Analysis of Pedal Operated Wheel Brake System of a Helicopter Using Adams Software
International Journal of Science and Research (IJSR)

International Journal of Science and Research (IJSR)
www.ijsr.net | Open Access | Fully Refereed | Peer Reviewed International Journal

ISSN: 2319-7064

Research Paper | Mechanical Engineering | India | Volume 3 Issue 6, June 2014

Analysis of Pedal Operated Wheel Brake System of a Helicopter Using Adams Software

Dr. Yadavalli Basavaraj, Pavan Kumar B. K, Gourishankar Hiremath

In wheel type of landing gear helicopters landing gear wheels and tyres are used for ground maneuvering. So for smooth ground maneuvering; run on take off; run on landing and for helicopter spot turning a brake system is mandatory for wheel type landing gear helicopters. The objective of this paper is to give a simple; basic and generalized design procedure to design a wheel brake system of a wheel type landing gear helicopters; the design should meet INDUSTRY standard requirements and analyzing the kinematic behavior of wheel brake pedal system using ADAMS software. The pedal system is modeled in ADAMS software by using joints of the pedal system as definition points and individual part characteristics. After simulating the model for 20 degrees of pedal travel the characteristics of Brake Master Cylinder axial load and Pedal torque data are acquired from ADAMS postprocessor.

Keywords: Brake system, ADAMS, INDUSTRY standards, Master cylinder, helicopter

Edition: Volume 3 Issue 6, June 2014

Pages: 2651 - 2653

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How to Cite this Article?

Dr. Yadavalli Basavaraj, Pavan Kumar B. K, Gourishankar Hiremath, "Analysis of Pedal Operated Wheel Brake System of a Helicopter Using Adams Software", International Journal of Science and Research (IJSR), https://www.ijsr.net/search_index_results_paperid.php?id=2014823, Volume 3 Issue 6, June 2014, 2651 - 2653

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