TWM680840U - Defensive high-speed drone - Google Patents
Defensive high-speed droneInfo
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- TWM680840U TWM680840U TW114205230U TW114205230U TWM680840U TW M680840 U TWM680840 U TW M680840U TW 114205230 U TW114205230 U TW 114205230U TW 114205230 U TW114205230 U TW 114205230U TW M680840 U TWM680840 U TW M680840U
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Abstract
一種防禦型高速無人機,主要係包含高速無人機及飛控平台。其中,高速無人機的內部係設有包含指令接收及影像擷取等模組之控制電路,底緣係設有一光纖筒,於光纖筒收容適當長度,且連接高速無人機內部控制電路之光纖。該飛控平台係設有第二控制電路,該第二控制電路係連接於光纖,且使光纖連接於一捲軸。俾當高速無人機於飛行時,光纖由光纖筒釋出,使飛控平台得以藉由光纖傳輸飛行指令,且可藉由光纖將高速無人機所擷取的影像訊號回傳飛控平台,而當回收該高速無人機時,則藉由捲軸的轉動,將光纖纏繞於該捲軸的軸部。從而可防止高速無人機的操控訊號受到其他無線訊號干擾,或干擾周邊之其他設備。 A defensive high-speed drone mainly comprises a high-speed drone and a flight control platform. The high-speed drone's internal components include control circuitry with modules for command reception and image capture. A fiber optic tube is located at the bottom edge, housing a fiber optic cable of appropriate length that connects to the drone's internal control circuitry. The flight control platform includes a second control circuit connected to the fiber optic cable, which is then connected to a reel. When the high-speed drone is in flight, fiber optic cables are released from the fiber optic tube, allowing the flight control platform to transmit flight commands and transmit image signals captured by the drone back to the flight control platform. When the drone is being recovered, the fiber optic cables are wound around the shaft of the reel by rotation. This prevents interference with the drone's control signals from other wireless signals or with surrounding equipment.
Description
本創作係有關一種防禦型高速無人機,尤指一種藉由光纖傳輸飛行指令及影像訊號,以防止高速無人機的操控訊號受到其他無線訊號干擾之防禦型高速無人機。 This invention relates to a defensive high-speed drone, particularly a defensive high-speed drone that transmits flight commands and image signals via fiber optics to prevent interference with its control signals from other wireless signals.
按;無人機的飛行原理是透過空氣動力學產生升力和推力,由動力系統提供能量,飛行控制系統利用各種感測器收集數據並進行處理,然後控制馬達級舵面(固定翼機)來維持穩定和執行飛行指令,最後透過通訊系統與地面站進行資訊交換。現階段無人機的使用越來越普及,通常係應用於空拍攝影、電影拍攝、活動紀錄等攝影與錄影用途,或搜索救援、災害評估、交通監控、執法巡邏等公共安全用途,亦或野生動物追蹤、環境污染監測、地形測繪等環境監測用途。 Note: The flight principle of a drone is to generate lift and thrust through aerodynamics, with energy provided by the power system. The flight control system uses various sensors to collect and process data, then controls the motor-level control surfaces (for fixed-wing aircraft) to maintain stability and execute flight commands. Finally, information is exchanged with the ground station through the communication system. Currently, the use of drones is becoming increasingly widespread, typically for aerial photography, film shooting, event recording, and other photography and videography purposes; for public safety purposes such as search and rescue, disaster assessment, traffic monitoring, and law enforcement patrols; and for environmental monitoring purposes such as wildlife tracking, environmental pollution monitoring, and topographic mapping.
而現有的無人機操控方式,皆係以無線電操控為主,惟眾所周知,無線傳輸過程中可能會受到其他不明訊號的干擾,影響對無人機的操控。例如:無人機的飛行操控可能因不明訊號的干擾而不順暢甚至失控,或所擷取的影像訊號無法傳輸至地面等。 Current drone control methods primarily rely on radio control. However, as is well known, wireless transmission can be interfered with by unidentified signals, affecting drone control. For example, drone flight control may become unresponsive or even malfunction due to interference, or the captured image signals may fail to transmit to the ground.
而無人機本身的操控訊號,亦可能影響到周邊有關無線傳輸的設備。例如:若有玩家於民用機場附近使用無人機,其操控傳輸的無線電波可能被干擾而失控,或可能會影響到飛機的起降,故而,機場相關單 位只能於偵測到無線訊號時,以人為方式驅逐無人機玩家,惟如此較缺乏機動性及效率。 The control signals of drones can also affect surrounding wireless transmission equipment. For example, if a drone operator uses a drone near a civilian airport, its control transmission radio waves may be interfered with and cause it to go out of control, or it may affect aircraft takeoff and landing. Therefore, airport authorities can only manually remove drone operators when wireless signals are detected, but this method is relatively inflexible and inefficient.
