Mechanical Response of Additively Manufactured 304L Across a Wide Spectrum of Loading Conditions.
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Carroll, Jay↗
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Results for “Mechanical loading”
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DEFORMATION MECHANISMS AND ANNEALING EFFECTS IN 17X17 PWR FUEL RODS UNDER PINCH LOADING CONDITIONS
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Martinez, Oscar↗
Instability of a Mechanical System Induced by an Impinging Fluid Jet
Theoretical and experimental determination of critical loading by impinging fluid jet and instability of mechanical system
Feldt, W. T.↗
Crashworthy design of helicopter composite airframe structures
The crashworthy behavior of composite materials and generic structural elements is investigated. Cruciform structural elements are crushed in order to determine their energy absorption capability to rotorcraft crash-type loads, and quasi-static compression tests are conducted on a series of aluminum and composite cruciform elements. These elements are representative of keel beam and bulkhead intersections in the subfloor of rotorcraft. Various designs of 'trigger mechanisms' reducing initial peak failure loads and initiating stable crushing failure modes are considered. It is shown that a carbon-fiber-composite/aramid-fiber-composite hybrid element with a columnlike midsection behaves more like a well-designed tubular composite element. Specimens which fail primarily in bending are typical of structural components used in the upper and lower portions of rotorcraft airframes.
Boitnott, Richard L.↗
Transient Three-Dimensional Analysis of Nozzle Side Load in Regeneratively Cooled Engines
Nozzle side loads are potentially detrimental to the integrity and life of almost all launch vehicles. the lack of a detailed prediction capability results in reducing life and increased weight for reusable nozzle systems. A clear understanding of the mechanism that contribute to side loads during engine startup, shutdown, and steady-state operations must be established. A CFD based predictive tool must be developed to aid the understanding of side load physics and development of future reusable engine.
ng, Ten-See↗
Analysis of a Hybrid Wing Body Center Section Test Article
The hybrid wing body center section test article is an all-composite structure made of crown, floor, keel, bulkhead, and rib panels utilizing the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) design concept. The primary goal of this test article is to prove that PRSEUS components are capable of carrying combined loads that are representative of a hybrid wing body pressure cabin design regime. This paper summarizes the analytical approach, analysis results, and failure predictions of the test article. A global finite element model of composite panels, metallic fittings, mechanical fasteners, and the Combined Loads Test System (COLTS) test fixture was used to conduct linear structural strength and stability analyses to validate the specimen under the most critical combination of bending and pressure loading conditions found in the hybrid wing body pressure cabin. Local detail analyses were also performed at locations with high stress concentrations, at Tee-cap noodle interfaces with surrounding laminates, and at fastener locations with high bearing/bypass loads. Failure predictions for different composite and metallic failure modes were made, and nonlinear analyses were also performed to study the structural response of the test article under combined bending and pressure loading. This large-scale specimen test will be conducted at the COLTS facility at the NASA Langley Research Center.
Wu, Hsi-Yung T.↗
Direct measurement and calculation of rubber bulk modulus by piston-cylinder method using conventional mechanical testing equipment
This article describes a method to directly measure the bulk modulus of rubber using a piston-cylinder type apparatus. The function of the testing apparatus is to reliably transfer load to the water inside the vessel and allow for the accurate and continuous measurement of volumetric displacement as the contents are compressed. During the test, load is applied to a piston-cylinder containing the rubber test sample and water using a conventional mechanical testing load frame. Load and the travel of the piston are recorded by a load cell and extensometer, respectfully. A brass or stainless steel plug of the same dimensions as the test sample is tested as a control sample to isolate the compliance of the system, including the compressibility of water and compliance of the piston-cylinder. The results from this control test are used to disincorporate the compliance of the system from the sample test results. Load-linear displacement data are mathematically converted to pressure-volumetric displacement data, from which bulk modulus is calculated. The test apparatus and method are validated using the known bulk modulus of water. Finally, the bulk modulus for two similar rubbers is evaluated. The validity of the results and limitations of the device are discussed.
