Gas Turbine Engine chapter 1

Gas Turbine Engine chapter 1

University

10 Qs

quiz-placeholder

Similar activities

Inspect and Service Fuel System

Inspect and Service Fuel System

University

7 Qs

Features Of Wing Design

Features Of Wing Design

7th Grade - Professional Development

11 Qs

Quiz based on automobile engine cooling system

Quiz based on automobile engine cooling system

University

11 Qs

2 Speed Supercharger

2 Speed Supercharger

University

6 Qs

Turborreactores

Turborreactores

University

8 Qs

Electric Vehicle

Electric Vehicle

University

10 Qs

DSL 201 WEEK 1 DAY 2 WARM UP

DSL 201 WEEK 1 DAY 2 WARM UP

University

10 Qs

Pre Trip Inspection

Pre Trip Inspection

University

15 Qs

Gas Turbine Engine chapter 1

Gas Turbine Engine chapter 1

Assessment

Quiz

Education

University

Easy

Created by

Mas Gecol

Used 2+ times

FREE Resource

10 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the primary purpose of a gas turbine engine in an aircraft?

to provide thrust to propel the aircraft forward, by generating high-speed exhaust gases that push against the atmosphere.

to provide thrust to propel the aircraft forward, by generating low-speed exhaust gases that push against the atmosphere.

to provide drag to propel the aircraft forward, by generating low-speed exhaust gases that push against the atmosphere.

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What are the main types of gas turbine engines used in aircraft?

The main types of gas turbine engines used in aircraft are turbojets, turbofans, turboprops, and turboshafts.

The main types of gas turbine engines used in aircraft are piston engine.

The main types of gas turbine engines used in aircraft are hybird engine

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How does a turbofan engine differ from a turbojet engine?

A turbofan engine has a large fan at the front that bypasses a portion of the airflow around the core engine, producing additional thrust and improving fuel efficiency compared to a turbojet engine, which relies solely on the core engine’s exhaust for thrust.

A turbofan engine has a large fan at the front that bypasses a portion of the airflow around the core engine, producing additional thrust and improving fuel efficiency compared to a turbojet engine, which relies solely on the core engine’s exhaust for drag.

A turbofan engine has a large fan at the front that bypasses a portion of the airflow around the core engine, producing additional thrust and improving fuel efficiency compared to a turbojet engine, which relies solely on the core engine’s exhaust for lift .

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the purpose of the high bypass ratio in modern turbofan engines?

The high bypass ratio in modern turbofan engines improves fuel efficiency, reduces noise, and enhances thrust by allowing a greater proportion of the airflow to bypass the combustion chamber and turbine.

The high bypass ratio in modern turbofan engines improves fuel efficiency, reduces noise, and enhancesdrag

The high bypass ratio in modern turbofan engines improves fuel efficiency, reduces noise, and enhances lift

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What role does the engine nacelle play in an aircraft gas turbine engine?

The engine nacelle is the housing that encloses the engine, providing aerodynamic smoothness, reducing drag, and housing components like the thrust reverser and air intakes.

The engine nacelle is the housing that encloses the engine, providing aerodynamic smoothness, reducing lift, and housing components like the thrust reverser and air intakes.

The engine nacelle is the housing that encloses the engine, providing aerodynamic smoothness, reducing thurst, and housing components like the thrust reverser and air intakes.

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Why is cooling important in gas turbine engines used in aircraft?

Cooling is important to maintain engine temperatures within safe limits, prevent overheating of critical components, and ensure reliable performance and longevity of the engine.

Cooling is important to maintain engine temperatures within safe limits, prevent overheating of critical components, and ensure reliable performance and longevity of the wings.

Cooling is important to maintain engine temperatures within safe limits, prevent overheating of critical components, and ensure reliable performance and longevity of the cabine.

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is a thrust reverser, and how does it benefit aircraft during landing?

A thrust reverser is a mechanism that redirects the engine's thrust forward instead of backward, helping to slow down the aircraft more efficiently during landing by providing additional deceleration.

A full throttle is a mechanism that redirects the engine's thrust forward instead of backward, helping to slow down the aircraft more efficiently during landing by providing additional deceleration.

A midle fuel flow is a mechanism that redirects the engine's thrust forward instead of backward, helping to slow down the aircraft more efficiently during landing by providing additional deceleration.

Create a free account and access millions of resources

Create resources
Host any resource
Get auto-graded reports
or continue with
Microsoft
Apple
Others
By signing up, you agree to our Terms of Service & Privacy Policy
Already have an account?