STRUCTURAL STRESS ANALYSIS ON THE RUBBER DIAPHRAGM
OF AIR-OPERATED VALVE
Air-operated valves are used extensively in the
power-generation industry for process control and
system isolation functions. A study on the
prevention of damage of an air operated valve is
very important. Specially, diaphragm in an actuator
of an air-operated valve has the highest damage
rate.
In this study, the stress of diaphragm with
thickness change is analyzed. For this analysis,
four experiments were conducted to obtain material
properties of rubber. A stress analysis is carried
out by commercial FEM code, ANSYS 8.0. It is
compared with tension test to verify finite element
analysis. From the result of analysis, the maximum
stress happened at flange edge part, and the maximum
displacement happened between flange edge and spring
support. This study also finds out effect of the
thickness about variable thickness. Even if a
section area is same, the maximum stress is varied
with the thickness of edge side.
1.Introduction
Air operated valves are used extensively in the
power-generation industry for process control and
system isolation functions. Nuclear power plants
consist of many air-operated valves. Safety is a
primary issue in a nuclear power plant. A study on
the prevention of failure of an air-operated valve
is very important. The most critical and sensitive
component of the air-operated valve is the
diaphragm. This provides the seal that allows a
successful actuation to overcome spring pressure
that is used to return the valve to its
"safe" position.
Table 1 shows failure cases of air operated valves.
Table 1 is referred to "Air-operated valve
maintenance guide"[l]. From the Table.1, 30% of
total damage is failure of actuator. Of actuator
failures, the highest failure (35%) was diaphragm
failures, the second failure (29%) was seal and
seal, the third highest failure (13%) was bolting-
related failures, and next (4%) was piston binding.
In this study, structural stress analysis on the
rubber diaphragm is carried out by commercial FEM
code.

2. Structural Stress Analysis
2.1. Model of analysis

Fig. 3 The comparison of linear elastic and hyper elastic for metal and rubber material
[a| Stress -strain curve for metal material
[b] Stress-strain curve for rubber material
Fig. 1 shows a 2-inch globe type
air-operated valve. The shape and operating order of
the actuator is shown in Fig.2. The diaphragm push
the support plate by pressure imposed at the top.
The support plate is supported by spring. The
support plate budges stem, and the valve gets closed
by movement of stem. If the pressure of the actuator
is removed, the
support plate is initialized by the force of spring.
The failure of diaphragm is fatal to the function of
air-operated valve. Major material of diaphragm is
rubber. The modulus of elasticity of engineering
steel is 210 GPa, but rubber is 0.7-4.0 MPa. Rubber
has non• linear properties in stress-strain
relation. This is shown in Fig.3. The material
properties
of rubber are obtained by mechanical test applied to
finite element analysis.



Fig. 6 The stress-strain curves of rubber material
(a) Uniaxial tension (b) Planer tension
(c) Equi-biaxial tension (d) Uniaxial compression
2.2. Static material property test of diaphragm [2]
The non-linear rubber properties of Mooney-Rivlin
factor (CI, C2) are applied to finite element
analysis. Non-linear material factor is calculated
by experimental stress and strain curve. The
material property test of rubber is conducted by
using uni-axial tension test, compression test,
planer tension test and equi-biaxial tension test.
Fig. 4 shows material test of rubber specimen and
stress-strain curves. Fig. 5 shows the shape of test
specimen and rubber sheet for static material
property test. The applied extension speed is
50 mm/min
2.3. Verification offinite element analysis
The structural analysis of uni-axial tension
specimen is conducted. The FEM analysis was
conducted with the same boundary condition of the
experiment. The FEM analysis is carried out by
commercial FEM code, ANSYS 8.0. From the FEM
analysis, the stress is
1.2 MPa at stain 0.34. The analysis results are
similar to test results. As the results, the
experimental stress is 1.2 MPa at strain 0.32.
Therefore, the validity of FEM analysis is verified.

2.4. Structural analysis of diaphragm with constant
thickness
The stress analysis of diaphragm is carried out by
FEM. The boundary condition of diaphragm is shown in
Fig. 8. In the FEM analysis, the Hyper 58 element
was used in analysis. Considered thickness and air
pressure are 2~10mm and 0.1 MPa, respectively. The
analysis results of diaphragm with thickness 2 mm
are shown in Fig. 9. The maximum stress happened at
flange edge part and maximum displacement happened
between flange edge and spring support.


Analysis results about maximum stress and maximum displacement of diaphragm with thickness change are presented in Fig. 10 and Fig. 11. As thickness increases, deflection is decreases rapidly. However, maximum stress is increased as thickness is decreased.

2.5. Structural analysis of diaphragm with variable
thickness
The analysis was conducted with following three
models. The first model is decreasing thickness;
that is, edge thickness is larger than center. The
second model is the constant thickness; that is, the
thickness of center and edge are same. The third
model is increasing thickness; that is, edge
thickness is thinner than center. The analysis
result for three models is presented


3 . Conclusions
The structural analysis of uni-axial tension
specimen that has equal boundary condition with test
is carried out by FEM . Therefore, this study
obtained effectiveness of analysis method.
From the FE M analysis results, the maximum stress
happened at flange edge part and maximum
displacement happened between flange edge and spring
support.
As the diaphragm thickness increases, the maximum
deflection decreases.
Even if a section area is same, the maximum stress
is varied with the thickness of edge side. In case
of same section area, the maximum stress of
strengthen edge side is lower than that of constant
thickness