Advanced Materials Research
Vol. 58
Vol. 58
Advanced Materials Research
Vols. 55-57
Vols. 55-57
Advanced Materials Research
Vols. 53-54
Vols. 53-54
Advanced Materials Research
Vol. 52
Vol. 52
Advanced Materials Research
Vol. 51
Vol. 51
Advanced Materials Research
Vols. 47-50
Vols. 47-50
Advanced Materials Research
Vols. 44-46
Vols. 44-46
Advanced Materials Research
Vol. 43
Vol. 43
Advanced Materials Research
Vols. 41-42
Vols. 41-42
Advanced Materials Research
Vols. 39-40
Vols. 39-40
Advanced Materials Research
Vol. 38
Vol. 38
Advanced Materials Research
Vols. 33-37
Vols. 33-37
Advanced Materials Research
Vol. 32
Vol. 32
Advanced Materials Research Vols. 44-46
DOI:
ToC:
Paper Title Page
Abstract: An important requirement for a collaborative design platform in Concurrent Engineering
(CE) is the integration of various engineering software tools and utilities in product design and
development. Some CE platforms based on a client/server architecture or static Service Oriented
Architecture (SOA) are available in the marketplace, but they lack flexibility and reliability in the
constantly changing Internet environment due to the dynamic nature of the network. Based on the
current development of SOA, this paper presents a Service-oriented Collaborative Design platform
(SCoD) based on SORCER—a dynamic SOA infrastructure that allows federated integration of
engineering software components in CE environments. The architecture of SCoD is proposed, the
wrapping methodology used to integrate engineering software tools in SCoD is presented, and the
federated method invocation for services in SCoD is described. With the support of SCoD,
collaborative design in CE environments can be deployed, and scalability, reliability, and flexibility
can be achieved in the changing Internet environment.
717
Abstract: The theory of reliability sensitivity analysis and reliability-based optimization robust
design are extended to discuss the reliability design of electronic system. Firstly, a method of
measuring the relative importance (sensitivity analysis) of each element of system is studied. And
then, after establishing the mathematic model for reliability optimization, a procedure for robust
design is examined. Finally, a numeric example is presended to illustrate the procedure of sensitivity
analysis and robust design. After optimization, the mean life of system has increased than before, and
the cost has been greatly reduced; on the other hand, the sensitivity of system reliability to the mean
life of components also has decreased. The result shows that the proposed methodology is useful for
system design and quality improvement.
725
Abstract: Railway vehicle structure fatigue life consumption monitoring can be used to determine
fatigue damage by directly or indirectly monitoring the loads placed on critical vehicle components
susceptible to failure from fatigue damage. The sample locomotive carbody structure was used for
this study. Firstly, the hybrid fatigue analysis method was used with Multi-Body System (MBS)
simulation and Finite Element Method (FEM) for evaluating the carbody structure dynamic stress
histories. Secondly, the standard fatigue time domain method was used in fatigue analysis software
FE-FATIGUE and MATLAB WAFO (Wave Analysis for Fatigue and Oceanography) tools. And
carbody structure fatigue life and fatigue damage were predicted. Finally, and carbody structure
dynamic stress experimental data was taken from this locomotive running between Kunming-Weishe
for this analysis. The data was used to validate the simulation results based on hybrid method. The
analysis results show that the hybrid method prediction error is approximately 30.7%. It also
illustrates that the fatigue life and durability of the locomotive can be predicted with this hybrid
method. The results of this study can be modified to be representative of the railway vehicle dynamic
stress test.
733
Abstract: The prediction of aircraft structure service life is of great importance to safety of aircraft
structure and human beings. The relation between aircraft structure service life and reliability can
be found by utilizing the fatigue scatter factor of whole life. Only when the service life satisfies the
requirements of reliability, can the safety of airplane be ensured. The fatigue scatter factors of the
service life accords with lognormal distribution and Weibull distribution were studied to provide
important reference for predicting the safe service life of aircraft structure.
739
Abstract: The project presents the theory of active reliability-based design for predetermined life
targeted at their economic life. The structural reliability is designed from the view point of
economic efficiency and maintainability requirements, so that the destruction of products led by
fatigue and fracture is eliminated to the highest possible degree to provide the longest life, the
highest reliability and the lowest cost. The reliability assessment of conventionally finished product
is developed into an active reliability design at preset life, which is implemented before the design
of products is finalized, to improve the safety and reliability of structures.
