self aligned hydrogenated selective emitter for n-type ... - IEEE Xplore

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Seth D. Shumatel,2 Douglas A. Hutchings2 , Hafeezuddin Mohammed2, Genevra Beilkel,2,. I'. I. 34 ... Solutions LLC Fayetteville, Arkansas, USA, 3Department of Electrical Engineering, University of ... for real B-H complex data on highly doped material [8]. ..... [4] R. Low, A Gupta, H.J. Gossmann, J. Mullin, V. Yelundur, B.
SELF ALIGNED HYDROGENATED SELECTIVE EMITTER FOR N-TYPE SOLAR CELLS l2 2 l2 2 Seth D. Shumate , Douglas A. Hutchings , Hafeezuddin Mohammed , Genevra Beilke , , I I' 34 3 3 Benjamin S. Newton , Matthew G. Young , Husam Abu-Safe' , Sh'1UYU S-Q , and Naseem HA I

2 Microelectronics-Photonics, University of Arkansas, Fayetteville, Arkansas, USA, Silicon Solar 3 Solutions LLC Fayetteville, Arkansas, USA, Department of Electrical Engineering, University of 4 Arkansas, Fay tteville, Arkansas, USA, Natural Science Division, Lebanese American University,



Byblos, Lebanon ABSTRACT

-

Selective emitter cell architectures are one

avenue for increasing industrial solar cell efficiency. N-type cell based technology is also gaining considerable attention for the same purpose. T his paper describes a novel, single step selective emitter

process

using

acceptor impurities.

atomic

hydrogen

to

passivate

boron

Grid lines act as a mask to hydrogenation,

experimental results on aluminum doped polycrystalline thin fIlms shows its effectiveness.

Cell fabrication is being

developed to test this process on real solar cells to verify experimental results.

Special processing considerations will

be discussed.

which lowers the surface concentration of electrically active boron between grid lines.

Using EDNA to model this complex

emitter, it was shown that Jsc can be increased in the emitter by 2 O.94mAlcm with a short, low temperature atomic hydrogen treatment.

A hydrogenation system has been developed, and

initial experimental results on aluminum doped polycrystalline thin films shows its effectiveness.

Cell fabrication is being

II. THEORY EDNA, a new emitter modeling software, was used to model the effect of hydrogen passivation of boron dopants [6]. The functionality of user-defmed dopant profIles made this

developed to test this process on fabricated solar cells to verify

work possible.

theoretical

are

velocity was not built into the program and was a user-defIned

SELECTIVE

been reported in the literature that for passivated surfaces,

results.

Special

processing

considerations

discussed.

INDEX

The treatment of surface recombination

parameter not linked to the dopant profile. TERMS

HYDROGENATION,

-

EMIT T ER, PHOTOVOLTAIC CELLS, N-TYPE SILICON.

However, it has

both n-type and p-type diffusions show surface recombination velocities (SRV) increasing with dopant concentration [7]. For the presented work, it was asswned that SRV was

I. INTRODUCTlON Selective

emitter

cell

architectures

are

an

interesting

proposition for the solar industry. Many processing schemes have been proposed for selective emitters: laser-based doping, emitter etch back techniques, and ion implantation to name a few [1]-[4]. Most work, naturally, has focused on selective n­ type emitters for p-type cells.

However, there is growing

interest in moving to n-type cells despite abandoning the elegance of the aluminum paste BSF/front side metallization fIre-through in order to reach effIciencies above 20%. Besides Sanyo and Sunpower, with unconventional, high-effIciency architectures, Yingli's Panda cells are some of the only commercially available n-type cells, which currently do not employ a selective emitter [5]. This paper describes a novel, one step selective emitter The idea is simple: a screen printed grid makes ohmic contact to a highly boron-doped p+ emitter. Gridlines act as a mask during an atomic hydrogenation step which lowers the sheet resistance between the gridlines by passivating boron. system

has

been

developed,

978-1-4673-0066-7/12/$26.00 ©2011 IEEE

and

A

initial

by

boron

peak

dopant

density.

