AT103 Review Through Exam 1 Flashcards
Failed Engine Characteristics
Poor Efficiency
Lack of Dependability
High Cost
Excessive Weight
Low Power Produced
Successful Engine Characteristics
High power-to-weight ratio
Efficient
Reliable
Environmentally friendly
Who created the first practical gas engine in 1860?
Jean Joseph Etienne Lenoir of France
The first four-stroke engine was built in 1876 by ___ and ___.
August Otto and Eugen Langen of Germany
First truly successful gasoline engine was built in 1885 by ____.
Gottlieb Daimler
Wright Brothers and Charles Taylor Engine Characteristics
Water Cooled
Four Cylinders
12 Horsepower
180 Pounds
Engines developed during WWI
Radial Engines
In-Line Engines
V-Type Engines
Engines developed post WWI
Multiple Row Radial Engine
Opposed Engine
Flat Engine
Fan, H, W, and X Type Engine
First flight of a jet engine power aircraft was on ____ in _______.
1939, Germany
Gas-Turbine Engine Types
Turbojet Engine
Turbofan Engine
Turboprop Engine
Turboshaft Engine
Gas-Turbine Engine Challenges
Performance
Sound Levels
Fuel Efficiency
Ease of Maintenance
Dependability
Reliability
Types of Reciprocating Engines
Rotary-Type Radial Engines
In-Line Engines
V-Type Engines
Radial Engines
Multiple-Row Radial Engines
Opposed and Flat Type Engines
Rotary Types Radial Engines
Crankshaft is held stationary to the engine mount
Cylinders rotate about the crankshaft
Propeller is attached to the engine case
Examples of Rotary Type Radial Engines
LeRhone
Gnome
Bentley
Rotary Type Radial Engines Disadvantages
Torque and gyro effect of the engine’s large rotating mass made aircraft difficult to control
Castor oil was used as the engine lubricant. The castor oil fumes from the engine’s exhaust was often nauseating to pilots
In-Line Engines
Cylinders of an in-line engine are arranged in a row parallel to the crankshaft
Cylinders can be above or below (inverted) the crankshaft
V-Type Engines
Cylinders are arranged in two rows, formed the letter V
Angles between the rows are usually 90, 60, or 45°
There are always an even number of cylinders per row
Upright V-Type Engines
When the cylinders are above the crankshaft
Inverted V-Type Engines
When the cylinders are below the crankshaft
Single-Row Radial Engine
Odd number of cylinders extending radially from the centerline of the crankshaft
Cylinders range from 5-9
All pistons are connected to a single-throw 360° crankshaft
Double-Row Radial Engine
Resembles two single-row radial engines on a single crankshaft
Cylinders range from 14-18
A two-throw 180° crankshaft is used to allow stagger between each row of cylinders
Radial Engine Disadvantages
Large frontal area creates a lot of drag
Cooling problems
Multiple-Row Radial Engines
The largest and most powerful reciprocating engine
Examples of Multiple-Row Radial Engines
Pratt & Whitney R-4360
3,500 hp
4,300 hp using two turbochargers and one supercharger
What were Multiple-Row Radial Engines replaced by?
gas-turbine engines
Opposed and Flat Engine Type
Most popular for light conventional aircraft and helicopters
Engine Classification (In-line)
Upright, inverted
Engine Classification (V-Type)
Upright, inverted, Double V, X
Engine Classification (Opposed and Flat)
Opposed, flat
Engine Classification (Radial)
Single row, double row, multiple row
Difference between letters and numbers to determine engine designation
Letters are employed to indicate characteristics
Numerical are employed to indicate displacement
L
Left-Hand Rotation
T
Turbocharged
I
Fuel Injected
G
Geared
S
Supercharged
O
Opposed Cylinders
R
Radial Engine
#
Displacement to the nearest 5 in^3
How is excessive heat is undesirable for reciprocating engines?
Adversely affects behavior of the combustion of the air fuel charge
Weakens and shortens the life of engine parts
Impairs Lubrication
Excessive heat generated by the engine is removed from the engine by the
Convection process
Projects from the engine cylinders
Cooling fins
Used around the cylinders to direct the air flow and obtain maximum cooling
Baffles
Advantages of Air Cooling
Weight of an air cooled engine is usually less than a liquid cooled engine
Less affected by cold weather operations
Less vulnerable to gunfire (Military)
Disadvantages of Air Cooling
Requires forward movement for ram air to sufficiently cool the engine
Liquid cooling systems consists of
Liquid passage around the cylinders and specific hot spots in the engine
Radiator to cool the liquid
Thermostatic element to decide amount of cooling to the liquid
Connecting pipes and hoses
Relief valve to prevent excessive pressure
How does liquid cooling work?
Cooling liquid is circulated through the engine areas that require heat removal
Heat is transferred to the liquid
Heated liquid then passes through a heat exchanger (radiator) and cools down
The cooled liquid is then cycled back into the engine to repeat the cooling process
The Crankcase
The foundation of the engine
Must support itself
What does the crankcase provide?
Mounting to the aircraft and cylinders
Three groups of the Crankcase
Opposed-Engine Crankcases
Radial-Engine Crankcases
In-Line and V-Type Crankcases
Opposed-Engine Crankcases
Consists of two matching, reinforced aluminum-alloy castings
Castings are divided vertically at the centerline
Fastened together with studs and nuts
Lubricating system are contained in the crankcase
Oil passages are drilled in sections of the case to supply lubrication to
Crankshaft Bearings
Camshaft Bearings
Radial-Engine Crankcase
Consists of multiple sections (3-7)
The Front Section (Nose)
Main Power Section
Fuel Induction and Distribution Section (Blower or Supercharger)
Accessory Section
What is in the Accessory Section of the Radial-Engine Crankcase
Provides mounting pads for accessory units
Fuel Pump
Vacuum Pump
Lubrication Oil Pump
Starters
Magnetos
In-Line and V-Type Engine Crankcases Sections
Front Section
Power Section
Fuel Induction and Distribution Section
Accessory Section
In-Line and V-Type Engine Crankcases Front Section
May be cast as part of the power section or be a separate part
Houses the propeller shaft, propeller thrust bearing… etc.
In-Line and V-Type Engine Crankcases Power Section
May be one part or two part
Supports crankshaft bearings
Cylinders are mounted onto this section
Provides attachment points to the engine mount
In-Line and V-Type Engine Crankcases Fuel Induction and Distribution Section
Houses the diffuser vanes
Supports the internal blower impeller
In-Line and V-Type Engine Crankcases Accessory Section
Can be a separate unit mounted onto the Fuel Induction and Distribution Section or form a part of the section
Houses the accessory drives
What is in the Accessory Section of the In-Line and V-Type Engine Crankcases
Mounting pads for:
Fuel Pump
Coolant Pump
Vacuum Pump
Magnetos
Other devices operated by engine power
Bearings
A part in which devices turns or revolves on:
Journal
Pivot
Pin
Shaft
etc.
Aircraft bearings
Produces minimum friction
Maximum wear resistance
Characteristics of a good bearing
Made of material strong enough to withstand the pressure imposed on it
Permit the other surface to move with minimum wear and friction
Be held in position with very tight tolerances
Provide quiet and efficient operation while not sacrificing freedom of motion
Bearings are called Thrust Bearings when in addition to reducing friction of moving parts they also take:
Thrust Loads
Radial Loads
Combination of Thrust and Radial Loads