An example of landing gear shimmy experience on small jet aircraft

‐, Inoue, Kohei

説明

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

収録刊行物

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

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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詳細情報詳細情報について

CRID: 1050574036225144192

NII論文ID: 120006827505

NII書誌ID: AA11984031

ISSN: 1349113X

Web Site: http://id.nii.ac.jp/1696/00003438/

本文言語コード: en

資料種別: conference paper

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