TWM640912U - Joined-wing triphibious unmanned aerial vehicle - Google Patents

Abstract

一種連翼型三棲無人航行器，包括一機身、一組前機翼、一組後機翼、一組垂直翼片及至少一推進器，該機身、前機翼或後機翼兩側進一步延設有複數個位置相對應的垂直螺旋槳，該機身下方更包含一組機輪，據此，可不受跑道或波浪等地形限制，依實際狀況於水面或陸地等地形輕易上昇或降落，達到水、陸、空三棲作業的目的。A wing-type amphibious unmanned aerial vehicle, comprising a fuselage, a set of front wings, a set of rear wings, a set of vertical wings and at least one propeller, the fuselage, front wings or rear wings The side is further extended with a plurality of vertical propellers corresponding to the positions, and a set of wheels is included under the fuselage. According to this, it can be easily ascended or landed on water or land according to the actual situation without being restricted by terrain such as runways or waves. , to achieve the purpose of water, land and air amphibious operations.

Description

連翼型三棲無人航行器Winged amphibious unmanned aerial vehicle

本創作涉及一種連翼型的航行器結構，特別指一種具有垂直螺旋槳的連翼型三棲無人航行器，令具有較佳操控性能及航行穩定性的連翼型飛行裝置，增加垂直升降及著陸機能的航行器新型創設。This creation relates to a wing-type aircraft structure, especially a wing-type amphibious unmanned aerial vehicle with a vertical propeller, so that the wing-type flying device with better control performance and navigation stability can increase vertical lift and landing A new design of functional aircraft.

在航行器的領域中，水上飛機是一種具有浮筒結構，可停滯於水面上，也可從水面起降的飛行器，突破一般飛機被陸地限制的問題；而同樣是一種可從水面起降的「飛翼船」載具，與水上飛機不同的是飛翼船沒有浮筒，是用機腹或水橇降落在海面上，藉由在適當速度下所形成的地面效應力，減少機體阻力、燃料消耗以及節省飛行時間。In the field of aircraft, a seaplane is a kind of aircraft with a buoy structure that can stay on the water surface and can also take off and land from the water surface, breaking through the problem of ordinary aircraft being restricted by land; Flying wing boats are different from seaplanes in that flying wing boats have no buoys, and land on the sea surface with the belly or water skis. The ground effect force formed at an appropriate speed reduces the body resistance and fuel consumption. and save flight time.

基本的飛翼船結構主要包括一機身及一對機翼，並利用水平設置的推進器作為動力來源，由於該單翼型的飛翼船閃避障礙物或突發狀況時，反應的動作遲鈍且幅度大，遂有如第1圖所示的雙翼船問世，利用分別設於兩對機翼的升降舵同時作動及作用力互相偶合，令連翼構型之飛翼船以極小角度的上下升降或側滑移動，大幅提昇飛翼船的機動力及狀況反應。The basic structure of a flying wing boat mainly includes a fuselage and a pair of wings, and uses a horizontal propeller as a power source. When the single wing flying wing boat avoids obstacles or emergencies, its reaction is slow And the range is large, so there is a biplane boat as shown in Figure 1. Using the elevators respectively installed on the two pairs of wings to act simultaneously and to couple the forces with each other, the flying wing boat in the wing configuration can move up and down at a very small angle. Or side-slip movement, greatly improving the maneuverability and status response of the flying wing ship.

近幾年搭載有照相機、攝影機功能的無人空拍機應用廣泛，該無人空拍機具有極佳的機動能力，可在隨意地形上升至高空進行地面觀察、場地偵察或休閒娛樂等用途，應用上相當實用方便。有鑑於此，若能進一步思考該雙翼型飛行裝置的結構改進，提升地形的限制，應能增加雙翼型飛行裝置的應用範圍。In recent years, unmanned aerial cameras equipped with camera and video camera functions have been widely used. This unmanned aerial camera has excellent maneuverability and can be raised to high altitudes on random terrain for ground observation, site reconnaissance or leisure and entertainment. Quite practical and convenient. In view of this, if the structural improvement of the biplane flying device can be considered further and the limitation of the terrain is improved, the application range of the biplane flying device should be increased.

