M358789 五、新型說明： 【新型所屬之技術領域】 本創作為一種輕於空氣之飛行器’尤指係「飛行器起降推進 控制器」結構，該係針對懸浮於空中飛船類的方向控制改良，使 飛船飛行器不僅能夠漂浮於空中，更能改變漂浮的角度與控制加 速前進。 【先前技術】 按，飛船等型態之飛行器，係利用輕於大氣的氣體加注於飛 船内，使飛船能夠漂浮於空中俾進行移動，雖然該種飛行方式緩 慢’使用當成交通工具不具經濟價值，但卻能夠·來當成，商 業廣告宣傳、觀光旅遊、地理探勘、農藥肥料倾之用，正因飛 船能夠停滯鮮，或緩慢移動，因此用於上述崎，效果甚至更 優於移動迅速的飛機。 對方向的控制設 /船所使用的W原理’僅能單純的改變離地高度 做位置的移動，因此還需另外裝設推進器^法 氣動力方式n法使賴料伽紅° Λ③^係為空 體遇高溫容耐;：===飛船所使用的氣 十尤其是飛船移動的高度與角度均可變化。 向，還 而目_胁控⑽觀㈣績_触 見改變垂直糊度麵物辦㈣計方 M358789 【新型内容】 欲解決之技術問題點 目則習知_的_僅能控制前進速度與水平移動方向 未見改《直方向奴與迅速改變漂浮高度之設計，跡畔 勘之攝影上使用效果欠佳，此乃欲解決之技術問題點。、 解決問題之技術特點： • 本創作係提供—種飛行器起降推進控制器，係包含：—引擎 本體’設有賴π與出風σ ;二鋪風雜，係裝設於引擎本體 ⑽’以轉動吸人氣體再排出產生推力；複數控制板組成，該些 複數控制板係水平且平行設置於該出風口位置，且具角度擺動特 性；-擺動控· ’係連接該複數控雛，供鋪該控制板同步 產生擺動的肖錢化，藉此俾峨可㈣起降與推進的飛行器 制器。 °工 對照先前技術之功效： 本創作之主要目的乃係提供飛行器起降推進控制器，係利用 该旋轉風扇組轉動產生的推力，經過該控制板，而該控制板並被 該擺動控制組控制而能調整擺動角度，其角度係能水平方向、下 賴角度與上仰角度，藉此使飛行器得以水平方向直線移動，或傾 斜。周正下降向度，又或傾斜§周整上昇高度而移動，令飛行器能夠 迅速的改變漂浮高度者。 M358789 【實施方式】 為使貴審查委員對本創作之目的、特徵及功效能夠有更進 一步之瞭解與認識，以下茲請配合【圖式簡單說明】詳述如后： 首先，先請由第1、2及3圖所示觀之，包含有： 引擎本體10，5亥如方一側各具有一進風口 η，後方且有— 出風口 12，該引擎本體1〇係裝設於飛行器上； 二旋轉風扇組20，係裝設於引擎本體10内部，具有控制旋轉 動力，該旋轉風扇組20轉動係由該進風口 u吸入氣體再由該出 風口 12排出，以使該引擎本體10與裝設的飛行器產生—股推 另該出風口 12並呈現下縮上凸出的傾斜狀； 稷數控制板30組成，該些複數控制板3〇係水平且平行設置 於該㈣口 12位置，且具角度擺動雛，由额轉㈣組^排 出的乳體係經過該複數控制板30再由該出風口 12排出· ⑽一擺動控制㈣，係包含：-馬達41、—連接桿42,、一擺動 ^以… 4及—連動桿45，該侧設在刻擎本體10， ^馬達41偏心插接該連接桿42 一端，再以該連接桿 ==:43—端，該固定桿44係固定在刻擎本體10端部 該連動、中&樞接，S_桿43另—端則與連動桿45樞接， 干5連接該各控制板30，該馬達41的轉氣备 桿42帶動哕d 專動係控制該連接 動句罷動桿43於該固定桿44上擺動 擺動並令該遠勒炉^ ^ ώ 与 碳杬動杯43的 _干45在-絲上婦，如鱗動桿&控制該 M358789 各控制板30同步產生上、下擺動的角度變化。 用則工制月；(進暨起降時，該旋轉風扇組别的轉動，使由該進 風口 π吸入氣體後由該出風口 12排出而產生一股推力，該推力 的方向亚由該複數控制板加操作，先由第4圖觀之，當飛行器需 ^水平角度前進時，動控制組4〇的馬達41作動於活動範圍 x。亥連接才干42赵由該擺動桿43將該連動桿45拉動， 細妾該連動捍45的複_板3_被_動，且擺動為 ’令該旋轉風扇組2〇產生的推力順著該控制板3〇的水 w又Λ Λ時飛行器即為水平方向直線移動； 再由第5圖觀之，當飛行器需要調整高度而下降時 ==崎41物输，喝跡42經蝴咖 f 45住上拉動’使連接該連動桿45的複數控制板3〇同 的L工制擺動呈現内上外下的下傾角度，令該旋轉風扇組2〇產生 、力在斜下方噴出’㈣飛行^則呈現頭部往下的傾斜前進， 即為下降之調整高度移動； 的^後由第6圖觀之，當飛行器需要上昇時，該擺動控制組40 r沾/1作動在則推’以該連接桿42經由該擺動桿43將該連動 見下內推動㈣接該連動桿45的複數控制板3〇同時被控制 ^上下夕上角度’令該旋轉風扇組20產生的推力往 ，㈣肪綱雜上關㈣ 之調整高度移動。 馮上汁 M358789 本創作的起 藉上述具體實施例之結構，可得到下述之效益： 降推進控制器，利用兮 ^ 麻如,麵轉風扇組20轉動產生的推力，經過該控 蝴空制板30並被該擺動控制組40控制而能調整擺動 时又，其肖度絲水平方向、下_度與上仰肢，藉此使飛行 糾寻以水平方向錄移動，或傾斜調整下降高度，又或傾斜調整 上昇高度而料，令齡軸改魏浮高度者。 M358789 【圖式簡單說明】 第1厨.係摘作的結構組成立體圖。 第―2圖.係本創作另—歧的結構組成立體圖。 第3圖.係本到作仰视剖面暨吸風排風示意圓。 第4圖係本創作側視剖面暨控制水平前進 f 5圖.:係摘作舰剖面暨控制下傾前私= 第6圖.係摘作側視剖面暨控制上仰—^ 疋不意圖 【主要元件符號說明】 本創作部份： 進風口 〜 旋轉風扇級. 擺動控制級. 連接桿一〜. 固定桿一〜. 引擎本體〜〜—10 11 20 40 42M358789 V. New Description: [New Technology Field] This creation is a lighter-than-air vehicle, especially the structure of the "aircraft take-off and landing propulsion controller", which is designed to improve the direction of suspension in the airship. The spacecraft can not only float in the air, but also change the angle of floating and control to accelerate. [Prior Art] According to the spacecraft of the spacecraft, it is filled with the gas lighter than the atmosphere, so that the spacecraft can float in the air and move, although the flight mode is slow, the use of the vehicle is not economical. However, it can be used as a commercial, commercial propaganda, sightseeing, geo-exploration, pesticides and fertilizers, because the spacecraft can be stagnant or slowly moving, so it is even better than the fast-moving aircraft. . The control principle of the direction/the W principle used by the ship can only simply change the height from the ground to make the position move. Therefore, it is necessary to additionally install the propeller to control the aerodynamic method. For the air body to meet the high temperature tolerance;: === The gas used by the spacecraft, especially