PIPE Elements 2

93 flashcardsby Juhn
Study these flashcardsFree · spaced repetition · iPhone, Android, Mac & web

All cards

1
Improving the efficiency of an air-standard Otto cycle engine depends chiefly on
a. increasing the compression ratio
b. increasing the temperature and pressure
c. decreasing density
d. increasing specific
a. increasing the compression ratio
2
Increasing the piston diameter or piston stroke of Otto cycle engine will
a. decrease the efficiency of the engine
b. increase the efficiency of the engine
c. increase the work
d. decrease the work
b. increase the efficiency of the engine
3
The work output per cycle also depends strongly on the compression ratio as well as the
a. bore of the engine
b. isentropic compression
c. isentropic expansion
d. volumetric displacement of the engine
d. volumetric displacement of the engine
4
The mean effective pressure of Otto cycle can be increased by increasing the heat transfer into the engine per cycle or by
a. decreasing volumetric expansion
b. increasing the volumetric efficiency
c. increasing pressure ratio
d. decreasing pressure ratio
c. increasing pressure ratio
5
_______the engine in Otto cycle can increase the power of the cycle but not to increase efficiency
a. Discharging
b. Charging
c. Supercharging
d. Scavenging
c. Supercharging
6
A________ is used in aircraft engines and some automotive engine. In this method a turbine driven by the exhaust gases is used to provide power to compressor or blower at the inlet.
a. discharging
b. turbocharging
c. supercharging
d. scavenging
b
7
The practical disadvantage of supercharging is that the pressure P3 will be greater in the supercharge engine resulting in
a. choking
b. knocking
c. trickiting
d. blocking
b
8
Most supercharged of turbo-charged engines use fuel injection of gasoline directly to
a. heat exchanger
b. furnace
c. recuperator
d. combustion chamber
d. combustion chamber
9
The ideal cycles are
a. externally reversible
b. internally reversible
c. externally irreversible
d. internally irreversible
b. internally reversible
10
The thermal efficiency of an ideal cycle is less than that of a totally reversible cycle operating between
a. temperature decrease
b. temperature limits
c. temperature increase
d. none of these
b. temperature limits
11
The only devices where the changes in kinetic energy are significant are the
a. compressor
b. pumps
c. nozzles and diffusers
d. none of these
c. nozzles and diffusers
12
The T-S diagram is useful in the analysis of
a. actual power cycles
b. ideal power cycles
c. combined power cycles
d. none of these
b. ideal power cycles
13
Equations pertaining to steady flow systems should be used in the analysis of
a. Carnot cycle
b. Otto cycle
c. Brayton cycle
d. Rankine cycle
d. Rankine cycle
14
Equations pertaining to closed systems should be used in the analysis of
a. Otto cycle
b. Brayton cycle
c. Absorption system
d. Stirling cycle
a. Otto cycle
15
The carnot cycle is a function of the
a. absolute temperature
b. limit temperature
c. critical temperature
d. sink and source temperature
d. sink and source temperature
16
Thermal efficiency of Carnot cycle increases with______at which heat is added to the system or with a decrease in the average temperature at which heat is rejected from the system
a. a constant average temperature
b. an increase in average temperature
c. a decrease in average temperature
d. none of these
b. an increase in average temperature
17
Spark-ignition automobile engines diesel engines and the conventional gas turbines are devices which operate on______. They are also internal combustion engines.
a. steam cycles
b. gas cycles
c. heat cycles
d. none of these
b. gas cycles
18
Another assumption which is often utilized to simplify the analysis of air standard assumptions is that air has ______whose values are determined at room temperature (25C)
a. variable specific heat
b. all of these
c. thermal specific heat
d. constant specific heat
d. constant specific heat
19
A cycle for which the air-standard assumptions are applicable is frequently referred as