申請人有鑑於此,經不斷研究、實驗,遂萌生設計一種防禦型高速無人機,藉由光纖傳輸飛行指令及影像訊號,以達到防止高速無人機的操控訊號受到其他無線訊號干擾或干擾周邊設備之目的。 In light of this, and through continuous research and experimentation, the applicant conceived the idea of designing a defensive high-speed drone that transmits flight commands and image signals via fiber optics to prevent interference with the drone's control signals from other wireless signals or from interfering with surrounding equipment.
本創作之主要目的,即在提供一種防禦型高速無人機,藉由光纖傳輸飛行指令及影像訊號,以改善習知無人機因藉由無線訊號操控,易受到其他無線訊號干擾或干擾周邊設備之缺失。 The primary objective of this invention is to provide a defensive high-speed drone that transmits flight commands and image signals via fiber optics, thereby addressing the shortcomings of conventional drones, which are susceptible to interference from other wireless signals or interference with surrounding equipment due to their wireless signal control.
前述之防禦型高速無人機,係包含高速無人機及飛控平台。其中,高速無人機的內部係設有包含指令接收及影像擷取等模組之第一控制電路,底緣係設有一光纖筒,於光纖筒收容適當長度,且連接高速無人機內部控制電路之光纖。該飛控平台係設有第二控制電路,該第二控制電路係連接於光纖,且使光纖連接於一捲軸。俾當高速無人機於飛行時,光纖由光纖筒釋出,使飛控平台得以藉由光纖傳輸飛行指令,且可藉由光纖將高速無人機所擷取的影像訊號回傳飛控平台,而當回收該高速無人機時,則藉由捲軸的轉動,將光纖纏繞於該捲軸的軸部。從而可防止高速無人機的操控訊號受到其他無線訊號干擾,或干擾周邊之其他設備。 The aforementioned defensive high-speed drone comprises a high-speed drone and a flight control platform. The high-speed drone's interior includes a first control circuit containing modules for command reception and image capture. A fiber optic tube is located at its bottom edge, housing a fiber optic cable of appropriate length that connects to the drone's internal control circuitry. The flight control platform has a second control circuit connected to the fiber optic cable, which is then connected to a reel. When the high-speed drone is in flight, fiber optic cables are released from the fiber optic tube, allowing the flight control platform to transmit flight commands and transmit image signals captured by the drone back to the flight control platform. When the drone is being recovered, the fiber optic cables are wound around the shaft of the reel by rotation. This prevents interference with the drone's control signals from other wireless signals or with surrounding equipment.
前述之防禦型高速無人機,其中之飛控平台係設有一收藏空間,以及一可由該收藏空間拉出之停機台,以供高速無人機置於該停機台,將高速無人機收容於收藏空間或由收藏空間拉出。 The aforementioned defensive high-speed drone includes a flight control platform with a storage compartment and a pull-out platform. This platform allows the high-speed drone to be placed on the platform, either stored within or pulled out of the storage compartment.
前述之防禦型高速無人機,其中之高速無人機之第一控制電 路係包含但不限於指令接收模組、影像擷取模組,以及供應整台高速無人機電力之電源模組。 The aforementioned defensive high-speed drone's first control circuit includes, but is not limited to, a command receiving module, an image acquisition module, and a power supply module that supplies power to the entire high-speed drone.
前述之防禦型高速無人機,其中之飛控平台之第二控制電路係包含但不限於指令傳輸模組、操控模組、影像接收模組及充電模組。俾當高速無人機收容於飛控平台之收藏空間時,得以藉由充電模組對高速無人機之電源模組進行充電。 The aforementioned defensive high-speed drone's flight control platform includes, but is not limited to, a command transmission module, a control module, an image receiving module, and a charging module. This allows the high-speed drone's power module to be charged via the charging module when it is housed in the flight control platform's storage space.
前述之防禦型高速無人機,其中之飛控平台的上方表面,係設有適當面積之太陽能板,藉由太陽能板吸收陽光所轉換之電力,提供充電模組之電源。 The aforementioned defensive high-speed drone has a solar panel of appropriate size on the upper surface of its flight control platform. The solar panel absorbs sunlight and converts it into electricity to power the charging module.
前述之防禦型高速無人機,其中之飛控平台的上方表面,係設有一風力發電機,藉由風力發電機受風轉動所轉換之電力,提供充電模組之電源。 The aforementioned defensive high-speed drone features a wind turbine mounted on the upper surface of its flight control platform. The electricity generated by the wind turbine's rotation powers the charging module.
