TW201300285A - Helicopter with three axles - Google Patents
Helicopter with three axles Download PDFInfo
- Publication number
- TW201300285A TW201300285A TW100121198A TW100121198A TW201300285A TW 201300285 A TW201300285 A TW 201300285A TW 100121198 A TW100121198 A TW 100121198A TW 100121198 A TW100121198 A TW 100121198A TW 201300285 A TW201300285 A TW 201300285A
- Authority
- TW
- Taiwan
- Prior art keywords
- axis
- helicopter
- load
- shaft
- assembly
- Prior art date
Links
Landscapes
- Toys (AREA)
Abstract
Description
本發明係有關於一種三軸直升機，尤其是指一種具有收折機構，而能將展開時體積龐大之三軸直升機縮減所佔用之空間，以方便收藏或運送者。The present invention relates to a three-axis helicopter, and more particularly to a folding mechanism that can reduce the space occupied by a three-axis helicopter that is bulky during deployment to facilitate collection or transport.
按，直升機一直是最便利的空中交通工具，也是重要的空中武力之一，而直升機之所以被廣泛運用，主要是因為直升機是以垂直的方式進行起飛與降落，無須跑道助跑，不受空間的限制。According to the helicopter, the helicopter has always been the most convenient air transport and one of the important airborne forces. The reason why the helicopter is widely used is mainly because the helicopter takes off and land in a vertical way, without running the runway, without space. limit.
觀察目前用於救災的直昇機均是採用真人駕駛的方式，因此出動救災任務時，必須先考量天候或環境等外在因素是否會影響到救援者的人身安全，而救災又具有急迫性，尤其受難者的生命一刻也不容延緩，但因為上述之情形，常常使救災的時效性受到延誤，失去救災的先機。Observing that the helicopters currently used for disaster relief are driven by real people, when dispatching disaster relief tasks, it is necessary to first consider whether external factors such as weather or environment will affect the personal safety of rescuers, and disaster relief is urgent, especially suffering. The life of the person can not be delayed for a moment, but because of the above situation, the timeliness of disaster relief is often delayed, and the opportunity for disaster relief is lost.
另外，在農業上，通常是以人力揹負農藥桶進行噴灑農藥之作業，此情形不僅增加農民體力的消耗，而且長時間的揹負重物也容易造成農民身體受傷，不僅費時且傷身。這種情形，在大面積的農藥噴灑作業時，更顯吃力，而且必須花費相當長的時間。尤其目前供使用於噴灑農藥的輕型飛機，並不具有可收折之功能，因此在不使用收藏時，或是搬遷運輸時，因其體積過於龐大備顯困擾與不便。In addition, in agriculture, it is usually carried out by manpower carrying pesticide buckets to spray pesticides. This situation not only increases the consumption of farmers' physical strength, but also causes heavy injuries to farmers during long periods of time, which is not only time-consuming but also harmful. In this case, it is more difficult to spray a large area of pesticides, and it takes a long time. In particular, the light aircraft currently used for spraying pesticides does not have the function of being able to be folded. Therefore, when the collection is not used, or when the transportation is moved, the volume is too large and it is troublesome and inconvenient.
若能提供一種直升機，使其平常可供遊戲消遣，而在需要提供其他如救災或農用之時，又可隨時裝載，具備高機動性，並能減少其受天候或地形之限制，以及在收藏或運載時的體積能夠縮減，將可提升該直升機的適用性；緣是，本發明人即是基於此，而研發創設出本發明之三軸直升機。If you can provide a helicopter that is usually available for game play, and when you need to provide other disaster relief or agricultural use, you can load it at any time, it is highly maneuverable, and it can reduce its weather or terrain restrictions, and in the collection. Or the volume at the time of carrying can be reduced, which will improve the applicability of the helicopter; the reason is that the inventors have developed a three-axis helicopter of the present invention based on this.
本發明之三軸直升機的主要目的，係提供一種在未飛行時能將二側之翼軸部件收折，以縮小體積，進而減少空間的佔用，而利於收藏或承載、運送之三軸直升機者。The main purpose of the three-axis helicopter of the present invention is to provide a three-axis helicopter capable of folding the wing components of the two sides when not flying, thereby reducing the volume and thereby reducing the space occupation, and facilitating the collection or carrying and transporting. .
本發明之三軸直升機的其一次要目的，是能夠因應三軸直升機執行任務的不同，而掛載不同之負載。One of the primary purposes of the three-axis helicopter of the present invention is to be able to mount different loads depending on the tasks performed by the three-axis helicopter.
本發明之三軸直升機的其二次要目的，是利用摩擦的方式將動力傳遞給螺旋槳，以受到外力時，能夠釋放衝擊力，避免損及動力組，且亦無崩牙之情形產生。The secondary purpose of the three-axis helicopter of the present invention is to transmit the power to the propeller by means of friction, so that when the external force is applied, the impact force can be released, the power group can be prevented from being damaged, and no broken teeth are generated.
本發明之三軸直升機的其三次要目的，是透過降落傘的配置，使該三軸直升機在失去動力之時，仍然可以安然著陸。The three main purpose of the three-axis helicopter of the present invention is that through the configuration of the parachute, the three-axis helicopter can still land safely when power is lost.
本發明之三軸直升機的其四次要目的，是透過控制尾軸部件的偏轉角度，達到控制三軸直升機行進方向者。The four-time objective of the three-axis helicopter of the present invention is to control the direction of travel of the three-axis helicopter by controlling the deflection angle of the tail shaft member.
上述本發明之主要目的與各次要目的，是由以下之具體技術手段所達成：The above main objectives and secondary objectives of the present invention are achieved by the following specific technical means:
本發明之三軸直升機，係在一三軸組裝座體上等角銜接一尾軸部件與二翼軸部件，該尾軸部件與該二翼軸部件上均搭載動力組與為動力組所驅動之螺旋槳，且該二翼軸部件與該三軸組裝座體間具有收折機構，當不使用該三軸直升機時，並能令該二翼軸部件藉由該收折機構而收折且靠置於尾軸部件的二側，以縮減三軸直升機所佔用之空間，方便使用者收藏與運送。The three-axis helicopter of the present invention is a three-axis assembly body that equidistantly engages a tail shaft member and a two-wing shaft member, and the tail shaft member and the two-wing shaft member are both powered by a power pack and driven by a power pack. a propeller having a folding mechanism between the two-shaft assembly and the three-axis assembly body, and when the three-axis helicopter is not used, the two-wing shaft member can be folded by the folding mechanism It is placed on the two sides of the tail shaft component to reduce the space occupied by the three-axis helicopter, which is convenient for users to collect and transport.
本發明之三軸直升機，係在該三軸組裝座體下方組裝一負載，其中，該負載的二側各有容置空間，以搭載人員或物品，使該直升機可作為救援用之飛行用具。The three-axis helicopter of the present invention assembles a load under the three-axis assembly base, wherein each side of the load has a receiving space for carrying people or articles, so that the helicopter can be used as a rescue flying device.
其中，該容置空間內可進一步裝載儲液桶，儲液桶內可盛裝水或農藥，再配合負載上所設置之噴灑裝置，便能令本發明之三軸直升機作為灑水或噴灑農藥之消防或農用機具。Wherein, the storage space can be further loaded with a liquid storage tank, and the liquid storage tank can hold water or pesticide, and then the spray device provided on the load can make the three-axis helicopter of the present invention be used as a watering or spraying pesticide. Fire or agricultural equipment.
本發明之三軸直升機，在負載處裝設有起落架，使該三軸直升機能降落於地面上；或是在負載處裝設有浮板，使該三軸直升機能降落於水面上。The three-axis helicopter of the present invention is equipped with a landing gear at the load to enable the three-axis helicopter to land on the ground, or a floating plate at the load to enable the three-axis helicopter to land on the water surface.