a. gas standard cycle
b. adiabatic cycle
c. reversible cycle
d. air standard cycle
d. air standard cycle
20
_________ basically a piston-cylinder device.
a. centrifugal engine
b. steam engine
c. moving engine
d. reciprocating engine
d. reciprocating engine
21
_________is the position of the piston when it forms the smallest volume in the cylinder.
a. middle dead center
b. Top dead center
c. bottom dead center
d. approach dead center
b. top dead center
22
_________is the position of the piston when it forms the largest volume in the cylinder.
a. middle dead center
b. Top dead center
c. bottom dead center
d. approach dead center
c. bottom dead center
23
The distance between TDC and BDC in which the piston can travel is the
a. right extreme position
b. displacement stroke
c. stroke of the engine
d. swept stroke
c. stroke of the engine
24
The air or air-fuel mixture is drawn into the cylinder through the
a. intake valve
b. exhaust valve
c. intake pump
d. jet pump
a. intake valve
25
The combustion products are expelled from the cylinder through the
a. intake valve
b. exhaust manifold
c. exhaust valve
d. none of these
c. exhaust valve
26
The minimum volume formed in the cylinder when the piston is at TDC is called the
a. compression
b. expansion valve
c. volume change
d. clearance volume
d. clearance volume
27
The volume displaced by the piston as it moves between TDC and BDC is called
a. free mixture
b. clearance volume
c. piston discharge
d. displacement volume
d. displacement volume
28
The ratio of the maximum volume formed in the cylinder to the minimum volume is called the ______of the engine
a. expansion ratio
b. cut-off ratio
c. intake volume ratio
d. compression ratio
d. compression ratio
29
Compression ratio is a
a. pressure ratio
b. temperature ratio
c. entropy ratio
d. volume ratio
d. volume ratio
30
_______is the fictitious pressure which if it acted on the piston during the entire power stroke, would produce the same amount of net work as that produced during the actual cycle is called
Mean Effective Pressure
31
Reciprocating engines are classified as a
a. spark ignition engines or compression ignition engines
b. spark ignition engines
c. compression ignition engines
d. heat engines
a. spark ignition engines or compression ignition engines
32
in spark ignition engine the combustion of the air-fuel mixture is initiated by a
a. carburator
b. injector
c. feed pump
d. spark plug
d. spark plug
33
In compression-engine the combustion of air-fuel mixture is self-ignited as a result of compressing the mixture above its
a. self developed temperature
b. mixing temperature
c. self feed temperature
d. self ignition temperature
d. self ignition temperature
34
_________ the piston executes four complete strokes (two mechanical cycles) within the cylinder and crankshaft completes 2 revolutions for each thermodynamic cycles
a. one stroke internal combustion engine
b. two stroke internal combustion
c. three stroke internal combustion engine
d. four stroke internal combustion engine
d. four stroke internal combustion engine
35
Shortly before the piston reaches its highest position
the spark plug fires_______of the system
a. decreasing the temperature and density
b. increasing the volume and temperature
c. increasing the pressure and temperature
d. decreasing pressure and entropy
36
In four stroke cycle the useful output is done during the
a. exhaust stroke
b. expansion or compression stroke
c. intake stroke
d. heat stroke
b. expansion or compression stroke
37
The pressure in the cylinder is ______ during the exhaust stroke and slightly below during intake stroke
a. slightly above
b. slightly below
c. is atmospheric
d. approaches infinity
a. slightly above
38
Two stroke engines are generally _____than four-stroke engines because of isentropic expulsion of the exhaust gases and partial expulsion of fresh air-fuel mixture with the exhaust gases
a. less efficient
b. more efficient
c. generally more efficient
d. critically efficient
a. less efficient
39
Two stroke engines has ________ compares to four stroke engine
a. less power
b. more power
c. less efficient
d. more efficient
b. more power
40
The thermal efficiency of an ideal Otto cycle depends_________of the working fluid
a. the pressure ratio of the engine and the specific heat ratio
b. the temperature ratio of the engine and the specific heat ratio
c. the moles ratio of the engine and the the specific heat ratio
d. the compression ratio of the engine and specific ratio
d. the compression ratio of the engine and specific ratio
41
The thermal efficiency of Otto cycle increases as the compression ratio.
