Subscale Aircraft Brake Dynamometer - Lab E36

The machine tests a pair of scaled-down brake rings under scaled braking conditions, which simulate taxi and landing conditions of an airplane. The translational energy of the aircraft is simulated via the rotational energy of the inertia section, in the section painted yellow. The rotational inertia is selected by adding or removing disks of various sizes to the axis. The range of inertias is 0.2 to 4.625 slug-ft2 (2.7 – 6.3 kg-m2). The maximum initial rotational speed is 5000 rpm (524 rad/s). The brake control of the machine can be operated in either constant torque or constant load mode.

 


CENTER FOR ADVANCED FRICTION STUDIES .

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