本發明之三軸直升機，其動力組之動力輸出軸上套設有主傳動輪，主傳動輪的上、下位置處設有轉動元件，在上、下轉動元件間且與主傳動輪相對應之處設有輔助傳動輪，主傳動輪與輔助傳動輪之輪面與上、下轉動元件之輪面摩擦接觸，使主傳動輪利用摩擦傳動方式帶動上、下轉動元件旋轉。當遇到鳥擊時，能釋放衝擊力，避免動力組損壞。In the three-axis helicopter of the present invention, the power transmission shaft of the power unit is sleeved with a main transmission wheel, and the upper and lower positions of the main transmission wheel are provided with rotating elements, and the upper and lower rotating elements are corresponding to the main transmission wheel. The auxiliary transmission wheel is provided, and the tread surface of the main transmission wheel and the auxiliary transmission wheel is in frictional contact with the tread surface of the upper and lower rotating elements, so that the main transmission wheel drives the upper and lower rotating elements to rotate by the friction transmission mode. When a bird strike is encountered, the impact force can be released to avoid damage to the power pack.
本發明之三軸直升機，進一步在三軸組裝座體上配設降落傘，在動力組無法提供動力時，能利用降落傘使該三軸直升機安全著陸。The three-axis helicopter of the present invention further has a parachute on the three-axis assembly base, and the three-axis helicopter can be safely landed by the parachute when the power unit cannot provide power.
本發明之三軸直升機，更進一步在三軸組裝座體與尾軸部件之間裝設有方向控制裝置，以利用該方向控制裝置驅動尾軸部件正向或反向偏轉，使該三軸直升機能執行轉彎之動作。The three-axis helicopter of the present invention further includes a directional control device between the three-axis assembly base and the tail shaft member to drive the tail shaft member to deflect forward or reverse by using the directional control device to make the three-axis helicopter Can perform the turning action.
為令本發明所運用之技術內容、發明目的及其達成之功效有更完整且清楚的揭露，茲於下詳細說明之，並請一併參閱所揭之圖式及圖號：For a more complete and clear disclosure of the technical content, the purpose of the invention and the effects thereof achieved by the present invention, it is explained in detail below, and please refer to the drawings and drawings:
請參第一圖，本發明之三軸直升機係包括有一三軸組裝座體（１）、一尾軸部件（２）、二翼軸部件（３）、三動力組（４）及三螺旋槳（５）；其中：Referring to the first figure, the triaxial helicopter of the present invention comprises a three-axis assembly base (1), a tail shaft member (2), two wing members (3), a three-power group (4) and three propellers. (5); where:
在該三軸組裝座體（１）上等角設置有延伸臂（１１），各延伸臂（１１）內裝載有燃料【圖中未表示】，且各延伸臂（１１）末端分別銜接該尾軸部件（２）與該二翼軸部件（３），且該尾軸部件（２）與該二翼軸部件（３）上各自搭載一動力組（４）與一螺旋槳（５），並令各動力組（４）各自驅動該些螺旋槳（５），該些螺旋槳（５）均是由上、下螺旋槳（５１）、（５２）組成；另，該二翼軸部件（３）與該三軸組裝座體（１）的二延伸臂（１１）間各自透過一收折機構（６）銜接組設。An extension arm (11) is disposed at an equiangular angle on the three-axis assembly base (1), and each extension arm (11) is loaded with fuel (not shown), and the ends of each extension arm (11) respectively engage the tail a shaft member (2) and the two wing member (3), wherein the tail shaft member (2) and the two wing member (3) are respectively equipped with a power unit (4) and a propeller (5), and Each of the power units (4) respectively drives the propellers (5), and the propellers (5) are composed of upper and lower propellers (51) and (52); in addition, the two-wing shaft members (3) and the three The two extension arms (11) of the shaft assembly base (1) are respectively connected to each other through a folding mechanism (6).
