Improved Pneumatic-Fluidic Antiskid System and Preliminary System Integration Study.
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1975
- Accession Number
- ADA018859
Entities
People
- H. H. Straub
- N. S. Attri
- R. H. Lichtenwalter
Organizations
- Boeing Commercial Airplanes