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Bearingless helicopter main rotor development. Volume 2: Combined load fatigue evaluation of weathered graphite/epoxy composite

机译：无轴承直升机主旋翼发展。第2卷：风化石墨/环氧复合材料的组合载荷疲劳评估

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摘要

Small scale combined load fatigue tests were conducted on six artificially and six naturally weathered test specimens. The test specimen material was unidirectionally oriented A-S graphite - woven glass scrim epoxy resin laminate.

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作者
Rackiewicz, J. J.;
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年度 1977
页码 1-50
总页数 50
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
FATIGUE TESTS; GRAPHITE; LOAD TESTS; ROTARY WINGS; COMPOSITE MATERIALS; EPOXY RESINS; HELICOPTERS; LAMINATES;

机译：疲劳测试;石墨;负荷试验;旋转翼;复合材料;环氧树脂;直升机; LamINaTEs;

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专利

1. An Aeroelastic Analysis Methodology for Bearingless Main Rotor Helicopters [J] . Farhan Gandhi, Inderjit Chopra Journal of the American Helicopter Society . 1998,第1期

机译：无轴承主旋翼直升机的气动弹性分析方法
2. A Lower Bound Estimate of the Critical Load for Helicopter Main Rotor Composite Blade According to the Limit Equilibrium Theory. The Basic Steps of an Algorithm [J] . A. V. Gorelov, I. N. Sidorov Russian Aeronautics . 2011,第3期

机译：根据极限平衡理论，对直升机主旋翼复合材料叶片的临界载荷进行下界估计。算法的基本步骤
3. A Lower Bound Estimate of the Critical Load for Helicopter Main Rotor Composite Blade According to the Limit Equilibrium Theory. Analysis Results [J] . A. V. Gorelov, I. N. Sidorov Russian Aeronautics . 2011,第4期

机译：根据极限平衡理论，对直升机主旋翼复合材料叶片的临界载荷进行下界估计。分析结果
4. THE APPLICABILITY AND RELIABILITY OF UNIDIRECTIONAL CARBON FIBER REINFORCED PLASTIC COMPOSITE (T-1000G/EPOXY 3651) TO HELICOPTER BEARINGLESS ROTOR FLEXBEAM [C] . Faisal Alzaidi, Toshio Ogasawara, Masahisa Takashi International Conference on Composite Materials: Extended Abstracts . 2005

机译：单向碳纤维增强塑料复合材料（T-1000G /环氧3651）到直升机无轴承转子柔性轴的适用性和可靠性
5. Investigation into the static and fatigue behaviour of a helicopter main rotor yoke made of composite materials. [D] . Lalonde, Stephanie. 2000

机译：研究复合材料制成的直升机主旋翼轭的静态和疲劳行为。
6. Evaluation and Modeling of the Fatigue Damage Behavior of Polymer Composites at Reversed Cyclic Loading [O] . Ilja Koch, Gordon Just, Martin Brod, 2019

机译：反向循环载荷下聚合物复合材料疲劳损伤行为的评估与建模
7. Fatigue Safe Life Analysis of Helicopter Bearingless Rotor Hub Composite Flexbeam [O] . Taejoo Kim, Youngjoong Kee, Deog-Kwan Kim, 2013

机译：直升机轴承转子轮毂复合柔性柔性疲劳安全寿命分析

Bearingless helicopter main rotor development. Volume 2: Combined load fatigue evaluation of weathered graphite/epoxy composite

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