Mold pattern technological CAD design of the compressor cross-head.
Eftimie, Lucian ; Tierean, Mircea ; Baltes, Liana 等
1. INTRODUCTION
Reciprocating compressors (fig. 1) usually compress gas inside of
cylinder, which inner volume is diminished due to piston movement. The
compressed gas goes out through the discharge valves. The new cycle is
starting with the admission of the gas, through the suction valve, as a
result of the depression caused by the expansion of the inner volume of
the cylinder. All the variable volumes of the inner cylinder are
obtained as a result of a linear movement of the piston. If the piston
is not moving following a straight line, the different supporting
elements will wear.
The target of this paper is to show how is generated the additional
shallows to reach the necessary shape of a pattern, especially for the
compressor's cross head application used in hydrogen processing.
2. APPLICATION FOR CROSS HEAD STRUCTURE
The cross-head body is a complex part which allows compensating all
efforts of the connecting rod transferring only the axial movement
relative to the piston rod.
During the function the cross-head slides, on the cylindrical side
faces, covered by low friction material. It is necessary to use a
strong, but light design, to force on minimum the oil sliding film. Such
a design is presented in the Fig. 2 using CATIA V5 software (Balc et
al., 2004).
The part will be made by steel, using green sand casting technology, which requires specific steps to be followed as we show on a
simple sample.
Let's suppose that the part is as simple as a cylinder, and
applying all the following technological steps.
We analyze the body and choose the splitting plane as symmetry into
the horizontal plane (see fig. 3). Having a symmetry system, we can work
only on a half body, and we choose to work on the upper side generating
the final assembly by symmetry. We add all around the side surface the
necessary material to compensate the thermal contraction (figure 3).
[FIGURE 1 OMITTED]
[FIGURE 2 OMITTED]
[FIGURE 3 OMITTED]
Machining will be necessary to obtain a smooth surface. We apply a
new layer of material to allow the safe machining of the surface (see
fig. 3) (Chu et al., 2006).
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
[FIGURE 6 OMITTED]
The moulding technology uses cline or taper walls to the extraction
direction minimizing the friction to the walls mould cavity (fig. 3)
(Madan et al., 2007).
To prevent contraction cracks on the edges of the casting steel
when cooling, we apply required fillets on the inner or outer edges
(fig. 4). Applying symmetry, we can reconstruct the full body of the
sample.
The final analysis will be made on the cross-section of the full
body of the sample.
We have applied all the necessary technological steps on the
finished part design shown in figure 1, and we have obtained the final
shape of the cross-head body, as shown in figure 6. Into this moulding
technology, caused by the complex empty inner part, we have applied also
some spatial support--red colour represented--for the mould core. This
red marked supports will be included both in pattern and core.
[FIGURE 7 OMITTED]
[FIGURE 8 OMITTED]
By symmetry, we can extend the CAD part to the full body (fig. 7)
(Cooper, 2001).
The pattern was produced by wood, because it is cheaper for only
one part, using CAM technology on a vertical machining centre Fadal
4525, as shown in figure 8.
It can be observed that all the round surfaces connected to the
splitting plane, are not modified as a cline surface because they are
enough curved and they are not modifying the cavity when extracting
(Homburg et al., 2006).
The full body was oriented one against the other--half by
half--using two pins crossing the splitting plane.
The core box was realised using the same technology. It means that
we have applied all the necessary layers to allow the thermal
contraction, the machining layers, radius to prevent cracks and setting
extensions to fix the core inside the mould.
3. CONCLUSION
Using CAD design and CAM technology can be obtained complex and
precise patterns.
This is a simple method to produce other more complex parts. The
method is applicable to the green sand moulding technology. It is
necessary to respect all conventional marking colours for outer
surfaces, for inner core marks and splitting plane.
The mould must have correct sized risers to feed rapidly the melted
steel into the casting case during solidification. The casting designer
will take in consideration the steel flows into the mould, to avoid
turbulent flow as well as rapid fill of the mould. Gates and risers are
added during the moulding process.
Foundry manufacturing methods specific to green sand moulds,
applied for this moulding technology, improves quality of the final
products.
4. REFERENCES
Balc, N. & Campbell, R.I. (2004) From CAD and RP to innovative
manufacturing, Computing and solutions in manufacturing engineering,
COSME '04
Chu, C.H.; Song, M.C. & Luo, V.C.S. (2006) Computer Aided
Parametric Design for 3D Tire Mold Production, Computers in Industry,
Volume 57, Issue 1, p. 11-25
Cooper, K. (2001). Rapid prototyping technology: selection and
application, Marcel Dekker, New York
Homburg, N. & Wellbrock, E. (2006) Knowledge-based
manufacturing strategy and methods for foundries, RTejournal, Ausgabe 3,
p. 1-10
Madan, J.; Rao, P. V. M. & Kundra, T. K. (2007) Computer Aided
Manufacturability Analysis of Die-cast Parts, Computer-Aided Design
& Applications, Vol. 4, No. 1-4, pag. 147-158