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