Browse Topic: Metals

Items (33,868)
Investigating the load-bearing capacity of Titanium Matrix Composites (TMCs) open-hole panels and their mechanically connected components is of great significance for the application of titanium matrix composites in the aerospace field. This paper investigates the failure behavior of TMC open-hole panels with a [45°/45°/-45°/-45°] laminate configuration under tensile loading. Tensile tests were conducted in conjunction with finite element modeling to analyze the damage evolution process and identify the failure modes of the tensile samples. The results show that the simulation outcomes exhibit good consistency with the experimental results, providing a foundation for the structural optimization and theoretical study of TMC open-hole panels.
Gao, Ximan, Jia, Qiuyue, Liu, Shanshan, Meng, Fanling
To solve the critical challenges of uncoordinated operational node selection and premature mission termination caused by dynamic energy or coating depletion during anti-corrosion spraying on largescale steel structures, this paper proposes an advanced path planning methodology for UAVs. The proposed approach is built upon a BIMSLAM fusion model. Specifically, a high-fidelity three-dimensional (3D) environmental model is reconstructed by integrating offline BIM structural priors with real-time SLAM data. Furthermore, the framework implements the ICP algorithm and Kalman filtering simultaneously to eliminate point cloud noise and compensate for perceptual occlusions, thereby achieving a 5 cm localization accuracy in cluttered industrial environments. A dual-stage pipeline is established for pre-screening and dynamic evaluation. In the offline phase, geometrically inaccessible task points are identified and pruned via spatial accessibility analysis. During real-time operations, the onboard system continuously calculates the battery State of Charge (SoC), operational power, and remaining paint volume to eliminate inefficient flights. For the path generation stage, a hybrid search strategy is developed, which implements a Genetic Algorithm for task sequencing alongside a multi-objective cost function parameterized by four metrics: energy consumption, paint requirements, obstacle proximity, and task density. Additionally, Softmax is used to dynamically regulate the weight coefficients, enabling the system to balance operational safety and efficiency based on the instantaneous state vector. Finally, a fifth-order B-spline parameterization is used to maintain flight stability under complex wind disturbances and heavy time-varying payloads. Consequently, the results show that the proposed method significantly outperforms conventional baselines. The recorded 96.7% mission completion rate demonstrates its operational reliability for the maintenance of bridges and towers.
Qian, Lei, Huang, Chen, Tan, Libin, Huang, Tao
To suppress the formation of brittle intermetallic compounds typically generated during conventional joining of Cu/Al dissimilar materials in the automotive lightweighting sector, this study examines the interface properties and process simulation of electromagnetic pulse welding technology for connecting copper terminals to aluminum conductors. High-quality welds exhibit a wavy interface composed of interpenetrating metallic phases, according to microstructural research. To represent workpiece dynamics, magnetic field distribution, and impact behavior under discharge voltages ranging from 4 to 5.5 kV, a linked electromagnetic-structural finite element model was developed. According to simulation data, increasing the discharge voltage significantly enhances impact pressure, strain rate, and magnetic flux density, all of which support strong contact bonding. The study offers a reference for the lightweight production of automobile electrical connectors by demonstrating the impact of process factors on weld quality.
Li, Liang, Lei, Xiaokun, Fang, Cheng, Li, Yaxiong, Tang, Ming, Wang, Hu, Xie, Chong, Du, Changqing
This paper examines the corrosion of vehicle body metal panels and external chrome-plated components under typical climatic conditions. Specifically, we analyse the potential corrosion mechanisms and influencing factors, and propose protective and improvement measures. The research indicates that corrosion at the interface between body sheet metal and exterior chrome-plated parts is predominantly characterized by galvanic corrosion and crevice corrosion. These problems are caused by the potential difference between the materials, assembly gaps, moisture retention, and the influence of contaminants. The authors analyse climatic data from seven representative cities in eastern, southern, southwestern, northeastern, and northwestern China. The study reveals the synergistic effects of environmental factors (such as NO2, SO2, precipitation, temperature, and relative humidity) on metal corrosion. The results show that the static corrosion rate of carbon steel is higher in the southwestern, southern, and eastern coastal regions (reaching over 98 μm/a at maximum) and lower in the northeastern and northwestern regions (approximately 10 μm/a). Field investigations of more than ten vehicle models in eastern coastal cities of China have found that chrome-plated parts in areas such as engine compartment cover plates, window trims, and trunk lid panels are prone to corrosion due to structural interference, assembly-induced damage, and poor drainage performance. Consequently, the authors propose protection measures through optimizing Chromium plating processes, improving structural designs (e.g., adding sealing strips, designing rounded transitions, and increasing drainage gaps), and adjusting assembly methods (e.g., adopting adhesive bonding or encapsulated clips), which effectively reduce corrosion risks. Finally, the authors conduct professional tests to verify the corrosion resistance of vehicle chrome-plated parts. This paper provides a reference framework for enhancing the corrosion resistance of vehicle exterior components, offering crucial guidance for improving the overall aesthetic quality of vehicles and enhancing customer satisfaction.
Liu, Peng, Zhuang, Mengmeng, Chen, Junjie, Wang, Jiayu, Wu, Weixing, Ren, Kaixu, Wang, Wentao, Li, Yan
Accurate representation of strain-rate dependent stress–strain behavior is essential for reliable structural analysis and crashworthiness assessment in automotive engineering as vehicle structures and safety-critical components experience a wide range of loading conditions, from quasi-static deformation during forming and durability events to high strain-rate loading during crash and impact scenarios. Conventional material characterization approaches rely on extensive experimental testing to generate strain-rate dependent constitutive data, including specialized high strain-rate techniques that are costly, time intensive, and require dedicated infrastructure, which often limits the availability of comprehensive material data during early vehicle development phases and supplier evaluation. This paper presents a data-driven methodology for predicting strain-rate dependent stress–strain behavior of automotive steels using limited experimental input data. The proposed approach integrates physically meaningful material properties with a machine-learning framework to construct a generalized stress prediction model that remains consistent with classical material mechanics principles. Fundamental parameters governing material behavior, including strain, strain rate, yield stress, density, Poisson’s ratio, and elongation limit, are used as inputs to capture the combined influence of deformation state, loading rate, and intrinsic material characteristics. A Random Forest regression algorithm is employed to model nonlinear relationships without relying on predefined analytical hardening or rate-sensitivity formulations. The methodology is developed and validated using experimentally obtained stress–strain data from multiple automotive steel grades under quasi-static and dynamic loading conditions, and model performance is evaluated through correlation analysis between predicted and experimental stress responses across the full strain range. The results demonstrate strong agreement with experimental observations and robust generalization capability across different materials and strain-rate regimes, with minor deviations observed at very high strain levels attributed to limited data density near fracture conditions. The proposed framework significantly reduces dependence on extensive physical testing while maintaining accurate representation of material behavior, providing a practical and efficient alternative for material characterization that supports faster material selection, reduced testing effort, and improved robustness of automotive computer-aided engineering simulations.
Shedolkar, Pravinkumar, Dudhewar, Swapnil, Shukla, Anurag, Mhaskar, Dnyaneshwar, Chavan, Avinash, Kakade, Ajit
This specification covers a maraging steel in the form of welding wire.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a nitriding grade of premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a corrosion-resistant steel in the form of investment castings, solution and precipitation heat treated to 150 ksi (1034 MPa) tensile strength.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a premium aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
AMS E Carbon and Low Alloy Steels Committee
This study investigates the creep response of the high-temperature titanium alloy Ti-1100 over a temperature range of 550-700 °C under applied stresses varying from 150 to 450 MPa. Under different combinations of stress and temperature, the creep rate, stress exponent, and activation energy for creep were determined using the Arrhenius relationship, while the corresponding creep characteristics and microstructural changes were examined through optical microscopy (OM), electron backscatter diffraction (EBSD), and transmission electron microscopy (TEM). The findings indicate that an alloy is highly sensitive to temperatures and stresses when subjected to long-term creep. At the temperature of 550-700 °C, the Ti-1100 alloy has relatively high creep activation energy when subjected to an applied stress of 300 MPa. For the Ti-1100 alloy, the stress exponent was determined to be 5.33 within the stress interval of 150-450 MPa at 600 °C. When considered alongside the observed microstructural characteristics, this result indicates that dislocation climb serves as the primary mechanism controlling creep during prolonged exposure. Within the investigated temperature and stress window, creep deformation in Ti-1100 gives rise to localized regions with elevated residual stress, and this tendency becomes more pronounced as both temperature and applied stress increase. These areas are likely to grow and evolve into microcracks, thus contributing to the microstructural instability of the alloy.