緣此，本創作之主要目的在提供一種具有垂直升降功能及陸路著地的連翼型航行器結構。For this reason, the main purpose of this creation is to provide a kind of wing-jointed aircraft structure with vertical lifting function and land landing.

為達到上述目的，本創作所提出的技術手段在於提供一種連翼型三棲無人航行器，包括一機身、一組前機翼、一組後機翼、一組垂直翼片及至少一推進器，該垂直翼片設置於前機翼與後機翼的翼端，其主要特徵在於：該機身、前機翼或後機翼兩側延設有複數個位置相對應的垂直螺旋槳。In order to achieve the above purpose, the technical means proposed in this creation is to provide a wing-type amphibious unmanned aerial vehicle, including a fuselage, a set of front wings, a set of rear wings, a set of vertical wings and at least one propulsion The vertical wing is arranged on the wing ends of the front wing and the rear wing, and its main feature is that a plurality of vertical propellers corresponding to the positions are extended on both sides of the fuselage, the front wing or the rear wing.

上述連翼型三棲航行器之改進，其中該垂直翼片下方進一步設有一水橇，該水橇兩端設有一垂直螺旋槳。The improvement of the above wing-type amphibious aircraft, wherein a water ski is further provided under the vertical wing, and a vertical propeller is provided at both ends of the water ski.

上述連翼型三棲航行器之改進，該航行器更包含複數個機輪，設置於機身下方。As an improvement of the above-mentioned wing-type amphibious aircraft, the aircraft further includes a plurality of wheels arranged under the fuselage.

利用上述結構加以實施之後可知，本創作連翼型三棲無人航行器可依實際狀況，於水面或陸地等地形輕易上昇或降落，達到不受跑道或波浪等地形限制的水、陸、空三棲作業功能，據此，可利用本創作進行水域巡航、海岸偵防、資源探勘、環境監測、災難搜救等用途，相當實用。After using the above structure to implement, it can be seen that the wing-type amphibious unmanned aerial vehicle of this creation can easily rise or land on the water surface or land and other terrains according to the actual situation, and achieve the three-dimensional water, land and air three-dimensional space that is not restricted by terrain such as runways or waves. According to this, this creation can be used for water cruising, coastal detection and defense, resource exploration, environmental monitoring, disaster search and rescue, etc., which is quite practical.

為使本創作之結構特徵、功效及其他優點能進一步被瞭解，茲以較佳實施例並配合圖式詳細說明如后。 In order to further understand the structural features, effects and other advantages of this creation, a preferred embodiment and accompanying drawings are described in detail below.

首先，請參考第2圖及第3圖所示，圖中是示出本創作連翼型三棲無人航行器較佳實施例，該航行器包含一機身(10)、一組前機翼(20)、一組後機翼(30)、一組垂直翼片(40)、至少一推進器(50)、及複數個垂直螺旋槳(60)；該前機翼(20)及後機翼(30)是分別設於機身(10)兩側的前段及後段，該前機翼(20)向後形成一適當的後掠角度，該後機翼(30)則向前形成一適當的前掠角度；該垂直翼片(40)是設置於前機翼(20)與後機翼(30)的翼端，令該前機翼(20)與後機翼形成相互連結；垂直翼片(40)下方進一步可設一水橇(70)，提供維持船身平衡之輔助，本實施例以設置於垂直翼片(40)下方做說明，但不限制設置於上述之位置。 First of all, please refer to Fig. 2 and Fig. 3, which shows the preferred embodiment of the wing-type amphibious unmanned aerial vehicle of this invention, which includes a fuselage (10) and a group of front wings (20), a set of rear wings (30), a set of vertical fins (40), at least one propeller (50), and a plurality of vertical propellers (60); the front wing (20) and the rear wing (30) are respectively located at the front section and the rear section on both sides of the fuselage (10). The front wing (20) forms a suitable sweep angle backward, and the rear wing (30) forms a suitable front Sweep angle; This vertical wing (40) is arranged on the wing end of front wing (20) and rear wing (30), makes this front wing (20) and rear wing form interlinkage; Vertical wing ( 40) A water skid (70) can be further provided below to provide assistance for maintaining the balance of the hull. In this embodiment, it is set under the vertical fin (40) for illustration, but it is not limited to the above-mentioned position.