a. increases
b. decrease
c. remains constant
d. none of these
a. increases
42
Typical compression ratio of Otto cycle is
a. 6.0
b. 7.0
c. 8.0
d. 9.0
c. 8.0
43
The premature ignition of the fuel is called
a. super ignition
b. autoignition
c. ignition delay
d. pre-ignition
b. autoignition
44
Autoignition in spark-ignition engine can ______to the engine
a. explode
b. cause drastic change
c. cause damage
d. cause separation
c. cause damage
45
_____has been added to gasoline because it is the cheapest method of raising the octane rating.
a. tetraethyl lead
b. unleaded
c. super leaded
d. blaze
a. tetraethyl lead
46
is a measure of the engine knock resistance of fuel
a. Ucrain
b. Anti knock rating
c. octane rating
d. saybolt rating
c. octane rating
47
leaded gasoline engine has
a. best effect
b. produce double effect
c. undesirable side effect
d. none of these
c. undesirable side effect
48
most cars have been designed to use unleaded gasoline and the compression ratio had to be lowered to avoid
a. infinite revolution
b. zagging knocking
c. super knock
d. engine knock
d. engine knock
49
The thermal efficiency of car engines has been decreased somewhat as a result
a. increased compression ratio
b. decreased compression ratio
c. dead weight ratio
d. zero clearance
b. decreased compression ratio
50
The second parameter affecting the thermal efficiency of an ideal Otto cycle is the
a. density
b. air condition
c. specific heat ratio
d. compression ratio
c. specific heat ratio
51
Using monatic gas the thermal efficiency of Otto cycle
a. increases
b. decreases
c. remains constant
d. none of these
a. increases
52
The thermal efficiency of actual spark-ignition engines range feom about
a. 25 to 30%
b. 30 to 35%
c. 35% to 40%
d. 40 to 50%
a. 25 to 30%
53
The diesel engine is the ideal for CI(compression ignition) is
a. reciprocating engine
b. combustion engine
c. external engine
d. two way engine
a. reciprocating engine
54
Invented diesel engine is ________in the 1890
a. Rudolph Hitler
b. Ronnie Diesel
c. Rodel Diesel
d. Rudolph Diesel
d. Rudolph Diesel
55
If the density of air increases its ______ will increase
a. temperature
b. specific volume
c. entropy
d. pressure
d. pressure
56
The difference between enthalpy and work flow is
a. internal work
b. internal energy
c. specific heat
d. kinetic energy
b. internal energy
57
At critical point of TS diagram in Rankine cycle
what is the relation of saturated enthalpy of liquid and vapor?
a. hf=hg
b. hf>hg
c. hg>hf
d. hg is slightly greater than hf
58
The fuel used in diesel is ___than in the fuel used in gasoline engine
a. less expensive
b. more expensive
c. P10 more
d. none of these
a. less expensive
59
The fuel injection process in diesel engines starts when the piston_____ and continuous during the first part of power stroke
a. and of BDC
b. becore TDC
c. approaches BDC
d. approaches TDC
d. approaches TDC
60
In diesel engine
combustion process during combustion occurs during
a. isothermal process
b. constant pressure process
c. isentropic process
d. adiabatic
61
The Otto and Diesel cycle differs during
a. expansion process
b. intake process
c. exhaust process
d. combustion process
d. combustion process
62
A measure of performance for any power cycle is its
a. back work ratio
b. thermal efficiency
c. autoignition efficiency
d. none of these
b. thermal efficiency
63
Is the ratio of cylinder volumes after and before the combustion process
a. expansion ratio
b. back work ratio
c. cut-off ratio
d. compression ratio
c. cut-off ratio
64
The thermal efficiency of Otto cycle is always ______ the thermal efficiency of Diesel cycle when both operates in the same compression ratio
a. greater than
b. less than
c. equal
d. none of these
a. greater than
65
If the cutoff ratio decreases
the efficiency of diesel cycle
a. increases
b. decreases
c. remains constant
d. none of these
66
If the cutoff ratio is unity
the diesel and Otto cycle are
a. performs different field
b. separately exited
c. fixed
d. identical
67
The diesel engines also burn the fuel more completely since they usually operate ____than spark ignition engines
a. higher revolutions per minute
b. medium speed
c. lower revolutions per minute
d. none of these
c. lower revolutions per minute
68
Thermal efficiencies of diesel engines range from about
a. 30 to 45%
b. 65 to 89%
c. 50 to 55%
d. 35 to 40%
d. 35 to 40
69
The______of diesel engines make them the clear choice in applications requiring relatively large amounts of power
such as locomotive engines
70
A diesel engine can be built as much as __________at 122 rpm
a. 20
500 hp
b. 27
71
A better approach would be to model the combustion process in both gasoline and diesel engines as a combination of two heat transfer process. This process is known as
a. gas cycle
b. Otto cycle
c. Diesel cycle
d. Dual cycle
d. Dual cycle
72
In dual cycle
the heat is added during constant volume and ______process.
