Aircraft Powerplant Assessment 30 questions

0.0(0)
studied byStudied by 0 people
learnLearn
examPractice Test
spaced repetitionSpaced Repetition
heart puzzleMatch
flashcardsFlashcards
Card Sorting

1/29

encourage image

There's no tags or description

Looks like no tags are added yet.

Study Analytics
Name
Mastery
Learn
Test
Matching
Spaced

No study sessions yet.

30 Terms

1
New cards

Absolute Pressure

 

Sum of the gauge pressure and atmospheric pressure.

2
New cards

Boundary


Separates the substance to its surroundings.

3
New cards

Every body persists in its state of rest, or of motion in a straight line, unless acted upon by some outside force

Newton’s first law of motion generally termed the law of Inertia. States:


4
New cards

Brayton Cycle


A turbojet engine operates on a?

5
New cards

an isentropic process

Entropy is also defined as that function of the working substance which remain constant during:

6
New cards

Stroke


It is referred to as the distance the piston travels from its outward limit.


7
New cards

53.5


A certain spring when stretched measures 15.5 cm requiring a work of 564 joules to do it. Its free length is 5.4 cm. What is the spring constant (in kN/meter)?

8
New cards

Torque bending force

A type of force that occurs as air resistance opposes the rotational motion of the propeller's blades. This force tends to bend the blades opposite the direction of rotation.

9
New cards

Diesel Cycle


A four stroke cycle engine in which air only is taken into the cylinder on the suction stroke and liquid fuel is lower injected. No spark plug used. High temperature due to high Compression. Constant pressure combustion.

10
New cards

Pressure


In the P-V diagram of the Brayton Cycle, which parameter is constant?

11
New cards

centrifugal and axial flow

The two types of compressor commonly used on jet engines are

12
New cards

converted into another

The first law of thermodynamics states that one form of energy may be?


13
New cards

the less tendency of gasoline to detonate


The detonation properties of gasoline are measured by an octane number, the higher the number,

14
New cards

N2 Compressor

In a dual axial-flow compressor, the first stage turbine drives__________.


15
New cards

0.01 cu m

The temperature of an ideal gas remains constant while the absolute pressure changes from 103.4 kPa to 827.2 kPa. If the initial volume is 80 liters, what is the final volume?

16
New cards

It increases the surface area of the cylinder for convection.

How do cooling fins help in dissipating heat from the cylinder assembly?

17
New cards

Opposed


The _____ type engine has two banks of cylinders directly opposite each other with a crankshaft in the middle.

18
New cards

As a fail-safe in case one of the springs fail.


Why is it preferred to have two sets of valve springs?

19
New cards

Boyle's Law

This shows the relationship of the pressure, volume, temperature and mass of a gas in reference to its universal gas constant.

20
New cards

203


In a certain location, the barometer reads 13.45 psi and a pressure gauge reads 86 psig. Solve for the absolute pressure in inches mercury.

21
New cards

Crankpin

These are offset from the main bearing journal to provide attachment points for connecting rods.

22
New cards

Front of the compressor and the aft end of the turbine.

Engine pressure ratio is the total pressure ratio between the

23
New cards

Volume


Which of the following is not an intensive property?

24
New cards

287.08 J/kg-K

Universal gas constant is equal to __________.


25
New cards

Connecting Rod


The _____ is the link which transmits forces between the piston and the crankshaft.

26
New cards

blue

100LL aviation fuel is colored


27
New cards

Bypass ratio

It is the ratio of the mass of secondary air to the mass of primary air

28
New cards

Complete 2 strokes

A crankshaft completes one rotation in order to:

29
New cards

mineral or synthetic based.


The recommended aircraft engine lubricants are

30
New cards

9,996

Calculate the pressure (in kPa) at the start of power stroke of an internal combustion engine, assuming the specific heats and gas constant for the fuel-air mixture are approximated by the air values alone. The temperature at the start of the power stroke is 3490 deg K. The temperature at the end of the compression stroke is 550 deg K. and the pressure at the end of the compression stroke is 15.5 atm.