據此，透過在三軸組裝座體（１）之延伸臂（１１）內部裝載之燃料供應予動力組（４），使各動力組（４）同時驅動各個上、下螺旋槳（５１）、（５２）旋轉，使該三軸直升機得以上升與飛行。Accordingly, the fuel loaded inside the extension arm (11) of the three-axis assembly base (1) is supplied to the power group (4), so that each power group (4) simultaneously drives each of the upper and lower propellers (51), ( 52) Rotation to allow the three-axis helicopter to rise and fly.
當不使用該三軸直升機時【參第二、三圖】，便能透過解除位在該三軸組裝座體（１）之二延伸臂（１１）與該二翼軸部件（３）間之收折機構（６）展開固定之上鎖狀態，令該二翼軸部件（３）自該收折機構（６）處凹折，並因此收折靠置於該尾軸部件（２）的二側，藉以縮減該三軸直升機所佔用之空間，進而方便使用者收藏與運送。When the three-axis helicopter is not used [refer to the second and third figures], it can be released between the two extension arms (11) of the three-axis assembly base (1) and the two-wing shaft member (3). The folding mechanism (6) is unfolded in a fixed upper lock state, so that the two wing member (3) is concavely folded from the folding mechanism (6), and thus the folding hinge is placed on the tail shaft member (2) On the side, the space occupied by the three-axis helicopter is reduced, thereby facilitating the collection and transportation of the user.
請參第三、四圖，上述之收折機構（６）是透過設在該延伸臂（１１）與該翼軸部件（３）一側之鉸鍊元件（６１）及設置在相對側之鎖固元件（６２）組成，當釋放鎖固元件（６２）之上鎖狀態時，便能藉由鉸鍊元件（６１）的樞連將該二翼軸部件（３）收折於該尾軸部件（２）的二側；而當令該鎖固元件（６２）上鎖時，該二翼軸部件（３）則成展開狀態。Referring to Figures 3 and 4, the above-mentioned folding mechanism (6) is through a hinge member (61) provided on one side of the extension arm (11) and the wing member (3) and a locking member disposed on the opposite side. The component (62) is configured to fold the two-wing shaft member (3) to the tail shaft member by pivoting the hinge member (61) when the locking member (62) is locked. The two sides of the locking member (62) are in an unfolded state when the locking member (62) is locked.
本發明之三軸直升機，係進一步在該三軸組裝座體（１）下方組裝一負載（７）【請參第二圖】，其中，該負載（７）在其重心處設置一組裝軸（７１），而在該三軸組裝座體（１）之重心處設有組裝孔（１２），利用該組裝軸（７１）穿設該組裝孔（１２）後並加以鎖設固定，便能將該負載（７）裝載於三軸組裝座體（１）的下方，同時藉由連結組裝處均在重心位置，故能保持該三軸直升機飛行時的平穩性。The three-axis helicopter of the present invention further assembles a load (7) under the three-axis assembly base (1) [refer to the second figure], wherein the load (7) is provided with an assembly shaft at its center of gravity ( 71), an assembly hole (12) is disposed at a center of gravity of the three-axis assembly base (1), and the assembly hole (12) is inserted through the assembly shaft (71) and locked and fixed. The load (7) is loaded under the three-axis assembly base (1), and at the center of gravity by the joint assembly, the stability of the three-axis helicopter during flight can be maintained.
其中，該負載（７）的二側各有容置空間（７２），可供搭載人員或物品，使該三軸直升機成為一救援用或運送物資之飛行用具。The two sides of the load (7) each have a receiving space (72) for carrying people or articles, so that the three-axis helicopter becomes a flight aid for rescue or transportation materials.
