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TWM640913U - Joined-wing structure of hydrofoil boat - Google Patents

Joined-wing structure of hydrofoil boat Download PDF

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Publication number
TWM640913U
TWM640913U TW111213491U TW111213491U TWM640913U TW M640913 U TWM640913 U TW M640913U TW 111213491 U TW111213491 U TW 111213491U TW 111213491 U TW111213491 U TW 111213491U TW M640913 U TWM640913 U TW M640913U
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wing
boat
flying
wings
fuselage
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TW111213491U
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Chinese (zh)
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賈澤民
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賈澤民
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Abstract

一種飛翼船之連翼結構,係具有前機翼及後機翼二對機翼,且該二對機翼分別向前後形成一適當角度之掠角,並於翼端處相互連接,令該連翼構型之飛翼船具有較高結構強度與穩定度,同時可產生直接升力或側向力,提高控制性能的靈巧度。A winged structure of a flying wing boat has two pairs of wings, a front wing and a rear wing, and the two pairs of wings respectively form a sweep angle of an appropriate angle forward and backward, and are connected to each other at the wing ends, so that the The flying wing boat with wing configuration has high structural strength and stability, and can generate direct lift or lateral force at the same time, improving the dexterity of control performance.

Description

飛翼船之連翼結構Wing structure of flying wing boat

本創作涉及一種飛翼船之機翼結構,特別指一種飛翼船之連翼結構,該飛翼船之前機翼與後機翼相連接,可有效提升該連翼飛翼船高度爬升與側向移動能力的新型創設。This creation relates to a wing structure of a flying-wing boat, especially a wing-connecting structure of a flying-wing boat. New creations towards mobility.

「飛翼船」是航空與航海科技結合的混合體,其英文名稱為Wing In Ground Effect Vehicle(地面效應載具,簡稱WIG),如第1圖即揭示一種已知的飛翼船,該飛翼船具有一機身及一對機翼,與水上飛機不同的地方是,飛翼船沒有浮筒,是用機腹或水橇降落在水面上;飛翼船加速起飛至脫離水面後,運用機翼接近水面時所產生特有的翼地效應(Ground Effect)使得機翼的升力大增,但阻力卻減小的現象,使所需之動力較少,亦即降低燃油之消耗,來達成水上運輸最難擁有的高速特性,以及維持原有高載運能力的優點。"Flying wing boat" is a mixture of aviation and navigation technology. Its English name is Wing In Ground Effect Vehicle (WIG for short). As shown in Figure 1, a known flying wing boat is revealed. The wing boat has a fuselage and a pair of wings. The difference from the seaplane is that the flying wing boat has no buoys and lands on the water with the belly or water skids; The unique ground effect (Ground Effect) produced when the wing is close to the water surface makes the lift of the wing greatly increased, but the drag is reduced, so that less power is required, that is, fuel consumption is reduced to achieve water transportation The most difficult high-speed characteristics, and the advantages of maintaining the original high carrying capacity.

目前「飛翼船」的運行過程大致會經遇下述四種狀態。1.低速滑行時段:其航行狀態與水面船舶一樣,因機體之下半部設計如船形,故易於操控。2.準備加速時段:為了快速將機體帶入地面效應範圍之內,以節省時間、燃料消耗以及機體阻力;但在起飛至正式進入地面效應力之階段前,其阻力會增加,飛翼船所需推進力為一般巡航推進力的2倍至3倍,亦即飛翼船之起飛所需的推力,得等到進入地面效應階段後才得以降低。3.地面效應階段:當速度介於120~500km/h之間時,地面效應力會自然產生於機翼下平面與水面之間,令飛翼船可以低阻力的在水面上方低空掠行。4.面對特殊狀況的應變方式:飛翼船遇到障礙物或閃避突發狀況時,可採取的應變作為大致為側轉彎閃過障礙物,或拉高飛翼船飛行高度越過障礙物。At present, the operation process of the "Flying Wing Ship" will generally experience the following four states. 1. Low-speed taxiing period: its sailing state is the same as that of a surface ship, and the lower half of the body is designed like a boat, so it is easy to control. 2. Preparing for acceleration period: In order to quickly bring the body into the range of ground effect to save time, fuel consumption and body resistance; but before it takes off and officially enters the stage of ground effect, its resistance will increase. Needed propulsion is 2 times to 3 times of general cruising propulsion, that is, the thrust required for the take-off of the flying wing boat must wait to be reduced after entering the ground effect stage. 3. Ground effect stage: When the speed is between 120-500km/h, the ground effect force will naturally be generated between the lower plane of the wing and the water surface, so that the flying wing boat can skim above the water surface with low resistance. 4. Response methods in the face of special situations: when the flying wing boat encounters an obstacle or evades an unexpected situation, the response that can be taken is roughly turning sideways to flash over the obstacle, or raising the flying height of the flying wing boat to cross the obstacle.

