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夏双满,林长亮,张体磊,等. 典型飞行状态桨榖交变载荷和机体振动水平预估[J]. 科学技术与工程, 2021, 21(8): 3387-3392.
XIA Shuang-man,LIN Chang-liang,ZHANG Ti-lei,et al.Prediction of Hub Alternating Loads and Airframe Vibration Response in Typical Flight Conditions[J].Science Technology and Engineering,2021,21(8):3387-3392.
典型飞行状态桨榖交变载荷和机体振动水平预估
Prediction of Hub Alternating Loads and Airframe Vibration Response in Typical Flight Conditions
投稿时间:2020-06-07  修订日期:2020-12-22
DOI:
中文关键词:  直升机  桨榖交变载荷  振动响应  飞行实测  
英文关键词:helicopter  hub alternating loads  vibration response  flight test
基金项目:第一作者:夏双满(1984—),男,满族,辽宁北镇,硕士,高级工程师。研究方向:直升机动力学。E-mail:xia19840229@163.com。*通信作者:姓 名(1984—),男,满族,辽宁北镇,硕士,高级工程师。研究方向:直升机动力学。E-mail:xia19840229@163.com。 (1. Aircraft Design and Research Institute,AVIC Harbin Aircraft Industry Group Co.Ltd, Harbin 150066, China; 2. The Military Representative Office of the Army Aviation Department in Harbin Region,Harbin 150066, China;)
              
作者单位
夏双满 航空工业哈尔滨飞机工业集团有限责任公司飞机设计研究所
林长亮 航空工业哈尔滨飞机工业集团有限责任公司飞机设计研究所
张体磊 陆军航空军事代表室驻哈尔滨地区军事代表室
崔荫 航空工业哈尔滨飞机工业集团有限责任公司飞机设计研究所
袁胜弢 航空工业哈尔滨飞机工业集团有限责任公司飞机设计研究所
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中文摘要:
      预估机体振动响应需要桨毂振动载荷,以某型直升机为算例,采用综合气弹分析方法对其典型飞行状态下进行桨毂振动载荷计算;通过模块化方法建立某型直升机有限元模型,以计算一阶通过频率下的桨毂振动载荷为输入,预估了机体驾驶员座椅处的振动响应,并与相同飞行状态实测振动水平做了对比分析,分析结果表明,机体响应预测结果与飞行实测结果一致性较好,计算结果符合该型机机体振动随飞行速度变化的规律。
英文摘要:
      In order to predict the vibration response of the aircraft, the hub alternating loads were needed. The hub alternating load of helicopter were calculated in the typical flight conditions by the comprehensive aeroelastic analysis method. The finite element model of helicopter was established by the modular method ,the vibration response were calculated under the first pass frequency hub load. The vibration response at the pilot seat of the helicopter were estimated and compared with flight test results ,The results show that the predicted results are in good agreement with the test results, and the calculated results are in accordance with the law of the variation of the vibration of the airframe with the flight speed.
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