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Rotor-Blade Separation

机译:转子-叶片分离

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Citing a 2007 accident that followed the in-flight separation of a section of a Eurocopter EC 130B4 main rotor blade, the U.S. National Transportation Safety Board (NTSB) has recommended daily checks of main rotor blades on specific helicopters for cracks and surface deterioration. The pilot and seven passengers were not injured in the July 7 accident, but the helicopter was substantially damaged during the emergency descent and autorotation into the Hudson River in New York. The NTSB said the probable causes of the accident were "the fatigue fracture and in-flight separation of a section of the composite main rotor blade trailing edge aft of the spar, due to inadequate manufacture, and the manufacturer's failure to detect an out-of-specification deviation in the rotor blade's trailing-edge roving." (A "roving" is defined by the NTSB as a "collection of fibers in a parallel bundle with little or no twist.") The NTSB said that because the fibers were misaligned, loads were transferred to the skin, which is more susceptible than the fibers to cracking.
机译:美国国家运输安全委员会(NTSB)引用了2007年的事故,当时是在飞行中分离了欧洲直升机公司EC 130B4主旋翼桨叶的一部分后,建议每天检查特定直升机上的主旋翼桨叶是否有裂纹和表面劣化。飞行员和7名乘客在7月7日的事故中没有受伤,但在紧急下降和自转入纽约哈德逊河的过程中,直升机受到了严重损坏。 NTSB表示,事故的可能原因是“由于制造不充分,以及由于制造商未能检测到超出极限,导致翼梁后部复合主旋翼叶片后缘的一部分发生疲劳断裂和飞行中分离。转子叶片后缘粗纱的规格偏差。” (NTSB将“粗纱”定义为“几乎没有或没有扭曲的平行束中的纤维集合。”)NTSB表示,由于纤维未对齐,因此负荷转移到皮肤上,比纤维开裂。

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    《Aerosafety world》 |2011年第4期|p.10|共1页
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