Transport helicopter blade root cuff attachment modernization concepts

The article discusses the issue of modernizing the blade root cuff attachment of the main rotor blade of a Mi-8 type transport helicopter. Several geometry options were designed and the stress-strain state of various options in a nonlinear formulation under the influence of operational loads was calculated using numerical methods. Conclusions are provided regarding the strength and mass of the blade root cuff attachment options under consideration. The influence of the tightening value of fasteners and the use of adhesive on the stress distribution along the connection is analyzed. Analytical methods were used to determine the optimal dimensions of fastening elements.

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Publication Details

Journal
Наука і техніка Повітряних Сил Збройних Сил України
Published
2024-09-02
DOI
https://doi.org/10.30748/nitps.2024.55.03
Primary Topic
Mechanical Failure Analysis and Simulation
Type
article
Field-Weighted Citation Impact
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article

Transport helicopter blade root cuff attachment modernization concepts

Сергій Олександрович Дегтяренко, Mykhaylo Kybalnyy, Valentyn P. Pelykh
Наука і техніка Повітряних Сил Збройних Сил України
Mechanical Failure Analysis and Simulation
article

Transport helicopter blade root cuff attachment modernization concepts

Сергій Олександрович Дегтяренко, Mykhaylo Kybalnyy, Valentyn P. Pelykh
article en

Abstract

The article discusses the issue of modernizing the blade root cuff attachment of the main rotor blade of a Mi-8 type transport helicopter. Several geometry options were designed and the stress-strain state of various options in a nonlinear formulation under the influence of operational loads was calculated using numerical methods. Conclusions are provided regarding the strength and mass of the blade root cuff attachment options under consideration. The influence of the tightening value of fasteners and the use of adhesive on the stress distribution along the connection is analyzed. Analytical methods were used to determine the optimal dimensions of fastening elements.

Наука і техніка Повітряних Сил Збройних Сил України(2(55))
Ivchenko Progress (Ukraine) (UA), Chery Automobile (China) (CN)
Openalex Percentile: Top 79%
Mechanical Failure Analysis and Simulation
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