PURPOSE: To facilitate the balanced design of an airframe by annexedly providing a controller used for operating the rudder of a jet airplane or additionally providing a united generator for controlling actuators as a dissolution type generator for each actuator for composing a private power generation system to omit a feeder, and to remove influence clue to electromagnetic interference and contact mine.
CONSTITUTION: A multipletype generator 1 is provided in each actuator for operating the rudder of a jet airplane through a manifold or the like, and a hydraulic motor 3 is connected to both the ends of the rotary shaft of the generator 1 through a one-way clutch 2, and a pressure compensation type flow regulating valve 5 is insertedly provided in a hydraulic line 4. Thus a dissolution type generating system is composed.
ARAI YUTAKA
KIKUCHI TOSHIMICHI
OKAMOTO HATSUZO
FUSHIMI AKIHIRO
KAYABA INDUSTRY CO LTD
KAWASAKI HEAVY IND LTD
| JPH05147894A | 1993-06-15 | |||
| JPS5814427U | 1983-01-29 |