a. constant temperature
b. constant pressure
c. constant volume
d. constant pressure and temperature
73
Is the process during which heat is transferred to a thermal energy storage device
a. adiabatic
b. regeneration
c. recuperation
d. isentropication
b. regeneration
74
The regenerator is a device that borrows ____ from the working fluid during one part of the cycle and pays it back during another part of the cycle
a. heat
b. energy
c. work
d. none of these
b. energy
75
In stirling cycle
regeneration process works during _______ process.
a. constant volume
b. constant pressure
c. constant heat addition
d. none of these
76
In Ericsson cycle
the regeneration process occur during _____process
a. constant volume
b. constant temperature
c. constant pressure
d. none of these
77
Invented Stirling engine is _____. It is very heavy and complicated
a. Robert Deniro
b. Robert Boyle
c. Robert Sreri
d. Robert Sterling
d. Robert Sterling
78
Both the Stirling and Ericsaon cycles are totally reversible as is the
a. Carnot cycle
b. Otto cycle
c. Diesel cycle
d. Gas turbine cycle
a. Carnot cycle
79
_________have the same efficiency when operating the same temperature limits.
a. Stirling and gas turbines
b. Carnot and Otto cycles
c. Stirling
Ericsson and Carnot cycles
d. none of these
80
Both the Stirling and Ericsson cycles are
a. internal combustion engines
b. external combustion engines
c. Otto engine
d. Stirling engine
b. external combustion engines
81
Are two gases commonly employed in Stirling and Ericsson cycles
a. Hydrogen and Helium
b. Water and Brine
c. Salt and water
d. Oxygen and Nitrogen
a. Hydrogen and Helium
82
Advantage of Stirling and Ericsson cycle
a. can use variety of fuels as a source of energy
b. There is more time for combustion
c. They operate on closed cycles
d. all of these
d. all of these
83
In Stirling cycle
Regeneration can
a. decrease efficiency
b. increase efficiency
c. limit efficiency
d. control efficiency
84
Brayton cycle is invented by
a. George Bragat
b. George Smith
c. George turbine
d. George brayton
d. George Brayton
85
Gas turbines usually operates on an
a. closed cycle
b. open cycle
c. controllable cycle
d. none of these
b. open cycle
86
in gas turbine the gas is expanded to the
a. vacuum pressure
b. negative pressure
c. gage pressure
d. atmospheric pressure
d. atmospheric pressure
87
Brayton cycle is made up of ________internally reversible process
a. one
b. two
c. three
d. four
d. four
88
In brayton cycle
the ________during constant pressure process.
a. work is added
b. heat is transferred
c. pressure is rejected
d. energy is added
89
The thermal efficiency on an ideal Brayton cycle depends on
a. pressure ratio of the gas turbine and specific volume ratio
b. temperature ratio of the gas turbine and specific heat ratio
c. pressure ratio of the gas turbine and isentropic process
d. pressure ratio of the gas turbine and specific heat ratio
d. pressure ratio of the gas turbine and specific heat ratio
90
The highest temperature of Gas turbine cycle occurs at the end of
a. expansion process
b. compression process
c. combustion process
d. extraction process
c. combustion process
91
For a fixed turbine inlet temperature
the net work output per cycle increases with the pressure ratio
92
In most common design of Gas turbine
the pressure ratio ranges from
a. 10 to 12
b. 11 to 16
c. 13 to 18
d. 12 to 20
93
In gas turbines
an air fuel mass ratio of ____is not common
a. 10 or above
b. 20 or above
c. 30 or above
d. 50 or above
Study all 93 cards for free