Kinematic Motion Analysis and Structural Analysis of Bellcrank Structures Using FEM 55
4. Conclusions and Discussion
In this paper, FE structural analysis and Fatigue pre-
diction analysis of the flight control actuators for capa-
city are presented. Aileron actuator 3 main parts of the
piston, bell crank, divided by the stroke of 3D analysis
model was developed. Verification calculations prove the
model developed in Sim Design and ABAQUS 5.7 and
FEMFAT 4.6 as being accurate. FE structural analysis
and Fatigue prediction analysis performed on the basis of
stress distribution and the amount of displacement could
be predicted. Analysis of aileron actuator model experi-
ments and simulations to create the actual equipment that
would reduce costs and time are considered. In addition,
through the optimization of the analytical model analysis
time and results can be predicted more accurately than is
believed to be Through comparison of the test results and
analysis, aileron actuator of the results for the endurance
can secure the trust stroke, piston, bell crank, depth due
to the number of design guidelines to provide for the en-
durance in life expectancy. By including the results from
process simulations, significant improvements regarding
correlation of fatigue life predictions to test results can be
achieved. Among the biggest effects are influences from
material. Methods and interfaces have been implemented
in FEMFAT to account for the manufacturing influences.
Benefits from applying these new features are high at
reasonable efforts because results from process simula-
tion are usually available during concurrent engineering.
5. Acknowledgment
This research was supported by the Korea Institute for
Advancement of Technology, supporting fund of Honam
Leading Industry Office in 2013 by grant No. 2013-0114.
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