Browse Topic: Metal finishing

Items (3,662)
This specification covers the requirements for computer-controlled laser peening of metal part surfaces to induce residual compressive stresses at and beneath the surface.
AMS B Finishes Processes and Fluids Committee
This specification covers corrosion-preventive organic substances dissolved or emulsified in a volatile solvent and supplied in the form of a ready-to-use liquid.
AMS B Finishes Processes and Fluids Committee
This study used the L-M (Levenberg-Marquardt) algorithm to analyze the fitting of the flexibility coefficient of fasteners in the mixed connection structure of metal composite materials to address key challenges in aircraft structural design. Through parametric modeling and finite element simulation of single lap joints, the system evaluates eight key factors, including the direction of the composite material layer, the elastic modulus of the metal plate, the plate thickness ratio, the fastener diameter, the elastic modulus of the fastener, the Poisson’s ratio of the fastener, the magnitude of the preload force, and the type of bolt configuration, covering convex and countersunk variants. Advanced material modeling techniques are introduced in the study to accurately capture the anisotropic behavior of the composite material layer and its interaction with metal components under different load conditions. The results show that the higher modulus and thickness of the composite material plate and metal plate significantly reduce the flexibility of fasteners, and larger fastener diameters are associated with reinforcement. The elastic modulus further reduces flexibility. The flexibility of convex head bolts is significantly lower than that of countersunk head bolts, while Poisson’s ratio, preload force, and humidity have little effect. Based on these findings, a new flexible calculation formula containing nine undetermined parameters is proposed. The L-M algorithm is used for nonlinear regression to derive formulas with physical significance. The verification shows that the proposed formula is highly consistent with the finite element results, with a corrected coefficient of determination of 0.956. Among 864 test sample points, 73.61% have an error of less than 5%, and only 0.23% have a deviation of more than 15%. Comparative analysis with twelve existing methods, including the Delft University and Boeing formulas, confirms that the proposed method has better accuracy. This method effectively expands the applicability of traditional flexible formulas, provides solid theoretical support for advanced aircraft connection design, and realizes diverse mixing in aerospace engineering and accurate calculation of connection configuration.
Fan, Zhuotao, Wang, Xu, Wang, Tong, Li, Xianchao
This paper focuses on analytical solutions for studying the vibrations of partially cracked orthotropic plates with piecewise boundaries using the symplectic elasticity method. Crack compliance coefficients are derived from the line spring model and introduced into the governing equations. In this paper, by establishing the Hamiltonian system and solving the Hamiltonian canonical equations, the vibration problem of cracked plates with piecewise boundaries can be reduced to finding the symplectic eigenvalues and symplectic eigensolutions. In the Hamiltonian system, the problem is transformed into seeking the solution of an algebraic equation system by the aid of symplectic eigensolutions and the adjoint symplectic orthogonal relations between the eigensolutions. Thus, for orthotropic plates with cracks under piecewise boundary conditions, this work presents a set of analytical solutions. Specifically, expressions for the free vibration behavior are derived. Furthermore, the steady-state response is determined. Finally, the transient dynamic response is also formulated and solved. The numerical results show that this method is effective and the natural frequency obtained in this paper is consistent with experimental results. A parametric investigation is performed, with the aim of comprehensively investigating the dynamic behavior of cracked plates subjected to piecewise boundaries. Significant findings include how aspect ratio, piecewise boundary conditions, and crack length affect structural vibration characteristics. For the plates containing cracks under piecewise boundaries, the frequency-response and the time-history curves for the forced vibration are plotted. These curves clearly illustrate the corresponding vibration characteristics of the plates. Some of the results can provide benchmarks for validating numerical or approximate methods. The method presented in this paper can provide a pathway for solving similar problems in the field.
Qu, Jianlong, Yu, Qinyu, Jia, Jufang, Xu, Xinsheng
Impacts of laser shock peening (LSP) on the evolution characteristics of microstructure in commercially pure α-phase titanium (α-Ti) are explored by molecular dynamics (MD) simulations of high strain-rate compression. The EAM potential (Zhou potential) is selected for its ability to capture the evolution of microstructures. Considering the LSP-induced peak plasma pressure, the strain rate during the simulated shock compression process is set at 10^9 s-1 to replicate the LSP process. The stress-strain curve of the α-Ti under high strain-rate compression is obtained. The maximum equivalent stress reaches 3.6 GPa, consistent with the theoretically calculated value. The simulation results reveal that mechanical twins (MTs) are activated at a strain of 3%. The number of mechanical twins increases and eventually stabilizes, forming a network structure throughout the grains. In the meantime, numerous partial dislocations are generated adjacent to the grain boundaries. The dislocation density also increases with strain and dislocation reactions occur. Moreover, grain refinement is identified. The grain size is refined from the initial ~ 8 nm to ~ 4 nm in the polycrystalline α-Ti. Twinning, together with dislocation-mediated plasticity, drives the refinement of grain size. Gradients of twin density, dislocation density, and grain size density are induced by LSP on the surface of α-Ti. This study comprehensively investigates how LSP influences the evolution of microstructures by MD simulations. It develops an innovative numerical strategy that offers a foundation for elucidating the underlying mechanisms of LSP.
Zhao, Congshan, Zhang, Linbing, Xu, Yidi, He, Jianye, Fang, Jing, Li, Zezhou, Ruestes, Carlos J., Cheng, Xingwang
This SAE Recommended Practice describes chemical analysis, hardness, microstructure, and physical characteristic requirements for low carbon cast steel shot to be used for shot peening or blast cleaning operations.
Surface Enhancement Committee
Based on the principle of the bimetallic effect of the electrothermal microdrive, polymer SU-eight glue is used as the functional material, nickel metal is used as the structural material, and copper metal is used as the sacrificial layer to make the electric heating microdrive. We process and manufacture them based on specific MEMS processes such as lithography, mask plating, and magnetron sputtering, and perform basic characterization, observation, and electrical signal analysis on the samples. The results show that the overall electrothermal micro-driver device is complete, the electrode and resistance wire structure is complete, and the I-V signal is normal.
Xue, Yunhao, Tan, Xiaolan, Jiang, Xin
Laser directed energy deposition (LDED) is widely used in various fields due to its fine forming structure and superior performance. However, the characteristics of the hot forming process result in significant residual tensile stress in the formed materials, which affects the capability and useful life of the mechanism accessory. The hybrid manufacturing technology of shot peening (SP) and LDED has a significant influence on the elimination of defects and the improvement in microstructure of formed materials and reducing residual stress, but it also has limitations. To solve the problems, such as the introduction of powders and the difficulty in recycling and classification when using heterogeneous materials for shot peening in hybrid processes, this paper proposes a method of strengthening with the same material, establishes a thermal shot peening simulation model for the hybrid process, and conducts experimental verification. The research finds that the average generated stress of SP in hybrid manufacturing technology is -215.6 MPa, and the thickness of the strengthening layer is about 40 μm. The subsequent hot forming process will eliminate part of the induced stress by SP on the previous deposition, but the deposited stress on the surface is reduced compared with that in the single process. The hybrid manufacturing technology of SP and LDED, based on the same material, effectively utilizes the residual heat from the forming process, providing feasibility for engineering applications.
Zhang, Xiaoyu, Zhang, Min, Li, Dichen, Jiang, Yunfeng, Chen, Xinjin, Fei, Ya, Hu, Ying, Liu, Yuyang
Current lithium-ion batteries should generally only be charged above 0 °C, as charging below this temperature can promote lithium plating and irreversible degradation. However, conventional pack-level heating elements increase system mass and design complexity. In addition, heat is transferred from outside into the cell, causing the temperature inside the cell to rise slowly. This study evaluates internal Joule heating of cylindrical Li-ion cells using a zero-mean square-wave current excitation and quantifies the associated aging impact. LG INR21700-M50L cells were tested at 0 °C, −10 °C, and −20 °C with three excitation frequencies (50 Hz, 1 Hz, 10 mHz) at 5 A amplitude. Each cycle consisted of 30 min heating followed by 60 min cooling; reference capacity-based state of health (SOH) was assessed every 50 cycles up to 400 cycles. A maximum surface temperature rise of 14.3 K was achieved, with larger temperature rise at lower ambient temperature and lower excitation frequency. Capacity fade remained below approximately 1% for most conditions; however, at −20 °C and 10 mHz a pronounced SOH decrease to 87% was observed, indicating a critical operating regime. The results provide practical guidance for pulse-heating parameter selection and highlight the need for safeguards and further diagnostics in extreme low-frequency excitation at very low temperatures. This heating approach is particularly suitable for simpler battery-electric applications without thermal management, such as e-bikes or power tools. However, it may also be relevant for applications with existing thermal management systems, as it simplifies battery pack design.
Raiber, Stefan, Allmendinger, Frank, Degler, David, Parschau, Anke
This specification covers the requirements for electrodeposited gold plate.
AMS B Finishes Processes and Fluids Committee
Researchers at Columbia Engineering have developed a new gel electrolyte that both improves the lifetime and safety of anode-free lithium batteries, an emerging battery architecture that could dramatically boost energy density while simplifying manufacturing. Although such design promises higher energy density and lower cost, the approach has long been plagued by short battery life and safety concerns caused by unstable lithium plating and parasitic reactions at the electrode-electrolyte interface.
This specification establishes requirements for chrome-free surface pretreatment materials used for surface preparation of metallic surfaces prior to applying organic coatings.
AMS G8 Aerospace Organic Coatings Committee
This specification covers the requirements for an electroless nickel-thallium-boron or nickel-boron deposit on various substrates.
AMS B Finishes Processes and Fluids Committee
The growing demand for lightweight, high-strength materials in marine and aerospace structures has promoted the use of friction stir welding (FSW) for welding dissimilar aluminum alloys. However, tensile residual stresses and microstructural heterogeneities often degrade weld integrity. This study investigates the combined impact of base material positioning, single- and double-pass FSW, and post-weld shot peening (SP) on the metallurgical and mechanical properties of AA6061–AA2017 joints. Five welding configurations were examined to evaluate how varying base material positions on the advancing and retreating sides affect material flow and mechanical behavior. Post-weld SP effectively presented compressive residual stresses, reduced surface defects, and refined surface grains. The average grain size in the stir zone was reduced from 5.2 μm (single-pass) to 2.0 μm (double-pass U-turn) after SP, confirming significant grain refinement through dynamic recrystallization. Mechanical testing revealed that double-pass FSW with opposite weld direction (U-turn) followed by SP achieved the highest performance, with ultimate tensile strength (UTS) improving from 246 MPa to 289 MPa (≈17% increase) and tensile elongation rising from 8.78% to 9.41%. Microhardness in the heat-affected zone improved up to 127 VHN, countering thermal softening effects. The synergistic effect of double-pass welding and SP enhanced homogeneity, fatigue resistance, and surface integrity. The results establish SP as an efficient post-FSW treatment for dissimilar aluminum joints, offering quantifiable improvements in strength and ductility, making the process highly suitable for demanding marine and aerospace structural applications.
Nukathoti, Raja Sekhar, Battina, N. Malleswara Rao, Vanthala, Varaha Siva Prasad, Chirala, Hari Krishna, Maloth, Balu
This research demonstrates a new way to make carbon-based battery materials much safer, longer lasting, and more powerful by fundamentally redesigning how fullerene molecules are connected. Today’s lithium-ion batteries rely mainly on graphite, which limits fastcharging speed and poses safety risks due to lithium plating. These research findings mean progress toward safer electric vehicles, longer-lasting consumer electronics, and more reliable renewable-energy storage.
This study systematically investigates methods to enhance the fast-charging capability of lithium-ion batteries through advanced simulation. The electrochemical reaction mechanism, heat generation mechanism, and lithium plating mechanism are analyzed in detail, and an electrochemical–thermal coupled model incorporating a lithium plating sub-model is established. A hybrid parameter identification strategy, combining random search, grid search, and manual adjustment, is employed to calibrate the model across different operating conditions, thereby improving its accuracy in reproducing real battery behavior. Lithium plating is selected as the primary indicator to evaluate fast-charging performance. Based on simulation results, the effects of both operational parameters and structural parameters on lithium plating are thoroughly analyzed. The results indicate that lower charging rates, elevated charging temperatures, higher electrode porosity, and reduced tortuosity are favorable for suppressing lithium plating. These conditions improve the uniformity of lithium deposition while alleviating concentration gradients of lithium ions, thus offering valuable insights for battery material design and practical applications. Furthermore, optimized charging protocols are developed on the basis of conventional strategies and their associated impacts on battery behavior. Two novel approaches—the group-based optimized charging protocol and the adaptive optimization-based charging protocol—are proposed by dynamically adjusting the charging rate according to real-time electrochemical states. Validation on the developed electrochemical–thermal model confirms that the proposed protocols can achieve high-rate charging without inducing lithium plating. As a result, charging time is significantly reduced while ensuring safety and reliability. Overall, this research not only provides a comprehensive methodology for modeling and parameter identification but also offers practical strategies for protocol optimization. With solid-state batteries regarded as a promising future technology, the present work provides a potential basis for their advancement.
Zhao, Peiqiang, Zhan, Wenwei, Qi, Ji, Yi, Yong
In practical applications, power cells face a mix of external influences such as temperature variations and structural limits (rigid constraints) that trigger intricate electrochemical and mechanical reactions. This study systematically explores the temporal evolution of surface pressure in lithium-ion pouch cells subjected to rigid mechanical constraints under varying thermal conditions, with a specific focus on the interplay among mechanical stress, lithium intercalation, and lithium plating. To investigate the battery’s electrochemical and mechanical responses, this work integrates experimental measurements with an electrochemical–mechanical coupling model. The analysis is performed under initial loads of 0.3, 0.5, and 1.0 MPa at 25 °C (ambient temperature) and 0 °C (representative low-temperature condition). At 25 °C, surface pressure followed a two-stage pattern: first, stress relaxation occurred, followed by a shift into quasi-steady cycling (cycle-to-cycle variations are minimal). This pattern is largely driven by the reversible volume changes in the electrodes as lithium ions are alternately inserted (intercalation) and removed (deintercalation) during electrochemical cycling of the cells. At 0 °C, slower ion transport and reaction kinetics promoted lithium plating, causing irreversible anode expansion and a continuous rise in surface pressure. Concurrently, the depletion of active lithium diminished the electrode’s maximum achievable state of charge (SOC). This limitation curtailed the degree of electrode expansion and contraction throughout charge–discharge cycles, resulting in a decrease in the amplitude of pressure fluctuations on the battery surface during cycling. Numerical simulations confirmed that lithium plating and SOC degradation collectively shaped the mechanical response at low temperatures. The proposed model accurately replicates experimental pressure evolution and distinguishes between reversible and irreversible contributions to volume changes. This work reveals how temperature and mechanical loading jointly regulate surface pressure and capacity retention, offering insights relevant to battery pack design and the optimization of low-temperature performance.
Du, Yingyue, Chen, Ying, Luan, Weiling, Chen, Haofeng
Lithium-ion batteries (LIBs) have become indispensable components in diverse energy applications driven by their high energy density, long cycle life, and low self-discharge. These excellent characteristics are directly influenced by their manufacturing processes, where variations in battery design and processing parameters will lead to significant differences in performance. Therefore, reliable and efficient evaluation of battery performance across manufacturing processes is essential for quality assurance and process improvement. Traditional methods rely on formation cycling and associated electrochemical tests, which are time and cost intensive. Different from them, a simulation-based approach for manufacturing performance evaluation is proposed in this study. The method employs the pseudo two dimensions (P2D) electrochemical model within the PyBaMM framework, where model parameters such as electrode type, electrode size, and particle size are derived from manufacturing data and built-in parameter data. The model predicts key performance indicators including capacity, resistance, and loss of lithium inventory (LLI) under specified tests conditions. A LGM50T cell was tested under varying operational scenarios, demonstrating the feasibility of the approach. Results indicate that low temperature condition significantly accelerates degradation and Lithium plating, with the capacity degradation at 5 °C reaching about three times that at 25 °C, while moderate variations in charge current rate induce only minor differences of about 0.5%. Simultaneously, depth of discharge (DOD) and average state of charge (SOC) have similar effects on capacity degradation and LLI. By replacing extensive reality tests with physics-based simulations, this method enables rapid evaluation of manufactured or unprocessed battery process formulas, substantially reducing time and material costs while providing mechanistic insights into process performance interactions.
Yan, Yifei, Meng, Jinhao, Song, Zhengxiang, Zhang, Shirui, Pan, Yuhao, Yang, Peihao, Peng, Jichang
With the growing global demand for sustainable energy and high-performance mobile devices, lithium metal solid-state batteries (LMBs) have emerged as a research hotspot in the field of energy storage due to their exceptional high energy density and significant safety advantages. However, the growth of lithium dendrites and their penetration through the solid electrolyte remain key issues leading to battery short-circuiting and failure. To date, there has been a lack of effective in situ research methods to reveal the failure mechanisms, which has severely restricted the commercialization of LMBs. This study innovatively employs in situ electrochemical impedance spectroscopy (EIS) to investigate lithium plating behavior in symmetric cells during critical current density (CCD) tests under room temperature and elevated temperature conditions. By analyzing characteristic signals at 1 MHz, this study presents the in situ impedance changes at the grain boundaries and interfaces of the battery, revealing that lithium plating is a dynamic reduction-oxidation process. We summarize two modes of lithium plating: one involves lithium metal deposition at the interface due to local current density inhomogeneity; the other involves lithium metal deposition at grain boundaries far from the electrode due to concentration gradient differences. The study further reveals that lithium plating at grain boundaries is the primary cause of battery failure. This research highlights the unique advantages of in situ EIS in the field of solid-state battery research and its applicability to various material systems. Moreover, the proposed lithium plating mechanism provides a theoretical basis for optimizing battery design and enhancing battery safety, thereby facilitating the realization of high-energy-density solid-state batteries.
Liu, Zexuan, Wu, Senming, Chen, Ying, Luan, Weiling, Chen, Haofeng
This SAE Recommended Practice defines requirements for equipment and supplies to be used in measuring shot peening intensity and other surface enhancement processes. It is intended as a guide toward standard practice and is subject to change to keep pace with experience and technical advances. Guidelines for use of these items can be found in SAE J443 and SAE J2597.
Surface Enhancement Committee
This specification covers the requirements for an inorganic blackening solution for steel, applied at room temperature.
AMS B Finishes Processes and Fluids Committee
Composite materials have become widely adopted in commercial aviation, as aerospace manufacturers look to use them to drive weight reduction and improved fuel efficiency in new aircraft designs. In the case of aircraft rotary blades, the poor wear properties of these materials have necessitated the development of metal leading edge guards that can provide critical protection against erosion and impact damage during flight. Electroforming has been a leading process for the manufacture of these protective guards, with nickel parts providing excellent wear resistance that significantly extends the service life of the rotary blade assembly. Currently there has not been a focus on utilizing direct electrodeposition of metal on to carbon filled epoxy composite structures, as traditional plating-on-plastics approaches require considerable effort in surface preparation and normally do not provide adequate adhesion to the underlying structure. Alpha Metalcraft Group has been working in cooperation with aerospace suppliers in the design of an electroplating ready composite structure that would allow for direct nickel deposition, provide excellent adhesion, and significantly reduce both the time and cost for the manufacture of ready-to-assembly rotary blade structures. Test panels were constructed of commercially available prepreg materials or by resin infusion of dry fabrics that incorporated different metal containing conductive layers to allow for the direct deposition through a nickel sulfamate electrodeposition process. Different surface modification strategies were investigated to expose the metal conducting layer and thereby provide the metal-to-metal bonding surfaces required for successful electrodeposition.
Cazzaniga, Luigi
This specification covers the requirements for silver deposited on metal parts with a copper strike between the basis metal and the silver deposit.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for electrodeposited cadmium on metal parts.
AMS B Finishes Processes and Fluids Committee
This research paper investigates the failure of an isolator clip used in the seat slider assembly, which guides and restricts the sliding motion of the tooth bracket within the seat. The component is made of C80 high-carbon spring steel, known for its high strength. According to the manufacturing process details, zinc plating was applied to the component for corrosion protection, as confirmed by EDS analysis. A fractographic examination of the failed part revealed a brittle, intergranular fracture morphology with visible cracks. Certain areas also exhibited micro-void coalescence, indicating a dimpled fracture surface. The primary failure mode was intergranular (IG) fracture. The delayed fracture was attributed to intergranular fracture mechanisms, micro-void coalescence, and the high strength of the steel, which made the component susceptible to hydrogen embrittlement. Hydrogen embrittlement occurs when hydrogen atoms become trapped along the grain boundaries, where they form hydrogen molecules, leading to crack initiation. Hydrogen embrittlement also impacts on mechanical properties by reducing ductility and increasing brittleness. This suggests that hydrogen absorption likely took place either during the pickling process before galvanization or during the galvanizing process itself. During zinc plating, the electrochemical reaction (H₂ → 2H+ + 2e-) generates cathodic hydrogen on the surface, ultimately causing hydrogen embrittlement and leading to the sudden and unexpected isolator clip failure under stress. To prevent such failures, a post-fabrication heat treatment (baking) at 200-300°C for a few hours was recommended to remove absorbed hydrogen from the material. Following the implementation of this measure, no further failures of the isolator clip have been reported.
Saindane, Mehul Kishor, Bali, Shirish
Aluminium is widely used across various industries due to its lightweight properties, high strength-to-weight ratio, and cost-effectiveness. However, its susceptibility to corrosion, particularly in harsh environmental conditions, presents challenges to its long-term durability and performance. To mitigate these issues, nickel plating was applied as a protective measure, creating a barrier to minimize aluminium’s direct exposure to corrosive environments and enhance its resistance to degradation. In this study, nickel-plated aluminium was subjected to controlled corrosion testing under simulated real-world conditions, including humidity, saline atmospheres. The primary objective was to evaluate the effectiveness and longevity of nickel plating as a corrosion prevention method. Periodic observations and measurements were conducted to monitor material changes, such as surface degradation, corrosion pattern and corrosion increasing rate. The findings highlight the critical role of plating type, deposition type and environmental conditions in determining the corrosion resistance of nickel-plated aluminium. Based on the study results, recommendations for improving corrosion resistance were proposed, such as optimizing the plating process and incorporating post-plating treatments like passivation or sealing. These insights contribute to advancing corrosion protection strategies, ensuring the sustainability and reliability of aluminium in exposed environments for usage in automotive field.
Narain, Aditya, Venugopal, Sivakumar, Gopalan, Vijaysankar, Varatharajan, Senthilkumaran
The Ro-dip Cathodic Electrodeposition (CED) process is new technology used by automotive manufacturers for higher quality corrosion protection in new generation automobiles. This process involves multiple 360-degree rotation of automotive body-in-white (BIW) which exert higher hydrostatic pressure and drag forces on large surface panels of BIW like hood. For maintaining consistent gaps and flushness control at vehicle level, it is important to safeguard the dimensional stability of light weight (crash performance sensitive) steel hood panel while undergoing through this CED process. This study investigates the enhancement of hood structure supports through strategic optimization of support rod placement and quantity within the Ro-dip CED paint shop system. This Paper underscore the importance of tailored fixture design in the Ro-dip CED process, offering a scalable solution for automotive manufacturers aiming to improve quality while reducing costs associated with dimensional inaccuracies, overall weight reduction and crash worthiness of vehicle.
Tile, Vikrant, Unadkat, Siddharth, Askari, Hasan, Jadhav, Devidas
This specification establishes the requirements for anodic coatings on aluminum alloys.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for a manganese phosphate coating on ferrous alloys.
AMS B Finishes Processes and Fluids Committee
This SAE Standard defines the method for deriving and verifying the peening intensity exerted onto a part surface during shot peening or other surface enhancement processes.
Surface Enhancement Committee
This specification and its supplementary slash specifications establish the requirements for electrodeposition of metals by brush plating.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for electrodeposited hard chromium plate.
AMS B Finishes Processes and Fluids Committee
This specification covers a coating consisting of finely powdered graphite in a heat-resistant inorganic binder applied to parts.
AMS B Finishes Processes and Fluids Committee
This specification establishes engineering requirements for electropolishing metallic parts and materials using Computer Aided Engineering simulation to reduce the process risks related to electropolishing.
AMS B Finishes Processes and Fluids Committee
This SAE Standard covers the engineering requirements for peening surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot.
Surface Enhancement Committee
This specification covers the engineering requirements for producing an anodic coating on aluminum and aluminum alloys which are subsequently sealed with an organic resin.
AMS B Finishes Processes and Fluids Committee
This specification describes the engineering requirements for producing a non-powdery anodic coating on titanium and titanium alloys and the properties of such coatings.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for producing a continuous compound zone (white layer) with controlled extent of porosity by means of a gaseous process, automatically controlled to maintain nitriding and carburizing potentials that determine properties of the nitrocarburized surface. Automatic control is intended to ensure repeatability of nitrogen and carbon content of the compound zone, which influences properties such as wear and corrosion resistance, ductility, and fatigue strength.
AMS B Finishes Processes and Fluids Committee
This SAE Aerospace Recommended Practice (ARP) describes training and approval of personnel performing certain thermal processing and associated operations that could have a material impact on the properties of materials being processed. It also recommends that only approved personnel perform or monitor the functions listed in Table 1.
AMS B Finishes Processes and Fluids Committee
This SAE Aerospace Standard (AS) covers components of rotary flap assemblies to be used with portable equipment for peening of metal parts. The flap assemblies consist of a flap attached to a mandrel and shall be of the following sizes:
AMS B Finishes Processes and Fluids Committee
Compressive residual stresses are very important at fatigue life, therefore this work has an objective to determine compressive residual stresses longitudinally, along a surface, with three levels of deflection causing tensile prestresses on the surface fibers, of 750 MPa, 1100 MPa and 1500 MPa, supported in one support position on the compression side, 150 mm, equidistant from the longitudinal center of the samples, which are made of EN 47 steel (DIN 51CrV4), with dimensions of 15 mm thick, 70 mm width and 1500 mm long. The samples are submitted to quenching, tempering, surface polishing and stress relief processes, with radius of 2500 mm and concavity downwards, and after they are immersed in a tank with mineral and conventional quenching oil compound, then the samples are tempered and the concave surfaces are polished to remove decarburization and took into the furnace to relieve stress caused by the surface polishing process. Next step, the samples are peened, with deflections of 750 MPa, 1100 MPa, 1500 MPa with support distance of 150 mm, in a machine with controlled parameters, to introduce compressive residual stresses on polished surfaces, this process is called stress shot peening – SSP. Specimens are extracted to perform a tensile test for metallographic analysis and hardness determination and residual stresses are determined by X ray diffraction, from the surfaces of the samples longitudinally and uniaxially. The compressive residual stress at deflections of 750 MPa, 1100 MPa and 1500 MPa are -801,67 MPa, -851,37 MPa and -914,51 MPa average, respectively. The samples are submitted to cyclic fatigue testing to verify the influence of compressive residual stresses developed from the three deflections. The fatigue tests maximum results are 32877 (750 MPa), 67347 (1100 MPa) and 104952 (1500 MPa) cycles, fracturing at contact points of the plate.
Chiqueti, Cleber Michel, de Almeida Benassi, Adriano, Gomes, Bárbara Miranda, dos Santos, Marcos, de Lima, Alexandre Santana, Rolim, José Ronaldo Agostinho, da Silva, Fernando Vilanova
This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of ceria-zirconia ceramic shot.
AMS B Finishes Processes and Fluids Committee
This specification covers procedures for tab marking of bare welding wire to provide positive identification of cut lengths and spools.
AMS B Finishes Processes and Fluids Committee
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the engineering requirements for producing brazed joints in parts made of steels, iron alloys, nickel alloys, and cobalt alloys using gold-nickel alloy filler metal.
AMS B Finishes Processes and Fluids Committee
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This specification covers the procurement of granular heat-treating salts suitable for use in the molten state.
AMS B Finishes Processes and Fluids Committee
This specification establishes the engineering requirements for producing an anodic coating on titanium and titanium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
This specification covers the requirements for a hard anodic coating on magnesium alloys and the properties of the coating.
AMS B Finishes Processes and Fluids Committee
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