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

Report Date:

1975-08-01

Pagination or Media Count:

104.0

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.

Subject Categories:

  • Aircraft
  • Fluidics and Fluerics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE