Primary Flight Control Hydraulic Actuation System Interface Definition
NORMA vydána dne 1.10.2015
Označení normy: SAE AIR4922A
Datum vydání normy: 1.10.2015
Země: Americká technická norma
Kategorie: Technické normy SAE
This SAE Aerospace Information Report (AIR) provides a description of the interfaces and their requirements for generic and specific hydraulic actuation systems used in the flight control systems of manned aircraft. Included are the basic control system characteristics and functional requirements, and the essential interfaces (structural, mechanical, hydraulic power, control input, status monitoring, and environment). Major design issues, requirements, and other considerations are presented and discussed.
SUBJECT TAXONOMY: Flight control systems, Hydraulic systems, Aircraft
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
Stabilized: Oct 2015