This

assumption has been shown experimentally for both boron and phosphorus emitters [7].

For a theoretical comparison, a

boron dopant profile was modified from the one generated by EDNA to include the hydrogen passivated profile calculated for real B-H complex data on highly doped material [8]. These profIles were then entered into the "Measured Data" section of the program to determine the effects on the quality of the emitter.

Hydrogen passivation of boron has been

characterized by Herrero, et

al., and the concentration of B-H

complexes was found to reach 99% passivation near the surface after only 30 minutes of hydrogenation at Tsubstrate = 150°C [8].

The B-H complex data were digitized using

OriginPro 8.6.

using atomic hydrogen to passivate boron acceptor impurities.

hydrogenation

influenced solely

Figure 1 shows the original boron profIle as

well as the hydrogenated profIle based on the experimental data. EDNA was used to compare the emitter characteristics of the two doping profiles in Fig. 1. It should be noted that the program does not consider current generated or collected from the base. All simulated emitters were illwninated with AM1.5 global data built into the software.

001110

III. HYDROGENATION SYSTEM lE+21

A hydrogenation system with independent substrate heating -- Original Boron Profile

lE+20

! lE+19 .� � lE+18 .[ o Q

Hydrogen gas is catalytically cracked by a

heated tungsten filament.

m

Q bQ

was constructed.

I



- -

Hydrogenated Profile

The advantage of this system is an

absence of plasma damage.

The tungsten filament in our

system is 10 cm away from the substrate, minimizing heating

,

from the filament.

The substrate is heated by two 500 W Initial

halogen lamps directly above the substrate holder.

acceptor impurity passivation studies have been carried out by

lE+17

varying

substrate

temperature

and

Polycrystalline films of thickness 300

lE+16

nrn

gas

pressure.

were prepared on

glass by top-down aluminum induced crystallization [10]. Films were used to measure increase in film resistivity due to

lE+15 o

0.1

0.2

0.3

0.5

0.4

0.6

Depth h1m)

Samples were then thermally

hydrogenation treatments.

recovered to the original resistivity values. Figure 3 shows results for varying substrate temperature on

Figure 1 Simulated boron profile from EDNA and hydrogenated profile calculated with experimental data from Herrero,et at., [8].

increase in resistivity for samples hydrogenated for 30 minutes

It is possible that a hydrogenated emitter will not behave the

Original resistivity was just over 0.05Q-cm. Not surprisingly,

same way as a lightly doped emitter in terms of decreased

the optimal substrate temperature from this study was 150°C.

SRV.

It is also possible that high quality passivation could

prove difficult at temperatures below 200°C.

Therefore, the

at 1 Torr with a filament temperature of T fiI

=

I900°C.

These samples showed an average increase in resistivity of over 400%. At Tsub

=

I90oe, resistivity is less because of the

surface recombination velocity of both profiles was varied 6 from 250 cmls to 1x10 cm/s. The behavior of each emitter is

cooling time at the end of the process, where, for a period of

shown in Fig. 2. At low SRV, the hydrogenated emitter out­

which B-H complexes begin to break.

several minutes, the sample was above the temperature at

performs the heavily doped emitter. Absolute increase in Jsc 2 from the hydrogenated emitter is as much as 0.94 mA/cm •

Resistivity vs. Temperature

This value is typical for both experimental and theoretical studies of selective emitters [1], [9].

0.3

However, as SRV

increases, the hydrogenated emitter experiences severe losses

0.25

due to surface SRH recombination according to the model.

"W

The

"/5

original

boron

profile

is

less

sensitive

to

surface

recombination.

;0.15 ·s '"



::R. 0

>. u c Q)

Ti �

01�------------------so

90

1SO

200

2SO

Figure 3 Resistivity versus substrate temperature for 30 minute hydrogenation treatment of p+ polysilicon thin films. The first data point was the average resistivity for all samples before hydrogenation.

80

c

70

Thermal recovery of the resistivity of these samples versus

Q)

'5

()

100

Substrate Temperature (0e)

UJ

.Q t5

0.1

o.OS

100



0.2

E

temperature is shown in Fig. 4.