36 MATERIALS SCIENCE↗
Influence of Deep Cryogenic Treatment on the Mechanical Properties of Spring Steels
Leaf springs are mechanical elements responsible for supporting the vertical load on heavy duty vehicles. For this critical structural component, the required mechanical performance depends mainly on chemical composition and heat treatment. SAE 5160 and SAE 6140 steels are widely used as springs, because after heat treatments, the strength requirements of impact and fatigue are obtained. 51CrV4-ACF steel is another spring steel option which also exhibits excellent mechanical properties. The objective of this work was to study the influence of conventional heat treatments and cryogenic treatment on properties involving fatigue and impact resistance of spring steels. Furthermore, fracture toughness was measured for these materials, and the fracture surfaces were analyzed. The results showed that the cryogenic cycles used did not provide positive effects on spring steel performance. On the other hand, the chemical composition and the application of cleanliness technology promoted higher mechanical strength: Fracture toughness of 51CrV4-ACF was 100% higher than SAE 5160 steel.
36 MATERIALS SCIENCE↗
Damage mechanisms in three-dimensional woven reinforced ceramic matrix composites under tensile and flexural loading at room and elevated temperatures
Three-dimensional Nicalon SiC/SiC matrix composites made through a chemical vapor infiltration process were studied under tensile and flexural loading at 23, 1200, and 1550 C in air. In situ damage accumulation monitoring NDE techniques were utilized to identify failure mechanisms in these materials. The effectiveness and durability of a chemical vapor deposition SiC surface coating were also evaluated in severe oxidizing environment. Results show that the failure response was very similar for the 23 and 1200 C specimens, while at 1550 C there were significant changes in both the composite mechanical behavior and the matrix microstructure. Extensive fiber pull-out was observed only in the 1550 C specimen. It is also found that the SiC surface coating can protect the composite up to the critical matrix cracking strength.
Chulya, Abhisak↗
Characterization of Static Performance and Failure of Resistance Spot Welds of High-Strength and Press-Hardened Steels
The static performances and failure characteristics of resistance spot welds (RSW) of steel sheets were studied in this work. Both similar and dissimilar joints of press-hardened steel grade 22MnB5 and as-rolled high-strength steel grade 1000 were examined. From metallographic analyses and micro-hardness measurements, it was shown that the microstructures of base metal (BM), heat affected zone (HAZ) and fusion zone of steel joints were noticeably different. In particular, the HAZ close to BM or subcritical HAZ (SCHAZ) of 22MnB5 steel exhibited greatly decreased hardness due to occurring tempered martensite, in which carbide precipitation was clearly observed. Furthermore, tensile shear test and cross-tension test of the welded steel sheets were carried out. The determined maximum loads, energy absorbability and corresponding failure mechanisms were analyzed and compared. The RSW samples of similar steel grade 1000 provided the highest load-carrying capacity and absorbed energy in both tests. Due to the large hardness difference and soft zone in weldment of dissimilar steel specimen, failure loads and static absorbed energies were deteriorated up to 17 and 68%, respectively. The observed fracture occurrences of all investigated joints were pullout failure mode, in which BM and HAZ were the crack initiation sites of grades 1000 steel and 22MnB5 steel, respectively. The SCHAZ of welded boron steel considerably caused the failure onset in tension shear test, but seemed to have negligible effect on cross-tension test.