由第3圖所示本創作較佳實施例的俯視來看，前述垂直螺旋槳(60)是設於水橇(70)的兩端，該推進器(50)則設於機身(10)頂部後方，當然，該垂直螺旋槳(60)也可以延設於機身(10)、前機翼(20)或後機翼(30)兩側的相對位置上；是以，藉由推進器(50)的推力驅動航行器，可令航行器加速至適當的速率，據以與水面形成地面效應作用力。本創作航行器之機翼為連翼構型，因此結構強度增加，本身結構強度的設計要求可降低，相對的整體重量也減輕。兩對機翼可同時裝置兩對升降舵與兩對副翼，當這兩對升降舵與副翼若同時作動且作用力互相偶合時，該連翼構型航行器可做出零度俯仰角上升、下降，或垂直於飛行方向的平移運動，進而增益航行器在穩定性與控制性方面的效能。From the top view of the preferred embodiment of the invention shown in Fig. 3, the aforementioned vertical propeller (60) is located at the two ends of the water ski (70), and the propeller (50) is located at the top of the fuselage (10) Rear, of course, this vertical propeller (60) also can be extended on the relative position on fuselage (10), front wing (20) or rear wing (30) both sides; Therefore, by propeller (50) ) thrust to drive the aircraft, which can accelerate the aircraft to an appropriate speed, so as to form a ground effect force with the water surface. The wing of the aircraft of this invention is a wing configuration, so the structural strength is increased, the design requirements for the structural strength itself can be reduced, and the relative overall weight is also reduced. Two pairs of wings can be equipped with two pairs of elevators and two pairs of ailerons at the same time. When the two pairs of elevators and ailerons are activated at the same time and the forces are coupled with each other, the aircraft with wing configuration can ascend and descend at a pitch angle of zero degrees. , or translational motion perpendicular to the direction of flight, thereby increasing the performance of the aircraft in terms of stability and controllability.

請再參閱第4圖所示，由本創作較佳實施例的側視來看，本創作更包含複數個機輪（80），是設於機身（10）的下方並可支撐起航行器整體的姿勢，透過前述所設垂直螺旋槳（60）的設置，本創作連翼型三棲無人航行器可依實際狀況自水面或陸地上昇至空中，甚至定點滯空，或反之自空中降落於水面或陸地，進而達到不受跑道或波浪等地形限制的水、陸、空三棲作業功能；據此，利用本創作可以進行水域巡航、海岸偵防、資源探勘、環境監測、災難搜救等用途，相當實用。可以理解到的是，本創作之航行器並不限於無人操作，在適當的設計調變之下，亦可作為載人目的使用的航行器。Please refer to Figure 4 again, from the side view of the preferred embodiment of this invention, this invention further includes a plurality of wheels (80), which are located under the fuselage (10) and can support the entire aircraft Through the setting of the above-mentioned vertical propeller (60), the creative wing-type amphibious unmanned aerial vehicle can rise from the water surface or land to the air according to the actual situation, or even stay in the air at a fixed point, or vice versa from the air to land on the water surface or Land, and then achieve the functions of water, land and air amphibious operations that are not restricted by terrain such as runways or waves; accordingly, this creation can be used for water cruising, coastal detection and defense, resource exploration, environmental monitoring, disaster search and rescue, etc. practical. It can be understood that the aircraft of this invention is not limited to unmanned operation, and can also be used as an aircraft for manned purposes under appropriate design adjustments.

透過上述實施例說明之後，可以輕易理解到，本創作至少具有以下數個優點：1、本創作連翼型航行器重量輕、結構穩定，具有較佳反應能力及操控性能，相對地提昇航行安全性。2、本創作連翼型航行器具有垂直升降能力，自然可排除諸多地形限制。3、進一步，本創作連翼型航行器具有水、陸、空三棲性能，大幅提高航行器機動性，相當適合被廣泛應用。After the description of the above embodiments, it can be easily understood that this creation has at least the following advantages: 1. The wing-shaped aircraft of this creation is light in weight, stable in structure, has better response ability and control performance, and relatively improves navigation safety sex. 2. The airfoil aircraft of this creation has the ability to lift vertically, so many terrain restrictions can be eliminated naturally. 3. Furthermore, the wing-shaped aircraft of this creation has the amphibious performance of water, land and air, greatly improves the maneuverability of the aircraft, and is quite suitable for being widely used.

