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An Approach to the Isolation and Control of Vibration in Light Business Aircraft
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English
Abstract
This paper presents an approach utilized by a light business aircraft manufacturer in resolving vibrational problems. The discussion relates the principle sources of vibration; objective briefly explores the consideration of priority in the operational range of the aircraft. The approach phases--preventive measures, theoretical application, and practical application--are illustrated through an actual vibration problem solution. It is concluded that this approach has proved satisfactory and that the importance of the practical aspect cannot be underestimated.
Authors
Citation
Burgess, W., "An Approach to the Isolation and Control of Vibration in Light Business Aircraft," SAE Technical Paper 640436, 1964, https://doi.org/10.4271/640436.Also In
References
- “Dynofacts,” Magazine of Vibration/Shock/Noise Control 6 3
- Freberg C. R. Kemler E. N. “Aircraft Vibration and Flutter.” New York John Wiley and Sons 1944
- McFarland Ross A. “Human Factors in Air Transport Design.” New York McGraw-Hill 1946
- Flight Test Data Sheets -- pertinent to PA-30 vibration tests Piper Aircraft Corp
- Pilots Comment Book for N7000Y -- prototype PA-30 Piper Aircraft Corp.
- Fatigue Tests of PA-30 Engine Mount Piper Aircraft Corp.
- Engine Mount Service Test Piper Aircraft Corp.