36 MATERIALS SCIENCE↗
Correlation of Tensile Deformation-Induced Strain in HSLA Steel with Residual Stress Distribution
During service, due to the dynamic loading rates encountered, structural components experience varying levels of plastic deformation which leads to changes in the mechanical behavior of materials. The dynamic loading leads to non-homogenous plastic deformation which changes the residual stress distribution. In this study, the magnitude and distribution of residual stress in tensile tested specimens of high-strength low-alloy steel were investigated using x-ray diffraction technique, by varying the deformation rate. Tensile testing was performed at four different strain rates, and residual stress measurement was done along the length of the fractured specimens. Distribution of residual stress was observed all along the length of the specimens which is attributed to the varying levels of plastic deformation. Measured residual stresses are correlated with elastic strain and plastic strain obtained from the tensile tests. Consistent decrease in the magnitude of residual stress with an increase in plastic strain is observed with decreasing strain rate at the necking region. Specimen with lower yield strength experienced higher plastic strains, hence lower elastic residual stresses. The reasons for the observed distribution of residual stress are discussed with XRD peak broadening associated with plastic deformation.
36 MATERIALS SCIENCE↗
Microstructural Model for Creep-Fatigue Interaction in Grade 91 Steel
This report describes the completion of a crystal plasticity finite element simulation framework for creep-fatigue deformation and damage in Grade 91 steel. In addition to a description of the framework and a set of verification calculations, the report details an initial set of simulations applying the framework to examine low cycle fatigue and creep-fatigue interaction in Grade 91 at 600° C. Grade 91 is a likely material for future advanced microreactors and creep-fatigue will be a limiting structural damage mechanism, particularly for mobile reactors or load following systems. The framework described here could provide a better understanding of creep-fatigue damage mechanisms and directly examine creep, fatigue, and creep-fatigue interaction for Grade 91 at realistic component service conditions. This in turn could lead to improved design methods and component life estimation approaches, leading to more efficient and economical component designs.
36 MATERIALS SCIENCE↗
Advances in Electrospun Poly(ε-caprolactone)-Based Nanofibrous Scaffolds for Tissue Engineering
Tissue engineering has great potential for the restoration of damaged tissue due to injury or disease. During tissue development, scaffolds provide structural support for cell growth. To grow healthy tissue, the principal components of such scaffolds must be biocompatible and nontoxic. Poly(ε-caprolactone) (PCL) is a biopolymer that has been used as a key component of composite scaffolds for tissue engineering applications due to its mechanical strength and biodegradability. However, PCL alone can have low cell adherence and wettability. Blends of biomaterials can be incorporated to achieve synergistic scaffold properties for tissue engineering. Electrospun PCL-based scaffolds consist of single or blended-composition nanofibers and nanofibers with multi-layered internal architectures (i.e., core-shell nanofibers or multi-layered nanofibers). Nanofiber diameter, composition, and mechanical properties, biocompatibility, and drug-loading capacity are among the tunable properties of electrospun PCL-based scaffolds. Scaffold properties including wettability, mechanical strength, and biocompatibility have been further enhanced with scaffold layering, surface modification, and coating techniques. In this article, we review nanofibrous electrospun PCL-based scaffold fabrication and the applications of PCL-based scaffolds in tissue engineering as reported in the recent literature.
Polymer Science↗
Mechanical properties of Al/ω-Al-Cu-Fe composites synthesized by the SPS technique
Highlights: • For the first time, Al/ω-Al-Cu-Fe composites are produced by Spark Plasma Sintering. • Cu diffusion in Al matrix leads to precipitation of θ′-Al{sub 2}Cu. • The σ{sub 0.2%} drop at around 523 K is due to coarsening of θ′-Al{sub 2}Cu precipitates. • At high temperature, load transfer is the main strengthening mechanism. • At low temperature, SPS Al/ω composites have higher σ{sub 0.2%} than HIP Al/ω composites. - Abstract: Al/40 vol%ω-Al-Cu-Fe composites were produced from Al powder and i-Al-Cu-Fe quasi-crystalline particles using spark plasma sintering (SPS) technique. The mechanical properties of the composite were evaluated over the temperature range 293 K–823 K by performing compression tests at constant strain rate. The temperature dependence of the σ{sub 0,2%} yield stress gives evidence of two temperature regimes with a transition in the range 473 K–523 K. The decrease of σ{sub 0,2%} with increasing temperature, more pronounced in the low temperature regime, indicates that the two temperature regimes correspond to two different thermally activated deformation mechanisms. Based on microstructural analyses of the Al matrix, where plastic deformation takes place, the different strengthening contributions are discussed and the results are finally compared to those obtained for composites produced by hot isostatic pressing (HIP), for which the σ{sub 0,2%} temperature dependence is similar. In the low temperature regime, the σ{sub 0.2%} stress of the SPS composites is higher than that of the HIP composites. In this temperature regime, the stress difference is mainly ascribed to the different reinforcement phases present in the Al matrix. In the high temperature regime, the temperature dependence of σ{sub 0.2%} is comparable for the two composites whatever the processing route: load transfer is thus the main strengthening mechanism, which is similar for the two Al/ω-Al-Cu-Fe composites, the temperature dependence being ascribed to cross slip and climb processes.
