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Training / Education
2015-10-05
The challenges associated with using composites as a replacement for aluminum reside primarily in the complex manufacturing processes and technologies for fabricating composite parts. The high cost of composites material and its manufacturing complexity have been inhibitors to the wide transfer of this technology to the non-aerospace market. The search for solutions to high manufacturing costs and efficient manufacturing processes have resulted in intense research by government, aerospace industry companies, and space agencies worldwide. This one day seminar will introduce participants to composites technologies that have applications beyond aerospace, including such markets as trucks, automobiles, and wind turbines.
Training / Education
2015-03-09
Through the years there has been a significant and increasing volume of fraudulent and counterfeit electronic parts entering the aerospace supply chain. Left undetected, these parts can pose significant performance, reliability, and safety risks. In response to these threats, the SAE AS6081 Counterfeit Electronic Parts Avoidance – Distributors standard was developed to provide uniform requirements, practices, and methods to mitigate the risk of electronics distributors purchasing and supplying these counterfeit electronic parts throughout the aerospace supply chain. This course will begin with a one-hour, pre-recorded session that covers background information on the proliferation of counterfeit electronics.
Training / Education
2014-12-15
This seminar introduces participants to all aspects of threaded fasteners including nomenclature, geometric considerations, metallurgy, material properties, applied stresses, and considerations for fatigue, corrosion, brittle fracture and temperature. Methods are developed for the analysis and design of bolted joints under axial and shear loads. Other topics include assembly practice and methods to control preload.
Event
2014-11-19
This session focuses on hardware not associated with the engine and drivetrain that supports the purpose of the vehicle such as suspensions, lighting, dampers, marine hulls, steering, vehicle frame, and heating and cooling systems.
Technical Paper
2014-11-11
Alessandro Franceschini, Emanuele Pellegrini, Raffaele Squarcini
Nowadays the challenge in design auxiliary device for automotive small engine is focused on the packaging reduction and on the increase of the performances. This requirements are in contrast to each other and in order to fulfil the project specifications, new and more refined design tools and procedures need to be developed. This paper presents a calculation loop developed by Pierburg Pump Technology Italy S.p.a. (PPT). It supports the design of a variable displacement oil pump component for engine applications. The work is focused on the fatigue life evaluation of a joint, which transmits the drive torque from the engine to the oil pump. The aim of the procedure is to calculate the onset of the surface fatigue phenomenon in the hexagonal joint which drives the oil pump, taking into account the axes misalignment and the flat to flat clearance. The study has involved several matters, experimental measures, CFD, MBA and FEM analyses. A calculation procedure has been set up in order to consider all the necessary loads applied on the joint.
Technical Paper
2014-11-11
T Manikandan, S Sarmadh Ameer, A Sivakumar, Samaraj Dhinagar
The proposed paper is on electrical energy conservation in a two wheeler. Electrical energy generation adds a maximum of 10% excess load torque on an engine and hence saving electrical energy would ultimately reduce the consumption of fuel. Load Control Module is a single intelligent device which is placed in between electrical energy generation and consumption. The Module controls and distributes energy to the corresponding loads depending on parameters like battery voltage, engine RPM, overhead light illumination levels and load usage time. The Module prioritizes battery charging for maintaining the life of the battery. The Module has a microcontroller and it is programmed with algorithm for prioritization and energy distribution with respect to input conditions. A vehicle fitted with the Load Control Module was tested in city driving cycle (CDC) condition as per ARAI (Automotive Research Association of India) standard and it was found that the electrical loading decreased to about 30% when compared to vehicle with uncontrolled loading.
Technical Paper
2014-11-11
T Manikandan, S Sarmadh Ameer, A Sivakumar, Davinder Kumar, R Venkatesan, VenkataKalyana Kumar
The proposed paper is on advanced vehicle information panel which shall display instant mileage zone in which the user is operating with inputs from engine crank sensor and vehicle speed sensor alone. And moreover, gear assistance and throttle assistance through visuals is provided. Mileage data for different engine loading at different Speeds is pre-calculated at standard conditions and fed into a micro-controller. In real time, the engine loading, by means of intelligent software, is sensed by engine crank sensor and based on the pre-fed value, the mileage zone of the vehicle at that particular instant is to be displayed using an information panel. Based on the relation between speed sensor and engine crank sensor when the vehicle is running, the gear in which the vehicle is running is to be calculated. For a vehicle running in a certain gear and in certain speed, the ideal engine loading and mileage zone is predefined. So when the user is riding in a certain gear with certain engine load, the micro controller compares that with the programmed data which is the ideal condition data, and assists the user, in case the rider is not riding the vehicle as per the ideal data, by gear up/down prompt or throttle up/down prompt by means of the said information panel.
Training / Education
2014-11-05
Through the years there has been a significant and increasing volume of fraudulent and counterfeit electronic parts entering the aerospace supply chain. Left undetected, these parts can pose significant performance, reliability, and safety risks. In response to these threats, the SAE AS6081 Counterfeit Electronic Parts Avoidance – Distributors standard was developed to provide uniform requirements, practices, and methods to mitigate the risk of electronics distributors purchasing and supplying these counterfeit electronic parts throughout the aerospace supply chain. This two-day seminar will begin with background information on the proliferation of counterfeit electronics and the development of a consensus standard for the procurement, detection, reporting, and disposition of these parts.
