動而 飛了。另如美國專利公告第6,54〇，m號所揭露的飛行器，主 要疋使用了數個連桿的作動而模擬出蜻蜓的飛行運動。而美國 專利a。第6’530, 540號專利案岐揭露了搭載人類的飛行裝 斜專利案或習用飛行器，雖可運作而具有一定的效果， 裝置不是過於理想而難以實現，要不就是結構相當複 ^成本昂貴絲則、咖，⑽有缺撼 【新型内容】 有鐘於此，本創作乃揭雪 簡單而易於小型化之優勢種微行裝置，其具有結構 M290065 依據本創作所揭露之微型飛行裝置，主要包含了機體、第 -與第—飛行翼組、第—與第二角度控制器、掣動件與動力模 組。機體設有對應的右軸柱與左軸柱，第—飛行翼組設於機體 的右側，其包含有第—揮動臂與第-飛行翼，第-揮動臂之中 f適當處形成有可供右姉穿伸的第—透孔。第-角度控制器 又；第揮動#上，用以控制第一飛行翼相對於第一揮動臂的 擺㈣度。至於第二飛行翼組的組成與第-飛行翼組大致相 同1二角度控制器的配置與作用也與第—角度控制器一樣。 勺人拏動件的^與第—揮動臂、第二揮動臂相連。動力模組 匕3有驅動齒輪’以及用以連細I動錄旋轉的動力馬達。掣 動件之另端連設於驅動齒輪，以當驅動齒輪旋轉時，藉由掣動 件=併㈣第—揮動臂與第二揮動臂，致使第—飛行翼與第 氣行翼，分別以右軸柱與左軸柱為軸心而往復拍動。 ⑤為讓本創作之上述目的和其他目的、特徵、及優點能更明 ’’、、員易僅’下文特舉—較佳實施例，並配合所關示，作詳細說 明如下。 【實施方式】 依據本創作所揭露之微型飛行裝置，請參考「第丨圖」至 「第5圖」來說明其主要元件組成、結構特徵及其作動方式。 本創作之較佳實施例主要包含了機體1〇、第一飛行翼組 20、第一角度空翅翼30、第二飛行翼組40、第二角度控制器 50、掣動件80與動力模組60。機體1〇上分別設有右軸柱n M290065 與左軸柱12，第一飛行翼組2〇設在機體1〇的右側，主要由第 一揮動臂21與第一飛行翼22所組成。第一揮動臂21之一端開 設有第一透孔23與第一鎖孔24，而底侧設有長筒25，其中第 一透孔23穿套於右軸柱11。第一飛行翼22裝入長筒25内， 而可相對第一揮動臂21自由旋轉擺動。 第一飛行翼組40設在機體1〇的左侧，對稱於第一飛行翼 組20，其組成元件與元件作動關係與第一飛行翼組2〇相同。 丨 第二飛行翼組40，主要包含第二揮動臂41與第二飛行翼42所 組成。第二揮動臂41之一端開設有第二透孔43與第二鎖孔 44，而底侧設有長筒45，其中第二透孔仙穿套於左軸柱12。 第一飛行翼42裝入長筒45内，而可相對第二揮動臂41自由旋 轉擺動。 機體10上設有動力模組60，其包含有驅動齒輪62，動力 馬達61设在機體1〇的底側，動力齒輪肋設於驅動齒輪肋與 動力馬達61之間，並與兩者相互齧合。如此，動力馬達61將 可連動驅動齒輪62產生旋轉。 掣動件80的前端鑽設有第一圓孔81與第二圓孔82，後端 則設有擴孔83。使用固定件7〇穿越第一飛行翼組2〇的第一鎖 孔24而鎖於第一圓孔81，以讓第一飛行翼組2〇相連於掣動件 80。同理，將固定件71穿越第二飛行翼組40的第二鎖孔44， 而鎖於掣動件80的第二圓孔82，讓第二飛行翼組20相連於掣 動件80。固定件73穿越擴孔83，讓掣動件80的後端與驅動齒 8 M290065 輪62上的軸柱相連。 於是，動力馬達61被啟動後，將連_動齒輪62產生旋 轉’而一併牽動了掣動件80產生前進後退的直線往復運動，進 而帶動第—飛行翼組2G與第二飛行翼組分別以第右轴柱 η、左軸柱12為軸心而相對機體1G前後拍動，產生了如同昆 蟲拍動薄翼的飛翔作動。 下文將說明本創作之較佳實施例中的兩個角度控制器。本 創作中所包含的第-角度控制器3〇與第二角度器5〇，分別安 裝在第—-飛行翼組2G的第—揮動臂21上，以及第二飛行翼組 40的第一揮動臂41上。這兩個角度控制器的作用相同，因此 =下文帽以第-角度控㈣3{)為例予以制。第—角度控制 益30具有兩個活動板件，而這兩個活動板件是由第—倾 31來控制其相對展開的角度，藉以限制第一飛行翼&的擺動 角度耗圍。當第-飛行翼組2G以及第二飛行翼組4q變換拍動 方向時，所產生的跟隨氣流與慣性使得第—齡翼22盘第 ^翼42開始鶴，但是擺動會受稱―、第二角度控制器加、M290065 VIII. New description: [New technical field] This creation relates to an aircraft, especially a miniature flying device with a simple structure and miniaturization. [Prior Art] The flying movement of insects is an esoteric study. In the case of common fruit flies, their flight movements include rapid takeoff, > hovering, dive, sharp turns, and so on. These superb flying skills allow the fruit fly to easily attack the food while avoiding people's pursuit. How did they do it? The thin wings of insects clearly differ from the large wings of birds. Animals, aerospace, and fluid mechanics experts have always had a great interest in the natural movements of the creatures. However, the sport has not yet been fully and fully understood. The difficulty is that it is difficult to make accurate predictions about the airflow in three-dimensional space, especially the gas flow around the wing of the H-worm. The wings of H are particularly small, moving very fast and particularly complex. Early scientists used the analysis (steady-state aerodynamics) and the calculation of the jNavie's St〇kes equation to explore the mechanism of insect flight, but ~ these two methods still explain the behavior of insects taking off or stagnating in the air. It is also impossible to fly the entire insect. In the 1980s, the researchers changed the way of direct measurement to quantify the movement patterns of insects, and gradually unveiled the corner of the mysterious veil of insect flying. 5 M290065 With regard to the principle of insect flight, many papers have been discussed and studied, and there is a preliminary understanding. In general, the direction of the wing's swing is different from the angle, which will produce a sturdy force. Leading-edge vortex, delayed stall, rotating lift (r〇tati〇nHft) and wake capture, etc., the gas flow phenomenon discovered by scientists from insect flight movements Now there are some applications. Although many principles have been studied by scientists, it does not mean that small aircraft can be produced in this regard. At the practical level, there are still many technical issues that need to be overcome. Based on the known principle of gas flow, U.S. Patent No. 2, 55,145 ships unveiled the flight device. In this case, the cam with the first-view portion and the second groove-stop portion is connected to the wing-= end, and the drive plate is used to drive the disk to rotate, thereby