The Analysis of Motion Characteristics of Variable Forward-Swept Wing Mechanism with a Double Slideways

Article Preview

Abstract:

Based on the variable forward-swept wing configuration, this paper utilized a variable forward-swept wing mechanism with a double slideways, which make it possible for the aircraft to switch among orthogonal wing, forward-swept wing and delta wing freely. The general configuration of the variable forward-swept wing mechanism with a double slideways was elucidated by means of a three-dimensional model plot and then the mathematic simulation model was also established. The motion characteristics of linear motion were simulated, analyzed and optimized. The results indicated that the variable forward-swept wing mechanism with a double slideways can meet the aerodynamic requirements better. Moreover, there exists great linear relationship between the position of nut and the wing forward-swept angle. Therefore, this mechanism may serve as a useful reference when developing a morphing aircraft.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

137-141

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Brett A N, Robert L S. Classical Flight Dynamics of A Variable Forward-Sweep-Wing Aircraft. Journal of Guidance, 1986, 9(2), pp.352-362.

DOI: 10.2514/3.20113

Google Scholar

[2] Northrop Grumman Corporation. Aircraft with Variable Forward Sweep Wing: USA, US5984231. (1999).

Google Scholar

[3] Shigeru Horinouchi. Variable Forward Swept Wing Supersonic Aircraft Having Both Low-Boom Characteristics and Low-Drag Characteristics: USA, US Fresh Patent 20050230531. (2005).

Google Scholar

[4] Wang X, Liu W F, Mi K. A Design of Wing-Body Revolved Mechanism for UAV with Variable Forward-Swept Wing. Journal of Air Force Engineering University: Natural Science Education, 2009, 10(3), pp.1-4.

Google Scholar

[5] Wang D Z, Dong E B, Xu M. Structural Design and Kinematics Simulation for t he Variable Forward swept Wing. Machinery and Electronics, 2011(4), pp.8-11.

Google Scholar

[6] Liang J H, Liu H X, Shu X B. A 90-Deg-Alterable and Self-Lockable Mechanism for Variable Backward-Swept Wing: China, 2010 10116741. (2010).

Google Scholar

[7] Woldemar Voigt. Swept Wing with Unswept Span: USA, 3018985. (1962).

Google Scholar

[8] Lu C W. World's Aircraft Handbook. Beijing: Aviation Industry Press, 1988, pp.30-163.

Google Scholar

[9] Fang B R. Aircraft aerodynamic Configuration Design. Beijing: Aviation Industry Press, 1997, pp.363-367.

Google Scholar

[10] Chen P, Wang X, Hu M Q, Yu C. The Design of Wing-Body Switching Mechanism with Two Slideway. Acta Aeronautica Et Astronautica Sinica, 2012, 33(11), p.2010-(2017).

Google Scholar