windows-1256__wet compression.pdf
TRANSCRIPT
Mohsen Assadi
L U N D U N I V E R S I T Y
Inlet Air Cooling & Wet Compression
ETN- Brussels
2006-10-12
Prof. Mohsen Assadi 2
LUN D UN IVER SITY
Inlet Air Cooling - Overview
• Why do we need inlet air cooling?
• Cooling techniques available– A short description of its functionality and
applicability
– Operating experience and analysis (PG & PG I)
• No time left for questions - do not hesitate to stopme and ask your question while still in your head
Prof. Mohsen Assadi 3
LUN D UN IVER SITY
Why Do We Need Inlet Air Cooling?
• The general benefits associated with inlet cooling are:
– Decreases the work of compression
– Increase air density also means that the gas turbinecan operate with higher mass flow
– The compressor discharge temperature is beinglowered giving the possibility to burn more fuel in orderto reach the same TIT, hence increasing power output
Prof. Mohsen Assadi 4
LUN D UN IVER SITY
Potential enhancementInlet cooling techniques
Potential performance enhancement - GT10B
15000
17000
19000
21000
23000
25000
27000
0 10 20 30 40 50 60
Ambient temperature [C]
Pow
ero
utp
ut[
kW]
ISO conditions GT10B
Media based evaporative cooler, RH 60%
Media based evaporative cooler, RH 30%
Fogging, RH 60%
Fogging, RH 30%
Chiller, RH 60%
Chiller, RH 30%
Cooling notapplicable dueto icing risk
ISO
RH 60%
RH 30%
Chillers
Prof. Mohsen Assadi 5
LUN D UN IVER SITY
Cooling Techniques AvailableMedia based evaporative cooler
Wet compressionInlet fogging
Mechanical Chiller
Prof. Mohsen Assadi 6
LUN D UN IVER SITY
Cooling Techniques AvailableMechanical Chiller
• Mechanical chiller– Refrigerant cooling technique– Has cooling coils placed in the airstream– Consists of
• One huge fridge• Inlet coils• Cooling tower
Prof. Mohsen Assadi 7
LUN D UN IVER SITY
Cooling Techniques AvailableMechanical Chiller
Prof. Mohsen Assadi 8
LUN D UN IVER SITY
Cooling Techniques AvailableMechanical Chiller
• Found in study– Performance
• Can cool the inlet air back to 15°C from any ambient condition– Great power output augmentation. 15% at 35°C and 50% RH
• The gas turbine will regain its original efficiency
– Economy• Expensive, High investment, and O&M costs• Construction time is 6-9 months and require a turbine down time
about 7-10 days
– Advantages• Not susceptible to ambient conditions
– Disadvantages• Large footprint, bulky construction, water tower• Require large face area across chilling coil• Added pressure drop in the air intake system
Prof. Mohsen Assadi 9
LUN D UN IVER SITY
Cooling Techniques AvailableMedia Based Evaporative Cooler
• Based on the principle of adiabatic saturation• Media where water and air interacts is
placed in the airstream– Water evaporates from the surface– The air is cooled by the latent heat of
vaporization• Consist of:
– Media based cooler unitDistribution padsMedia
Prof. Mohsen Assadi 10
LUN D UN IVER SITY
Cooling Techniques AvailableMedia Based Evaporative Cooler
• Found in study– Performance
• Usually have an effectiveness of 85-90 %• Increases the power output. 5 % at 35°C and 50% RH
– Economy• Investment cost is low. About 1 00 000 Euro• O&M is low. Media change every 3 year• Construction time: 30 days. Turbine down time 7-10 days
– Advantages• Low risk for overspray, Passive system• Potable water can be used• No integration with GT needed
– Disadvantages• The effectiveness is limited by ambient conditions• Added pressure drop in the air intake system
Prof. Mohsen Assadi 11
LUN D UN IVER SITY
Cooling Techniques AvailableInlet Fogging
• Based on the adiabatic saturationprocess
• Water is injected through nozzles
– Small droplets in the airstream
– Droplets evaporate and air iscooled
• Consists of
– Pump skid
– Nozzle rack
Prof. Mohsen Assadi 12
LUN D UN IVER SITY