36 MATERIALS SCIENCE↗
Response relationship between loading condition and corrosion fatigue behavior of nickel-aluminum bronze alloy and its crack tip damage mechanism
Highlights: • The differences of corrosion fatigue behavior of NAB alloy in air and in 3.5% NaCl solution are carefully compared. • The corrosion environment significantly accelerates the crack growth of NAB alloy and decreases the fatigue threshold. • The corrosion fatigue crack growth rate increases with the decrease of loading frequency. • The acidification and the dealumination occur in process of corrosion fatigue, resulting in the deterioration of crack tip. - Abstract: Corrosion fatigue is one of the major forms for nickel‑aluminum bronze alloy used in marine propeller. It is greatly important to understand the corrosion fatigue behavior of nickel‑aluminum bronze alloy in seawater for the purpose of improving the service life of marine equipment. In this study, corrosion fatigue crack growth rate of nickel‑aluminum bronze alloy in 3.5% NaCl solution was tested under various stress intensity factors, stress ratios and loading frequencies to reveal its corrosion fatigue mechanism. The results show that corrosion environment significantly accelerates the crack growth and decreases the corrosion fatigue threshold, which is attributed to the corrosion reactions between the metals of crack tip and corrosive medium. Among the various factors, loading frequency has more predominant influence on the corrosion fatigue crack growth rate of nickel‑aluminum bronze alloy, which can be rationally explained by the hydrogen embrittlement mechanism. Additionally, in the process of corrosion fatigue crack growth, the acidification and the dealumination would occur at the crack tip, resulting in the corrosion dissolution of κ phases and the deterioration in mechanical properties of crack tip.
36 MATERIALS SCIENCE↗
Mechanical and Tribological Behavior of ZrB{sub 2}-TiB{sub 2} System Prepared by Mechanical Activation Spark Plasma Sintering Technique
ZrB{sub 2}-TiB{sub 2} system among varying amount of TiB{sub 2} loading (5, 10, 15, 20 and 30 wt.%) was prepared by mechanical activation spark plasma sintering at 2100 °C for 15-min dwell time under 50 MPa uniaxial pressure in argon atmosphere. The effect of the TiB{sub 2} loading on properties like physical, mechanical and tribological of the prepared samples was studied and evaluated with monolithic ZrB{sub 2} ceramic. Finally, almost fully dense samples (> 96% of theoretical density) were fabricated. Microstructural observation and XRD phase analysis of sintered compact revealed that TiB{sub 2} completely went into the ZrB{sub 2} structure by formation of solid solution with ZrB{sub 2} phase. ZrB{sub 2}-TiB{sub 2} (30 wt.%) showed the highest Vickers micro-hardness (H{sub V}) of 20.64 GPa at 10 N load. On addition of TiB{sub 2}, the fracture toughness of the ZrB{sub 2}-TiB{sub 2} improved up to 4.69 ± 0.43 MPa m{sup 1/2} over monolithic ZrB{sub 2} at 10 N load. At 10 N load, the scratch resistance coefficient, wear rate and wear resistance coefficient of ZrB{sub 2}-TiB{sub 2} (30 wt.%) reached a lowest value of 0.32, 0.35 mm{sup 3}/N m and 0.008, respectively, at 10 N load than other ZrB{sub 2} compositions.