the height and angle of the spacecraft movement can be changed. To, but also the purpose _ threat control (10) view (four) performance _ touch change vertical paste surface material office (four) meter side M358789 [new content] to solve the technical problems point of knowledge _ _ can only control the speed and level of advancement The direction of movement has not changed. The design of direct-slave and rapid change of floating height, the use of photography on the trailside survey is not good, this is the technical problem to be solved. Technical characteristics of solving problems: • This creative department provides a kind of aircraft take-off and landing propulsion controller, which includes: - the engine body 'is provided with π and feng σ; the second shop is windy, is installed on the engine body (10)' Rotating the inhaling gas to discharge and generating the thrust; the plurality of control panels are formed, the plurality of control panels are horizontally and parallelly disposed at the position of the air outlet, and have an angular swing characteristic; - swing control · 'connects the complex NC chick, for paving The control panel synchronously generates the oscillating weight, thereby enabling the aircraft to take off and land with the propulsion. The main purpose of this work is to provide an aircraft take-off and landing propulsion controller, which uses the thrust generated by the rotation of the rotating fan group, passes through the control board, and the control board is controlled by the swing control group. The angle of the swing can be adjusted, and the angle can be horizontal, the lower angle and the upper angle, thereby allowing the aircraft to move linearly in the horizontal direction, or tilt. Zhou Zheng is descending, or tilting § to move around the height of the rise, so that the aircraft can quickly change the height of the float. M358789 [Embodiment] In order to enable your review committee to have a better understanding and understanding of the purpose, features and effects of this creation, please refer to the following [Simplified description of the drawings] as follows: First, please first 2 and 3, including: the engine body 10, 5 haifang side has an air inlet η, the rear has - air outlet 12, the engine body 1 is mounted on the aircraft; The rotating fan unit 20 is mounted inside the engine body 10 and has control of rotational power. The rotating fan unit 20 is rotated by the air inlet u and then discharged by the air outlet 12 to install the engine body 10 and the engine. The aircraft generates - the other air outlet 12 and presents a downwardly convex slanting shape; the number of control panels 30 are formed, the plurality of control panels 3 are horizontally and parallelly disposed at the (four) port 12 position, and The angle swinging, the milk system discharged from the front turn (four) group ^ is discharged from the air outlet 12 through the plurality of control panels 30. (10) A swing control (4), comprising: - a motor 41, a connecting rod 42, a swing ^ With ... 