其中，該容置空間（７２）內可進一步裝載儲液桶（７３），該儲液桶（７３）內可盛裝水或農藥，再搭配該負載（７）上所設置之噴灑裝置【圖中未表示】，便能令本發明之三軸直升機成為一灑水或噴灑農藥用之消防或農用機具。Wherein, the accommodating space (72) can further be loaded with a liquid storage tank (73), wherein the liquid storage tank (73) can be filled with water or pesticide, and then matched with the spraying device provided on the load (7). Not shown, the three-axis helicopter of the present invention can be used as a fire or agricultural implement for sprinkling water or spraying pesticides.
其中，本發明之三軸直升機，可再進一步於該負載（７）底部裝設支撐用之起落架（７４），藉由該起落架（７４）的設置，使該三軸直升機能降落、停放於地面上；或是在該負載（７）的底部裝設有浮板（７５），以利用該浮板（７５）的設置，使該三軸直升機能降落並停放於水面上。Wherein, the three-axis helicopter of the present invention can further install a support landing gear (74) at the bottom of the load (7), and the three-axle helicopter can be landed and parked by the setting of the landing gear (74). On the ground; or at the bottom of the load (7) is equipped with a floating plate (75) to enable the three-axis helicopter to land and park on the water surface by the arrangement of the floating plate (75).
另外，本發明之三軸直升機的動力組（４）在其動力輸出軸（４１）上固設有一主傳動輪（４２）【參第五圖】，該主傳動輪（４２）的表面為一粗糙面，該主傳動輪（４２）的上、下位置處各設置有一與其表面接觸的轉動元件（４３），該上、下轉動元件（４３）在與該主傳動輪（４２）相接觸的表面亦為呈粗糙面，又為了平衡該上、下轉動元件（４３）的支撐力，故在相對於該主傳動輪（４２）設置處的一側，且為該上、下轉動元件（４３）之間設有一輔助傳動輪（４４），該輔助傳動輪（４４）的表面亦為一粗糙面，該上、下轉動元件（４３）各自分別與上、下螺旋槳（５１）、（５２）固接；藉此，當動力組（４）之動力輸出軸（４１）將動力傳遞給主傳動輪（４２），使該主傳動輪（４２）因此旋轉時，該主傳動輪（４２）便能透過其粗糙表面與該上、下轉動元件（４３）之粗糙面的摩擦接觸，以及該輔助傳動輪（４４）的輔助支撐與之輪面的摩擦接觸，使該主傳動輪（４２）以摩擦傳動方式帶動該上、下轉動元件（４３）同時做不同方向之旋轉，進而分別傳動該上、下螺旋槳（５１）、（５２）做不同方向之旋轉。In addition, the power unit (4) of the three-axis helicopter of the present invention has a main transmission wheel (42) fixed on its power output shaft (41) [refer to FIG. 5], and the surface of the main transmission wheel (42) is one. a rough surface, the upper and lower positions of the main transmission wheel (42) are each provided with a rotating element (43) in contact with the surface thereof, and the upper and lower rotating elements (43) are in contact with the main transmission wheel (42). The surface is also rough, and in order to balance the supporting force of the upper and lower rotating members (43), on the side opposite to the main transmission wheel (42), and the upper and lower rotating members (43) Between the auxiliary transmission wheel (44), the surface of the auxiliary transmission wheel (44) is also a rough surface, the upper and lower rotating elements (43) are respectively associated with the upper and lower propellers (51), (52) Secured; thereby, when the power take-off shaft (41) of the power pack (4) transmits power to the main drive wheel (42) so that the main drive wheel (42) thus rotates, the main drive wheel (42) Can penetrate The frictional contact between the rough surface and the rough surface of the upper and lower rotating elements (43), and the auxiliary support of the auxiliary transmission wheel (44) in frictional contact with the tread, the frictional transmission of the main transmission wheel (42) The method drives the upper and lower rotating elements (43) to rotate in different directions at the same time, and then drives the upper and lower propellers (51) and (52) to rotate in different directions.