driving the cam and the wing to generate motion and fly. In addition, as disclosed in U.S. Patent Publication No. 6,54, the aircraft disclosed in the No. m, the main cymbal uses several linkages to simulate the flying motion of the cymbal. And the US patent a. Patent No. 6'530, No. 540 discloses a patented mobile aircraft or a conventional aircraft equipped with humans. Although it can operate with certain effects, the device is not too ideal and difficult to implement, or the structure is quite complex and expensive. Silk, coffee, (10) has a lack of [new content] There is a clock here, this creation is a simple and easy to miniaturize the micro-row device, which has the structure M290065 according to the micro-flight device disclosed in this creation, mainly It includes the body, the first and the first flight wing group, the first and second angle controllers, the swaying parts and the power module. The body is provided with a corresponding right axis column and a left axis column. The first flight wing group is disposed on the right side of the body, and includes a first-swinging arm and a first-flying wing, and the first-swinging arm is formed at an appropriate position. The first through hole of the right ankle. The first-angle controller is further configured to control the pendulum (four) degrees of the first flying wing relative to the first swinging arm. As for the configuration of the second flight wing group and the first flight wing group, the configuration and function of the two angle controllers are also the same as those of the first angle controller. The scooping person's holding member is connected to the first-swinging arm and the second swinging arm. The power module 匕3 has a drive gear 'and a power motor for rotating the fine I. The other end of the swaying member is connected to the driving gear, so that when the driving gear rotates, by the swaying member=and (4) the first-swinging arm and the second swinging arm, the first flying wing and the second air-winging wing are respectively The right and left shaft columns are pivoted and reciprocated. 5 The above and other objects, features, and advantages of the present invention will become more apparent, and the description of the preferred embodiments will be described in detail below. [Embodiment] According to the micro-flight device disclosed in this creation, please refer to "Diagram" to "5th" to explain the main components, structural features and actuation methods. The preferred embodiment of the present invention mainly includes a body 1〇, a first flight wing group 20, a first angle air wing 30, a second flight wing group 40, a second angle controller 50, a tilting member 80 and a power module. Group 60. The right body column n M290065 and the left axis column 12 are respectively disposed on the body 1 , and the first flight wing group 2 is disposed on the right side of the body 1 , and is mainly composed of the first swing arm 21 and the first flying wing 22 . One end of the first swing arm 21 is provided with a first through hole 23 and a first lock hole 24, and the bottom side is provided with a long cylinder 25, wherein the first through hole 23 is sleeved on the right shaft column 11. The first flight wing 22 is loaded into the elongated cylinder 25 and is free to oscillate relative to the first swing arm 21. The first flight wing set 40 is disposed on the left side of the body 1 , and is symmetrical to the first flight wing set 20, and its constituent elements and component actuating relationship are the same as those of the first flight wing set 2〇. The second flying wing group 40 mainly comprises a second swinging arm 41 and a second flying wing 42. One end of the second swing arm 41 is provided with a second through hole 43 and a second lock hole 44, and the bottom side is provided with a long cylinder 45, wherein the second through hole is sleeved on the left shaft post 12. The first flight wing 42 is loaded into the elongated cylinder 45 and is free to swing relative to the second swing arm 41. The power module 60 is disposed on the body 10 and includes a driving gear 62. The power motor 61 is disposed on the bottom side of the body 1 , and the power gear rib is disposed