Accession Number : ADA018859
Title : Improved Pneumatic-Fluidic Antiskid System and Preliminary System Integration Study.
Descriptive Note : Final rept. Sep 74-Jun 75,
Corporate Author : BOEING COMMERCIAL AIRPLANE CO SEATTLE WASH
Personal Author(s) : Straub,H. H. ; Lichtenwalter,R. H. ; Attri,N. S.
Report Date : AUG 1975
Pagination or Media Count : 104
Abstract : Improvements of an existing pneumatic-fluidic antiskid system leading to operating efficiencies above 85% and installation concepts for a full system test on the T-43A aircraft are described. A fluidic locked wheel and touchdown protection circuit is proposed. Initial design of the integrated fluidic circuit and the modification of the antiskid valve in accordance with a detailed system specification are shown.
Descriptors : *Landing gear, *Skidding, *Jet aircraft, *Fluidic control, Pneumatic valves, Safety equipment, Breadboard models, Performance, Braking, Fluidics
Subject Categories : Aircraft
Fluidics and Fluerics
Distribution Statement : APPROVED FOR PUBLIC RELEASE