60

Samples were sequentially

annealed for 30 minutes from 125°e to 325°e in steps of 500e with resistivity measured after each heating cycle until

50

the original resistivity was recovered. 102

103

10'

10S

106

Surface Recombination Velocity (cm/s)

This figure indicates

that B-H complexes are stable for more than an hour at temperatures above I75°e.

Figure 2 Emitter collection efficiency for both original profile and hydrogenated profiles shown in Fig. 1.

978-1-4673-0066-7/12/$26.00 ©2011 IEEE

001111

samples

%Original Resistivity vs. Annealing Temperature

450 400 350 � �300 250 � 200 c 'i 150 '" � 100 .: 50 0 -50

To

-+-75C __ noc __ 150C

-190C

calculate

the

junction

depth,

software

tungsten from

the

It calculates

depth of 2.6 !Jm was calculated. This is much deeper than the ideal junction depth for solar cells. This depth of 2.6 !Jm was used to calculate the theoretical dopant profiles for modeling in EDNA. Figure 5 shows a theoretical 2.6 !Jm profile as well as a 30 minute hydrogenated profile. emitter

100

qJ

300

200

400

Annealing Temperature (DC)

Several

considerations

be

made

for

cell

processing

based

on

simulation

results

and

is

clear

that

to

As

(high SRV) hydrogenated cell shows a degradation compared to

the unpassivated (high SRV) non-hydrogenated cell. 2 EDNA predicted this degradation to be 1.23 mA/cm • Figure

lE+21

·DODD / ODDOOO�

-Original Boron Profile

DDOOOO� 0000-;

_

'"

6

lE+20

I=:

This is true of normal selective emitter

are more susceptible to SRH surface recombination [9]. must

be

deposited

at

·P.IE+19 0 0 I=:

...0 0



lE+18

temperatures below about 200°C or quickly to retain the desired profile. This is assuming heating and deposition times of less than an hour, which is dependent on deposition configuration and processing parameters. PlasmaTherm PECVD requires

only

system 5

we use

minutes

For example, the for

to

reach

substrate

The wafer used for the boron diffusion was single crystal, n 3 15 type, with a background doping of lxlO cm- • The

Using a PDS® P-type boron nitride source for the

boron diffusion, the pre-deposition soak was completed for 1 hour at 1l00°C.

- - 30 minutes H

,

r r

J

lE+17 0.0

0.5

Next, the drive in lasted for 30 minutes at

1100°C. Finally, the wafer underwent a boron deglaze in HF. An aluminum grid and back side metallization were added to complete the solar cell. One cell was hydrogenated for 30 minutes with a filament ° temperature of 1900 C and a hydrogen pressure of 1 Torr. Two 500 W halogen lamps heated the substrate holder and

978-1-4673-0066-7/12/$26.00 ©2011 IEEE

1.5

1.0

Depth (�m)

2.0

2.5

Figure 5 Simulated 2.6 11m boron diffusion (blue solid line) and calculated 30 minute hydrogenation active dopant profile (red dashed line).

V. DISCUSSION

Before the boron pre-deposition

and diffusion, the wafer underwent a piranha clean and HF oxide etch.

I

anti-reflection

temperatures of 250°C.

thickness was 500-550 !Jm.

I I



eo

layer

both

observed after hydrogenation.

structures because, as shown in Fig. 2, lightly doped emitters passivation

for

7 shows the Light J-V curves for the cell before and after 2 hydrogenation. There was a 1 mA/cm degradation in Jsc

whether atomic hydrogen treatment can be used as a selective

any

efficiency

was the case with the 0.5 !Jm junction depth, the unpassivated

determine

emitter technology.

and

�.

passivation layer must be applied

hydrogenated

�-;

a

collection

Figure 6 shows the

original profiles versus surface recombination velocity.