然而,飛翼船以上述的高速在水平面上掠行,可反應的時間非常有限,因此,飛翼船需要再進一步研究發展的方向便在於:1.強化飛翼船起飛前的氣/水動力設計及維持水面上地面效應飛行的穩定度;2.提升飛翼船於飛行時瞬間爬升高度或側偏轉彎之動態穩定性能等。However, the time for the flying wing craft to skim on the horizontal plane at the above-mentioned high speed is very limited. Therefore, the directions for further research and development of the flying wing craft are as follows: 1. Strengthen the air/hydrodynamic force of the flying wing craft before taking off Design and maintain the stability of ground effect flight on the water surface; 2. Improve the dynamic stability of flying wing boats when they climb instantly or turn sideways during flight.

有鑑於此,本創作係要提供一種具有良好爬升能力與側向移動能力之飛翼船結構。In view of this, this creation system will provide a kind of flying wing boat structure with good climbing ability and lateral movement ability.

為達到上述目的,本創作提供一種飛翼船之連翼結構,該飛翼船結構包含機身及一對前機翼,該機身外型符合空氣力學及流體力學設計,具有適當的浮力;該對前機翼設於機身的兩側,該前機翼向外伸展,並向後形成一適當的後掠角度;其特點是:所述結構還包括一對後機翼,其由機身尾端两側延伸而出,並向前形成一適當的前掠角度;該前機翼與該後機翼的翼端處相互連結。In order to achieve the above purpose, this creation provides a wing structure of a flying wing boat. The flying wing boat structure includes a fuselage and a pair of front wings. The shape of the fuselage conforms to the design of aerodynamics and hydrodynamics, and has appropriate buoyancy; The pair of front wings are arranged on both sides of the fuselage, and the front wings extend outwards and form an appropriate sweep angle backward; the feature is: the structure also includes a pair of rear wings, which are formed by the fuselage Both sides of the tail end extend out and form an appropriate forward sweep angle forward; the wing ends of the front wing and the rear wing are connected to each other.

上述飛翼船結構之改進,其中該前機翼與後機翼係分別位於機身前後不同的高度處。The improvement of the structure of the above-mentioned flying wing boat, wherein the front wing and the rear wing are respectively located at different heights at the front and rear of the fuselage.

上述飛翼船結構之改進,該結構更包含一垂直翼片,設置於前機翼與後機翼的翼端處使前機翼與後機翼連接。The improvement of the structure of the above-mentioned flying wing boat, the structure further includes a vertical wing, which is arranged at the wing ends of the front wing and the rear wing to connect the front wing and the rear wing.

上述飛翼船結構之改進,該結構更包含一水橇,該水橇設置於垂直翼片下方。The improvement of the structure of the above-mentioned flying wing boat, the structure further includes a water ski, and the water ski is arranged under the vertical wing.

利用上述結構加以實施之後可知,本創作提高飛翼船的結構強度與巡行穩定度,同時具有零度俯仰角上升、下降,或水平側滑的運動性能,大幅提升控制的靈巧度。After implementing the above structure, it can be seen that this creation improves the structural strength and cruising stability of the flying wing boat, and at the same time has the motion performance of rising, falling, or horizontal skidding at a pitch angle of zero degrees, which greatly improves the dexterity of control.