Yongquan, Yang, Lihui, Yang, Feng, Du, Baohui, Zhu, Xiaochen, Hu, Lihua, Shen, Jianfeng, Li, Shaofu, Kang
To address the urgent need for high-performance self-lubricating ceramic materials for rolling bearings under high-speed operating conditions in the aerospace sector, this study employs Si3N4 as the matrix and incorporates nano lignin and graphene nanoplatelets (GNPs) to develop a self-lubricating composite ceramic system. This paper systematically studies the tribological characteristics and wear mechanisms of the composites. The results indicate that nano lignin undergoes pyrolysis during sintering, forming nitrogen-doped graphene quantum dots (N-GQDs). These structures are uniformly distributed at grain boundaries and participate in the formation of a lubricating film during the friction process, thereby significantly improving the material’s friction and wear properties. Under the special conditions (10 N, 1000 r/min), the composite material exhibited optimal tribological performance when the nano-lignin content was 2 wt.%, The friction coefficient decreased to 0.22 and a significant decrease in wear rate, demonstrating excellent friction- reducing and wear-resistant effects. In contrast, the introduction of GNPs failed to effectively improve friction performance, which may be attributed to their poor dispersion in the matrix and weak interfacial bonding. Mechanistic analysis indicates that during friction, Si N hydrolyzes to form SiO, which, together with the metal transfer layer and N-GQDs, forms a composite lubricating film; under shear stress, the N-GQDs undergo oriented alignment, reducing interfacial shear strength and achieving a synergistic effect of friction reduction and wear resistance. This study gives a new perspective into the application of biomass-derived lubricating phases in high- performance ceramics.
Chen, Wei, Zhao, Wenzhuo, Zhou, Ao, Li, Yetong, Wang, Chao, Yang, Yongqiang, Lou, Rui
Aircraft skin is a critical external structural component that provides aerodynamic profile, sustains and transfers aerodynamic loads, and protects internal systems from harsh environments. High machining precision is essential to ensure assembly accuracy and flight performance. However, large scale thin walled skin components are prone to significant machining deformation due to their low stiffness. Traditional deformation control methods, which relying heavily on experiments and full-process simulations, are inefficient and costly for industrial applications. To address this issue, this paper establishes a correlation model among machining parameters, residual stress, equivalent bending moment, and machining deformation. Single-factor experiments are conducted to reveal the effects of spindle speed, feed rate, and cutting depth on surface residual stress. Based on plate-shell theory, the relationship between residual stress and equivalent bending moment is established. The quantitative relationship between equivalent bending moment and machining deformation of the skin is obtained via finite element simulation modeling. Finally, a deformation control strategy for the skin during finish machining is established by optimizing the cutting depth. Experimental results show that after parameter optimization, the overall machining deformation of the 5A06 aluminum alloy skin is reduced by 81%, and the maximum deformation is controlled within 0.17 mm, which fully meets the aeronautical assembly requirements. This work provides an efficient and low-cost process optimization strategy for the machining deformation control of large weak-stiffness thin-walled components.
