HELICOPTER VIBRATION REDUCTION USING STRUCTURAL OPTIMIZATION WITH AEROELASTIC MULTIDISCIPLINARY CONSTRAINTS - A SURVEY

被引：49

作者：

FRIEDMANN, PP

机构：

[1] University of California at Los Angeles, Los Angeles, CA

[2] Mechanical, Aerospace, and Nuclear Engineering Department

来源：

JOURNAL OF AIRCRAFT | 1991年 / 28卷 / 01期

关键词：

D O I：

10.2514/3.45987

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a survey of the state-of-the-art in the field of structural optimization when applied to vibration reduction of helicopters in forward flight with aeroelastic and multidisciplinary constraints. It emphasizes the application of the modern approach where the optimization is formulated as a mathematical programming problem, the objective function consists of the vibration levels at the hub, and behavior constraints are imposed on the blade frequencies and aeroelastic stability margins, as well as on a number of additional ingredients that can have a significant effect on the overall performance and flight mechanics of the helicopter. It is shown that the integrated multidisciplinary optimization of rotorcraft offers the potential for substantial improvements, which can be achieved by careful preliminary design and analysis without requiring additional hardware such as rotor vibration absorbers or isolation systems.

引用

页码：8 / 21

页数：14

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