Circuit Design - aircraft system application Draw the circuit of the flap and aileron actuation system of a small aircraft. The hydraulic system uses a variable engine driven pump as power supply. The pump takes flow from a reservoir. The circuit is protected against overload by a pressure relief valve. The speed and the direction of rotation of the flap motor are controlled using an electrically operated proportional valve. The aileron actuator contains a double acting cylinder, which is also controlled by an electrically operated proportional valve. Draw the circuit using ISO standard! Use the following symbol for the electrically operated proportional valve A

Circuit Design - aircraft system application Draw the circuit of the flap and aileron actuation system of a small aircraft. The hydraulic system uses a variable engine driven pump as power supply. The pump takes flow from a reservoir. The circuit is protected against overload by a pressure relief valve. The speed and the direction of rotation of the flap motor are controlled using an electrically operated proportional valve. The aileron actuator contains a double acting cylinder, which is also controlled by an electrically operated proportional valve. Draw the circuit using ISO standard! Use the following symbol for the electrically operated proportional valve A

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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