Browse Topic: Coating processes

Items (493)
AMS120425-1
A-10 Aircraft Oxygen Equipment Committee
AIR120425-1
A-10 Aircraft Oxygen Equipment Committee
Verifying large alternate product code for an AIR document
A-10 Aircraft Oxygen Equipment Committee
Maintaining the operational readiness of military helicopters demands repair solutions that are fast, reliable, and adaptable. This paper presents the integration of Gamma Alloys' advanced metal matrix composites (MMCs) into additive manufacturing (AM) techniques - specifically Cold Spray and Friction Stir Additive Manufacturing (FSAM) - as a transformative approach to helicopter repair and replace for the US Army.
Peabody, MicahHarrigan, William
This specification covers tungsten carbide-cobalt chrome in the form of powder.
AMS F Corrosion Heat Resistant Alloys Committee
This SAE Recommended Practice sets forth a method for determining the compatibility of automotive sealers with cathodic electrocoat primer.
Materials, Processes and Parts Council
The continual replacement of the bleed band actuator caused a supply shortage resulting in production work stoppage. A re-design effort restored the actuator housing through rework modification of a sleeve repair. The re-design substantion is presented along with the qualification test and manufacturing process. Significant value engineering savings and increased supply readiness resulted from the re-design effort for the U. S. Army. However, the re-designed sleeved actuator housing became costly and inefficient over time and subsequently stopped. The overhaul discrepancy is still present on the newer T55 gas turbine engine model. A review of new repair technology available identified another solution that does not generate hazardous industrial waste. That solution is cold spray technology. Cold spray solid state additive technology is evaluated for re-design of the housing as comparison to the existing sleeve re-design. Cost decrease and manufacturing efficiency increase are both a result from this evaluation. Two cold spray powders presented are options for the re-design housing. While both powders provide a better overall solution to the sleeve re-design, the cold spray hard coat powder appears to provide improved wear resistance, e.g. 20 times better than hexavalent chrome plating.
Cass, Wesley
Researchers have shown how to coat glass and plastic with porous titanium dioxide. The fabrication process is straightforward, the materials are cheap, and the ceramic’s gas sensing performance is considerably improved compared with current devices.
This specification covers tungsten carbide-cobalt in the form of powder.
AMS F Corrosion Heat Resistant Alloys Committee
This specification covers tungsten carbide-cobalt chrome in the form of powder.
AMS F Corrosion Heat Resistant Alloys Committee
Experimental Study on Tool Wear and Cutting Temperature during Machining of Nimonic C-263 and Waspaloy Based on Taguchi Method and Response Surface Methodology2019-28-014410/11/2019
Nickel based materials of Nimonic C-263 and Waspaloy are used nowadays for aerospace applications owing to its superior strength properties that are maintained at a higher temperature. Tool wear and cutting temperature in the vicinity of cutting edge are two essential machinability characteristics for any cutting tool. In this regard, this study is pursued to examine the influence of factors on measuring of tool wear (Vba) and cutting temperature (Ts) during dry machining of two alloys studied experimentally based on Taguchi method and response surface methodology. Taguchi’s L16 orthogonal array is used to design the experiment and a PVD (TiAlN), CVD (TiN/Al2O3/TiCN) coated carbide inserts are used on turning of two alloys. The factor effect on output responses are studied using analysis of variance, empirical models, and responses surface 3D plots. To minimize the response and to convert into one single optimum level, responses surface desirability function approach is applied. The results show that progress of flank wear associated with Waspaloy is faster that of Nimonic C-263 due to high cutting temperature for Waspaloy that of Nimonic C-263. Abrasion is active wear mechanism for both the alloys with the investigated cutting parameters. Also, plastic deformation and mechanical fracture are observed for both inserts on turning of two alloys. In overall, PVD tool brings down the cutting temperature (10% for Nimonic C-263 and 4% for waspaloy), and flank wear land (31% for Nimonic C-263 and 41% for waspaloy) than that of CVD tool due to its superior tribological properties.
