Design of light aircraft, transport, military and advanced aircraft brakes which require higher torques and capacities, lighter weights, and small sizes; examples of methods for improving designs, such as approach whereby landing gear, brakes and wheels are designed as integrated unit; auxiliary units for cooling brake assembly during or after brake heat was developed; liquid cooled brake system, developed by B.F. Goodrich whereby heat from brake area is removed and dissipated; results obtained.
Review of past, present and future aircraft brake
Can Aeronautical J
Canadian Aeronautical Journal ; 7 , n 9
1961
10 pages
Article (Journal)
English
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