AIRCRAFT WHEEL BRAKING PERFORMANCE COMMUNICATIONS SYSTEMS AND METHODS

Systems and methods for providing aircraft braking signal alerts for aircraft are described including a first braking condition signal generated by a first aircraft (12) or a control station (16). The first braking condition signal may include, for example, a timestamp, an airfield identifier, a run...

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Bibliographische Detailangaben
1. Verfasser:	GADZINSKI, JOHN
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PARACHUTES PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OFVEHICLES SIGNALLING SURVEYING TESTING TRAFFIC CONTROL SYSTEMS TRANSPORTING VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	Systems and methods for providing aircraft braking signal alerts for aircraft are described including a first braking condition signal generated by a first aircraft (12) or a control station (16). The first braking condition signal may include, for example, a timestamp, an airfield identifier, a runway identifier, and/or first braking condition information. A runway to be used by a second aircraft (14) may be determined automatically, and a determination made regarding the relevance of the first braking condition information to the second aircraft. A braking alert signal for the second aircraft may be generated and/or updated based on the first braking condition information, and a visual indicator (7) may be presented to an operator of the second aircraft based on the braking alert signal. The first braking condition information may be overwritten based on a second braking condition signal received from a third aircraft or the control station.