Chen, Shu-Guang, Wang, Jing-Kai, Wu, Chao, Wang, Tian-Rui, Yuan, Hao
To prepare reliable thick aluminum alloy tailor welded blanks for cryogenic forming, 2219 aluminum alloy friction tailor welded blanks that has the thickness of 12 mm were selected as the research object in our study. Vickers hardness tests were employed to clarify the property distribution across the weld cross-section. Room temperature uniaxial tensile tests have been used to reveal through- thickness deformation behavior under tensile loading. The mechanical tests at room and cryogenic temperatures were employed to investigate the effects of welding parameters of the friction tailor welded blanks on the mechanical properties, and evaluate the cryogenic formability of the welded blanks. Results show that the single-sided FSW specimens exhibit decreased hardness values from the top to the bottom surface, causing more severe deformation in bottom region and macroscopic bending under tension stress condition. In contrast, the double-sided FSW specimens exhibit a more uniform hardness distribution across the weld cross-section, resulting in nearly symmetric deformation and no significant bending. Lower welding speeds combined with higher rotational speeds significantly improved the ductility of the tailor welded blanks. The optimal welding parameters are identified as 200 mm/min and 800 rpm, showing a 321.1 MPa tensile strength and a 22.2% elongation, at room temperature after water quenching and solution treatment. These values increase to 385.5 MPa and 33.5% at liquid nitrogen temperature, showing a more than 20% enhancement in strength and around 50% enhancement in ductility, indicating excellent formability. This study offers a reliable material and process basis for the integrally forming of ultra-large components.
Liu, Hanyu, Yang, Guang, Zhang, Zhichao, Li, Yajun, Hu, Lan, Fan, Xiaobo
To improve the thermal shock resistance of the shell steel, a Cr coating was deposited on its surface using arc ion plating technology. The protective capability of the Cr coating on the shell steel at 900 °C following a water-cooling cycle was investigated. Automatic scratch tester, scanning electron microscopy (SEM), X-ray diffraction (XRD), and energy-dispersive spectroscopy (EDS) were employed to characterize adhesion to the substrate, the microstructure, phase composition, and elemental composition of the shell steel and the Cr coating. The results indicate that the adhesion strength of the Cr coating is approximately 26.21 N, which is about 20.16% lower than the 32.83 N adhesion strength of the original Cr coating. At 900 °C, Fe₃O₄ and Fe₂O₄ form on the surface of the shell-and-tube steel. The oxide film exhibits cracking, peeling, and thermal fatigue, while oxidation defects accumulate within the steel, accompanied by significant precipitation of Ni. A dense Cr₂O₃ oxide film formed on the surface of the Cr coating, releasing thermal stress in the form of grid-like cracks. Under 10× magnification, no oxidation defects were observed within the Cr coating, and Fe from the substrate did not diffuse into the Cr coating; Under 100× magnification, the Cr coating exhibits fewer oxygen channels than the steel tube body. Oxygen is concentrated within these channels, and the Cr coating demonstrates significant resistance to thermal fatigue, providing markedly superior protection against thermal shock compared to the steel tube body.
Sun, Huixian, Lu, Xudong, Zhang, Rui, Guo, Cean
Achieving energy efficiency and high surface quality in the turning of hard-to-machine materials such as AISI 4340 steel requires effective decision-making frameworks. While single-objective optimization techniques are widely reported in the literature, comparative studies evaluating the consistency and reliability of multi-criteria decision-making (MCDM) methods remain limited. This study considers different machining conditions, including cooling strategies, cutting speed, and feed rate, and evaluates multiple performance indicators, namely tool wear, surface roughness, sound pressure level, and current consumption, using evaluation based on distance from average solution (EDAS), complex proportional assessment (COPRAS), grey relational analysis (GRA), weighted aggregated sum product assessment (WASPAS), and VlseKriterijumska Optimizacija I Kompromisno Resenje (VIKOR) methods. Objective criterion weights were determined using the criteria importance through intercriteria correlation (CRITIC) method. All five MCDM methods consistently identified Experiment 8 (nanofluid-assisted minimum quantity lubrication [nano-MQL], 150 m/min cutting speed, and 0.10 mm/rev feed rate) as the optimal parameter combination. This condition achieved the lowest surface roughness (0.81 μm), minimum tool wear (0.150 mm), lowest sound pressure level (88.1 dB), and minimum current consumption (4.18 A) among all experimental trials. The consistency of the ranking results confirms the robustness and reliability of the proposed decision-making framework for energy-efficient machining applications.
