Resumen:
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Consulta en la Biblioteca ETSI Industriales (Riunet)
[EN] This
project
relates
to
the
second
part
of
a
PhD
thesis
carried
out
by
Dr.
Peter
Crawforth
of
the
Advanced
Manufacturing
Research
Centre
( gAMRC h)
at
the
University
of
Sheffield,
Englan ...[+]
[EN] This
project
relates
to
the
second
part
of
a
PhD
thesis
carried
out
by
Dr.
Peter
Crawforth
of
the
Advanced
Manufacturing
Research
Centre
( gAMRC h)
at
the
University
of
Sheffield,
England,
UK.
While
being
not
only
an
important
centre
of
research
in
aerospace
within
Europe,
AMRC
is
also
important
within
the
fields
of
machining
and
modelling.
In
his
thesis,
Crawforth
reaches
the
conclusion
that
tool
geometry
is
an
important
factor
which
has
an
influence
on
cutting
forces
which
can
affect
chip
width,
resistance
and
mechanical
and
thermal
stress.
In
drawing
upon
that
thesis,
this
project:
explores
Crawforth fs
thesis
in
further
depth,
and;
analyses
how
composition
can
affect
the
machining
process,
particularly
in
the
context
of
the
steady
state
of
force-- ]time
graphs.
It
is
hoped
that
as
a
consequence
of
this
project
we
will
be
able
to
further
understand
the
mechanism
by
which
we
can
produce
the
cutting
of
materials
until
it
reaches
a
permanent
state.
To
that
end,
particular
materials
have
been
studied,
such
as
titanium,
and
11
tests
have
been
carried
out.
Within
those
11
tests,
5
were
completed
using
the
same
roundness
tips
with
the
remaining
6
being
varied.
The
methodology
employed
during
the
above
trials
was
as
follows:
(1) Using
orthogonal
cutting,
including
the
preparation
of
the
bills
(as
explained
at
Part
5);
(2) Applying
a
low
band
pass
filter
to
all
the
graphs
to
avoid
noise
and
plotting
of
graphs
force-- ]effective
federate;
(3) Calculating
the
gMo
Equivalent
number h
of
each
material
and
analysing
any
relation
between
it
and
the
cutting
forces,
gradient
of
the
line
during
steady
state,
and
roundness
values,
and;
(4) Recording
and
looking
for
and
correlation
between
the
chip
width,
wear
and
tear
of
the
tool,
beta
trans
temperature,
young
modulus
and
final
stress.
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