由於該主傳動輪（４２）、該轉動元件（４３）、該輔助傳動輪（４４）之間是以摩擦的方式傳動，因此在遇到外力（如鳥擊）時，能利用滑移的方式瞬間釋放受到撞擊的衝擊力，進而避免該動力組（４）的損壞。Since the main transmission wheel (42), the rotating element (43), and the auxiliary transmission wheel (44) are driven by friction, when the external force (such as a bird strike) is encountered, the slipping manner can be utilized. The impact of the impact is instantaneously released, thereby avoiding damage to the power pack (4).
再者，本發明之三軸直升機可在該三軸組裝座體（１）上裝設配置一降落傘（８）【參第六圖】，以在該三軸直升機之動力組（４）無法再提供飛行的動力時，利用被觸發而開展的降落傘（８）使該三軸直升機安全著陸，降低損壞之機率。Furthermore, the three-axis helicopter of the present invention can be equipped with a parachute (8) on the three-axis assembly base (1) [see the sixth figure], so that the power unit (4) of the three-axis helicopter can no longer be used. When providing flight power, the trike helicopter is safely landed using a triggered parachute (8) to reduce the chance of damage.
又，本發明之三軸直升機，更進一步在該三軸組裝座體（１）與該尾軸部件（２）之間裝設有方向控制裝置（９）【參第七圖】，藉由該方向控制裝置（９）驅動該尾軸部件（２）正向或反向偏轉，使該三軸直升機能執行轉彎之動作。Moreover, the three-axis helicopter of the present invention further includes a direction control device (9) between the three-axis assembly base (1) and the tail shaft member (2), The direction control device (9) drives the tail shaft member (2) to deflect forward or reverse, enabling the three-axis helicopter to perform a turning action.
其中，該方向控制裝置（９）包括一轉軸（９１）、至少一驅動源（９２）及一連桿組（９３）；該轉軸（９１）穿設於該三軸組裝座體（１）之其一延伸臂（１１）與該尾軸部件（２）之間，且與該尾軸部件（２）相互固接，該驅動源（９２）透過該連桿組（９３）與該轉軸（９１）接設，當該驅動源（９２）傳動該連桿組（９３）往左或右方向偏擺時，便能帶動該轉軸（９１）呈正方向或反方向偏轉，且進一步使該尾軸部件（２）亦隨該轉軸（９１）做正方向或反方向偏轉，而達到驅動本發明之三軸直升機轉向之效果。The directional control device (9) includes a rotating shaft (91), at least one driving source (92) and a connecting rod set (93); the rotating shaft (91) is disposed through the three-axis assembling base (1) An extension arm (11) is interposed between the extension shaft (11) and the tail shaft member (2), and the drive shaft (92) passes through the linkage group (93) and the rotation shaft (91). Connected, when the driving source (92) drives the connecting rod set (93) to yaw in the left or right direction, the rotating shaft (91) can be deflected in a positive or negative direction, and the tail shaft component is further driven (2) The rotation shaft (91) is also deflected in the forward or reverse direction to achieve the effect of driving the three-axis helicopter of the present invention.
本發明之三軸直升機可更進一步裝載攝影裝置【圖中未表示】，以透過攝影裝置擷取欲勘查區域之影像，以提供相關單位在作業上的參考數據。The three-axis helicopter of the present invention can further load a photographing device (not shown) to capture an image of the area to be surveyed through the photographing device to provide reference data of the relevant unit on the job.
以上所舉者僅係本發明之部份實施例，並非用以限制本發明，致依本發明之創意精神及特徵，稍加變化修飾而成者，亦應包括在本專利範圍之內。The above is only a part of the embodiments of the present invention, and is not intended to limit the present invention. It is intended to be included in the scope of the present invention.
