Silent cyclorotor with low-friction material placed on the blade surface.

Low-friction materials on cyclo-rotor blades address noise reduction and maintenance issues by dispersing airflow turbulence, enhancing noise reduction and durability.

JP2026073905AActive Publication Date: 2026-05-01田中 芳明
View PDF 8 Cites 0 Cited by

Patent Information

Authority / Receiving Office
JP · JP
Patent Type
Applications
Current Assignee / Owner
田中 芳明
Filing Date
2024-10-20
Publication Date
2026-05-01

AI Technical Summary

Technical Problem

Existing cyclo-rotors lack effective noise reduction designs using three-dimensional serrated structures due to dirt accumulation and maintenance issues, leading to reduced noise reduction efficacy and durability concerns.

Method used

Application of a low-friction material, such as carbon nanotubes or graphene, in a stripe pattern on the blade surface to disperse airflow and suppress turbulence, enhancing noise reduction while maintaining ease of cleaning and durability.

Benefits of technology

The low-friction material effectively reduces noise by dispersing airflow turbulence and prevents dirt accumulation, improving maintainability and durability of cyclo-rotors.

✦ Generated by Eureka AI based on patent content.
Patent Text Reader

Abstract

While cyclorotors are quieter than conventional propeller-type rotors, further noise reduction is desirable. A quiet blade design using a jagged structure based on the principle of an owl's wing is conceivable, but its complex shape makes it prone to dirt and difficult to maintain. Therefore, instead of a jagged structure, this design provides a cyclorotor form that reduces noise by strategically arranging low-friction materials. [Solution] By arranging low-friction material in a vertical stripe pattern on the surface and / or back of the blade, from the leading edge to the trailing edge and / or from the trailing edge to the leading edge, the air flowing within the boundary layer on the surface and / or back of the blade is straightened, forming a dispersed pattern in which air of different velocities is arranged alternately in a vertical direction, thereby suppressing the generation of large turbulence on the surface and / or back of the blade. As a result, noise generated from turbulence is reduced.
Need to check novelty before this filing date? Find Prior Art

Description

Background Art

[0001] By means of the comb-like three-dimensional serrated structure on the wings, owls can finely disperse the air flowing within the boundary layer of the wings, suppress the generation of large-scale turbulence, reduce the noise generated from the turbulence, and fly quietly. There are already noise reduction designs applying this principle, such as the introduction of three-dimensional serrated structures in the blades of wind turbines and the fan blades of aircraft engines. Detailed Description of the Invention

[0002] Cyclo-rotors have better mobility compared to conventional propeller systems and are expected to be installed in aircraft such as drones, wind power generation systems, and blowers. Although cyclo-rotors reduce noise by effectively controlling the air flow, it is desirable to further reduce the noise. Regarding the noise reduction design for cyclo-rotors, there is currently no such noise reduction design using a three-dimensional serrated structure on the blade surface as described in 0001, but it is considered as one of the methods to reduce noise. However, three-dimensional serrated structures tend to have complex shapes, and it is considered that dirt easily adheres to and accumulates in the grooves of the serrated structures. If dirt adheres to and accumulates in the grooves of the serrated structure, the effect of finely dispersing the air flowing within the boundary layer of the blade surface will be lost, and thus the noise reduction effect cannot be exerted. And due to their complex shapes, three-dimensional serrated structures are difficult to clean, resulting in poor maintainability, and it is also expected that they have poor durability, such as being prone to cracking starting from the grooves of the serrated structure. Therefore, instead of a three-dimensional serrated structure, a method was considered where a low-friction material is characteristically arranged on the blade surface of the cyclo-rotor to finely disperse the air flowing within the boundary layer of the blade surface and suppress the generation of large-scale turbulence to reduce noise. Embodiments of the invention will be described. As an example of a conceivable embodiment, a cyclo-rotor is considered in which a low-friction material such as carbon nanotubes or graphene is arranged in a stripe shape in the longitudinal direction on the front and / or back surfaces of the blade by means of coating or arrangement of materials from the leading edge to the trailing edge and / or from the trailing edge to the leading edge of the blade. Within the boundary layer of the blade surface where low-friction material is placed, the friction is low, so the air flowing within the boundary layer is slippery. Therefore, the airflow velocity differs between "air flowing within the boundary layer of the blade surface where low-friction material is not placed" and "air flowing within the boundary layer of the blade surface where low-friction material is placed". According to this embodiment, by arranging low-friction material in a vertical stripe pattern on the surface and / or back of the blade from the leading edge to the trailing edge and / or from the trailing edge to the leading edge, the air flowing within the boundary layer on the surface and / or back of the blade is rectified, forming a dispersed pattern in which air of different velocities is arranged alternately in a vertical direction, thereby suppressing the generation of large turbulence on the surface and / or back of the blade. As a result, noise generated from turbulence is reduced. Furthermore, because it does not have a complex three-dimensional shape such as a jagged structure, it is easy to clean and maintain, less prone to dirt accumulation, and less likely to crack.

Claims

[Claim 1] A cyclorotor characterized by having low-friction material arranged in a vertical stripe pattern on the surface and / or back of the blade, from the leading edge to the trailing edge and / or from the trailing edge to the leading edge.

Citation Information

Patent Citations

  • Integrated thunder protection and electrical deicing for aerodynamic structure

    JP2019112051A

  • Propeller blade machining for acoustic control

    JP2019513602A

  • Wind power generator has eccentric an axis multi cycloid system

    KR1020110010241A

  • High-altitude wind power generation system with cycloidal turbine and motor-generator, and method of operating the same

    US20140252776A1

  • Cycloidal Rotor Micro-Air Vehicle

    US20190337616A1