J. Am. Ceram. Soc., 84 [5] 915–20 (2001)
journal
Effect of Heating Rates on the Synthesis of Al O –SiC Composites by
2
3
the Self-Propagating High-Temperature Synthesis (SHS) Technique
Lokesh Chandra Pathak, Debajyoti Bandyopadhyay, Srinivasan Srikanth,
Swapan Kumar Das, and P. Ramachandrarao
National Metallurgical Laboratory, Jamshedpur 831 007, India
Various aspects of in situ formation of Al O –SiC composites
by the self-propagating high-temperature synthesis (SHS)
technique have been investigated using thermal analyses (TG/
The RH-SHS technique has shown the feasibility of fabrication
8,9
2
3
of Al O –SiC in situ composites, but several aspects, which
2 3
include heating rates, green density, composition, etc., have not yet
been investigated. In this paper, an attempt has been made to
investigate the influence of heating rates on the synthesis of
Al O –SiC composites.
DTA) of a powder mixture (4Al, 3SiO , 3C) and pellets in an
2
argon atmosphere at different heating rates. Both the reaction
initiation and peak temperatures are found to increase with
the heating rates. At lower heating rates, the powder samples
do not reveal any exothermic peak possibly because of poor
reactivity and sluggish exothermic reaction. The appearance of
exothermic peaks in the DTA plots after melting of aluminum
indicates reduction of silica by liquid aluminum. Conversion of
aluminum is found to decrease marginally with an increase in
heating rates. The apparent activation energy of the process
compares well with the interdiffusion activation energy of
silicon and oxygen, indicating that oxygen diffusion in Si
formed at the reaction front may be the rate-controlling factor
for this SHS process. From SEM studies it appears that the
formation of SiC whiskers is through liquid-phase mass
transfer.
2
3
II. Experimental Procedure
Stoichiometric amounts of silica (SiO ) (99% pure), aluminum
2
(
99% pure), and carbon (graphite, 98% pure) powders in 4:3:1
molar ratio were taken in a stainless steel container and milled for
6
2
1
h. Approximately 6 g of milled powder mixture was pressed to
.5 cm diameter pellets at a pressure of Ϸ100 MPa. Approximately
wt% of poly(vinyl alcohol) (PVA) was added as a binder during
pelletization. The green pellets were dried at 150°C for 3 h to
remove the moisture.
Simultaneous differential thermal analyses (DTA) and thermo-
gravimetric analyses (TGA) of the powder mixture and the pellets
were conducted in a Seiko TG/DTA apparatus (Model No. 320).
The average particle size of the powder sample was 30 m and the
green densities of the pellets were found to be 60% of the
theoretical density. Before the thermal analysis experiments, the
I. Introduction
LUMINA-BASED ceramic-matrix composites have shown prom-
A
ise as advanced materials for high-temperature applications
sample chamber was flushed with pure argon gas (O ϳ 2 ppm)
2
because of their excellent refractoriness, low susceptibility to
oxidation, and good mechanical properties at elevated tempera-
and the investigations were conducted under continuous flow of
argon gas at a rate of 50 mL/min. The samples were heated from
the ambient temperature to 1200°C at several heating rates ranging
between 5 and 100°C/min. On attainment of the desired tempera-
tures the samples were cooled down to room temperature. The
experimental conditions used for this study are summarized in
1
–4
tures.
Besides the conventional powder metallurgical route,
synthesis of these composites by in situ fabrication methods is
gaining momentum due to certain inherent advantages. In situ
fabrication techniques eliminate the problems of using fine ceram-
ics, particularly whiskers, and the chances of segregation of the
constituents are relatively low compared with mechanical mixing
methods. There are also fewer processing steps in this route.
Several techniques for the synthesis of in situ composites have
Table I. The reaction initiation temperature (T ) was measured
i
from the DTA plots using the three-point method. The time
interval between T and the exothermic peak temperature, T , was
i
p
noted. In one of the experiments, the pellet was heated at a rate of
00°C/min from ambient temperature to 1450°C and soaked for 10
min in a graphite furnace. Then the pellet was furnace cooled and
characterized.
The samples were characterized by XRD, SEM, and energy-
dispersive X-ray spectroscopy (EDS). XRD analyses of the sam-
ples were conducted at different stages of processing. Fractured
surfaces of the samples were studied with a JEOL-840A SEM
system equipped with a Kevex EDS system.
5
–8
been reported in the literature.
4
A new combustion synthesis technique for the fabrication of
Al O –SiC in situ composite using a rapid-heating self-
2
3
w
propagating high-temperature synthesis (RH-SHS) has recently
8
,9
been reported by the authors. During synthesis of composites
through the SHS technique, heating rates may have a significant
influence on the reaction initiation temperature (T ), the mecha-
i
nism of the combustion reaction, as well as the quality of the
1
0–12
products.
The synthesis of Ti–Al intermetallic compounds by
the SHS route has shown that the mechanism of the reaction
changes from solid–liquid interaction to solid–solid interaction
1
2
III. Results and Discussion
with an increase in the heating rates. It has also been reported
that an increase in the heating rates improves the density of the
1
1
In the combustion synthesis technique, the self-sustainability of
the exothermic reaction and the propagation of a combustion wave
front mostly depend on the enthalpy change associated with the
SHS product.
1
3,14
reaction and the rate of energy dissipation from the system.
The adiabatic temperature, T , indicates that the maximum tem-
N. S. Jacobson—contributing editor
ad
perature attained by the products under adiabatic conditions is an
important SHS parameter. It has been reported that a value Tad
above 1800 K is required for the self-sustainability of the exother-
1
4,15
Manuscript No. 189888. Received September 8, 1998; approved January 18, 2000.
mic reaction.
It is also well known that most of the exothermic
9
15