1:高速無人機 1: High-speed drones
11:光纖筒 11: Optical fiber tube
12:光纖 12: Optical Fiber
2:飛控平台 2: Flight Control Platform
21:停機台 21: Terminal
22:捲軸 22: Roller
23:太陽能板 23: Solar Panels
24:風力發電機 24: Wind turbines
3:第一控制電路 3: First control circuit
31:指令接收模組 31: Command Receiving Module
32:影像擷取模組 32: Image Capture Module
33:電源模組 33: Power Module
4:第二控制電路 4: Second control circuit
41:指令傳輸模組 41: Command Transmission Module
42:操控模組 42: Control Module
421:操控單元 421: Control Unit
422:處理單元 422: Processing Unit
43:影像接收模組 43: Image Receiving Module
44:充電模組 44: Charging Module
5:GPS定位天線 5: GPS positioning antenna
51:直桿 51: Straight rod
52:圈體 52: Circle Body
圖1係本創作之高速無人機立體圖。 Figure 1 is a 3D rendering of the high-speed drone created in this work.
圖2係本創作之飛控平台立體圖。 Figure 2 is a 3D view of the flight control platform of this invention.
圖3係本創作之飛控平台開啟立體圖。 Figure 3 is a 3D view of the flight control platform of this creation in operation.
圖4係本創作之較佳實施例電路方塊圖。 Figure 4 is a circuit block diagram of a preferred embodiment of this invention.
圖5係本創作之高速無人機飛行狀態圖。 Figure 5 shows the flight status of this high-speed drone.
圖6係本創作之高速無人機回收狀態圖。 Figure 6 shows the recovery status of the high-speed drone in this creation.
圖7係本創作之另一實施例高速無人機立體圖。 Figure 7 is a 3D view of another embodiment of this invention: a high-speed drone.
請同時參閱圖1及圖2,並配合圖3及圖4,係為本創作之無人機立體圖、飛控平台立體圖及飛控平台開啟立體圖、較佳實施例電路方塊圖。如圖所示,本創作係包含高速無人機1及飛控平台2。其中,高速無人機1的內部係設有第一控制電路3,底緣係設有一光纖筒11,於光纖筒11收容適當長度,且連接高速無人機1內部第一控制電路3之光纖12。於本實例,該第一控制電路3係包含但不限於指令接收模組31及影像擷取模組32,以及供應整台高速無人機1電力之電源模組33。 Please refer to Figures 1 and 2, and in conjunction with Figures 3 and 4, which show the three-dimensional view of the drone, the three-dimensional view of the flight control platform, the three-dimensional view of the flight control platform in operation, and the circuit block diagram of a preferred embodiment. As shown in the figures, this invention includes a high-speed drone 1 and a flight control platform 2. The high-speed drone 1 has a first control circuit 3 internally, and an optical fiber tube 11 is located at its bottom edge. An optical fiber 12 of appropriate length is housed in the optical fiber tube 11 and connected to the first control circuit 3 inside the high-speed drone 1. In this embodiment, the first control circuit 3 includes, but is not limited to, a command receiving module 31, an image acquisition module 32, and a power supply module 33 supplying power to the entire high-speed drone 1.
該飛控平台2,係設有一收藏空間,以及一可由該收藏空間拉出之停機台21,以供高速無人機1置於該停機台21,收容於收藏空間或由收藏空間拉出。飛控平台2內部係設有第二控制電路4,該第二控制電路4係連接於光纖12,且使光纖12捲繞於一設於飛控平台2前方下緣之捲軸22。於本實例,該第二控制電路4係包含但不限於指令傳輸模組41、操控模組42、影像接收模組43及充電模組44,其中之操控模組42又包含操控單元421及處理單元422。該飛控平台2的上方表面,係分別設有適當面積之太陽能板23,以及一風力發電機24,俾藉由太陽能板23於吸收陽光所轉換之電力,提供充電模組44之電源,以及藉由風力發電機24於受風轉動所轉換之電力,提供充電模組44之電源。 The flight control platform 2 is equipped with a storage space and a landing platform 21 that can be pulled out from the storage space, so that the high-speed drone 1 can be placed on the landing platform 21, stored in the storage space, or pulled out from the storage space. The flight control platform 2 is equipped with a second control circuit 4, which is connected to an optical fiber 12 and the optical fiber 12 is wound around a spool 22 located at the lower front edge of the flight control platform 2. In this embodiment, the second control circuit 4 includes, but is not limited to, a command transmission module 41, a control module 42, an image receiving module 43, and a charging module 44, wherein the control module 42 includes a control unit 421 and a processing unit 422. The upper surface of the flight control platform 2 is equipped with a solar panel 23 of appropriate size and a wind turbine 24. The solar panel 23 generates electricity from sunlight to power the charging module 44, and the wind turbine 24 generates electricity from wind-driven rotation to power the charging module 44.