745
Abstract: Critical fatigue safety state is investigated on RD2 type axle of China railway freight cars.
Attention is paid on the grooves near axle boxes, where more fatigue cracks were early appeared even
result in at least six derailed accidents. Load history was obtained by vehicle dynamics simulation
combining with on-line inspection. Braking loads and effects of maintenance and off-round of wheels
are also incorporated. Semi-elliptical and external circumferential cracks are employed for crack
growth simulation. Crack shape change and shear stressing of the semi-elliptical crack are taken into
account. New crack growth rate modeling in which covers from cracking threshold to toughness
related fracture state is applied for residual life evaluation. Critical fatigue safety state is defined as the
crack size from which the axle can be safely operated to next overhaul inspection. Critical crack size
is estimated step-by-step with the crack shape change. Results show that the external circumferential
crack is more dangerous than the semi-elliptical crack. Application more than two years in production
verifies that the present assessment is available and reliable.
751
Abstract: Critical safety wheel wear size is investigated through considering the fatigue safety effect
on RD2 type axle of China railway freight cars. The wheel wear size increase results in a rise of the
wheel-rail contact forces, which increase the fatigue stress history of the axle in service. Therefore,
the size must be controlled to maintain the axle safety in service before the next overhaul inspection.
A field investigation was firstly made on the wear size change regularity. Then, the size related
wheel-rail impact forces are solved by a non-linear Hertzian contact theory with a vehicle multi-body
dynamic model. In addition, a statistical method is further developed for incorporating the impact
forces into the wheelset service load history. Finally, a wear size related critical state equation is
established for ensuring the axle safety in service. A stationary solution is statistically obtained for
the critical wear sizes with respect to the axle circumferential crack and semi-elliptical crack. It is
concluded that the critical safety wear size should be controlled in the range of 100 mm at the
statistical level of survival probability 0.99 and confidence 95%.
759
Abstract: The glass-to-metal seals are usually used in the solar thermal power (STP) and electronic
devices. However, the requirement of mechanical properties in the STP is much higher than that of
electronic devices, because the glass-to-metal joints used in the STP need to have anti-fatigue
performance in adition to higher static tensile strength. Under the repeated fluctuating loads, damage
and failures of glass-to-metal seals in the STP often lead to serious consequences. Therefore, analysis
of damage evolution and fracture behavior of glass-to-metal diffusion welded joints was performed in
this paper. Firstly, the finite element (FE) model of glass-to-metal welded joints was established in
accordance with the STP welded structures. And damage simulation was carried out by the FE
software ABAQUS. Also, the work illustrates the modeling of damage in terms of traction versus
separation to simulate crack propagation and introduces the use of traction-separation law as a
damage initiation and evolution criteria. The microgram of damage distribution in the glass side near
the interface could be characterized by Scanning Electron Microscope (SEM), which was compared
with predictions obtained by finite element method (FEM) analysis. As result, the damage criteria on
the lap joints in conjunction with FM analysis were used to optimize the glass-to-metal diffusion
welding technology. The above results provide the basis of design against damage and reliable
estimation of glass-to-metal seals.
765
Abstract: The plastic deformation as a main form of failure of Interference Joints may happen in
engineering works if it is designed unreasonably. In this paper, the contact stress and the strength of
Interference Joint parts were analyzed deeply. Based on the theory of the reliability design, the general
formulas and the method of the reliability design and computation for Interference Joint were
established in consideration of joint structure, machining precision, interference value, mechanical
properties of the joint parts and their randomicity. The practical design method, which would promote
the reliability of Interference Joint effectively, was proposed for larger size and some other important
Interference Joints. Compared to the conventional design method, the working reliability of
Interference Joints can be improved obviously by means of the reliability design method.
773
Abstract: The life of bevel gear dies is determined by its stress state mainly. During the forging, the
die teeth fractured and the bottom corner cracked in a few times. Finite Element Analysis (FEA) was
employed to investigate the reason of failure. The results show that the tip fracture and the bottom
corner crack mainly resulted from excessive tensile stress. In accordance with the FEA results, the
non-plane parting face was changed into plane parting face and the radius of bottom hole was
enlarged. The FEA result proves that the modification can greatly reduce stress concentration and the
application proves that the modification can effectively solve the premature failure of the die.
779