High-efficiency propeller and unmanned aerial vehicle
By using variable pitch design and segmented span optimization of the propeller blades, the problems of efficiency fluctuation and insufficient aerodynamic layout of traditional UAV propellers have been solved, achieving efficient and stable UAV flight performance.
CN224529030UActive Publication Date: 2026-07-21ZHONGSHAN YIXING INNOVATION TECHNOLOGY CO LTD
View PDF 0 Cites 0 Cited by
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- ZHONGSHAN YIXING INNOVATION TECHNOLOGY CO LTD
- Filing Date
- 2025-05-26
- Publication Date
- 2026-07-21
Smart Images
Figure CN224529030U_ABST
Abstract
The utility model provides a kind of high-efficiency propeller and unmanned aerial vehicle, including hub, with the hub connection blade, the installation angle β between the blade from 0.16±0.005L any position to blade tip is decreased from 25.2°±0.3° to 3.83°±0.3°;Wherein, L is the distance from the hub center axis to blade tip.In this scheme, the end of the blade away from the hub is the blade tip, the end close to the hub is the blade root, the arbitrary position of the blade 0.16±0.005L is the part of the blade close to the hub / blade root end.The installation angle β is also pitch angle, the included angle between the straight line direction of the leading edge and the trailing edge of the blade section and the rotating plane is pitch angle.Setting the installation angle of the blade can reduce the speed, reduce power, improve force efficiency under the same pull force as traditional blade.
Need to check novelty before this filing date? Find Prior Art