Mechanical Power System for Aircraft Intermittent Utility Functions.
Final technical rept. Mar 75-Feb 79,
ROCKWELL INTERNATIONAL EL SEGUNDO CA LOS ANGELES DIV
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The program reported upon herein is designed to develop a satisfactory method for utilizing flywheel energy in an aircraft control system. To attain this objective, the program will design, fabricate and demonstrate a mechanical power package MPP for controlling and powering a high-horsepower utility actuation function. The MPP will consist of a hydraulic motor, a flywheel, an adapter gearbox, a controller, and a screwjack actuator, and will be designed to replace an existing hydraulic actuator. Author
- Electric Power Production and Distribution
- Machinery and Tools