a comparison of thermal and flow modulation gcxgc with ... · a comparison of thermal and flow...

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R.C. Striebich, L.M. Shafer, Z.J. West, S. Zabarnick University of Dayton Research Institute Gulf Coast Conference, October 16-17, 2018 A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL) This material is based on research sponsored by the Air Force Research Laboratory under agreement number FA8650-16-2-2605. The U.S. Government is authorized to reproduce and distribute reprints for Governmental purposes notwithstanding any copyright notation thereon. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of Air Force Research Laboratory or the U.S. Government. Case Number: 88ABW-2018-5035 The material was assigned a clearance of CLEARED on 10 Oct 2018. Federal Aviation Adminstration (FAA)

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Page 1: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

R.C. Striebich, L.M. Shafer, Z.J. West, S. ZabarnickUniversity of Dayton Research Institute

Gulf Coast Conference, October 16-17, 2018

A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels

Air Force Research

Laboratory (AFRL)

This material is based on research sponsored by the Air Force Research Laboratory under

agreement number FA8650-16-2-2605. The U.S. Government is authorized to reproduce and

distribute reprints for Governmental purposes notwithstanding any copyright notation thereon.

The views and conclusions contained herein are those of the authors and should not be

interpreted as necessarily representing the official policies or endorsements, either expressed

or implied, of Air Force Research Laboratory or the U.S. Government.

Case Number: 88ABW-2018-5035 The material was assigned a clearance of CLEARED on 10 Oct 2018.

Federal Aviation

Adminstration (FAA)

Page 2: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Introduction: Hydrocarbon Type Analysis, GCxGC

11/9/2018 2

• ASTM D2425 HC type by MS is difficult– D2425 requires multiple instruments and analyseso HPLC-refractive index detection, HPLC-fraction collection, GC-MS of 2 different fraction and

computing routine to examine the results

– Quantified by MS single ion response

• GCxGC improvements– Improved separation in two dimensions

– quantified by FID, simultaneous MS

• Original preference: flow modulation– non-polar primary column (DB-5MS)

– moderately polar 2nd column (DB-17MS)

Page 3: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Hydrocarbon Type Analysis – Flow modulation GCxGC

11/9/2018 3

• Demonstrated method with complex mixtures of standards

• Characterized petroleum and alternative Jet A plus:– F24

– JP-5

– Diesel

– JP-7

– Gasoline

– RP-1,2

– others

0

2

4

6

8

10

0 2 4 6 8 10

mea

sure

d,

GC

xG

Cknown, wt%

0

5

10

15

20

25

30

35

0 5 10 15 20 25 30 35

n-, iso-paraffinscycloparaffinsalkylbenzenesindans,tetralinsdiaromatics

Measure

d, G

CxG

C, w

t%

Known, wt%

92 different jet fuel components blended

into 12 different mixtures

Energy and Fuels, 2014

Aromatics

Saturates

FT-

SPK

Jet-AAromatics

Saturates

Page 4: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Original applications were for “normal” phase GCxGC

11/9/2018 4

Normal phase: non-polar primary column

Reverse phase:polar primary column

Difficult area

Page 5: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Hydrocarbon Type Analysis – can also determine carbon number within compound class

11/9/2018 5

Weight % Volume % Weight % Volume % Weight % Volume %

Aromatics

Alkylbenzenes

benzene (C06) 0.01 0.01 <0.01 <0.01 <0.01 <0.01

toluene (C07) 0.16 0.14 <0.01 <0.01 0.08 0.07

C2-benzene (C08) 1.10 1.00 <0.01 <0.01 0.56 0.49

C3-benzene (C09) 2.97 2.73 <0.01 <0.01 1.54 1.37

C4-benzene (C10) 3.32 3.05 <0.01 <0.01 1.71 1.52

C5-benzene (C11) 2.22 2.03 <0.01 <0.01 1.15 1.02

C6-benzene (C12) 1.45 1.33 <0.01 <0.01 0.75 0.66

C7-benzene (C13) 0.73 0.67 <0.01 <0.01 0.40 0.35

C8-benzene (C14) 0.52 0.48 <0.01 <0.01 0.24 0.21

C9-benzene (C15) 0.28 0.25 <0.01 <0.01 0.13 0.12

C10+-benzene (C16+) 0.15 0.14 <0.01 <0.01 0.05 0.04

Total Alkylbenzenes 12.90 11.84 <0.01 <0.01 6.60 5.87

12381

ATJ

10325

Jet A

12382

50/50 Blend

Page 6: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Why thermal modulation?