綜上所述，本創作連翼型三棲無人航行器結構，確實已達到預設的目的，實已符合產業的需求，爰依法提出專利申請，惟，本創作雖已以前述較佳之實施例揭示，然而圖式所繪示的尺寸、形狀、或數量等並非用以限定本創作，任何熟悉此技藝者，在不脫離本創作之精神和範圍內，當可能加以潤飾或修改，因此本創作保護範圍當視後附的申請專利範圍所界定者為準。To sum up, the structure of the winged amphibious unmanned aerial vehicle of this creation has indeed achieved the preset purpose and has met the needs of the industry. A patent application has been filed according to law. However, although this creation has been based on the aforementioned preferred embodiment However, the size, shape, or quantity shown in the diagram is not intended to limit this creation. Anyone who is familiar with this skill may modify or modify it without departing from the spirit and scope of this creation. Therefore, this creation The scope of protection shall prevail as defined in the scope of the appended patent application.

10:機身 20:前機翼 30:後機翼 40:垂直翼片 50:推進器 60:垂直螺旋槳 70:水橇 80:機輪 10: Fuselage 20: Front wing 30: rear wing 40: vertical fins 50: Thruster 60:Vertical propeller 70:Water Ski 80:wheel

第1圖 為已知的雙翼型飛行船結構示意圖。 Fig. 1 is the structural schematic diagram of known biplane airship.

第2圖 為本創作之連翼型三棲航行器立體示意圖。 Figure 2 is a three-dimensional schematic diagram of the winged amphibious aircraft created by this author.

第3圖 為本創作之連翼型三棲航行器結構側視示意圖。 Figure 3 is a side view schematic diagram of the wing-type amphibious aircraft created by the author.

第4圖 為本創作之連翼型三棲航行器於侷限地形下的升降動作示意圖。 Figure 4 is a schematic diagram of the lifting action of the wing-type amphibious aircraft created by this creation under limited terrain.

10:機身 10: Fuselage

20:前機翼 20: Front wing

30:後機翼 30: rear wing

40:垂直翼片 40: vertical fins

50:推進器 50: Thruster

60:垂直螺旋槳 60:Vertical propeller

70:水橇 70:Water Ski

80:機輪 80:wheel

Claims (4)

一種連翼型三棲無人航行器，包括一機身、一組前機翼、一組後機翼、一組垂直翼片及至少一推進器，該前機翼及後機翼分別設於機身兩側的前段及後段，該垂直翼片設置於前機翼與後機翼的翼端，該推進器設於機身後方，其主要特徵在於：該機身、前機翼或後機翼兩側延設有複數個位置相對應的垂直螺旋槳。 A wing-type amphibious unmanned aerial vehicle, comprising a fuselage, a set of front wings, a set of rear wings, a set of vertical wings and at least one propeller, the front wings and the rear wings are respectively arranged on the The front section and the rear section on both sides of the body, the vertical fins are arranged at the wing ends of the front wing and the rear wing, and the propeller is arranged at the rear of the fuselage. Its main features are: the fuselage, front wing or rear wing A plurality of corresponding vertical propellers are extended on both sides. 如請求項1所述之連翼型三棲無人航行器，其中該垂直翼片下方進一步設有一水橇。 The wing-type amphibious unmanned aerial vehicle as described in claim 1, wherein a water ski is further provided under the vertical wing. 如請求項2所述之連翼型三棲無人航行器，其中該水橇兩端設有一垂直螺旋槳。 The wing-type amphibious unmanned aerial vehicle as described in claim 2, wherein a vertical propeller is provided at both ends of the water ski. 如請求項1所述之連翼型三棲無人航行器，該航行器更包含複數個機輪，設置於機身下方。 As the wing-type amphibious unmanned aerial vehicle described in claim 1, the aircraft further includes a plurality of wheels arranged under the fuselage.

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