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Rotor Vibration Reduction Using Mult...
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Su, Keye.
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Rotor Vibration Reduction Using Multi-Element Multi-Path Design.
紀錄類型:
書目-語言資料,印刷品 : Monograph/item
正題名/作者:
Rotor Vibration Reduction Using Multi-Element Multi-Path Design./
作者:
Su, Keye.
面頁冊數:
113 p.
附註:
Source: Masters Abstracts International, Volume: 51-06.
Contained By:
Masters Abstracts International51-06(E).
標題:
Engineering, Mechanical. -
電子資源:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1536305
ISBN:
9781303044557
Rotor Vibration Reduction Using Multi-Element Multi-Path Design.
Su, Keye.
Rotor Vibration Reduction Using Multi-Element Multi-Path Design.
- 113 p.
Source: Masters Abstracts International, Volume: 51-06.
Thesis (M.S.)--Duke University, 2013.
Multi-Element Multi-Path (MEMP) structural design is a new concept for rotor vibration reduction. This thesis explores the possibility of applying MEMP design to helicopter rotor blades. A conceptual design is developed to investigate the MEMP blade's vibration reduction performance. In the design, the rotor blade is characterized by two centrifugally loaded beams which are connected to each other through linear and torsional springs. A computer program is built to simulate the behavior of such structures. Detailed parametric studies are conducted. The main challenges in this thesis involve the blade hub load vibration analysis, the blade thickness constraint and the blade parameter selection. The results show substantial vibration reduction for the MEMP design but the large relative deflection between the two beams, conceptualized as an internal spar and airfoil shell, remains a problem for further study.
ISBN: 9781303044557Subjects--Topical Terms:
783786
Engineering, Mechanical.
Rotor Vibration Reduction Using Multi-Element Multi-Path Design.
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Multi-Element Multi-Path (MEMP) structural design is a new concept for rotor vibration reduction. This thesis explores the possibility of applying MEMP design to helicopter rotor blades. A conceptual design is developed to investigate the MEMP blade's vibration reduction performance. In the design, the rotor blade is characterized by two centrifugally loaded beams which are connected to each other through linear and torsional springs. A computer program is built to simulate the behavior of such structures. Detailed parametric studies are conducted. The main challenges in this thesis involve the blade hub load vibration analysis, the blade thickness constraint and the blade parameter selection. The results show substantial vibration reduction for the MEMP design but the large relative deflection between the two beams, conceptualized as an internal spar and airfoil shell, remains a problem for further study.
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