4 and - linkage rod 45, The side is disposed on the engraving body 10, the motor 41 is eccentrically inserted into one end of the connecting rod 42, and the connecting rod is fixed at the end of the engraving body 10 by the connecting rod==:43-end. & pivoting, the other end of the S_rod 43 is pivotally connected with the linkage rod 45, and the dry 5 is connected to the control panels 30, and the venting reserve rod 42 of the motor 41 drives the 哕d dictator system to control the connection verb The moving rod 43 swings and swings on the fixed rod 44 and synchronizes the far-reaching furnace with the carbon-powered cup 43 on the wire, such as the scale rod & controls the M358789 control boards 30. The angle of the upper and lower swings is varied. The working system is used for the month; (when entering and taking off and landing, the rotation of the rotating fan group causes the air inlet π to be sucked out of the air outlet 12 to generate a thrust, and the direction of the thrust is subdivided by the plural The control panel is added and operated. First, it is viewed from Fig. 4. When the aircraft needs to advance at a horizontal angle, the motor 41 of the motion control group 4 作 operates in the range of motion x. The connection function 42 Zhao is connected to the linkage rod by the swing lever 43. 45 pulling, finely tweeting the complex _ plate 3_ of the linkage 捍 45, and swinging to 'the thrust generated by the rotating fan group 2 顺 along the water of the control panel 3 Λ Λ Λ 飞行The horizontal direction moves linearly; then, as shown in Fig. 5, when the aircraft needs to adjust the height and descends, == Saki 41, the stalk 42 is pulled by the butterfly f 45, and the multi-control panel connecting the linkage rod 45 is made. 3 The same L-engine swing shows the downward tilting angle of the inner upper and lower sides, so that the rotating fan group 2〇 is generated, and the force is ejected obliquely downwards. ((4) Flight ^, the head is tilted downward, which is the descending Adjust the height of the movement; after the ^ is viewed by Figure 6, when the aircraft needs to rise, the pendulum When the control group 40 r/1 is actuated, the connecting rod 42 is pushed through the swing lever 43 to push the joint (4) and the plurality of control panels 3 of the linkage rod 45 are simultaneously controlled. The thrust generated by the rotating fan unit 20 is moved to the adjusted height of (4) the intermediate miscellaneous (4). Feng Shang juice M358789 The following benefits of the above specific embodiment can be obtained: By using 兮^麻如, the thrust generated by the rotation of the face-turning fan group 20 is controlled by the swing control panel 40 and can be adjusted by the swing control panel 40, and the horizontal direction and the lower _degree of the louver With the upper limb, thereby making the flight correction move in the horizontal direction, or tilting to adjust the descending height, or tilting to adjust the rising height, and the age axis is changed to the height of the Wei float. M358789 [Simple diagram description] 1st The kitchen is a three-dimensional diagram of the structural composition of the painting. The second figure is a three-dimensional diagram of the structure of the creation of the creation. The third figure is the outline of the vertical view and the wind and the exhaust. The fourth picture is the creation. Side view profile and control level advance f 5 diagram.: Extracted from the ship profile and control down the front private = Figure 6. The system is extracted as a side view and control up -^ 疋 Not intended [Main component symbol description] This part of the creation: Air inlet ~ Rotating fan level. Swing control Level. Connecting rod one ~. Fixing rod one ~. Engine body ~~10 11 20 40 42
出風口 —~ — ___ __ 12 控制板一一—gQ 馬達一一~~ — —<41 擺動桿一〜〜 連動桿一一~~ —45 44Air outlet —~ — ___ __ 12 Control panel one by one—gQ motor one by one~~ — —<41 swinging lever one~~ linkage lever one~~~45 44