Reciprocating Engine Theory 2 Flashcards
The recommended maximum number of hours that an engine can run between overhauls.
Time between overhauls.
TBO
The ratio of the weight of an aircraft engine to the brake horsepower it develops.
Specific weight.
NASA
National Aeronautics and space administration.
NACA
National advisory committee for aeronautics.
This assures a good flow of cooling air over the engine cylinders and produces a forward aerodynamic force.
NACA cowling
T/F
NACA cowlings actually produce a forward aerodynamic force.
True
The ability of an engine to perform as the manufacturer has promised is known as the _______ of an engine.
Reliability.
The durability of an aircraft engine may be indicated by the manufacturer’s recommended _______.
TBO
A reciprocating engine with all the cylinders arranged in a straight line.
In-line engine.
A form of reciprocating engine in which the cylinders are arranged in two banks which are separated by an angle between 45 and 90 degrees.
V-engine
An in-line or v-engine in which the cylinders are mounted below the crankshaft.
Inverted engine.
A radial engine in which the propeller, crankcase and cylinders revolve as a unit.
Rotary radial engine.
The end of a reciprocating engine on which many of the accessories are mounted.
Accessory end.
The end of a reciprocating engine to which the propeller mounts.
Propeller end.
The end of a reciprocating engine that does not attach to the propeller.
Antipropeller end.
T/F
All radial engines number the cylinders with the bottom cylinder as 1.
False.
Top cylinder is 1
T/F
Radial engine cylinder numbering progresses consecutively around the engine in a counterclockwise direction.
False.
Direction of the crankshaft
A reciprocating engine in which the cylinders are arranged like the spokes of a wheel radiating out from a small central crankcase
Radial engine.
The firing order of a nine-cylinder radial engine is _______.
1-3-5-7-9-2-4-6-8
The smoothness with which a reciprocating engine runs is determined by the ______.
Spacing and timing of the firing impulses.
T/F
All cylinders fire in two revolutions of crankshaft rotation.
True.
The reservoir on an aircraft engine that holds the lubrication oil.
Sump.
Two basic types of lubrication systems used on aircraft reciprocating engines.
Wet sump.
Dry sump.
________ lubrication systems are normally used by radial engines and inverted in-line and V-engines.
Dry-sump
_______ engines carry all the lubricating oil in an integral sump that is part of the crankcase.
Wet-sump
R =
Radial
O =
Opposed
A=
Aerobatic
G=
Geared nose section
H=
Horizontal, for helicopter
I=
Fuel injected
L (At beginning of sequence) =
Left hand engine rotation
L (At end of sequence)
Liquid cooled
S=
Supercharged
T or TS =
Turbocharged
V=
Vertical for helicopter