Toprak, İnayet Burcu, Fedai, Yusuf
The face milling process for hardened steels used in die and mold manufacturing involves precise parameter settings to achieve high-quality surfaces with high productivity. However, due to the nonlinear relationship between the machining parameters, it becomes challenging to optimize the machining process. This paper focuses on optimizing the face milling parameters for the DIN 2714 hardened steel by employing experimental approaches and AI-based modeling techniques. Taguchi’s L9 orthogonal array-based design of experiments with machining parameters of depth of cut, cutting speed, feed rate, and step-over is employed for the optimization. The material removal rate (MRR) and surface roughness (Ra) were considered as output responses. The results showed that surface roughness is significantly affected by cutting speed, while depth of cut primarily controls MRR. To improve the precision in predicting the output responses, two artificial intelligence (AI) based intelligent models were developed using hybrid modeling techniques—namely, PSO-FIS and GA-FIS. The experimental results demonstrated that the GA-FIS model was accurate in predicting the output response for surface roughness (Ra), with a lower error value (0.0162 μm), while the PSO-FIS model was accurate in predicting MRR with a high R2 value (0.9997), proving that fuzzy modeling techniques can be effectively used to optimize machining operations with high precision.
Tripathy, Chitta Ranjan, Moudgil, Prince Kumar, Katyayn, Arvind, Kumar, Aman
This specification covers an aluminum alloy in the form of sheet and plate 0.020 to 2.000 inches (0.51 to 50.80 mm), inclusive, in nominal thickness, supplied in the annealed (-O) condition. When specified, product shall be supplied in the “as fabricated” (-F) temper (see 8.6).
AMS D Nonferrous Alloys Committee
This specification covers an aluminum alloy in the form of sheet less than 0.250 inch (6.35 mm) thick (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a titanium alloy in the form of bars and hand forgings up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides and forging stock of any size. Bar over 6.000 inches (152.40 mm) in nominal thickness has a maximum cross-sectional area of 288 square inches (1858 square cm). Hand forgings with nominal thickness over 6.000 inches (152.40 mm) have a maximum cross-sectional area of 79 square inches (509 square cm) (see 8.7).
AMS G Titanium and Refractory Metals Committee
This specification defines the requirements for in-process and temporary marking material used on nickel, iron, cobalt, and titanium-based turbine engine components during processing or manufacture. Control is required as marking material may contain deleterious or low melting point elements that could negatively affect performance.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of bars, wire, and forgings up through 4.000 inches (101.60 mm), inclusive, in diameter or least distance between parallel sides and forging stock of any size (see 8.6).
AMS G Titanium and Refractory Metals Committee
Metastable β-titanium alloys have attracted considerable interest for structural applications, owing to their superior specific strength and the ability to obtain enhanced ductility through phase transformations induced by deformation. Nevertheless, in recently developed Ti-Zr-Al-V alloy systems, the interactions among dislocation slip, strain-induced martensitic transformation, and the consequent work-hardening response remains largely unclear. Under room-temperature uniaxial tension, this work systematically investigates how the microstructure evolves and how the alloy deforms for a metastable β-type Ti-42Zr-12Al-4V (at.%) alloy. To track the progression of strain-induced α″ martensite and dislocation activity across varying strain levels, techniques including quasi-in-situ scanning electron microscopy (SEM) and electron backscatter diffraction (EBSD), transmission electron microscopy (TEM), and focused ion beam (FIB) were employed. Findings indicate that the dominant strengthening mechanism stems from the strain-induced α″ martensite blocking dislocation motion, alongside dislocation cross-slip. Although the martensite volume fraction rises with increasing strain, its growth rate diminishes at higher strains. The martensite and the β matrix exhibited a clear Burgers-type orientation relationship, namely [001]α″//[110]β. Moreover, the appearance of martensite inside both primary and secondary slip bands generates a dynamic Hall-Petch effect, which reduces the dislocation mean free path and thereby supports continued strain hardening. These results provide deeper insight into the transformation-induced plasticity (TRIP)-assisted deformation mechanisms active in β-type titanium alloys and could guide the development of strong yet ductile materials.