Training / Education
2014-11-04
Counterfeit electronic parts have been found in almost every sector of the electronics industry and continue to be an increasing threat to electronic hardware. This threat poses significant performance, reliability and safety risks. Aerospace industry organizations, in particular, must produce and continually improve safe and reliable products that meet or exceed customer and regulatory authority requirements. The SAE AS5553 standard was created in response to the significant and increasing volume of counterfeit electronic parts entering the aerospace supply chain and standardizes requirements, practices and methods for counterfeit parts risk mitigation.
Training / Education
2014-10-29
The requirements for producing an FAA approved replacement part can be daunting. Understanding the steps required in the FAA Parts Manufacturer Approval (PMA) process can greatly streamline the approval life-cycle and reduce unnecessary costs and delays, thereby shortening the time and cost to market. This course is designed for those organizations and individuals interested in designing and manufacturing replacement parts for civil aviation aircraft. This two-day course covers the crucial subjects and steps of the FAA-PMA approval process. The instructor will begin with an overview of the Federal Aviation Administration (FAA) organizational structure.
Technical Paper
2014-10-13
Robert H. Barbour, Robert Quigley, Avtar Panesar
Abstract Diesel powered vehicles have grown in popularity over the last 15 years due to the introduction of advanced, high pressure, direct injection fuel systems that enable improved emissions, power and a more desirable driving experience. However, such vehicles only perform optimally when the fuel system is in a clean condition. When deposits form inside the injector nozzle holes, a measurable deterioration in power is observed. The CEC F-98-08 Peugeot DW10 engine test was introduced in 2008 in order to evaluate the nozzle fouling propensity of fuels and the beneficial effect of deposit control additives. Papers have been published demonstrating such effects, in particular the propensity of zinc and biodiesel contaminants to cause injector fouling and the performance of additives in both deposit control (keep clean) and removal (clean-up) modes. While running such tests with an advanced, proprietary deposit control additive, both the fuel flow (kg/hr) and engine power (kW) measured with the additised fuel were higher than the corresponding measurements made at the start of test with clean injectors running on base fuel.
Technical Paper
2014-10-13
Yingyi Wen, Shunichi Oshima
Agitation torque associated with oil lubricant is one important factor of torque loss in bearings under sufficient lubricating conditions. So far, efforts on reducing agitation torque were taken mostly by means of conventional experimental trials. Aiming for speedy, low-cost development, a calculation program for predicting the amount of agitation torque and oil distribution tendency in rolling bearings has been developed using computational fluid dynamics (CFD) analysis. At first, since rolling bearings are axially symmetric, sector models of bearings were adopted. To verify the method, torque losses and oil quantities in ordinary-sized bearings have been measured. Calculated values based on sector models are qualitatively in good agreement with measured results. The difference between the absolute values of measured and calculated torque may be caused by the difference between the vertical model used in CFD analysis and the horizontal torque-testing rig used in measurement. To improve the accuracy, full models of the bearings have been developed and verified by experiment.
Technical Paper
2014-10-13
Markus Behringer, Pavlos Aleiferis, Dave OudeNijeweme, Paul Freeland
Abstract One of the latest advancements in injector technology is laser drilling of the nozzle holes. In this context, the spray formation and atomisation characteristics of gasoline, ethanol and 1-butanol were investigated for a 7-hole spark eroded (SE) injector and its ‘direct replacement’ Laser-drilled (LD) injector using optical techniques. In the first step of the optical investigation, high-speed spray imaging was performed in a quiescent injection chamber with global illumination using diffused Laser light. The images were statistically analyzed to obtain spray penetration, spray tip velocity and spray ‘cone’ angles. Furthermore, droplet sizing was undertaken using Phase Doppler Anemometry (PDA). A single spray plume was isolated for this analysis and measurements were obtained across the plume at a fixed distance from the nozzle exit. The droplet measurements were grouped into bins and maps were created showing droplet sizes and velocities against time and position during and post injection.
WIP Standard
2014-09-30
This SAE Aerospace Standard will cover airframe plain spherical bearings ustilizing a Copper Nickel Tin ball and a Corrosion Resistant Steel outer race for use between -65F and+350F.
WIP Standard
2014-09-30
The intent is to ballot this drawing package and then stabilize it.
WIP Standard
2014-09-30
This SAE Aerospace Standard will cover airframe plain spherical bearings ustilizing a Copper Nickel Tin ball and a Corrosion Resistant Steel outer race for use between -65F and+350F.
WIP Standard
2014-09-30
The intent is to ballot this drawing package and then stabilize it.
WIP Standard
2014-09-30
This document defines the method for voltage identification by the use of color-coded insulators at the base of the lamps. Table 1 shows the design volts and corresponding insulator colors. The part numbers shown are for example purposes only, as an option. Insulator colors are to be easily distinguishable as green, yellow, red, and white. Additional colors may be added by a revision process as required.
Standard
2014-09-30
This SAE Aerospace Standard (AS) specifies standardized gland design criteria and dimensions for static face seals for internal pressure and external pressure applications for aerospace hydraulic and pneumatic applications using the same size range as AS4716 and AS5857 where applicable. Some small diameter sizes are excluded because they are not practical. The glands have been specifically designed for applications using AS568 size elastomeric O-rings with related Class 2 tolerances at nominal system operating pressures up to 3000 psi (20 680 kPa) utilizing no anti-extrusion (backup) rings. While the gland dimensions herein have been designed for pressures up to 3000 psi (20 680 kPa) these glands may be used for higher pressures, but extra precautions need to be taken and testing should be performed to ensure to ensure integrity of performance. This specification covers the basic design criteria and recommendations for use with standard size elastomeric O-rings, however, these glands are also suitable for use with other elastomeric and polytetrafluoroethylene (PTFE) based seal geometries.
Viewing 1 to 30 of 15432

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