藉由前述構件的組合,構成防禦型高速無人機,於高速無人機1未使用時,可收容於飛控平台2內,由充電模組44對電源模組33進行充電(係可藉由無線充電方式進行充電)。而當使用時,將停機台21由飛控平台2拉出,以供操控高速無人機1的飛行,俾當高速無人機1於 飛行時,光纖12由光纖筒11釋出,使飛控平台2得以藉由光纖12傳輸飛行指令,且可藉由光纖12將無人機所擷取的影像訊號回傳飛控平台2。而當回收該高速無人機1時,則藉由捲軸22的轉動,將光纖12纏繞於該捲軸22的軸部。從而可防止高速無人機1的操控訊號受到其他無線訊號干擾,或干擾周邊之其他設備。 The combination of the aforementioned components constitutes a defensive high-speed drone. When the high-speed drone 1 is not in use, it can be housed in the flight control platform 2, and the power module 33 can be charged by the charging module 44 (wireless charging is possible). When in use, the landing platform 21 is pulled out from the flight control platform 2 for controlling the flight of the high-speed drone 1. When the high-speed drone 1 is in flight, the optical fiber 12 is released from the optical fiber tube 11, allowing the flight control platform 2 to transmit flight commands via the optical fiber 12, and to transmit the image signals captured by the drone back to the flight control platform 2 via the optical fiber 12. When the high-speed drone 1 is retrieved, the optical fiber 12 is wound around the shaft of the reel 22 by the rotation of the reel 22. This prevents the control signals of the high-speed drone 1 from being interfered with by other wireless signals or by other surrounding equipment.
請參閱圖5,係為本創作之無人機飛行狀態圖。敬請配合圖4,如圖所示,本創作於使用時,係將停機台21由飛控平台2拉出,以供操控高速無人機1的飛行。俾當高速無人機1於飛行時,光纖12由光纖筒11釋出,使飛控平台2得以藉由操控模組42之操控單元421及處理單元422經光纖12傳輸飛行指令至高速無人機1,由高速無人機1之指令接收模組31接收後控制高速無人機1的飛行,且可藉由影像擷取模組32擷取影像,將所擷取的影像訊號經由光纖12回傳至飛控平台2。從而可防止無人機的操控訊號受到其他無線訊號干擾,或干擾周邊之其他設備。 Please refer to Figure 5, which shows the flight status of the drone in this invention. Please also refer to Figure 4. As shown, in use, the landing platform 21 is pulled out from the flight control platform 2 to control the flight of the high-speed drone 1. When the high-speed drone 1 is in flight, the optical fiber 12 is released from the optical fiber tube 11, allowing the flight control platform 2 to transmit flight commands to the high-speed drone 1 via the control unit 421 and processing unit 422 of the control module 42 through the optical fiber 12. The command receiving module 31 of the high-speed drone 1 receives the commands and controls the flight of the high-speed drone 1. Furthermore, the image capture module 32 can capture images and transmit the captured image signals back to the flight control platform 2 via the optical fiber 12. This prevents the drone's control signals from being interfered with by other wireless signals or interfering with other surrounding equipment.
圖6係本創作之無人機回收狀態圖,如圖所示,本創作當高速無人機1完成任務後,係由飛控平台2操控使捲軸22轉動,將光纖12纏繞於該捲軸22的軸部,進而將高速無人機1拉回停機台21,且將停機台21收入於飛控平台2內進行充電。於本創作之理想實施方式,其中之光纖12係於使用一次後即予以更新,以防止光纖12因拗折、彎曲受損影響訊號的傳輸。 Figure 6 shows the drone recovery status of this invention. As shown, after the high-speed drone 1 completes its mission, the flight control platform 2 controls the rotation of the reel 22, winding the optical fiber 12 around its shaft, thereby pulling the high-speed drone 1 back to the landing platform 21. The landing platform 21 is then stored in the flight control platform 2 for charging. In an ideal implementation of this invention, the optical fiber 12 is replaced after each use to prevent damage from bending or twisting from affecting signal transmission.