Kannan, Vetri VelmuruganKannan, VenkatesanSundararajan, Devendiran
The aluminum alloy Al7075 is commonly used in aircraft industry due to its high mechanical resistance to weight ratio. Nevertheless when the structure is being serviced upon the severe environmental conditions or loads degradation mechanisms could often been found in the material. To improve its behavior the cold spray process with various titanium powders (e.g. CP Ti, Ti-64) deposited onto Al7075 was investigated. The spraying of angular titanium powder was performed in the presence of nitrogen and helium supplied at process parameters (temperature, pressure), which were the maximum values attainable by the CS system used. The deposits were sprayed while maintaining a standoff distance in the range from 20 to 100 mm increased by 10 mm. The experimental data indicated that the deposition efficiency had increased significantly with increasing standoff distance. The coating porosity first decreased to minimum 0.6% and then increased significantly to 9.8%. The mechanical properties of the coatings reached the highest values when the porosity was minimum. No new phases were reported in the cold sprayed titanium coatings when compared with the starting feedstock. The same process parameters were transferred to Ti- 6Al-4V coral like powder deposition process. The shear strength between Ti coating material and Al7075 substrate was measured. Additionally the tensile strength of the deposit only, previously disintegrated from the substrate, was checked out. The data obtained indicate that the consolidation of Ti powder with Al7075 substrate made by cold spray could be served for both: materials integration and building a component by materials disintegration, where Al substrate is removed on spraying and machining; and simply used as a technological support for additive manufacturing of a self-standing real life component.
Sienicki, JaroslawŻórawski, Wojciech
The Structures Division at the Naval Air Systems Command (NAVAIR) continues to support capital investment in enabling technologies for sustainment of our aircraft which will lower total life cycle costs, ensure safety, and increase operational readiness. This paper presents a general overview of the major improvements which have been made in the area of Structural Health and Usage Management (SHUM), including: usage severity monitoring via regime recognition (RR), gross weight and center of gravity (GW/CG) estimation, local/global damage detection, environmental effects monitoring, damage alleviation, prognostication, and individual asset/component tracking (IAT). Advances in structural analyses have been made in the accuracy of predicted rotorcraft loads using coupled rotor and fuselage interactions. Innovative approaches to fatigue testing at both the component and full scale airframe levels will allow for more accurate introduction of vibratory loading content from operation, reveal failure modes, and improve fatigue life predictions. Additive manufacturing (AM) of fly-away aircraft parts and the standardization of cold spray repair applications present unique qualification challenges and benefits to the warfighter.
Semidey, RobertoGlucksman-Glaser, MarkPhan, Nam
The U.S. Army overhauls aircraft weapon system (AH-64, CH-47, UH-60) and associated components. Significant damage, corrosion, and wear are a main cause of component discrepancies. Typical issues with current fusion weld/thermal spray repair is high distortion and a large heat affected zone (HAZ) to an operational aviation component. These repairs often require large and complex fixtures and processes to stabilize the component during the repair process. The additive repair / manufacture (AR/M) has shown to give a very small HAZ and footprint not requiring the use of complex fixtures. This paper outlines the approach taken to develop and qualify AR/M necessary for airworthiness qualification. Two areas that are researched are laser additive manufacturing (LAM) powder fed systems (or directed energy deposition (DED)) and cold spray additive manufacturing. Establishment of mechanical and metallurgical properties of AR/M are presented. Significant return on investment is being shown using these AR/M repair processes.
Cass, Wesley
Within a gasoline direct injection (GDI) engine, the impingement of fuel droplet on substrates induces various problems such as particular matter emission, oil dilution and abnormal combustion. Therefore, in order to solve these problems, it is urgent to have a clear understanding of the impingement behavior of fuel droplet impacting on substrates. Most previous studies have focused on the impingement of either water droplet on dry solid surface or the impinging droplet on the liquid film of the same type of liquid, while little research has been conducted on the impingement of fuel droplet on relevant substrates existing in GDI engines. The impingement of fuel droplet with higher Weber number on dry surface, fuel film and oil film with different thickness and viscosity were investigated experimentally. Results show that fuel droplet impacting on dry wall is easy to be deposited to form a fuel film. The fuel film attached to the wall is the main reason for the splash. The thickness of fuel film adhered to the dry wall affects the splash degree of secondary droplets. As the fuel droplet impacts on pure oil film of different thickness and viscosity, there is no secondary droplets spattering into the air. After collision, the fuel droplet together with the jet deposits into the oil film causes the oil dilution.