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,係本創作飛翼船之連翼結構較佳實施例,該飛翼船包含:一機身10,該機身10外型係符合空氣力學及流體力學的設計,本身具有適當的浮力,於機身10上設有至少一推進器11,藉以產生推動飛翼船整體往前的動力;一對前機翼20,設於機身10之兩側,前機翼20除了向外伸展,並向後形成一適當的後掠角度;一對後機翼30,由機身10尾端兩側延伸而出,並向前形成一適當的前掠角度;一垂直翼片40,設置於前機翼20與後機翼30的翼端(Wing Tip)處,令前機翼20與後機翼30由機身10前後不同的高度於翼端形成相互連結的構型;該垂直翼片40下方更設有一水橇50,提供維持船身平衡之輔助,當然該水橇50不限設置於上述之位置,介於水面與機翼間之翼面下大致上都可設置。First of all, please refer to Fig. 2 and Fig. 3, which are the preferred embodiments of the wing structure of the flying wing boat of this invention. The flying wing boat includes: a fuselage 10, and the shape of the fuselage 10 conforms to aerodynamics And the design of hydrodynamics, itself has appropriate buoyancy, is provided with at least one propeller 11 on the fuselage 10, so as to produce the power that promotes the flying wing boat whole to move forward; On both sides, the front wing 20 extends outwards and forms an appropriate sweep angle backward; a pair of rear wings 30 extend from both sides of the rear end of the fuselage 10 and form an appropriate forward sweep forward. Angle; a vertical wing 40 is arranged at the wing tip (Wing Tip) of the front wing 20 and the rear wing 30, so that the front wing 20 and the rear wing 30 are formed at the wing tip by different heights of the front and rear of the fuselage 10 Interconnected configuration; a water skid 50 is further provided below the vertical fin 40 to provide assistance in maintaining the balance of the hull. Of course, the water skid 50 is not limited to the above-mentioned position, the airfoil between the water surface and the wing The following can be set in general.

本創作依上述結構實施後,由於二機翼端處得到垂直翼片40的強化支撐,故可以減少機翼所承受的彎矩,二機翼在翼根(Wing root)處可大幅的降低翼樑(Wing Spar)所承載的應力,因此二機翼的翼展(Wing Span)可設計的比傳統飛機的翼展為大,也由於該連翼構型之飛翼船具有較高的強度,因此本身結構強度的設計要求也可降低,有助於減低飛翼船的生產難度。有鑑於本創作連翼構型的飛翼船有較大的翼展,同時二對前後機翼的翼端有垂直的垂直翼片,阻擋了翼端三維氣流的流動,因此可以大幅的減小翼端渦流(Wing Tip Vortex)的強度,使得誘導阻力為之下降。After this creation is implemented according to the above structure, since the end of the second wing is strengthened by the vertical fins 40, the bending moment on the wing can be reduced, and the wing root of the second wing can greatly reduce the The stress carried by the beam (Wing Spar), so the wingspan of the two wings (Wing Span) can be designed to be larger than the wingspan of a traditional aircraft, and because the flying wing boat of this wing configuration has higher strength, Therefore, the design requirement of the structural strength itself can also be reduced, which helps to reduce the production difficulty of the flying wing craft. In view of the large wingspan of the winged boat of this creation, and the two pairs of front and rear wings have vertical vertical fins at the wing ends, which block the flow of the three-dimensional airflow at the wing ends, so it can be greatly reduced. The strength of the Wing Tip Vortex reduces the induced drag.

此外,緣於本創作連翼構型之飛翼船具有兩對機翼,故可同時裝置兩對升降舵與兩對副翼,這兩對升降舵與副翼若同時作動且作用力互相偶合的情況下,可使連翼構型之飛翼船如第4圖所示以零度俯仰角(Pitch Angle)上升或下降,或如第5圖所示,做出垂直於飛行方向的側滑運動(Sideslip);該等運動模式對於閃避障礙物或突發狀況之應變,可以提供更佳的動態操控性能,大幅提昇的穩定性,也有助於起降或巡行時的安全度。In addition, because the winged boat of this invention has two pairs of wings, two pairs of elevators and two pairs of ailerons can be installed at the same time. If the two pairs of elevators and ailerons operate simultaneously and the forces are coupled Next, the flying wing boat in the wing configuration can rise or fall at a zero pitch angle (Pitch Angle) as shown in Figure 4, or as shown in Figure 5, make a sideslip movement perpendicular to the flight direction (Sideslip ); These sports modes can provide better dynamic handling performance and greatly improved stability for avoiding obstacles or responding to unexpected situations, and also contribute to the safety of take-off and landing or cruising.

