AT 103 First Exam Flashcards
(155 cards)
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)