Simulation Research on Motion Law of Arresting Hook during Landing

Article Preview

Abstract:

The key of a safety landing is the arresting hook can engage an arresting wire. Thus, research on motion law of arresting hook during landing is essential. The construction features and function of typical arresting hook installation is studied. Take into consideration the influence on collision process produced by the deck friction in order to build an actual model of arresting hook during landing. So we can use the model to study the motion law of arresting hook during landing for the sake of supplying a beneficial reference to design of arresting hook and successful engagement with an arresting wire. Simulation results show that the value of height of first hook bounce diminishes linearly with increasing values of coefficient of friction and increases linearly with increasing values of sinking speed. Therefore, we should consider the deck friction in an arresting hook collision which is available for designing a reasonable damper and must ensure the value of sinking speed in a reasonable range to satisfy the condition of engagement with arresting gear.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

997-1002

Citation:

Online since:

February 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] The Chief Committee of Aircraft Design Manual. Aircraft design manual: takeoff and landing system design . Aviation Industry Press, Beijing , (2002).

Google Scholar

[2] Thomlinson J, A Study of the Aircraft Arresting-Hook Bounce Problem, The Principal Director of Scientific Research (Air), Ministry of Supply, (1954).

Google Scholar

[3] GAO Zejiong, A discussion of bounce kinematics of aircraft arresting hook and cable dynamics, J. Acta Aeronautica et Astronautica Sinica : Series B , Vol. 11, No. 12( 1990) B543-B546.

Google Scholar

[4] LIU Gang , NIE Hong, Dynamics of Arresting Hook Bounce After Initial Touchdown and Impacting with Deck ,J. Acta Aeronautica et Astronautica Sinica, Vol. 30, No. 9(2009)1672-1677.

Google Scholar

[5] LIU Gang, NIE Hong, Dynamics of Bounce of Aircraft Arresting Hook Impacting with Deck and Performance of Arresting Hook Longitudinal Damper, J. Act Aeronautica et Astronautica Sinica, Vol. 30, No. 11(2009)2093-(2099).

Google Scholar

[6] SUN Anyuan, HUANG Peitian, On the completly inelastic collision and the coefficient of restitution, J. College Physics, Vol. 20, No. 3(2001) 9-14.

Google Scholar

[7] WEN Shizhu, HUANG Ping , Principles of Tribology , third ed., TSINGHUA UNIVERSITY PRESS, Beijing, (2008).

Google Scholar

[8] ZHANG Xin, LI Yulong, LIU Yuanyong etal., Arresting Hook and Cable Dynamics of Aircraft Arrest Landing on or off Centre ,J. Journal of Mechanical Strength, Vol. 30, No. 4(2008) 549-554.

Google Scholar

[9] LIU Xin, WANG Siyi , The Preliminary Parameter Analysis for Arresting Gear of Carrier-based Fighter Aircraft ,J. AIRCRAFT DESIGN, Vol. 31, No. 4(2011)12-16.

Google Scholar

[10] YAO Niankui, SUI Fucheng , WANG Chengbo , Free Flight Engagement Condition of Carrier-based Aircraft ,J. AIRCRAFT DESIGN, Vol. 31, No. 6(2011)10-15.

Google Scholar

[11] Lyle W. Jones, Development of curves for estimating aircraft arresting hook loads AD-A119551. (1982).

Google Scholar