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PWR
Pressurized Water Reactor
Nuclear Propulsion
U.S. Submarines, Aircraft Carriers
Russian Submarines, Aircraft Carriers, Icebreakers, few commercial
Nuclear Pros
High energy density
“clean” — no exhaust
No refueling on regular basis
No air required to produce power
Less Space when considering fuel tanks
Nuclear Cons
High Cost in building and more in safety training
Radiation
Disposal of Spent Fuel
Not Welcome in Ports
Pressurized Water Reactor Components
Primary and Secondary Coolant Loops
Primary Coolant Loop
Water is used to cool the reactor, it goes through pressurizer and then to steam generator where it heats the secondary coolant in steam generator. Water remains liquid in primary loop because of the high pressure
Temp and Pressure of Primary Coolant
1800-2000 psi, 550F
Secondary Coolant Loop
Essentially steam plant that uses boiler without a superheater.
Nuclear Fuel
Uranium 235 enriched to about 20%, normally found at 0.7%; Uranium Dioxide Pellet; melts at 4500F
Nuclear Reaction
Low Speed Neutron (Thermal) →U235 splits (E=mc²; mass to energy as heat)→ releases fast (prompt) neutrons→ slow fast ones with moderator (water) == Self Sustaining Reaction
Water in PWR
Both coolant and moderator; when reactor gets too hot, water becomes steam and then there is less moderating so reaction fizzles out; has negative temperature coefficient
Reactor Control Mechanism
At steady State Heat Release
Steam Demand in Secondary Loop Drops
Primary Coolant Temp Rises
Density Drops
Reduces Moderating Effect
Reaction Slows Down
Remain in Equilibrium
Fuel Tubes
Zircaloy Tube → Zirconium; melting temp is 800F; permeable to radiation; maximum temp inside tubes is 600F to prevent melting
Control Rods
Raised and Lowered into grid of fuel rods, made of boron which absorbs neutrons, used to slow or stop reaction; scram
Reactor Vessel
Outside Lead shielding; housed in containment building to prevent explosion
Input and Outlet Nozzles
Spread around circumference of reactor vessel, 2 outlet. 4 inlet
Steam Generator
Generates Saturated Steam from the secondary coolant using the heat from the primary coolant, primary coolant enters at 550F and leaves at 500F. Different coolants do not interface
Tube Bundle
Group of U shaped tubes in steam generator that heat the secondary coolant. Maintain high pressure
Pressurizer
Maintains primary coolant pressure, T’ed into high pressure line. Changes the pressure of steam in the top in order change water pressure. Has pressure relief valve
Spray Line Nozzle
Sprays cold water into pressurizer to condense vapor and lower pressure in system
Heater Bundles
Raises Temperature in pressurizer which raises the pressure of the system
Future of Nuclear
Generation 4, SMR
SMR
Small Modular Reactors, factory build, tested to standard approved design =, whipped to site and assembles (50-100 MW)
MSR
Molten Salt Reactor, type of SMR with fluidized bed of molten salt and uranium fuel, mix of moderator and fuel. At atmospheric pressure. If accident fluid drains out of reactor and solidifies to prevent thermal runaway.
MSR vs PWR
MSR runs at higher temp —880C = 1600F which allows for superheating so its more efficient
NS Savannah
Nuclear ship owed by MARAD, ½ Cargo, ½ Passenger
Power Turbine
LP Turbine which provides output, only on ships, also called load turbine
How are GT Maintained
Taken out of ship through intake duct and maintenance done onshore, there are tracks in the exhaust duct to aid with removal
Soft Patch
Covering on intake duct after filters that can be removed when GT is being taken out and installed
Regenerator
Heats compressed air which lowers the fuel needed for a given load in a GT
Intercooler
Lowers temperature of outlet air from HPC, which allows for more heat to ab absorbed in regenerator and increases efficiency
Simple Cycle GT
Normal GT cycle without any increased efficiency
Regenerative-Cycle GT
GT with Regenerator to increase efficiency
Intercooled, Regenerative-Cycle GT
GT with intercooler and regenerator
Combined Gas and Steam Turbine
Simple GT Cycle which uses the exhaust gas to heat a boiler. Dual systems, more efficient
COGSAT Pros
Very efficient = 50% which is better than LSDE
COGAST Cons
Expensive, Heavy, Hard to maintain
Triple Shaft Turbine
2 concentric shafts for different speed compressors along with shaft for power turbine
Enclosure
Sound proof and insulated for safety. Prevents tampering
Debris Testing
Throw different size dead chickens into GT to see what size bird breaks the system.
Starter Motor
Runs up to 40% of full RMP, Hydraulic
Gear Box
Increases the speed on the starter motor and creates hydraulic pressure for auxiliaries during engine operation
Exhaust Gas Temp
1100 F
Heavy Duty Gas Turbines
Can use lower quality fuel, run only at constant speed, Not used in marine applications
Aero Derivative Gas Turbines
Light weight, high power, variable speed, little maintenance on ship, unit taken replaced and overhauled on shore
ADGT Pros
High Power Density, low Specific Weight
Rapid Start & Assumption of Load
Low Emissions
High Quality Exhaust Gas
ADGT Cons
Sensitive to fuel quality
high fuel consumption
High air and exhaust flows
reduced Performance at high
temps
High Maintenance Cost
High Thermal Profile
Pressure Ratio
Change in pressure from intake to compressor discharge
Turbine Temps and Pressures
260psi =18 atm,1250C in combustion section; 90psi= 6atm, 850C after HP turbine (compressor); 1atm, 550C=1100F after LP turbine
Gas Generator
Compressor + High Pressure (compressor) turbine
Turbine Cooling
Air Cooled
COGAG
Combined Gas Turbine and Gas Turbine, identical set of GT used for high speed
COGOG
Combined Gas Turbine or Gas Turbine, low power GT for cruising and high power GT for high speed
CODOG
Combined Diesel and Gas Turbine, diesel for cruising, GT for high speed
Prop for GT
Controllable Pitch Propeller
Flux
Number of Neutrons in Circulation
Channels
Spaces between Fuel Rods