Zhang, Fuen, Hu, Zhuoqian, Luan, Baifeng
Real-time monitoring of metal wear debris in lubricating oil is crucial for accurately assessing aerospace equipment health and preventing catastrophic mechanical failures. Although three-coil differential inductive sensors are widely used due to their high sensitivity and robust structure, their detection performance inevitably degrades under the influence of multi-physics coupling effects inherent in complex industrial environments. Existing analytical models were primarily limited to single electromagnetic field simulations, failing to capture the intricate electromagnetic-thermal-mechanical interactions, which reduced analytical accuracy and hindered the optimization of sensor designs for extreme conditions. To overcome these challenges, this study established a comprehensive parametric simulation model to conduct a rigorous electromagnetic-thermal-mechanical coupled analysis of the differential sensor. Specifically, the research analyzed the underlying mechanisms by which wide temperature variations from -55 °C to 200 °C and specific debris kinematics exert varying degrees of influence on the induced voltage. Quantitative results indicated that both the isolated thermal and mechanical fields altered the voltage by a maximum of 0.649%, demonstrating that the sensor maintains a relatively stable response across extreme thermal gradients. Furthermore, the analysis revealed that increased debris velocity decreased the induced voltage amplitude due to the intensified motion-induced eddy current effects. Notably, in complex multiple debris scenarios, the strong dominant signals generated by ferromagnetic wear debris severely masked the weaker responses from non-ferromagnetic ones, indicating a substantial missed detection risk under mixed contamination conditions. Ultimately, this research successfully filled the critical simulation gap for evaluating these sensors under multi-physics coupling, providing robust theoretical guidance for their reliable deployment in complex industrial applications.
Shi, Xinfa, Duan, Chenhao, Zhen, Huanyi, Zhao, Yihe, Li, Min, Wang, Xiaozhang, Zhang, Qing, Li, Zhikang, Zhao, Libo
This specification covers a premium aircraft-quality, corrosion-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and extrusions 7.00 inches (177.8 mm) and under in nominal diameter or least distance between parallel sides and stock of any size for forging, flash-welded rings, or extruding.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a titanium alloy in the form of cold-rolled sheet and strip up to 0.100 inch (2.540 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
AMS E Carbon and Low Alloy Steels Committee
This specification covers a titanium alloy in the form of hot-rolled sheet and strip up to 0.165 inch (4.20 mm), inclusive, in thickness (see 8.6).
AMS G Titanium and Refractory Metals Committee
This specification covers a gold-palladium-nickel alloy in the form of wire, rod, sheet, strip, foil, pig, powder, shot, chips, preforms, and a viscous mixture (paste) of the powder in a suitable binder.
AMS F Corrosion and Heat Resistant Alloys Committee
The information and data contained in this SAE Information Report are intended as a guide in the selection of steel types and grades for various purposes. Consideration of the individual types of steel is preceded by a discussion of the factors affecting steel properties and characteristics. SAE J4xx steels are generally purchased on the basis of chemical composition requirements (SAE J403, SAE J404, and SAE J405). High-strength, low-alloy (HSLA) steels (SAE J1392 and SAE J1442) are generally purchased on the basis of mechanical properties; different chemical compositions are used to achieve the specified mechanical properties. Because these steels are characterized by their special mechanical properties obtained in the as-rolled condition, they are not intended for any heat treatment by the purchaser either before, during, or after fabrication. In many instances, as in the case of steels listed in SAE J1268 and SAE J1868, hardenability is also a specification requirement. This information report can be used as a reference for determining the general characteristics and applications of commonly used SAE steels. The use of the typical heat treatments listed in Tables 1 through 7 is recommended. These and other heat treatments commonly used on steel are briefly described at the end of this section.
