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

See similar textbooks

Related questions

Q: I need part 10 answered pertaining to the print and instructions.

A: In the given sketch,Number 2 and Number 4 are relief valves. Number 2 is high-pressure relief…

Q: What is the purpose of using modes that control or limit "pressure delivery" with each breath in a…

A: The mechanical ventilator is a device used to regulate the optimum gases in the lungs. The working…

Q: Draw a simple flowchart of a hypothetical oxygen piping system containing the following components:…

A: The oxygen piping system follows this path:PSA generator creates oxygen.Compressor pressurizes the…

Q: Contrast the major differences between these three different mechanical ventilators: Puritan Bennett…

A: Three mechanical ventilators given

Q: give me actual picture base on this circuit, they are cylinder, doublr solenoid valve, check valve,…

A: Given:To find:Draw the actual picture of the double pump circuit.

Q: In hydraulic actuators, both linear and rotary, which depends directly on flow rate, and which…

A: To find : In hydraulic actuators, 1. Force of actuation depends on 2. Speed of actuation depends…

Q: The Pictorial diagram below shows a forklift used to lift loads It is operated by hand operated…

Q: A 5/2-way directional control valve, normally open with a spring return on the left end and is…

A: Given question is related to robotics engineering.

Q: Pick up 2 types of pneumatic control components given in the lesson. Explain the specific…

A: Since you have been posted multiple questions. So, we are solving only first question for you. If…

Q: Match the fluid power system with its suitable applications/lequipment Hydraulics A. Dump trucks v…

Q: 20. In a pneumatic flow ratio control system, the primary flow range is 0 to 50 gpm, and the…

A: Primary flow range, P=Secondary flow range,Q=To determine:the flow range ratio

Q: Which indicates the I/P transducer for a flow valve? . Select one: O a. 1 FY O b. 2 O c. 3 1002 1001…

A: An I/P transducer (short for current-to-pressure transducer) is a device used to control pneumatic…

Q: Describe this control valve, select specific answers Sol A

A: From Above Diagram it consists of Hydraulic Control Valve 2 - Positions 4 - Port Spring Return…

Concept explainers

Applied Fluid Mechanics

A fluid is a substance that is continuously deformed by the application of shear stress. The rate of deformation of a fluid depends on its viscosity. The fluid tries to flow when it interacts with some other system.

Question

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
THEL

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1: To draw circuit of the flap and aileron actuation system.

VIEW

Step 2: Circuit of flap and aileron system

VIEW

Solution

VIEW

Step by step

Solved in 3 steps with 1 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.

Similar questions

Please solve all four part
Q44 Name the different controls used in centrifugal compressors and explain their functions.
The system is designed so that the average outflow is 90 lpm and the operating range of the normally-closed (NC, air to open) linear valve is 0 - 207 lpm. The controller has a 4-20 mA output. Determine the equilibrium state for the valve? me = mA
## Draw and describe a simplified diagram of a section of an industrial sugar and alcohol piping system, which contains the following equipment: 1 Pump 1 Heat Exchanger Elbows for changing the flow path Flux Valves The ultimate goal is to calculate system and pump pressure losses.
Classify the air conditioner system if it is an open-loop or closed-loop system and give the reason of your choice, draw a simple block diagram with the name of input, output and control system used
The system is designed so that the average outflow is 108 gpm and the operating range of the normally-open (NO, air to close) linear valve is 0 - 206 gpm. The controller has a pneumatic 3 - 15 psig output. Determine the equilibrium output of the controller? me = psi
Draft a sketch of this system describe below
What is the main reason for conducting a 3-point stroke test on the pneumatic control valves on the 3-phase separator? To ensure that the control valves are not stuck when the controllers require the control valves to open or close precisely. To ensure that the control valves can move rapidly based on the controllers' output. To check that the controllers are functioning properly. To check that the valve positioner scales are accurate.