Rotational material fatigue testing equipment for drone propeller components.

TH28566UActive Publication Date: 2026-07-27BURAPHA UNIV
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Patent Information

Authority / Receiving Office
TH · TH
Patent Type
Utility models
Current Assignee / Owner
BURAPHA UNIV
Filing Date
2025-09-01
Publication Date
2026-07-27

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Abstract

OCR 07AP A fatigue testing device for drone propeller components, designed with a modular testing platform. It is constructed from T-slot aluminum metal profiles and can be customized to meet specific needs. Propeller suitability: This device works in conjunction with high-precision measuring instruments, including cantilever force gauges. Torque measuring devices and vibration monitoring systems are used to detect mechanical values ​​that occur during rotation. The propeller blades and data from each component are sent to a software system that can process the data. Real-time and data storage for post-test analysis.
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Claims

OCR 07AP 1. Rotational material fatigue testing equipment for drone propeller components, consisting of the main structure. (1) Made of aluminum profile material, it has the appearance of a rectangular shelf with 4 upright posts, serving as Supports all systems and provides stability. The rotating power generation unit consists of motor mounting brackets (3). It has the function of attaching to the side of the motor (2) to attach to the main structure (1) The bottom of the motor (2) has a load. Load cell (6) for measuring the lift force generated by the rotation of the drone propellers. The top part of The motor (2) is attached to the coupling (4) and receives rotational force from the motor (2) and transmits it to the propeller shaft mounting base. Drone (5) to perform the function of rotating the drone propeller set to be tested. The drone propeller is an external part for It is assembled onto the test equipment structure when testing is required, with the drone propellers not being a part of it. The main components of this testing equipment structure.