Peng, ZhenshanPei, YiqiangQin, JingLu, LiliZhu, Qingyang
Electric double layer capacitors prepared with polyvinyl alcohol and multi-walled carbon nanotubes2018-36-03139/3/2018
Portable electronics, wearables, electric vehicles and solar cells are sectors in increasingly development which include innovation and miniaturization of the devices. In this scenario, the development of smaller and lightweight energy storage devices, which store more energy, is required. Besides, it is desirable for these devices to be environmentally friendly to minimize pollution. In an attempt to meet these requirements, this work purposes the development and the characterization of nanofibers-based electrode composed of Polyvinyl alcohol (PVA) and multi-walled carbon nanotubes (MWCNT) for electric double layer capacitors (ELCDs) devices with aqueous electrolyte. This composite has been prepared by electrospinning technique and consolidate an electrical conductive and high-surface material electrode. After that, the PVA/MWCNT electrode was assembled in coin cell device with Sodium Sulfate (Na2SO4) electrolyte for electrochemical characterization. The characterization results showed that EDLCs devices present specific capacitance of ∼4.8 Fg-1, energy density of ∼0.1 Wh kg-1, power density of ∼600W kg-, fast charge transfer at electrode/electrolyte interface and high lifetime All these results encourage further development on PVA/MWCNT materials as electrode for EDLCs and Li-Air batteries devices. This new generation of devices are opening niches of applications on multi billionaire markets from communication to transport.
Real, Carla Giselle MartinsVicentini, RafaelNunes, Willian GonçalvesBoas, Otávio VilasCosta, Lenon HenriqueSoares, Davi MarceloZanin, Hudson
This paper was prepared to support supersession of MIL-S-8879C with Screw Thread Conformity Task Force selected industry standard AS8879C, published by the Society of Automotive Engineers (SAE). Other documentation changes will be covered by separate papers. Separate papers are anticipated for thread gaging issues, and thread gage calibration procedures. The STC-TF decided that the thread design standard needed to be completed before thread gage definition could be addressed. Thread gage definition has to be known before calibration procedures can be addressed.
E-25 General Standards for Aerospace and Propulsion Systems
A Comparative Study on Machinability Characteristics in Dry Machining of Inconel X-750 Alloy Using Coated Carbide Inserts2018-28-00317/9/2018
Nickel based superalloys have a wide range of applications due to high mechanical strength at high temperatures, fracture toughness and resistance to corrosion. However, because of their outstanding properties, it is considered as the difficult to machine materials. Inconel alloy X-750 is used extensively in rocket-engine thrust chambers. Airframe applications include thrust reversers and hot-air ducting systems along with large pressure vessels are formed from Inconel alloy X-750. Moreover, the comparative analysis of machinability aspect using coated carbide inserts is reported few. The current study explains the machinability investigation on Inconel alloy X-750 superalloys using coated carbides. To collect the experimental data, the L16 experimental design plan is used to experiment with a machining length of 40 mm. Four level of cutting speed (70,120,170,220 m/min), feed rate (0.1, 0.15, 0.2, 0.25 mm/rev) and cutting depth (0.3, 0.4, 0.5, 0.6 mm) are the cutting/machining parameters used. Cutting Forces, surface roughness, flank and crater wear are considered as target functions. With the application of response surface, coupled with desirability analysis, the optimal levels of the combination are determined. With determined optimal levels, tool life study has been carried out to compare the effectiveness of cutting inserts. Finally, the ranges for best cutting conditions are proposed for serial industrial production.
Kannan, Vetri VelmuruganKannan, Venkatesan
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