Browse Topic: Fuel systems
A bench was developed with the aim of making it possible to test direct injection fuel system of low-displacement engines (up to 2,000cc) outside of a conventional test bench. It has adjustable supports that make it possible to install various engines of different manufacturers. In addition, the bench has features an electric motor, an external oil pumping system and a programmable ECU. These accessory systems were necessary because the engine for which the bench was initially designed has undergone various adaptations that required external systems such as those mentioned above. The project was designed to provide great ease, agility and low manufacturing costs, so the entire bench chassis was manufactured using just one standardized steel profile that is easily found on the market. Still about manufacturing, the concept of the prototype was also developed around the need for it to be compact and easy to transport so that the tests could be carried out in different environments in an
In highly populated countries two-wheelers are the most convenient mode of transportation. But at the same time, these vehicles consume more fuel and produces emissions in urban driving. This work is aimed at developing a hybrid two-wheeler for reducing fuel consumption and emissions by incorporating electric vehicle technology in a conventional two-wheeler. The hybrid electric scooter (HES) made consisted of an electric hub motor in the front wheel as the prime mover for the electrical system. The powertrain of the HES was built using a parallel hybrid structure. The electric system is engaged during startup, low speeds, and idling, with a simple switch facilitating the transition between electric and fuel systems. The HES was fabricated and tested through trial runs in various operating modes. Before conversion to a hybrid system, the two-wheeler achieved a mileage of 34 km/liter. After conversion, the combined power sources resulted in an overall mileage of 55 km. It was observed
Slosh, a phenomenon occurring in a vehicle's tank during movement, significantly contributes to noise and vibration, often exceeding idle levels. Existing methods for evaluating NVH performance of fuel tanks primarily rely on subjective assessment, highlighting the need for a quantifiable approach to address this dynamic noise. This paper introduces a hybrid methodology to standardize the slosh phenomenon by establishing vehicle-level acceleration, braking, and driving profiles. Noise and vibration data capture, combined with defined boundary conditions, categorizes slosh noise into Impact and Roll noise, differentiated by distinct driving profiles and frequency content. Vehicle level performance is then cascaded down to subsystem level. A dedicated test rig is designed that replicates these conditions at the subsystem level where vehicle speed and braking profiles are translated into rig-specific acceleration and deceleration profiles, enabling consistent data capture for correlation
Hypersonic propulsion would allow for air travel at speeds of Mach 6 to 17, or more than 4,600 to 13,000 miles per hour, and has applications in commercial and space travel
The future of space travel is seemingly changing by the day and a Coventry University academic is doing his bit to stay at the front of the space race
This SAE Standard encompasses the recommended minimum requirements for non-metallic tubing and/or combinations of metallic tubing to non-metallic tubing assemblies manufactured as liquid- and/or vapor-carrying systems designed for use in gasoline, alcohol blends with gasoline, or diesel fuel systems. This SAE Standard is intended to cover tubing assemblies for any portion of a fuel system which operates above −40 °C (−40 °F) and below 115 °C (239 °F), and up to a maximum working gage pressure of 690 kPa (100 psig). The peak intermittent temperature is 115 °C (239 °F). For long-term continuous usage, the temperature shall not exceed 90 °C (194 °F). It should be noted that temperature extremes can affect assemblies in various manners and every effort must be made to determine the operating temperature to which a specific fuel line assembly will be exposed, and design accordingly. The applicable SAE standards should be referenced when designing liquid-carrying and/or vapor-carrying
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