Metals Technical Committee
This specification covers a corrosion-resistant steel in the form of two types of aircraft tubing.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers one type of nickel-aluminum bronze in the form of extruded bars, rods, and tubes up to 4.00 inches (101.6 mm) in nominal diameter, distance between parallel sides, or wall thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers one type of bronze in the form of round wire 0.500 inch (12.70 mm) and under in nominal diameter (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel product in the solution and precipitation heat treated (H1075) condition, 4 inches (102 mm) and under in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
For a company concerned with end-of-life automotive recycling, it makes sense to have a “metal” attitude. INDRA's slogan - Car destruction and automotive recycling specialist since 1985 - certainly fits the bill. INDRA, a subsidiary of The Future is Neutral (itself a subsidiary of the Renault Group and SUEZ), has been around for over 40 years and was on hand at the massive Automechanika Frankfurt expo, an event focused on the automotive aftermarket, in early September to promote Design For Recycling (DFR) and more options for recycling old cars. Since automobiles are at least 85% recyclable and at least 95% recoverable, INDRA said, it can fairly be thought of as a “main resource.” The problem is that new vehicles usually contain less than 30% recycled materials, which is why the company has a mission to collect and dismantle end-of-life vehicles and then reuse, revalue, and recycle their components and materials. With vehicle complexity increasing, older vehicles sticking around longer, and new regulations coming into effect, EVL services are in high demand.
Blanco, Sebastian
This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers an aluminum alloy in the form of sheet and plate up to 2.000 inches (50.80 mm), inclusive, in thickness. (see 8.5)
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of plate up to 3.00 inches (76.2 mm), inclusive, in nominal thickness.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a premium aircraft-quality steel in the form of bars, forgings, mechanical tubing, flash-welded rings up through 10.000 inches (254.00 mm), inclusive, in diameter or least distance between parallel sides, and stock of any size for forging or flash-welded rings.
AMS E Carbon and Low Alloy Steels Committee
The persistent rate of accidents and fatalities involving legacy tactical military vehicles underscores a critical need for Enhanced Situational Awareness (ESA) technologies. However, the prohibitive cost and lengthy development cycles associated with full MIL-STD ruggedization often prevent these safety systems from reaching the in-service non-combat vehicles with limited driver visibility. This paper suggests a strategic shift in procurement policy: The adoption of relaxed ruggedization standards for vehicles operating in non-combat, administrative, and training roles. By deriving requirements from high-stress commercial sectors— such as heavy mining, steel production, and NASCAR racing—the military can utilize electronics designed for "extreme industrial" rather than "battlefield" environments. The principal objectives of this relaxation is cost reduction, lowering the barrier to entry and increasing the likelihood of ESA deployment across the legacy fleet. Furthermore, this approach aligns with Modular Open Systems Approach (MOSA) principles by enabling the integration of non-proprietary commercial devices. Utilizing these accessible technologies on legacy platforms creates a real-world testbed to evaluate technological advances rapidly. These insights can then inform and accelerate the development of future MIL-STD systems for combat vehicles, effectively shortening the traditional development life cycle while prioritizing the immediate enhanced protection of service member lives.
Pilgrim, Robert A., Brown, Roy C.
This specification covers an aluminum alloy in the form of sheet and plate 0.008 to 4.000 inches (0.20 to 101.6 mm), inclusive, in thickness (see 8.5).
AMS D Nonferrous Alloys Committee
This specification covers a corrosion-resistant steel in the form of investment castings.
AMS F Corrosion and Heat Resistant Alloys Committee
This specification covers a corrosion- and heat-resistant cobalt-chromium-molybdenum alloy in the form of bars 2.500 to 4.000 inches (63.50 to 101.60 mm) inclusive, diameter or least distance between parallel sides.
AMS F Corrosion and Heat Resistant Alloys Committee
G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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