36 MATERIALS SCIENCE↗
Gripper Test Assembly Status Report (FY2020)
Refueling systems for fast reactors are designed to handle fresh and used core assemblies (fuel, reflector, and shield core assemblies) within the reactor vessel in an opaque coolant environment without visual reference. These refueling machines are designed to work in a sodium (or other fast reactor coolant) and argon vapor space environment and are engineered with the rotatable plug system to allow for the movement of fresh and spent fuel into and out of the reactor core. The refueling machines are a critical component in any reactor and thus need to undergo extensive testing in a prototypic environment to ensure that they will meet all of the system functions and requirements. Argonne has developed an innovative compact refueling system design for the Advanced Fast Reactor-100 that is based upon some mechanisms used in previous reactor designs, such as the U.K.’s Prototype Fast Reactor (PFR) and some mechanisms that have not been used in sodium. This compact refueling machine supports the reduction in size of the AFR-100’s reactor vessel, and if fully developed, would support and inform the development of the in-vessel refueling machines for such commercial reactors as the GEH PRISM reactor plant, the ARC Clean Energy’s ARC-100 reactor, and the Natrium reactor, among others. This refueling system is a vital component of a fast reactor that supports reducing the cost of the reactor and increasing its reliability. During the development of the compact fuel handling machine conceptual design for the AFR-100, a lack of testing data for many mechanical components in sodium under typical in-reactor loads and conditions was discovered. The reduction in lifetime of the various mechanical components in the liquid sodium environment needs to be quantified versus the calculated component lifetimes under normal conditions in the testing while they are subjected to typical loading profiles experienced in the past. The Gripper Test Assembly discussed here includes a full-size gripper device with appropriate mechanical features that will be tested in sodium to provide this testing data. The Gripper Test Assembly is used to test various mechanical fuel handling components submerged in high temperature liquid sodium. These mechanisms are gears, bearings, gripper jaws and head, universal joints and shafts, ball screws, among others. These components will be tested under the typical sodium environmental conditions experienced during refueling operations with appropriate loading conditions that simulate the removal and insertion of core assemblies into a fast reactor grid plate structure. This Gripper Test Assembly is the second in a series of refueling system mechanisms developed for testing in sodium. The first test assembly is the Gear Test Assembly (GTA) which was used to test the performance of gears and bearings operating in sodium. Because of the successful testing conducted with the GTA, it was decided to continue with the development of the Gripper Test Assembly which uses the same gears and bearings tested in GTA. Using the data collected during operation of this gripper test assembly, lifetime reduction factors of the various mechanical components can be calculated for the material combinations selected. These lifetime reduction factors can be used in the design of future mechanical systems which operate in these environments to accurately predict component end of life. In addition, an understanding of the ability of these components and mechanisms to operate under-sodium with the chosen materials will be accomplished. Again, this Gripper Test Assembly is the follow-on test article to the Gear Test Assembly which was testing the ability of gears and bearings operating in a sodium environment. Once fabricated and qualified, it will be tested in the Mechanism Engineering Test Loop (METL) facility located in Building 308 at Argonne National Laboratory.
21 SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS↗
Experimental Simulations of Field-Induced Mechanical Abuse Conditions
Mechanical failure of cell components is an important component to understanding safety outcomes for batteries subjected to external loading. Several key parameters governing the mechanical response at the component to the module level are discussed in this chapter. Specifically, nuances associated with experimental measurements of these properties – including development of test methods, fixturing the test articles, ways to minimize errors in measurements, and improving the repeatability of some of these experiments – are examined closely.
Torres-castro, Loraine↗