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place where air is expanded and accelerated rearward by the turbine, creating energy needed for reaction of the aircraft
Combustion section
an illustration or piece of equipment showing parts normally not visible when the covering sections are removed
Cutaway
the place where air is compressed as it passes along the axis of the engine rotating assembly
axial flow compressor
the air surrounding all sides of an engine
ambient air
place where fuel and air are mixed and then burned
Combustion chamber
a passage which becomes continuously smaller in the direction of flow
convergent duct
the part of the engine where air enters
air inlet section
the place where air enters and is compressed and accelerated in a perpendicular direction to the axis of the engine
Centrifugal flow compressor
a part of the engine that takes in a large mass of air, compresses it, and delivers it to the combustion section
compressor section
a jet engine having in its forward end a continuous inlet of air that depends on the speed of flight for the compressing effect produced on the air rather than by the use of a compressor
ramjet engine
the points of reference used to determine location, position, or movement of parts of an engine
directional references
a duct of varying cross-section used in discharging liquids or gases in which the velocity of the fluid is increased
nozzle
the action of driving forwardmatter the material a thing is made of
propulsion
a passage which becomes continuously larger in the direction of flow
Divergent duct
a part of the engine that collects and straightens the gas flow as it leaves the turbines, then accelerates the gases before they are discharged from the exhaust nozzle
exhaust section
a passage where the size of the duct remains the same
straight duct
a set of theoretical atmospheric conditions used as a reference in making technical order charts which are used for making engine adjustments and computing thrust
standard day
a propulsion system having a fan that is directly connected to and driven by a turbine and is used to supply air for cooling, ventilation, or combustion
turbofan engine
the forward force produced in reaction to escaping gases in jet propulsion
thrust
a propulsion system having a turbine-driven propeller designed to produce thrust principally by means of that propeller
turboprop engine
a propulsion system in which the power developed by a turbine is used to drive a compressor that supplies air to a burner and hot gases from the burner pass through the turbine and then to a rearward-directed thrust-producing exhaust nozzle
turbojet engine
the part of the engine that converts a portion of the heat energy of the exhaust gases into mechanical energy to drive the compressors and accessories
turbine section
changing to the position that streamlines the blades to the wind in case an engine must be shut off in flight
Feathering
a structure, piece, or body, shaped like a leaf in being wide and thin, designed to obtain a useful reaction upon itself in its motion through the air
airfoil
a device that converts fluid power into mechanical force or motion
actuator
a device used to ignite the pilot flame
flameholder
the component of a turbojet engine which transmits the power produced by the turbine wheels to the extension shaft assembly
Power section
a component that connects the power source to the reduction gear assembly
Extension shaft
to pull in
draw
the part of an engine that provides a means of attaching the propeller assembly to the propeller shaft while transmitting torque to the propeller blades
Barrel assembly
the part of an engine that provides additional thrust for short periods of time during takeoff and interception missions
Afterburner section
the first row of stationary blades in the axial flow compressor
Inlet guide vanes
a compressor with two spools
dual-spool
a part of a machine, shaped like a quarter of a circle
quadrant
the blades that are attached to the outer case of an axial flow compressor
Stator blades
an exhaust duct
tailpipe
a force that will produce rotation
torque
a drum
spool
the blades that are attached to the spool part of the compressor and increase the compression of the air at each stage and accelerate it rearward through several stages
Rotor blades
to the rear
rearward
the additional thrust provided by the afterburner section for short periods of time during takeoff and interception missions
Thrust augmentation
a compressor with one spool
single-spool
the component that allows the propeller shaft to be turned at a desirable speed and acts as an accessory mount
Reduction gear assembly
the thin, flat , or curved objects generally used for stationary airfoils within the engine
Vanes
to unite pieces of metal by heating until molten and fused until soft enough to hammer or press together
weld
a process by which air is removed from the system
bleed
a finned or vaned device for controlling the flow of air
louver
a chamber which consists of a housing and a liner; the liner consists of an undivided circular shroud extending all the way around the outside of the turbine shaft housing
Annular combustion chamber
a rotor; picks up and accelerates the air outwardly to the diffuser
impeller
branching outward in all directions from a common center
radial
a central line around which the parts of a thing, system, etc. are evenly spaced
axis
a stator; an annular chamber provided with a number of vanes forming a series of divergent passages into the manifold
diffuser
a chamber which consists of an outer case or housing, within which there is a perforated stainless steel combustion chamber liner or inner liner
Can combustion chamber
a small opening for the passage of fluid
port
a chamber which is a combination of the annular and can-type combustion chambers
can-annular combustion chamber
something that covers, screens, or guards
shroud
the technical name of an item
nomenclature
a formed edge, leg, lip, or rim; a narrow extension of a part that is formed at an angle to the main body of the part
flange
a detachable unit which consists of a fan inlet case and a low pressure compressor rotor and stator assembly
inlet fan module
accessory drive gear
ADG
compressor inlet variable vanes
CIVVs
a pipe fitting where fuel lines connect
fuel manifold
a divergent duct
diffuser case
a detachable unit which consists of the main gearbox assembly and the main oil pump assembly
gearbox module
a detachable unit with a specific function
module
a detachable unit which consists of a rear turbine case which contains a fan drive turbine rotor and stator assembly, a fan drive turbine shaft and a turbine exhaust case
fan drive turbine module
a cylindrical duct and liner combination extending from the aft end of a rear fan duct to the entrance of the nozzle
augmentor duct
a complete engine that consists of a high pressure compressor, a diffuser case with a combustion area, and a front turbine case with turbines
core engine
digital electronics engine control
DEEC
revolutions per minute
RPM
an element which consists of a shaft and a wheel; receives heated air from the stator element and takes this heat energy and converts it into mechanical energy to turn the high pressure turbine, which will turn the high pressure compressor
Rotor element
rear compressor variable vanes
RCVVs
the abbreviation for low rotor speed
N1
power takeoff
PTO
engine inlet total temperature
Tt2
an element which consists of an inner and outer shroud between which are fixed nozzle vanes; increases the velocity of heated air and directs the air onto the turbine rotors at the best angle
Stator element
the abbreviation for high rotor speed
N2