AT 103 First Exam Flashcards
Failure of early aircraft was primarily due to a:
lack of power source that could sustain flight
Failed engines had these characteristics:
poor efficiency, lack of dependability, high cost, excessive weight, low power produced
Challenges to aviation include wanting engines with:
high power-to-weight ratios, efficiency, reliability, and environmentally friendly aspects
Who built the first flight simulator
Edwin Link
In 1860 the first practical gas engine was built by _____ and these 400 engines powered _______
Jean Lenoir (France), lathes and printing presses
!! First four stroke engine was built in 1876 by ___ !!
August Otto and Eugen Langen
First gasoline engine was built in 1885 by ____ and operated on the four stroke principle
Gottlieb Daimler (similar one by Karl Benz)
First successful aircraft engine was built in 1903 by _____ and was ____ cooled with ____ cylinders
Charles Taylor, water (cooled), four (cylinders)
First flight of jet engine power on an aircraft was in _____ and an example is ______
1939, Heinkel HeS 3B or Heinkel He 178
First turbojet was built by _____ and was manufactured by _____
Sir Frank Whittle (W1 Engine), General Electric Company
Some challenges of gas-turbine engines include:
performance, sound levels, fuel efficiency, maintenance ease, dependability, and reliability
What engine is this: crankshaft is held stationary while cylinders rotate around with the prop
rotary type radial
Disadvantages of the rotary type radial include
torque and gyro effect making the aircraft difficult to control and the usage of castor oil
What engine is this: cylinders are arranged in a row parallel to crankshaft. Cylinders are above or below the crankshaft.
In-line engine
Characteristics of in-line engines include:
usage in low and medium horsepower applications, small frontal area for low drag and streamlining, harder to cool the bigger they get
What engine is this: cylinders are in two rows forming the letter V
V-type
Pros of radial engines
lowest weight to horsepower ratio of all reciprocating engines
Cons of radial engines
large frontal area, cooling problems, hard to see over
Multiple-Row Radial Engine facts:
largest and most powerful reciprocating engine, can produce 3,500 hp or 4,300 hp with two turbo and one super charger
what was the multiple row radial engine replaced by and why
gas-turbine engines, more lightweight and powerful, fewer moving parts, and TBO increased
Opposed and flat type engine characteristics:
100-400hp, cylinders and crankshaft horizontal, low weight to hp ratio, streamlined flat shape, reasonably free from vibration
Engine designation: L
left hand rotation
Engine designation: T
turbocharged
Engine designation: i
fuel injected (remember lack of I normally means carborated)
Engine designation: G
geared
Engine designation: S
supercharged
Engine designation: O
opposed cylinders
Engine designation: R
radial engine
Engine designation: ###s
volume displaced to nearest 5 in^3
Why is excessive heat bad for reciprocating engines
adversely affects behavior of combustion of air fuel charge, weakens/shortens life of engine parts, impairs lubrication
Air cooling advantages
weighs less (no radiator, no connecting hoses/lines, no coolant liquid), less affected by cold weather, less vulnerable to gunfire
air cooling disadvantages
requires forward movement for ram air to sufficiently cool engine
How does liquid cooling work?
coolant circulates through engine areas requiring heat removal and transfers heat to liquid
liquid goes to radiator and cools
coolant circulates back through engine
relief valve prevents excessive pressure
What is the common liquid for coolant
ethylene glycol mixed with water
crankcase characteristics
foundation of engine
must support self
enclosure for lubricating oil
mounting to aircraft and mounting to cylinders
needs strength and rigidity
What type of crankcase? Two matching, reinforced aluminum-alloy castings divided vertically at centerline and fastened with studs and nuts
opposed-engine
What type of crankcase? Multiple sections (3-7): front, main power, fuel induction and distribution, accessory
radial engine
What type of crankcase? Four main sections: front, power, fuel induction and distribution, accessory. Sections may be cast together
In-Line and V Type Engines
Purpose of aircraft bearings
produces minimum friction, max wear resistance
Good bearing characteristics:
material strong enough to withstand pressure, permit movement with minimum wear and friction, be held with very tight tolerances, quiet and efficient operation while not sacrificing freedom of motion
Name the bearing: low power engines, radial loads, can be used for thrust when flanges added
Used for: connecting rods, crankshaft, camshaft
Made of: silver, lead, bronze
Plain bearing
Name the bearing: high power application, tapered rollers can withstand radial and thrust loads
roller bearing
What does the crankshaft do?
transforms reciprocating motion of piston to rotary motion and turns propellor
What does the main journal do?
serves to keep crankshaft alignment
what does the crankpin do
when forced applied to pin other than direction parallel to crankshaft, it will rotate the crankshaft
why are crankpins usually hollow?
reduces weight
passage for oil
collects carbon deposits, sludge, other stuff
Crank Cheek / Arm characteristics
oil passages drilled through
connects crank pin to main journal
has counterweights for static balance
What do dynamic dampers do
relieve whip and vibration
overcome forces generated by power impulses causing deflection of crankshaft
Name the shaft: end has milled slot for key
treaded forward end of shaft receices propeller retaining nut
caused propellors to spin off
used on small motors now
tapered shaft
Name the shaft: high power uses
rectangular groves on shaft and in engine
one grove blocked by screw to ensure position
spline
Name the shaft: bolts need to be tightened in sequence
has short stub forward of it that secures prop
much flatter than other types
what the pipers have
flange
connecting rod characteristics
steel alloy or aluminum for low power
H or I cross sectional
end of connecting rod connecting to crankshaft:
large end (crankpin end)
end of connecting rod connecting to piston pin
small end (piston-pin end)
At each stroke connecting rods will:
stop, change direction, start
Name the connecting rod:
common in lin line and opposed engines
small end is bronze serving as bearing
large end has cap with two piece bearing
plain rod
name the connecting rod: used for V type
split on large end
other rod fits between split on large end
fork and blade rod
name the rod: used in radial engines
subject to a lot of stresses
design to highest quality
alloy-steel forging and heat treated
master and articulated rod
what does the master rod do
provides attachment points for articulated rods on large end
Articulated rods:
attached to paster by steel knuckle pins
lock plate on each side to prevent lateral movement
!! What does the connecting rod do? !!
Connects piston to crank shaft
How does the master and articulated rod work?
piston to articulated rod, articulated rod to master rod, master rod to crankshaft