Systemmmmssss exam Flashcards
A piston engine has _____ parts. _______ internal combustion and converts _____ energy to ______ energy.
Reciprocating, intermittent, heat, mechanical
A Jet engine has _____ parts. _______ internal combustion and uses _______ to provide _____.
Rotating, continuous, action/reaction, thrust.
A cycle is:
A series of events which are repeated in a regular sequence and constitute the principle of operation (Otto cycle)
A stroke is:
The distance which a piston travels up or down in a cylinder
TDC is the position ____ to the crankshaft.
Furthest
BDC is the position ____ to the crankshaft.
Closest
Swept volume is:
The volume in the cylinder that is swept by the piston between TDC and BDC
Clearance volume is:
The volume in the cylinder above the piston at TDC
Compression ratio formula
swept + clearance / clearance
The bore is:
Internal diameter of the cylinder
Firing interval is:
The interval measured in crank shaft rotation between and two cylinders in the ignition sequence. eg. Four stroke takes two revs of CS, (720/4), firing interval of 180 degrees.
Firing order
Numerical order in which the cylinders fire eg. 1,3,2,4
Manifold is:
Pipes/ducts that lead the charge from carb to cylinders and cylinders to main outlet
Manifold pressure is:
The pressure of charge existing at any one time in the induction manifold
Crank angle is:
Same as the crank rotation from a datum
Ideal gas law
pV = nRT
Boyles law
pV = C
for a given mass, at a constant temp, the pressure x volume = constant
Charles law
V = CT
for a given mass, at a constant pressure, the volume is directly proportional to the temperature
1-2 Otto cycle
Induction
Piston starts at TDC, moves to BDC, total mass of charge inside the cylinder increases throughout the stoke, pressure is constant
2-3 Otto cycle
Compression
Piston moves from BDC to TDC, compressing the constant mass of gas isentropically. At the top of this stroke, combustion takes place.
3-4 Otto cycle
Combustion
Combustion takes place rapidly before the piston has moved any notable distance, hence we take it as a process of constant volume. Since energy is released, temperature increases significantly. Because V is constant, pressure increases (pV = nRT)
4-5-6 Otto cycle
Power
The high pressure exerted on the face of the piston during combustion generates a strong force which drives the piston downwards. The gas expands isentropically to a lower pressure. At the bottom of this stroke, the exhaust valve opens. The pressure inside the cylinder adjusts to the exhaust manifold pressure.
5-6 Otto cycle
Exhaust
Piston pushes the burnt gases out of the cylinder to return to the conditions at p1.
The inlet valve _____ by _____ degrees.
Lags, 60
The exhaust valve ____ by _____ degrees.
Leads, 55
Advantages of valve overlap
Cooling of upper cylinder
Better waste scavenging
Increased charged induced
Why does the valve lag?
Charge has mass and therefore inertia, change in velocity takes take. Restricted by inlet valve and friction from walls of inlet pipe.
Why does the valve lead?
Improves expulsion burnt gases.
The piston travels faster in the ____ 90 degrees than it does in the ____.
First, second
Piston travels a ____ distance for a given crank rotation at the _____ of the stroke
greater, middle
Con rod thrust will be most effective when the angle between the ______ and the _____ is at ___ degrees
Con rod, crank web, 90
Usually the crank angle for max con rod thrust is:
67 degrees
How many seconds does the combustion process take?
0.003 - 0.004
At 2000 rpm the crank turns ____ degrees every ____ seconds.
15, 0.001
Factors affecting combustion time
Fuel/air ratio
Temperature of charge/cylinder
Grade of fuel
CR and manifold pressure
No of ignition points
Gas turbulence (swirl)
In order for peak pressure to develop before 90 the ignition must be ______ between _______ degrees _____ TDC.
Advanced ,15-40, before
Most engines spark advance is ______ degrees
25
Diesel engines are ______ ignited
Compression
CCM
1:15 complete combustion of fuel/air
Rich
more fuel that ccm eg 1:10
Lean
less fuel than ccm eg 1:18
Workable ignition limits for fuel/air ratio
1:9 - 1:18
Max power
1:12