Cooling Techniques AvailableInlet Fogging
• Found in study– Performance
• Effectiveness around 90-97 %• Increases the power output. 6 % at 35°C and 50% RH
– Economy• Investment cost is low. About 60 000 Euro• O&M is low. Nozzle replacement every 2nd year• Construction time: 20 days. Turbine down time 2-3 days
– Advantages• Achieves lower inlet temperature compared to media based evap.• Requires small footprint• No added pressure loss in air intake system
– Disadvantages• Integration with GT control system required• Demineralized water needed• Large droplet can cause erosion• Require inlet drain consideration & careful implementation
Prof. Mohsen Assadi 13
LUN D UN IVER SITY
EU Related Projects• Based on the adiabatic saturation process• Achieves cooling by
– Normal evaporative cooling– Intercooling effect in compressor
• Water is injected through nozzles– Small droplets in the air stream– Droplets evaporate and air is cooled
• Consist of:– Pump skid– Nozzle rack
Wet compressionrecommended location of
installation
Prof. Mohsen Assadi 14
LUN D UN IVER SITY
Cooling Techniques AvailableWet Compression
Power output vs. ambient temperature
Prof. Mohsen Assadi 15
LUN D UN IVER SITY
Cooling Techniques AvailableWet Compression
• Found in study Performance
Great power output augmentation. Increases by 10-15 %Great efficiency augmentation. Improves and regain efficiency by 1-3 %
Economy Investment cost about 3 00 000 Euro Low O&M costs. Nozzle replacements every 2-3 year Construction time: 30 days. Turbine down 5 days
AdvantagesMore independent of ambient conditions Can be placed downstream of media based cooler or inlet fogging
DisadvantagesMust be integrated with GT control systemGas turbine adjustments might be needed to adapt to new operating
conditions for compressor and combustor Risks associated with wet compression
Prof. Mohsen Assadi 16
LUN D UN IVER SITY
Wet Compression EvaluationResults
C - absolute velocity
W - relative velocity
Ca - axial velocity
U - blade rotational speed
• Velocity triangles
Axial velocity is lowered
Leads to off-design blade operation
Blade angles is no longer optimized to
the flow
Increased risk for stall and surge
Increased fouling is seen in the latter
stages. Increased incidence angles
can be the explanation
Rear stage
Prof. Mohsen Assadi 17
LUN D UN IVER SITY
Cooling Techniques AvailableWet Compression
• For a first time wet compression installation a couple of issues needsto be investigated
PulsationComponents life
Prof. Mohsen Assadi 18
LUN D UN IVER SITY
Operating Experiences
• Operating experience– Leading edge erosion seen. Worst at row 1 blades and
decreases downstream. In a 16 stage compressor, lastsigns of erosion can be seen at stage 12.
– Pitting corrosion is considered a medium risk if thesystem is not running constantly.
– Other potential risks have not been encountered orhave successfully been mitigated.
Prof. Mohsen Assadi 19
LUN D UN IVER SITY
Operating Experiences
• Erosion on inlet guide vane• Pitting corrosion potential
Prof. Mohsen Assadi 20
LUN D UN IVER SITY
Summation and Analysis• Media based evaporative cooler is well-known and proven technique
– Should be recommended for the present
• Inlet fogging is a cost-effective and promising technique but– Should be used on certain GT with enough inlet duct length
• Mechanical chillers– Great power output– Expensive and bulky installations. Inconvenient technique for medium
sized gas turbines.
• Absorption chillers– Great power output– Expensive and bulky installations. Promising technique if cheaper
• Wet compression– Great performance enhancement– Cost-effective and flexible. Involves a lot of unknown risks.– If risks can be mitigated, this technique is the best alternative
Prof. Mohsen Assadi 21
LUN D UN IVER SITY