A magneto ignition system:
a. Does not require a coil b. Produces AC power c. Produces a hotter spark at high speeds d. Does not require points
a. Does not require a coil
b. Produces AC power
c. Produces a hotter spark at high speeds
d. Does not require points
The dual fuel engine:
a. Does not require an injector b. May operate on a gas-air mixture only c. Do not have any valves d. None of the above
a. Does not require an injector
b. May operate on a gas-air mixture only
c. Do not have any valves
d. None of the above
Two types of steam nozzles used for steam turbines are convergent and;
Divergent Stationary Convergent-Divergent Low Flow High Velocity
Divergent
Stationary
Convergent-Divergent
Low Flow
High Velocity
As the steam passes through the convergent nozzle there is a;
Small pressure drop Large Pressure drop Small increase in pressure Large Increase in pressure Velocity decrease
Small pressure drop
Large Pressure drop
Small increase in pressure
Large Increase in pressure
Velocity decrease
A Reaction blade is characterized by a large entranced angle of almost (?) and a small discharge angle.
45 degrees 30 degrees 180 degrees 15 degrees 90 degrees
45 degrees
30 degrees
180 degrees
15 degrees
90 degrees
The distinguishing feature if the reaction turbine is the fact that the pressure does drop across the;
Stationary blades Moving blades There is no pressure drop Stationary and moving blades None of the above
Stationary blades
Moving blades
There is no pressure drop
Stationary and moving blades
None of the above
In order to reduce the steam and blade velocity, the following methods may be used;
Pressure compounding Velocity compounding Pressure-Velocity compounding Mass compounding Acceleration compounding
I, II
I, III, IV
I, II, III
III, V
IV, V
For large impulse turbines, it is very common to have a velocity compound first stage, followed by;
Several pressure compounded stages in the same casing
Several pressure-velocity compounded stages in the same casing
Several Acceleration compounded stages in a separate casing
Several Velocity compounded stages in a separate casing
Turbines fall into two major categories, Condensing and;
Low pressure
High Pressure
Double Flow
Non-condensing
Single flow
A non-condensing turbine is also called a;
Low-pressure turbine
Backpressure turbine
Front Pressure turbine
Bleed turbine
High pressure, high temperature casings used with temperatures above 550 degrees, are made of;
Cast iron
Carbon steel
Aluminum
Copper
Cast alloy steel with 3% chromium and 1% molybdenum
The term for a material at a given maximum temperature and under constant pressure that continues to deform with a very slow increasing strain on the material is called;
Creep
Slowness
Tension
Crawl
What percentage of pressure drop is there in a impulse turbine across the moving blades
5%
10%
30%
60%
Seal Strips, used to allow close running clearance with relatively large clearance between heavy parts are often made of;
Chrome-iron alloy
Nickel
In an impulse turbine, turbine thrust must be counteracted since failure to do so would result in;
Less pressure
Greater pressure
Contact between the moving and stationary parts
Contact between the moving parts and casing
From the thrust bearing the shaft must be free to expand in either direction, thus, the shaft can have only (?) thrust bearing(s)
1
2
3
4
5
Turbines can be used to drive;
Pumps
Compressors
Fans
Blowers
All of the above
What is the over speed trip for a turbine used for?
To shut down the turbine in case of low pressure
To shut down the turbine in case of high pressure
To shut down the turbine in case of high speed
Just another name for something that has no purpose
Lubricating oil pressure on turbines is usually in the (?) Range?
15psi – 40psi
15KPa – 40KPa
69KPa – 138KPa
69psi – 138psi
Before lubrication oil flows through the bearings of a turbine it needs to be cooled in the oil coolers. The typical outlet temperature, from the coolers, is in the (?) range.
43 degrees C – 49 degrees C
43 degrees F – 49 degrees F
23 degrees C – 42 degrees C
23 degrees F – 42 degrees F
When left cold and at a standstill the weight of the rotor of a turbine will tend to cause the rotor to sag slightly. This is called;
Bending
Tapering
Sagging
Bowing
Hogging