Arresting hook and cable dynamics of aircraft arrest landing on or off center

Xin Zhang; Yulong Li; Yuanyong Liu; Chuan Dai

Arresting hook and cable dynamics of aircraft arrest landing on or off center

Xin Zhang, Yulong Li, Yuanyong Liu, Chuan Dai

民航学院

科研成果: 期刊稿件 › 文章 › 同行评审

13 引用（Scopus）

摘要

Dynamic response of cable was studied when aircraft equipped with hook was arrested landing on or off center. Considering the kink-wave passing, the impact load and aircraft deceleration were calculated. As examples, American BAK-13 and E-28 arresting gears were studied and analyzed. The maximum arresting hook load of model simulation value was compared with test value using the BAK-13 arresting gear and several kinds of aircrafts. The results indicate that the presented model and analyzing results have fine precision, which can supply available references for aircraft/arresting gear compatibility and carrier aircraft arresting.

源语言	英语
页（从-至）	549-554
页数	6
期刊	Jixie Qiangdu/Journal of Mechanical Strength
卷	30
期	4
出版状态	已出版 - 8月 2008

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abstract = "Dynamic response of cable was studied when aircraft equipped with hook was arrested landing on or off center. Considering the kink-wave passing, the impact load and aircraft deceleration were calculated. As examples, American BAK-13 and E-28 arresting gears were studied and analyzed. The maximum arresting hook load of model simulation value was compared with test value using the BAK-13 arresting gear and several kinds of aircrafts. The results indicate that the presented model and analyzing results have fine precision, which can supply available references for aircraft/arresting gear compatibility and carrier aircraft arresting.",

keywords = "Arresting hook, Cable, Dynamic response, Kink-wave, Off center",

author = "Xin Zhang and Yulong Li and Yuanyong Liu and Chuan Dai",

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T1 - Arresting hook and cable dynamics of aircraft arrest landing on or off center

AU - Zhang, Xin

AU - Li, Yulong

AU - Liu, Yuanyong

AU - Dai, Chuan

PY - 2008/8

Y1 - 2008/8

N2 - Dynamic response of cable was studied when aircraft equipped with hook was arrested landing on or off center. Considering the kink-wave passing, the impact load and aircraft deceleration were calculated. As examples, American BAK-13 and E-28 arresting gears were studied and analyzed. The maximum arresting hook load of model simulation value was compared with test value using the BAK-13 arresting gear and several kinds of aircrafts. The results indicate that the presented model and analyzing results have fine precision, which can supply available references for aircraft/arresting gear compatibility and carrier aircraft arresting.

AB - Dynamic response of cable was studied when aircraft equipped with hook was arrested landing on or off center. Considering the kink-wave passing, the impact load and aircraft deceleration were calculated. As examples, American BAK-13 and E-28 arresting gears were studied and analyzed. The maximum arresting hook load of model simulation value was compared with test value using the BAK-13 arresting gear and several kinds of aircrafts. The results indicate that the presented model and analyzing results have fine precision, which can supply available references for aircraft/arresting gear compatibility and carrier aircraft arresting.

KW - Arresting hook

KW - Cable

KW - Dynamic response

KW - Kink-wave

KW - Off center

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JO - Jixie Qiangdu/Journal of Mechanical Strength

JF - Jixie Qiangdu/Journal of Mechanical Strength

IS - 4

ER -

Arresting hook and cable dynamics of aircraft arrest landing on or off center

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