11/9/2018 6

• More balanced flow to the secondary column– More mass spec sensitivity

• Focusses solute zones on column– Narrower peaks

– More resolution, in theory

• Many GCxGC users have thermal mod.– Systems too expensive to change

– Any developed methods should incorporate both modulators

C-18C-15

C-12

C-09

monocyclo

alkylbenzenes

diaromatics

Jet A

Thermal modulation, “reverse” column set (polar primary column)

Page 7: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Two experimental setups for doing GCxGC HC type

11/9/2018 7

Flow modulation Thermal modulation

Carrier gas: HydrogenHigh Split injection, no dilutionPrimary Column: DB-5MS (20 m, 0.18 mm ID)Secondary Column: DB17MS (5 m, 0.25mm ID)Capillary Flow technology modulator6 seconds modulation timeSecondary Column Flow: 36 mL/minQuickswap teeAgilent 5975 Mass spectrometerTransfer line to FID detection

Carrier gas: HydrogenHigh Split injection, no dilutionPrimary Column: DB-5MS (30 m, 0.25 mm ID)Secondary Column: DB17MS (2 m, 0.25mm ID)LECO cryogenic modulator6 seconds modulation timeSecondary Column Flow: 1.5 mL/minCapillary Flow Technology Purged SplitterTransfer line to LECO Peg IV TOF-Mass spectrometerTransfer line to FID detection

Different columns (same phases), different flows, different modulators

Page 8: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Two experimental setups for doing GCxGC HC type

11/9/2018 8

Flow modulation Thermal modulation

Modulator

C1

C2

TOFMS

CFTPurged splitter

FID

Modulator/2nd oven

Quad-MS

Page 9: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Flow modulation vs thermal modulation (Similar!)

11/9/2018 9

13294 F76,

Flow modulation,

Fid-quad-MS

Page 10: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Thermal modulation example: F76

11/9/2018 10

13294 F76,

Thermalmodulation,

Fid-TOFMS

Page 11: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Comparison example: naphthalenes

11/9/2018 11

1

87

654

321

87

6

32

54

• Slight differences, but overall, very close

• Different times, different amounts, tailing (streaking different)

• Programming rates also different

flow

thermal

Page 12: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Highly branched alkanes

11/9/2018 12

Flow ModulationThermal Modulation

Page 13: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

HC Type Results, comparing the thermal and flow modulation

11/9/2018 13

0

10

20

30

40

50

0 10 20 30 40 50

flow vs thermal modulation (no blobsplitting)

alkylbenz-Tdiarom-Tcycloarom-TisoPar-TnPar-Tmonocyclo-Tdicyclo-Ty=x

The

rmal M

odu

lation S

yste

m (

LE

CO

)

Flow Modulation System (Agilent)

• These are results for six different fuels, F-24s and F-76s

• The isoparaffins are lower in the flow mod system than in thermal. n-alkanes are correspondingly higher.

• Dicycloparaffins are somewhat lower for the thermal modulation system (LECO). Monos are a little higher for thermal mod.

Page 14: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

HC Type Results, comparing the thermal and flow modulation

11/9/2018 14

0

5

10

15

20

0 5 10 15 20

flow vs thermal modulation - aromatics

alkylbenzenes

diaromatics

cycloaromatics

linear

Th

erm

al M

od

ula

tio

n S

yste

m (

LE

CO

)

Flow Modulation System (Agilent)

0

10

20

30

40

50

0 10 20 30 40 50

flow vs thermal modulation (no blobsplitting)

isoPar-T

nPar-T

monocyclo-T

dicyclo-T

linear

The

rmal M

odu

lation S

yste

m (

LE

CO

)

Flow Modulation System (Agilent)

Aromatics Alkyl-, cyclo-paraffins

Page 15: A Comparison of Thermal and Flow Modulation GCxGC with ... · A Comparison of Thermal and Flow Modulation GCxGC with dual FID-MS for Aviation Fuels Air Force Research Laboratory (AFRL)

Conclusions

11/9/2018 15

• ASTM D2425 is a difficult technique for hydrocarbon type analysis. GCxGC has many advantages

• GCxGC: two main techniques of flow and thermal modulation.

• Thermal and flow modulation compared for Jet A, diesel fuels (6 processed so far), more now available

• Different (but similar) templates must be used

• Early work shows good agreement between modulators, in spite of other experimental differences

• Comparisons to other GCxGC systems are on-going