TWD234111S

TWD234111S - Quadcopter drone

Info

Publication number: TWD234111S
Application number: TW112305183F
Authority: TW
Inventors: 王宗源
Original assignee: 艾知科技股份有限公司
Priority date: 2023-10-11
Filing date: 2023-10-11
Publication date: 2024-10-11

Abstract

【物品用途】;本設計係關於一種飛行無人機，特別是有關四旋翼的飛行無人機。;【設計說明】;本設計揭露一種四旋翼無人機，如各視圖所示，具有一機身、四個機臂與四組機翼。又如立體圖所示，機身外觀呈現流線形曲面，四個機臂平均分佈在機身周圍，機臂尾端向上延伸設有一機翼。機身一側係為機頭，機頭係為扁平流線型；機身另一側係為機尾，機尾包含有一鰭片與二固定翼，鰭片設於機尾上方，二固定翼設於機尾下方向外延伸；各機翼設有兩片葉片。;如上所述，本設計具備新穎且獨特之樣式，可顯現出先前技藝所未有之視覺效果，符合設計專利新穎性和創作性要件，爰依法提出專利申請。[Item Usage];This design is about a flying drone, especially a flying drone with four rotors. ;[Design Description];This design discloses a flying drone with four rotors, which has a fuselage, four arms and four sets of wings as shown in the various views. As shown in the three-dimensional view, the fuselage has a streamlined curved surface, and the four arms are evenly distributed around the fuselage. The tail of the arm extends upward and is provided with a wing. One side of the fuselage is the nose, which is flat and streamlined; the other side of the fuselage is the tail, which includes a fin and two fixed wings, the fin is arranged above the tail, and the two fixed wings are arranged below the tail and extend outward; each wing has two blades. ;As mentioned above, this design has a novel and unique style and can show visual effects that have never been achieved by previous technologies. It meets the novelty and creativity requirements of design patents, and therefore a patent application is filed in accordance with the law.

Description

Quadcopter drone

本設計係關於一種飛行無人機，特別是有關四旋翼的飛行無人機。 This design is about a flying drone, especially a quad-rotor flying drone.

本設計揭露一種四旋翼無人機，如各視圖所示，具有一機身、四個機臂與四組機翼。又如立體圖所示，機身外觀呈現流線形曲面，四個機臂平均分佈在機身周圍，機臂尾端向上延伸設有一機翼。機身一側係為機頭，機頭係為扁平流線型；機身另一側係為機尾，機尾包含有一鰭片與二固定翼，鰭片設於機尾上方，二固定翼設於機尾下方向外延伸；各機翼設有兩片葉片。 This design discloses a quad-rotor drone, which has a fuselage, four arms and four sets of wings, as shown in the various views. As shown in the three-dimensional view, the fuselage has a streamlined curved surface, and the four arms are evenly distributed around the fuselage. A wing is extended upward from the tail end of the arm. One side of the fuselage is the nose, which is flat and streamlined; the other side of the fuselage is the tail, which includes a fin and two fixed wings. The fin is located above the tail, and the two fixed wings are located below the tail and extend outward; each wing has two blades.

如上所述，本設計具備新穎且獨特之樣式，可顯現出先前技藝所未有之視覺效果，符合設計專利新穎性和創作性要件，爰依法提出專利申請。As mentioned above, this design has a novel and unique style and can show visual effects that have never been achieved in previous technologies. It meets the novelty and creativity requirements of design patents, and therefore a patent application is filed in accordance with the law.