Turbine Engine

Turbine Engine

1st - 5th Grade

11 Qs

quiz-placeholder

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Turbine Engine

Turbine Engine

Assessment

Quiz

Mathematics

1st - 5th Grade

Medium

Created by

Gabriel Nievales

Used 3+ times

FREE Resource

11 questions

Show all answers

1.

FILL IN THE BLANK QUESTION

1 min • 1 pt

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is an internal combustion engine that uses air as its working fluid. It extracts chemical energy from fuel and converts it into mechanical energy by utilizing the gaseous energy of the working fluid (air) to drive the engine and propeller, propelling the airplane.

2.

FILL IN THE BLANK QUESTION

1 min • 1 pt

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is a jet engine which produces all of its thrust by ejecting a high energy gas stream from the engine exhaust nozzle.

3.

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1 min • 1 pt

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is a modern variation of the basic gas turbine engine.
It consists of a core engine surrounded by a fan at the front and an additional turbine at the rear. The fan and fan turbine, like the core compressor and core turbine, have many blades and are connected to an additional shaft.

4.

FILL IN THE BLANK QUESTION

1 min • 1 pt

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is a type of jet engine optimized to drive an aircraft propeller through reduction gearing.
Aircraft equipped with turboprop engines are highly efficient at lower flight speeds, consuming less fuel per seat mile and requiring shorter runways for takeoff and landing.

5.

FILL IN THE BLANK QUESTION

1 min • 1 pt

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engine is a variant of a gas turbine engine optimized to produce shaft power to drive machinery instead of generating thrust.

6.

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1 min • 1 pt

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designed to guide incoming air to the compressor with minimal energy loss due to drag or ram pressure. This ensures that the airflow into the compressor is free of turbulence, maximizing operating efficiency. The intake sits upstream of the compressor, and its main parts include the inlet cowl and fan cowl doors.

7.

FILL IN THE BLANK QUESTION

1 min • 1 pt

Media Image

gas turbine engine is responsible for providing a sufficient quantity of compressed air to meet the needs of combustion. It increases the pressure of the incoming air mass received at the inlet and supplies it to the combustion section at the required pressure.

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