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The Development of Non-Hydraulic Shimmy Dampers
Technical Paper
2000-01-1710
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
The development of non-hydraulic shimmy dampers for single engine aircraft at Lord Corporation is described.
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Authors
Citation
Meyers, A., "The Development of Non-Hydraulic Shimmy Dampers," SAE Technical Paper 2000-01-1710, 2000, https://doi.org/10.4271/2000-01-1710.Also In
References
- Esmailzadeh, E. Farzaneh, K. A. Shimmy Vibration of Analysis of Aircraft Landing Gears Journal of Vibration and Control 5 45 56 1999
- Young, Y A., US Patent 5,535,861 Dual-Rate Linear Damper Assignee - Lord Corporation Jul 16 1996
- Siwek US Patent 5,183,137 Dual-Rate Surface Effect Dampers Assignee - Lord Corporation Feb 2 1993
- Corcoran US Patent 5,257,680 Surface Effect Dampers Having Both Hysteresis and a Frictional Component Assignee - Lord Corporation Nov 2 1993
- Grossman, D. T. F-15 Nose Landing Gear Shimmy, Taxi Test and Correlative Analyses SAE Aerospace Congress & Exposition, 801239 1980
- Black, R. J. Realistic Evaluation of Landing Gear Shimmy Stabilization by Test and Analysis SAE, Business Aircraft Meeting, 760496 1976
- Podgorski, W. A. Krauter, A. I. Rand, R. H. The Wheel Shimmy Problem: Its Relationship to Wheel and Road Irregularities Vehicle System Dynamics 4 9 41 1975