前述本創作,係可供應用於驅逐一般玩家於民用機場附近使用無人機。由於一般無線操控傳輸的無線電波可能被干擾而失控,或可能 會影響到飛機的起降,本創作以利用光纖12傳輸訊號方式構成操控,故而不會造成被干擾或干擾周邊設備的問題,可於順暢的飛行操控狀態下,有效的驅逐玩家之無人機。改善現階段機場相關單位只能於偵測到無線訊號時,以人為方式驅逐無人機玩家,缺乏機動性及效率之缺失。 The aforementioned invention is applicable to deterring drone operators from using their drones near civilian airports. Since conventional wireless control transmissions can be interfered with and become uncontrollable, or may affect aircraft takeoff and landing, this invention utilizes fiber optic 12 for signal transmission, thus avoiding interference with surrounding equipment. It can effectively deter drone operators while maintaining smooth flight control. This improves upon the current practice where airport authorities can only manually deter drone operators upon detecting wireless signals, lacking flexibility and efficiency.
本創作進一步係可供應用於領空防禦作戰,於戰時若敵軍以無人機進行攻擊,現階段雖可同樣以無人機反制,惟對戰過程中同樣存在操控訊號被干擾而失控的問題,失去反制的目的。本創作之高速無人機1因藉由光纖12傳輸操控訊號,可有效且確實的防止訊號干擾的問題,順利的操控高速無人機1對敵機衝撞使其墜落,達到領空防禦之目的。 This invention can be further applied to airspace defense operations. In wartime, if the enemy attacks with drones, while current methods can counter with drones, the problem of control signal interference leading to loss of control and defeating the purpose of counterattack remains. This invention's high-speed drone 1, by transmitting control signals via fiber optic cable 12, effectively and reliably prevents signal interference, allowing for successful ramming of enemy aircraft and causing them to crash, thus achieving the purpose of airspace defense.
請參閱圖7,係為本創作之另一實施例高速無人機立體圖。如圖所示,本創作之高速無人機1,係可於前緣適當位置,設有複數之GPS定位天線5,該GPS定位天線5係包含一直桿51,以及以圈繞於該直桿51之彈簧狀之圈體52。該GPS定位天線5除了可供接收GPS訊號或如海巡長波訊號,以利於執行飛行任務外,且於敵軍以無人機進行來犯時,得以藉由該GPS定位天線5構成有效之攻擊。 Please refer to Figure 7, which is a three-dimensional view of another embodiment of the high-speed drone of this invention. As shown in the figure, the high-speed drone 1 of this invention can be equipped with a plurality of GPS positioning antennas 5 at appropriate positions at its leading edge. Each GPS positioning antenna 5 includes a vertical rod 51 and a spring-like coil 52 wound around the vertical rod 51. Besides receiving GPS signals or long-wave signals such as those from maritime patrol vessels to facilitate flight missions, the GPS positioning antenna 5 can also be used to launch an effective attack when enemy forces launch drone attacks.
前述實施例,僅為說明本創作之較佳實施方式,而非限制本創作之範圍,凡經由些微修飾、變更,仍不失本創作之要義所在,亦不脫本創作之精神範疇。 The foregoing examples are merely illustrative of preferred embodiments of this work and are not intended to limit its scope. Any minor modifications or alterations will not deviate from the essence or spirit of this work.
綜上所述,本創作以具有控制電路及光纖之高速無人機,配合設有停機台及充電模組之飛控平台,構成防禦型高速無人機。藉由光纖傳輸飛行指令及影像訊號,以改善習知無人機因藉由無線訊號操控,易受到其他無線訊號干擾或干擾周邊設備之缺失。為一實用之設計,誠屬一俱 新穎性之創作,爰依法提出專利之申請,祈 鈞局予以審查,早日賜准專利,至感德便。 In summary, this invention utilizes a high-speed drone equipped with control circuitry and fiber optics, combined with a flight control platform featuring a landing pad and charging module, to form a defensive high-speed drone. By transmitting flight commands and image signals via fiber optics, it overcomes the shortcomings of conventional drones, which rely on wireless signal control and are susceptible to interference from other wireless signals or interference with surrounding equipment. This is a practical and truly innovative design, and therefore, a patent application is filed in accordance with the law. We respectfully request the Bureau of Civil Engineering to examine and grant the patent as soon as possible.
1:高速無人機 1: High-speed drones
11:光纖筒 11: Optical fiber tube
2:飛控平台 2: Flight Control Platform
21:停機台 21: Terminal
22:捲軸 22: Roller
23:太陽能板 23: Solar Panels
24:風力發電機 24: Wind turbines
3:第一控制電路 3: First control circuit
32:影像擷取模組 32: Image Capture Module
33:電源模組 33: Power Module
Claims (6)
Publications (1)
| Publication Number | Publication Date |
|---|---|
| TWM680840U true TWM680840U (en) | 2026-03-11 |
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