首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Response of a Squeeze Film Damper-Elastic Structure System to Multiple and Consecutive Impact Loads
【24h】

Response of a Squeeze Film Damper-Elastic Structure System to Multiple and Consecutive Impact Loads

机译:挤压膜阻尼器-弹性结构系统对多次连续冲击载荷的响应

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

Squeeze film dampers (SFDs) are common in aircraft gas turbine engines, customized to provide a desired level of damping while also ensuring structural isolation. This paper presents measurements obtained in a test rig composed of a massive cartridge, an elastic structure, and an open-ends SFD with length L = 25.4 mm, diameter D = 127mm, and radial clearance c = 0.267mm. ISO VG 2 oil at room temperature lubricates the thin film. The measurements quantify the system transient response to sudden loads for motions departing from various static eccentricity displacements, e_s/c = 0-0.6. The batch of tests include recording the system response to (a) one single impact, (b) two (and three) impacts with an elapsed time of 30 ms in between, and (c) two or more consecutive impacts, without any delay, each with a load magnitude at 50% of the preceding impact. The load actions intend to reproduce, for example, a hard landing on an uneven surface or plunging motions from sudden contacts in a machine tool. The test system transient responses due to one or more impacts, each 30 ms apart, show the peak amplitude of motion (Z_(MAX)) is proportional to the magnitude of applied load (F_(MAX)). The identified system damping ratio (ζ) is proportional to the peak dynamic displacement as a linear system would show. Predictions of transient response from a physical SFD model accounting for fluid inertia correlate best with the experimental results as they produce greatly reduced peak dynamic motions when compared to predictions from a purely viscous SFD model. For the responses due to consecutive impacts, one after the other with no delay, the system motion does not decay immediately but builds to produce larger motion amplitudes than in the earlier cases. Eventually, as expected, after several oscillations, the system comes to rest. For an identical damper having a smaller clearance c_s = 0.213 mm (0.8c), its damping ratio (ζ_s) is ~7.5 to ~1.7 times greater than the damping ratio for the damper with a larger film clearance (ζ). Hence, the experimentally derived (ζ_s/ζ) scales with (c/c_s)~2 . The finding demonstrates the importance of manufacturing precisely the components in a damper to produce an accurate clearance.
机译:挤压油膜阻尼器(SFD)在飞机燃气涡轮发动机中很常见,可定制以提供所需的阻尼水平,同时还确保结构隔离。本文介绍了在测试装置中获得的测量结果,该测试装置由大型药筒,弹性结构和开放式SFD组成,长度L = 25.4 mm,直径D = 127mm,径向游隙c = 0.267mm。室温下的ISO VG 2油可润滑薄膜。这些测量结果量化了系统对突然载荷的瞬态响应,这些运动来自各种静态偏心距位移,e_s / c = 0-0.6。这批测试包括记录系统对(a)一次撞击,(b)两次(和三次)撞击的响应,两次撞击之间的间隔时间为30毫秒,以及(c)两次或多次连续撞击,而没有任何延迟,每一个的载荷大小为前一次冲击的50%。负载作用旨在重现例如不平表面上的硬着陆或机床中突然接触引起的剧烈运动。测试系统由于一次或多次撞击而产生的瞬态响应(每隔30毫秒)显示出运动的峰值幅度(Z_(MAX))与所施加负载的大小(F_(MAX))成比例。如线性系统所示,确定的系统阻尼比(ζ)与峰值动态位移成正比。考虑到流体惯性的物理SFD模型的瞬态响应预测与实验结果最相关,因为与纯粘性SFD模型的预测相比,它们产生的峰值动态运动大大降低。对于由于连续冲击而引起的响应,没有延迟,一个接一个地接一个进行,系统运动不会立即衰减,而是会产生比早期情况更大的运动幅度。最终,如预期的那样,在几次振荡之后,系统停止运行。对于具有较小间隙c_s = 0.213 mm(0.8c)的相同阻尼器,其阻尼比(ζ_s)是具有较大膜间隙(ζ)的阻尼器的阻尼比的7.5〜1.7倍。因此,实验得出的(ζ_s/ζ)缩放比例为(c / c_s)〜2。该发现证明了在阻尼器中精确制造零件以产生精确间隙的重要性。

著录项

  • 来源
    《Journal of Engineering for Gas Turbines and Power》 |2016年第12期|122504.1-122504.12|共12页
  • 作者单位

    ASME Turbomachinery Laboratory, Mechanical Engineering Department, Texas A&M University, College Station, TX 77843;

    Turbomachinery Laboratory, Mechanical Engineering Department, Texas A&M University, College Station, TX 77843;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号