A program was conducted to demonstrate and establish the applicability of using dual property steel armore (DPSA) integrally in complex Army aircraft critical components, thus eliminating or minimizing the requirement for adding armor plate (shielding) to protect these components from small-arms ballistic impacts. A CH-54B primary flight control hydraulic servo actuator was selected as the critical component and was redesigned using DPSA as the cylinder material. Three experimental units were fabricated and tested. (Author)
Design, Fabrication, and Performance Testing of Integral Armored Servo Actuators
1972
118 pages
Report
Keine Angabe
Englisch
Hydraulic & Pneumatic Equipment , Hydraulic actuators , Flight control systems , Hydraulic servomechanisms , Armor plate , Helicopters , Steel , Stability , Projectiles , Stresses , Pressure , Protection , Impact , Small arms ammunition , Fatigue(Mechanics) , Pins , Rods , Performance(Engineering) , Manufacturing , Design , Servoactuators , Ch-54 aircraft , H-54 aircraft
TIBKAT | 1964
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