TWD217752S - gyro drone - Google Patents

gyro drone Download PDF

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Publication number
TWD217752S
TWD217752S TW109304063F TW109304063F TWD217752S TW D217752 S TWD217752 S TW D217752S TW 109304063 F TW109304063 F TW 109304063F TW 109304063 F TW109304063 F TW 109304063F TW D217752 S TWD217752 S TW D217752S
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TW
Taiwan
Prior art keywords
design
drone
gyroscopic
tail
motor
Prior art date
Application number
TW109304063F
Other languages
Chinese (zh)
Inventor
約爾格 沙穆恩
Original Assignee
匈牙利商羅德傑有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by 匈牙利商羅德傑有限公司 filed Critical 匈牙利商羅德傑有限公司
Priority to TW109304063F priority Critical patent/TWD217752S/en
Publication of TWD217752S publication Critical patent/TWD217752S/en

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Abstract

【物品用途】;本設計係提供一種陀螺無人機,特別是指一種外觀上結合直升機和旋翼機並通過空氣動力學優化形狀,提供緊湊機身設計之陀螺無人機。;【設計說明】;如各視圖所示,本設計陀螺無人機不帶有具扭矩補償用途之尾旋翼,且還可以選擇使尾部不帶有尾翼和尾翼穩定器,藉以提供緊湊的機身設計,以使在直升機模式下的阻力最小化,並且包括在直升機模式下運行無人機的所有要素,且,主翼的翼尖處帶有電機,可確保電機與主體線之間保持較大距離,如此在直升機模式下提供扭矩補償,並在旋翼機模式下提供電機之牽引而有助於使機翼在向前飛行時為系統增加升力。另,本設計陀螺無人機以倒V形尾翼設計,可以控制在旋翼機模式下以較快速度向前飛行時的姿態,同時允許在所有電動機均出現故障而緊急著陸時滑行。相信透過緊湊的機身設計,配合主翼末端的電機及倒V形尾翼設計,確實能夠讓本設計陀螺無人機予人外觀獨特與性能前衛的風貌。;綜上所述,本創作陀螺無人機確為新穎且獨樹一格的設計,爰依法提出申請。[Use of item]; This design provides a gyroscopic drone, specifically a gyroscopic drone that combines a helicopter and a rotorcraft in appearance and optimizes the shape through aerodynamics to provide a compact body design. ;[Design Description];As shown in each view, the gyroscopic drone of this design does not have a tail rotor for torque compensation, and you can also choose to have a tail without a tail and a tail stabilizer to provide a compact fuselage design. , to minimize the drag in helicopter mode, and include all the elements to operate the drone in helicopter mode, and, the main wing has a motor at the wing tip to ensure a large distance between the motor and the main body line, so It provides torque compensation in helicopter mode and provides motor traction in rotorcraft mode to help the wing increase lift for the system when flying forward. In addition, the gyroscopic drone of this design is designed with an inverted V-shaped tail, which can control the attitude when flying forward at a faster speed in the gyroplane mode, while allowing it to glide when all motors fail and make an emergency landing. I believe that through the compact fuselage design, combined with the motor at the end of the main wing and the inverted V-shaped tail design, this gyroscopic drone can indeed give people a unique appearance and avant-garde performance. ; To sum up, the gyroscopic drone of this creation is indeed a novel and unique design, and an application must be filed in accordance with the law.

Description

陀螺無人機 gyro drone

本設計係提供一種陀螺無人機,特別是指一種外觀上結合直升機和旋翼機並通過空氣動力學優化形狀,提供緊湊機身設計之陀螺無人機。 This design system provides a gyroscopic UAV, especially a gyroscopic UAV that combines helicopter and gyrocopter in appearance and optimizes the shape through aerodynamics to provide a compact fuselage design.

如各視圖所示,本設計陀螺無人機不帶有具扭矩補償用途之尾旋翼,且還可以選擇使尾部不帶有尾翼和尾翼穩定器,藉以提供緊湊的機身設計,以使在直升機模式下的阻力最小化,並且包括在直升機模式下運行無人機的所有要素,且,主翼的翼尖處帶有電機,可確保電機與主體線之間保持較大距離,如此在直升機模式下提供扭矩補償,並在旋翼機模式下提供電機之牽引而有助於使機翼在向前飛行時為系統增加升力。另,本設計陀螺無人機以倒V形尾翼設計,可以控制在旋翼機模式下以較快速度向前飛行時的姿態,同時允許在所有電動機均出現故障而緊急著陸時滑行。相信透過緊湊的機身設計,配合主翼末端的電機及倒V形尾翼設計,確實能夠讓本設計陀螺無人機予人外觀獨特與性能前衛的風貌。 As shown in each view, the gyro UAV of this design does not have a tail rotor for torque compensation purposes, and can also choose to have no tail rotor and tail stabilizer at the tail, thereby providing a compact body design. drag is minimized in low and includes all elements of running the drone in helicopter mode, and the main wing has a motor at the tip, which ensures a large distance between the motor and the main body line, which provides torque in helicopter mode Compensation, and in gyroplane mode provides motor traction to help the wings add lift to the system in forward flight. In addition, the gyro UAV of this design is designed with an inverted V-shaped tail, which can control the attitude when flying forward at a relatively fast speed in the gyrocopter mode, and at the same time allows to glide when all the motors fail and land in an emergency. It is believed that through the compact fuselage design, combined with the motor at the end of the main wing and the design of the inverted V-shaped tail, the gyro drone of this design can indeed give people a unique appearance and avant-garde performance.

綜上所述,本創作陀螺無人機確為新穎且獨樹一格的設計,爰依法提出申請。 To sum up, the creation of the gyro drone is indeed a novel and unique design, and an application is made in accordance with the law.

TW109304063F 2020-07-22 2020-07-22 gyro drone TWD217752S (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
TW109304063F TWD217752S (en) 2020-07-22 2020-07-22 gyro drone

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
TW109304063F TWD217752S (en) 2020-07-22 2020-07-22 gyro drone

Publications (1)

Publication Number Publication Date
TWD217752S true TWD217752S (en) 2022-03-21

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ID=88921614

Family Applications (1)

Application Number Title Priority Date Filing Date
TW109304063F TWD217752S (en) 2020-07-22 2020-07-22 gyro drone

Country Status (1)

Country Link
TW (1) TWD217752S (en)

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