Aircraft brake control system having hydroplaning protection

Fluid-pressure and analogous brake systems – Speed-controlled – Having a valve system responsive to a wheel lock signal

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Details

188181C, 244111, 303 20, B60T 810

Patent

active

040069419

ABSTRACT:
Aircraft velocity information signals are utilized to provide a brake release signal to one or more, but not more than half of the wheels in each locked wheel set e.g. the two rear wheels in a four wheel set on a gear, so that if all braked wheels lock up and hydroplane, the brake relase signal holds half the brakes released and when the released wheels come out of hydroplaning and spinup, then they, in turn, provide conventional locked wheel protection to the remaining wheels in the same locked wheel set.

REFERENCES:
patent: 3260555 (1966-07-01), Packer
patent: 3756663 (1973-09-01), Fink et al.
patent: 3768874 (1973-10-01), Riordan
patent: 3866979 (1975-02-01), Rabus et al.

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