本創作飛翼船之連翼結構,與已知的飛翼船結構比較之後,至少具有下述特點:1.較大高寬比(Aspect Ratio)的機翼提供較佳的氣動力,具有較大升力,較小誘導阻力,進一步增加飛翼船滯空時間與飛行高度及穩定度。2.結構重量較輕,擁有靈巧的運動特性,可產生直接升力或側向力,提高控制性能。3.強度提高的飛機結構具有較高的酬載能力,可增加其攜油量及裝置航測儀器等。The winged structure of the flying-wing boat of this creation, after comparing with the known flying-wing boat structure, has the following characteristics at least: 1. The wing with the larger aspect ratio (Aspect Ratio) provides better aerodynamic force, has better Large lift, small induced resistance, further increase the flight time and flight height and stability of the flying wing boat. 2. The structure is light in weight and has dexterous movement characteristics, which can generate direct lift or lateral force and improve control performance. 3. The aircraft structure with increased strength has a higher payload capacity, which can increase its fuel carrying capacity and install aerial survey instruments.

經由上述實施例說明可知,本創作確實已達到預設之目的,完全符合產業利用性及專利要件,爰依法提出專利申請,惟,以上所述僅為本創作之較佳實施例,並非用以限定本創作,因此本創作之保護範圍當視後附之申請專利範圍所界定者為準。It can be seen from the description of the above embodiments that this creation has indeed achieved the preset purpose, and fully meets the industrial utilization and patent requirements. It is necessary to file a patent application according to law, but the above description is only a preferred embodiment of this creation, not for This creation is limited, so the scope of protection of this creation should be defined by the scope of the attached patent application.

10:機身10: Fuselage

11:推進器11: Thruster

20:前機翼20: Front wing

30:後機翼30: rear wing

40:垂直翼片40: vertical fins

50:水橇50: water sled

第1圖 為已知的飛翼船結構示意圖。 第2圖 為本創作之飛翼船結構立體示意圖。 第3圖 為本創作之飛翼船結構俯視示意圖。 第4圖 為本創作之飛翼船於爬升時的動作示意圖。 第5圖 為本創作之飛翼船於側閃時的動作示意圖。 Fig. 1 is the structural schematic diagram of known flying wing craft. Figure 2 is a three-dimensional schematic diagram of the structure of the flying wing boat created in this work. Figure 3 is a top view schematic diagram of the structure of the flying wing boat created in this paper. Figure 4 is a schematic diagram of the movement of the flying wing boat created by this creation when it climbs. Figure 5 is a schematic diagram of the action of the flying wing boat created by this creation when it is flashing sideways.

10:機身 10: Fuselage

11:推進器 11: Thruster

20:前機翼 20: Front wing

30:後機翼 30: rear wing

40:垂直翼片 40: vertical fins

50:水橇 50: water sled

Claims (4)

一種飛翼船之連翼結構,包含機身及一對前機翼,該對前機翼設於飛翼船機身的兩側,該前機翼向外伸展,並向後形成一適當的後掠角度;其主要特徵在於:還包括一對後機翼,其由機身尾端兩側延伸而出,並向前形成一適當的前掠角度;該前機翼與該後機翼的翼端處相連接。A winged structure of a flying wing boat, comprising a fuselage and a pair of front wings, the pair of front wings are arranged on both sides of the flying wing boat fuselage, the front wings extend outwards, and form a suitable rear Sweep angle; its main feature is: it also includes a pair of rear wings, which extend out from both sides of the rear end of the fuselage, and form an appropriate forward sweep angle forward; the wings of the front wing and the rear wing connected at the ends. 如請求項1所述之飛翼船之連翼結構,其中該前機翼與後機翼係分別位於機身前後不同的高度處。The wing-connected structure of the flying wing boat as described in Claim 1, wherein the front wing and the rear wing are respectively located at different heights at the front and rear of the fuselage. 如請求項1所述之飛翼船之連翼結構,該結構更包含一垂直翼片,設置於前機翼與後機翼的翼端處使前機翼與後機翼連接。The wing-connected structure of the flying wing boat as claimed in claim 1, the structure further includes a vertical wing, which is arranged at the wing ends of the front wing and the rear wing to connect the front wing and the rear wing. 如請求項3所述之飛翼船之連翼結構,該結構更包含一水橇,設置於垂直翼片下方。The winged structure of the flying wing boat as claimed in claim 3, the structure further includes a water ski, which is arranged under the vertical wing.
TW111213491U 2022-12-07 2022-12-07 Joined-wing structure of hydrofoil boat TWM640913U (en)

Priority Applications (1)

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TW111213491U TWM640913U (en) 2022-12-07 2022-12-07 Joined-wing structure of hydrofoil boat

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Application Number Priority Date Filing Date Title
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TWM640913U true TWM640913U (en) 2023-05-11

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