Aircraft automatic braking system

Fluid-pressure and analogous brake systems – Pipeless valves

Patent

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Details

244111, B60T 802

Patent

active

040763315

ABSTRACT:
An aircraft automatic braking system is provided having deceleration selecting apparatus which is responsive to nose wheel contact with the runway surface. The system applies a lesser deceleration level than commanded by the pilot while the nose wheels are in the air and switches to the pilot selected deceleration level upon nose wheel contact with the runway thereby preventing hard nose gear touchdown due to automatic braking pressure application prior to nose wheel touchdown.

REFERENCES:
patent: 3856365 (1974-12-01), Steigerwald et al.

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