綜上所述，本發明實施例確能達到所預期之使用功效，又其所揭露之具體技術手段，不僅未曾見諸於同類產品中，亦未曾公開於申請前，誠已完全符合專利法之規定與要求，爰依法提出發明專利之申請，懇請惠予審查，並賜准專利，則實感德便。In summary, the embodiments of the present invention can achieve the expected use efficiency, and the specific technical means disclosed therein have not been seen in similar products, nor have they been disclosed before the application, and have completely complied with the patent law. The regulations and requirements, the application for invention patents in accordance with the law, and the application for review, and the grant of patents, are truly sensible.
(1)．．．三軸組裝座體(1). . . Triaxial assembly body
(11)．．．延伸臂(11). . . Extension arm
(12)．．．組裝孔(12). . . Assembly hole
(2)．．．尾軸部件(2). . . Tail shaft part
(3)．．．翼軸部件(3). . . Wing shaft component
(4)．．．動力組(4). . . Power group
(41)．．．動力輸出軸(41). . . PTO shaft
(42)．．．主傳動輪(42). . . Main drive wheel
(43)．．．轉動元件(43). . . Rotating element
(44)．．．輔助傳動輪(44). . . Auxiliary drive wheel
(5)．．．螺旋槳(5). . . propeller
(51)．．．上螺旋槳(51). . . Upper propeller
(52)．．．下螺旋槳(52). . . Lower propeller
(6)．．．收折機構(6). . . Folding mechanism
(61)．．．鉸鍊元件(61). . . Hinge element
(62)．．．鎖固元件(62). . . Locking element
(7)．．．負載(7). . . load
(71)．．．組裝軸(71). . . Assembly shaft
(72)．．．容置空間(72). . . Housing space
(73)．．．儲液桶(73). . . Liquid storage tank
(74)．．．起落架(74). . . landing gear
(75)．．．浮板(75). . . Kickboard
(8)．．．降落傘(8). . . parachute
(9)．．．方向控制裝置(9). . . Direction control device
(91)．．．轉軸(91). . . Rotating shaft
(92)．．．驅動源(92). . . Drive source
(93)．．．連桿組(93). . . Connecting rod set
第一圖：本發明三軸直升機之立體外觀圖First picture: three-dimensional appearance of the three-axis helicopter of the present invention
第二圖：本發明三軸直升機於收折狀態且與負載之立體分解圖The second figure: the three-axis helicopter of the present invention is in a folded state and an exploded view of the load
第三圖：本發明三軸直升機於收折狀態且與負載組合之立體圖The third figure: a perspective view of the triaxial helicopter of the present invention in a folded state and combined with a load
第四圖：本發明三軸直升機之收折機構放大立體圖Fourth figure: enlarged perspective view of the folding mechanism of the three-axis helicopter of the present invention
第五圖：本發明三軸直升機之動力組放大立體圖Figure 5: enlarged perspective view of the power unit of the three-axle helicopter of the present invention
第六圖：本發明三軸直升機搭配有降落傘之立體示意圖Figure 6: Stereo view of a three-axis helicopter with a parachute of the present invention
第七圖：本發明三軸直升機之方向控制裝置的結構示意圖Figure 7: Schematic diagram of the directional control device of the three-axis helicopter of the present invention
(1)．．．三軸組裝座體(1). . . Triaxial assembly body
(11)．．．延伸臂(11). . . Extension arm
(2)．．．尾軸部件(2). . . Tail shaft part
(3)．．．翼軸部件(3). . . Wing shaft component
(4)．．．動力組(4). . . Power group
(5)．．．螺旋槳(5). . . propeller
(51)．．．上螺旋槳(51). . . Upper propeller
(52)．．．下螺旋槳(52). . . Lower propeller
(6)．．．收折機構(6). . . Folding mechanism
Claims (13)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW100121198A TWI408080B (en) | 2011-06-17 | 2011-06-17 | Helicopter with three axles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW100121198A TWI408080B (en) | 2011-06-17 | 2011-06-17 | Helicopter with three axles |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TW201300285A true TW201300285A (en) | 2013-01-01 |
| TWI408080B TWI408080B (en) | 2013-09-11 |
Family
ID=48137321
