Methanol as a low cost alternative fuel for emission ...

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1 Methanol as a low cost alternative fuel for emission reduction in gas turbines Joint Venture between IEC and Dor Chemicals THE 11TH ISRAELI SYMPOSIUM ON JET ENGINES AND GAS TURBINES Thursday, October 25, 2012 (9:00-17:00)

Transcript of Methanol as a low cost alternative fuel for emission ...

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Methanol as a low cost

alternative fuel for

emission reduction in

gas turbines

Joint Venture between

IEC and Dor Chemicals

THE 11TH ISRAELI SYMPOSIUM ON JET ENGINES

AND GAS TURBINES

Thursday, October 25, 2012 (9:00-17:00)

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The Need for Methanol

Dramatic increase in regulatory requirements for

reduced emissions.

Traditional methods of reducing NOx emissions, such

as:

modification of the firing system (DLN – Dry Low NOx)

injection of water into the firing system (WLN – Wet Low NOx)

post combustion treatment of the flue gas to remove NOx

(such as SCR – Selective Catalitic Reduction)

All are very expensive!

Low cost alternatives should be checked!

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Methanol is a synthetic alcohol

Properties:

• Chemical Formula CH3OH

• Molecular weight 32.04

• Flash point 12 C (to 41 C)

• Auto-ignition temperature 464 C

• Combustion (Adiabatic) temperature 2045 C

• Low heating value 4777 kcal/kg

• Density 793 kg/ M3 at 30 C

Methanol as an Option

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Methanol is Attractive Option

Methanol can achieve:

Reduced NOx emissions - lower flame temperature and no Fuel-Bound Nitrogen (FBN)

No SO2 emissions - has no sulfur

Clean heat surfaces and lower maintenance - clean burning characteristics of methanol (better than with HFO or even with LFO)

Higher power output relative to NG and FO - higher mass flow in GT engines

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Methanol Firing at FT4C

TWIN PAC 50 MW GT Unit

Two stage tests:

1 – to prove feasibility (Caesarea)

2 – to restore capacity and gain

operational experience (Eilat)

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Caesarea Power Plant Site

Tested unit

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TP -1 Base Plate Assembly

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FT4 – Engine & Power Turbine

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Liner

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Fuel Spraying Nozzles

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FO Atomizer Assembly

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Predicting the NOx Formation Calculated Flame Temperature

Distribution at 100% Load

Flame temperture distribution through liner length

1400

1450

1500

1550

1600

1650

1700

1750

1800

1850

1900

1950

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26

Calculation zone number

Tem

pera

ture

, C

Fuel oil#2

Methanol

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Predicting the NOx Formation Liner Wall Temperature Calculated

Distribution at 100% Load

Relative liner wall metal temperature reduction during

methanol burning

0.5

0.6

0.7

0.8

0.9

1

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26

Calculation zone number

Meta

no

l to

FO

#2 w

all

meta

l

tem

pera

ture

rati

o

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Predicting the NOx Formation Formation Through Liner NOx CalculatedComparison of

Length for FO#2 and for Methanol Firing at 100% Load

NOx emission formation through liner length

0

50

100

150

200

250

300

350

400

450

0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26

Calculation zone number

NO

x,m

g/d

Nm

3 @

15

% O

2,

Fuel oil#2, calculated

Methanol, calculated

Fuel oil#2, measured

Log. (Fuel oil#2, calculated)

Log. (Methanol, calculated)

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Diagram for Methanol Firing Test

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Methanol Tank With Dike

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Methanol Connection Junction

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Emission Measurements Instruments

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Test Results

TT7

Average TT7 as function of GT load

Tamb=22-24C

800825850875900925950975

100010251050107511001125115011751200

0 5 10 15 20 25 30

GT load, Mw

TT

7, F

Oil#2 Methanol Power (Oil#2) Linear (Methanol)

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Test Results

Temperature Spread

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Test Results

Heat Rate

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Test Results

NOx Reduction

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Test Results

CO

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Test results

Oxygen

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Test Results

Particulates

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Test Results

SO2

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Test Results

Formaldehyde

Formaldehyde as function of GT load

0

5

10

15

20

25

0 5 10 15 20 25 30

GT load, Mw

Fo

rmald

eh

yd

e,

mg

/dN

m3@

15%

O2

Methanol

Formaldehyde Limit

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Following Stage

Modification for a Long-Term

Methanol Firing Test in Eilat

The Plan

A project to convert FT4C TWIN PAC 50 MW GT Unit in Eilat to

Methanol firing (identical to the unit in Caesarea).

Objectives

To restore the full capacity of the machine and to gain long-term

operating experience of working with methanol-fueled GT.

Schedule

Following summers for two years.

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How To Restore Capacity?

The flow must be doubled.

There are a few bottle necks, as follows:

HP pumps (Gear Box Driven) – external pumps assembled on a skid

Modulating Valve – omitted – flows are controlled by a Variable

Speed Drive (VSD)

Pressure & Dump (P&D) valves – replacement of strainer

Firing nozzles – Excello Nozzles are replaced by set of High Flow

Delevan Nozzles (which were developed for water injection to

enable doubling the flow).

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Two-Phase Test (in Eilat)

Short-term:

Check feasibility of the system and validate performance

and low emissions (2-3 weeks).

Long-term:

Gain operational experience and confidence in the system

(2-3 years, 1500-2000 hours each year).

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Fuel oil

Methanol

Filters By others

psi

psi

Fuel SOVs (shut-off valves)

gpm

gpm

75 HP VSD

Engine

80 gpm pump

40 gpm pump

Control House

Mixing Block

30 HP VSD

PEPCO Fuel Control Proposal for dual methanol

system (one skid)

1.5” SS pipe

1.25” SS pipe Inlet piping both fuels 3”

400V 50Hz ~75KVA

Control Air 250-110 psi

Motor power wire from VSD

Control wires: 2 digital outputs 2 analog inputs

2 analog outputs

PEPCO Fuel Control

Control wires: 2 digital outputs

6 digital inputs 5 analog inputs

Restoring Capacity – Fuel Control & External Pumps

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External High-Pressure Pumps

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Replacing Nozzles to

Delevan High Flow

Excello Nozzles Delevan Nozzles

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Adapting Fuel Unloading

and Storage System

New unloading piping

Tank adaptation – floating roof

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Adapting Fire-Fighting System

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Fuel Unloading Platform

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Summary

The results presented here clearly show that with minor

low cost fuel system retrofit, methanol firing leads to

significant NOx, SO2, and particulates emission

reduction, without affecting performance.

We believe that the results of the present work can be

applied to other boilers and gas turbines.