... ...,.- .. DO

studies.

hydrogenation

coatings

heated

parameters. By entering the diffusion parameters and the SSL 3 20 of boron in silicon at 1100°C of 3.37xl0 cm- , a junction

IV. EXPERIMENTAL

Second,

The

junction depth of common dopants in silicon using user-input

Figure 4 Samples annealed at various temperatures until returned to original resistivity values.

it

° 150 C.

filament was used to catalytically crack hydrogen gas.

u

First,

approximately

University of Illinois named DifCad was used.



must

to

It is interesting to compare the polycrystalline TAlC films with the solar cells.

10 films were hydrogenated with the

same system and parameters, and they showed a 175%-250% increase in resistivity (see Table I). After a one hour anneal at 350°C, the seven films that were annealed had a decrease in resistivity indicating the hydrogen had left. Before the 5/2012 measurement,

films

3,

4,

and

5

underwent

another

hydrogenation step at 250°C, 1 torr, for 30 minutes. Then, a RTA at 500°C for 10 seconds was performed. The fact that samples 8, 9, and 10, which were not annealed, had consistent

001112

resistivity

measurements

over

a

long

period

of

time

hydrogenations of less than 10 minutes only marginally

demonstrates that hydrogen did not leave the TAlC samples.

increase

The performance of the hydrogenated cell, however, nearly

processes.

returned to its original value after a few months at room

enable better surface passivation, and enable higher Voc and

sheet

resistance

unlike

other

selective

emitter

This would enable low-shadowing grid designs,

temperature. There are two possible explanations for this: the

Jsc values without sacrificing the fill factor. More work will

boron-hydrogen passivation for this cell was not stable under

be done to determine the effectiveness of this treatment with

room temperature conditions or the native oxide growth over

excellent surface passivation and whether or not hydrogen can

that time passivated the cell well enough to lower the surface

passivate

recombination velocity to below lO,OOO cm/s.

reflection/passivation coatings.

There was

the

boron

diffused

emitter

through

the

anti­

insufficient evidence for either case and this will be an area of further investigation.

Initially, however, the degradation due

predicted by EDNA. one

of

these

cells

Another batch of cells was made and was

hydrogenated.

It

also

showed

degradation in Jsc after hydrogenation and also showed a recovery over time.

The grid from this cell was etched and

had only a 20% increase in resistivity compared to the other cells from the same batch.

Table 2 compares the sheet

-0.003 e u

--

< --- -0.005 >-

.... .... rrJ

s::

III

0

corresponding hydrogenation times. The measured increase in

s::

of

various

dopant

passivation

profiles

resistivity would point to an effective hydrogenation time of between 5 and 10 minutes.

....

-0.007

III

-0.009

= U

-0.011

t::

-0.013

70 -2.6 micron Boron Profile ---30

- - Post H

---

N

with

resistance

-PreH

-0.001

to hydrogenation seemed to be consistent with the degradation

minutes H

---

-

----

- -----

-0.015 0

0.2

0.6

0.4

Voltage (Volts) Figure 7 Light J-V curves before (blue solid line) and after (red dashed line) hydrogenation. TABLE I TAlC FILM RESISTIVITY MEASUREMENTS 0

45

p

3.E+02

3.E+03

3.E+04

(post-H)

O-cm

O-cm

1

0.052

0.144

0.052

0.052

2

0.057

0.190

0.057

0.057

3

0.058

0.189

0.053

0.069

4

0.074

0.259

0.066

0.074

5

0.055

0.167

0.053

0.060

6

0.056

0.187

0.059

0.061

7

0.058

0.194

0.058

0.057

8

0.053

0.148

No anneal

0.148

9

0.054

0.144

No anneal

0.143

Surface Recombination Velocity (cm/s)

VI. CONCLUSIONS A study of hydrogen passivation of boron acceptor impurities in n-type solar cells has been carried out.

It has been

concluded that for boron doped solar cells, a hydrogenation treatment initially passivates boron impurities, as indicated by a decrease in Jsc as predicted by EDNA. The simplicity of this method

to

potentially

form

selective

emitters

on

fully

fabricated cells clearly sets it apart from more complicated etch-back

or

laser

doping

steps.

978-1-4673-0066-7/12/$26.00 ©2011 IEEE

Likewise,

short

P

(pre-H)

(350 C anneal 1 hr.)