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW100121198A TWI408080B (en) | 2011-06-17 | 2011-06-17 | Helicopter with three axles |
Country Status (1)
| Country | Link |
|---|---|
| TW (1) | TWI408080B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103231802A (en) * | 2013-04-17 | 2013-08-07 | 华南农业大学 | Y-type non-coaxial multi-rotor aircraft |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104163238B (en) * | 2014-08-18 | 2016-04-27 | 国网湖北电力中超建设管理公司 | A kind of multi-rotor aerocraft horn folding device |
| US20170029103A1 (en) * | 2015-07-28 | 2017-02-02 | Inventec Appliances (Pudong) Corporation | Unmanned vehicle |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2444879Y (en) * | 2000-09-25 | 2001-08-29 | 纬华航太工业股份有限公司 | Helicopter parachute device |
| JP3673253B2 (en) * | 2002-10-06 | 2005-07-20 | ヒロボー株式会社 | Coaxial reversing radio control helicopter and blade tilt mechanism of radio control helicopter |
| GB2418405B (en) * | 2004-09-23 | 2010-03-10 | Paul Vincenzi | Rotorcraft |
| CN201049732Y (en) * | 2007-03-05 | 2008-04-23 | 银辉玩具制品厂有限公司 | Helicopter with horizontal control |
| PT2184229E (en) * | 2008-11-11 | 2012-12-20 | Agustawestland Spa | Helicopter rotor |
| CN101391651A (en) * | 2008-11-17 | 2009-03-25 | 西安智澜科技发展有限公司 | Foldable Y shaped three axis two-layer six rotorcraft |
-
2011
- 2011-06-17 TW TW100121198A patent/TWI408080B/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103231802A (en) * | 2013-04-17 | 2013-08-07 | 华南农业大学 | Y-type non-coaxial multi-rotor aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| TWI408080B (en) | 2013-09-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4899069B2 (en) | Spherical airplane | |
| US10239611B2 (en) | Hybrid multicopter and fixed wing aerial vehicle | |
| US10301017B2 (en) | Flying and walking drone | |
| ES2732717T3 (en) | Aerodino VTOL with one or more supporting axial fans | |
| US8646720B2 (en) | Modular flight vehicle with wings | |
| AU2014307569B2 (en) | Convertiplane with new aerodynamic and technical solutions which make the aircraft safe and usable | |
| RU2548444C2 (en) | Airborne vehicle | |
| US8540183B2 (en) | Aerovehicle system including plurality of autogyro assemblies | |
| US20160207368A1 (en) | Vertical Take-Off and Landing Roadable Aircraft | |
| US20150136897A1 (en) | Aircraft, preferably unmanned | |
| CN202071985U (en) | Novel plane symmetrical layout type multi-rotor unmanned air vehicle | |
| US20070246601A1 (en) | Manned/unmanned V.T.O.L. flight vehicle | |
| RU108016U1 (en) | FLYING MOTORCYCLE | |
| US11673657B2 (en) | Multi-rotor rotorcraft | |
| JP6583874B1 (en) | Delivery system, air vehicle, and controller | |
| CN107776892B (en) | Light-duty collapsible scouting and beating integrative unmanned aerial vehicle | |
| TWI408080B (en) | Helicopter with three axles | |
| CN205076045U (en) | Combined type aircraft of varistructure | |
| JP2022529504A (en) | Ground support equipment for high altitude long cruising time aircraft | |
| CA2840823A1 (en) | Vertical take-off and landing roadable aircraft | |
| EP2892803A1 (en) | Flying platform | |
| WO2020052106A1 (en) | Compact long-endurance crop protecting unmanned aerial vehicle | |
| JP5871508B2 (en) | Fluid machinery using parallel rotor blades | |
| TW201942022A (en) | Multi-purpose helicopter double fuselage structure | |
| CN107031840A (en) | A kind of aircraft |