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An example of landing gear shimmy experience on small jet aircraft
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Description
First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan
Wheel shimmy of an aircraft landing gear is one of self-induced vibration. Wheels and tires equipped at the bottom of a landing gear will have yaw oscillation about the vertical axis when shimmy occurs. Such shimmy was observed at the nose landing gear on a small jet aircraft. Investigation succeeded to replicate the shimmy at the laboratory component test, which determined some specific conditions where shimmy would occur. The shimmy problem was finally resolved by the following improvement - The steering collar was modified to have a viscous resistance feature for more damping and a more stable friction feature.
形態: 図版あり
Physical characteristics: Original contains illustrations
資料番号: AA1630046051
レポート番号: JAXA-SP-16-008E
Journal
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- 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application
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宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application JAXA-SP-16-008E 475-484, 2017-03-15
宇宙航空研究開発機構(JAXA)
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Keywords
Details 詳細情報について
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- CRID
- 1050574036225144192
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- NII Article ID
- 120006827505
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- NII Book ID
- AA11984031
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- ISSN
- 1349113X
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- Web Site
- http://id.nii.ac.jp/1696/00003438/
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- Text Lang
- en
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- Article Type
- conference paper
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- Data Source
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- IRDB
- CiNii Articles