3.E+05

Figure 6 EDNA results for collection efficiency versus surface recombination velocity for the original 2.6 11m doping profile (blue solid line) and the calculated 30 minute hydrogenation profile (red dashed line).

p

P

Meas. 5/2012

001113

10

No anneal

0.147

0.050

[9] M. Zanuccoli, P.F. bresciani, M. Frei, H.W. Guo, H. Fang, M. Agrawal, C. Feigna, E. Sangiorgi, "2-D Numerical Simulation and Modeling of Monocrystalline Selective Emitter Solar Cells," Thirty­ Fifth IEEE PVSC, 2010. [10] S. D. Shumate, M. K. Hafeezuddin, H. A Naseem, and D. A Hutchings, "Microstructural Influence of Hydrogenated Amorphous Silicon on Polycrystalline Emitter Solar Cells Prepared by Top-down Aluminum Induced Crystallization," Thirty-Seventh IEEE PVSC, 2011.

0.127

TABLE II SHEET RESISTANCE VERSUS HYDROGENATION TIME

Hydrogenation Time (minutes)

Sheet Resistance (DID)

0

33.53

5

38.63

10

49.77

20

60.39

30

97.67

ACKNOWLEDGEMENTS

This material was based on work supported Silicon Solar Solutions LLC and the National Science Foundation under EPS-lO03970. Altermatt

for

Thanks

to

creating

Keith

McIntosh

and

sharing

and

Pietro

EDNA

at

(http: //www.pvlighthouse.com.au/simulation/ hosted/EDNA/EDNA.aspx).

REFERENCES

[I] T.C. Roder,S.l Eisele,P. Grabitz,C. Wagner,G. Kulushich,lR. Kohler, and lH. Werner, "Add-On Laser Tailored Selective Emitter Solar cells," Progress in Photovoltaics: Research and Applications, 18,2010,pp. 505-510. [2] D.S. Ruby,P. Yang,M. Roy,and S. Narayanan,"Recent Progress on the Self-Aligned, Selective-Emitter Silicon Solar Cell," Twenty­ Sixth IEEE PVSC, 1997. [3] D. Rudoph, K. Peter, A Meijer, O. Doll, and I. Kohler, "Etch Back Selective Emitter Process with Single POCL3 Diffusion," Twenty-Sixth European Photovoltaic Solar Energy Conference and Exhibition,

2011. [4] R. Low, A Gupta, H.J. Gossmann, J. Mullin, V. Yelundur, B. Damiani, V.Chandrasekaran, D. Meier, B. McPherson, and A Rohatgi, "High Efficiency Selective Emitter Enabled Through Patterned Ion Implantation," Thirty-Seventh IEEE PVSC, 2011. [5] AR. Burgers,R.C.G. Naber,AJ. Carr,P.c. Barton,L.J. Geerligs, X. Jingfeng, L. Gaofer, S. Weipeng, A Haijiao, H. Zhiyan, P.R. Venema, and AH.G. Vlooswijk, "19% Efficient N-Type Si Solar Cells Made in Pilot Production," Twenty-Fifth European

Photovoltaic Solar Energy Conference and Exhibition, Fifth World Conference on Photovoltaic Energy Conversion,

2010. [6] K.R. Mcintosh and P. Altermatt, "A Freeware ID Emitter Model for Silicon Solar Cells," Thirty-Fifth iEEE PVSC, 2010. [7] P. Altermatt, H. Plagwitz, R. Bock, 1 Schmidt, R. Brendel, M.l Kerr, and A Cuevas, "The Surface Recombination Velocity at Boron-Doped Emitters: Comparison Between Various Passivation Techniques," Twenty-First European Photovoltaic Solar Energy Conference, 2006. [8] c.P. Herrero, M. Stutzmann, and A Breitschwerdt, "Boron­ Hydrogen Complexes in Crystalline Silicon," Physical Review B, 43, 2,1991,pp. 1555-1575.

978-1-4673-0066-7/12/$26.00 ©2011 IEEE

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