between the driving gear rib and the power motor 61. Hehe. Thus, the power motor 61 rotates the linkable drive gear 62. The front end of the damper member 80 is drilled with a first circular hole 81 and a second circular hole 82, and the rear end is provided with a reaming hole 83. The first flight hole group 2 is locked to the first flight hole 81 by using the fixing member 7 to pass through the first locking hole 24 of the first flight wing group 2 to connect the first flight wing group 2 to the rocking member 80. Similarly, the fixing member 71 passes through the second locking hole 44 of the second flying wing group 40, and is locked to the second circular hole 82 of the swaying member 80, so that the second flying wing group 20 is connected to the damper 80. The fixing member 73 passes through the reaming hole 83, and the rear end of the damper member 80 is connected to the shaft post on the wheel 62 of the driving tooth 8 M290065. Then, after the power motor 61 is activated, the rotation gear of the linkage gear 62 is rotated, and the linear reciprocating motion of the forward movement back is generated by the movement member 80, thereby driving the first flight wing group 2G and the second flight wing group respectively. With the right axis column η and the left axis column 12 as the axis, the body 1G flaps forward and backward, and a flying action like an insect flapping thin wing is generated. Two angle controllers in the preferred embodiment of the present invention will be described below. The first-angle controller 3〇 and the second angler 5〇 included in the present creation are respectively mounted on the first swing arm 21 of the first flight wing group 2G, and the first swing of the second flight wing group 40 On the arm 41. The two angle controllers function the same, so = the following cap is based on the first-angle control (four) 3{). The first-angle control benefit 30 has two movable panels, and the two movable panels are controlled by the first tilting angle 31 to limit the angle of the swing of the first flying wing & When the first flight wing group 2G and the second flight wing group 4q change the flapping direction, the generated following airflow and inertia cause the first-age wing 22 disc wing 42 to start the crane, but the swing will be called "-, second Angle controller plus,
5〇展開肢的限_停止’如此變換兩麵行翼㈣度 獲得最大的昇力。 J 以上所述者，僅為本創作其中的較佳實施例而已，並 =定本新型的實施範圍；即凡依本創作中請專利範圍所 句專變化與修飾，皆為本創作專利範圍所涵蓋。 【圖式簡單說明】 M290065 々第1圖為本創作之微型飛行裝置之分解示意圖。 第2圖為本創作之微型飛行裝置之組合示意圖。 第3圖為本創作之微型飛行裝置之角度控制器示意圖 —弟4圖為本創作之微型飛行裝置之第-作動示意圖。 H林創作之微魏行裝置之第二作動示意圖。 要疋件符號說明】5〇The limit of the extended limb _stop' So change the two sides of the wing (four) degrees to get the maximum lift. J. The above is only the preferred embodiment of this creation, and = the scope of implementation of the new type; that is, the specific changes and modifications of the patent scope in this creation are covered by the scope of the creation patent. . [Simple description of the diagram] M290065 々 Figure 1 is an exploded view of the miniature flying device of the creation. Figure 2 is a schematic diagram of the combination of the miniature flying device of the present invention. The third figure is a schematic diagram of the angle controller of the micro-flight device of the creation. The figure 4 is the first-acting diagram of the micro-flight device of the creation. The second actuating diagram of the Wei Weixing device created by H Lin. Instructions for the symbol
10機體 11 右軸柱 12 左軸柱 20 第一飛行翼組 21 第一揮動臂 22 第一飛行翼 23 第一透孔 Μ 第一鎖孔 25 長筒 30 第一角度控制器 31 第一伺服馬達 40 第二飛行翼組 41 第二揮動臂 42 第二飛行翼 43 第二透孔 44 第二鎖孔 10 M290065 長筒 ❿ 第二角度控制器 第二伺服馬達 動力模組 動力馬達 驅動齒輪 動力齒輪 固定件 固定件 固定件 掣動件 第一圓孔 第二圓孔 擴孔 1110 body 11 right axis column 12 left axis column 20 first flight wing group 21 first swing arm 22 first flight wing 23 first through hole Μ first lock hole 25 long cylinder 30 first angle controller 31 first servo motor 40 second flight wing group 41 second swing arm 42 second flight wing 43 second through hole 44 second lock hole 10 M290065 long cylinder ❿ second angle controller second servo motor power module power motor drive gear power gear fixed Piece fixing member fixing member first round hole second round hole reaming 11