Browse Topic: Fuel sensors
Automotives are provided with a lot of intelligence that monitors, controls, actuates, and diagnose the various aspects of vehicle functionalities. One of the critical parameters required to monitor is Vehicle fuel level. Fuel level in the vehicle is a key input for engine performance, drivability, and fuel level indication in Instrumentation cluster for customer. Most economic and reliable fuel level sensor is resistive sensor with float. The purpose of this paper is to address the wrong fuel level indication in Vehicle level. Wrong fuel level indication may be due to malfunction of Instrumentation cluster signal input or Fuel level sensor function. To verify this, Instrumentation cluster is tested with HIL system instead of real time Fuel level sensor. By configuring the HIL module to analogue resistance channel, cluster is tested for fuel level bar indication. Fuel level sensor is tested by Vehicle level fuel calibration and exact issue is simulated. The failed fuel level sensor is stripped open for analysis and found resistance track length is not adequate, and it leans on the edge of the track due to vibrations. To address this issue, length of the resistance track is increased. When length is increased, the angle of the track changes and it implicates wrong fuel indication. Using this simulation, actions are taken in such a way that length and angle of the track modified to give correct resistance and indication. To rely on this actions, Camera enabled measuring systems is used to measure the length and angle of the resistance track. Corrected samples are taken for accelerated endurance test with the help of pressure cylinders setup and examined for action effectiveness. The details on failure simulation, action taken and validation for corrective samples are discussed in this paper.
Most automotive fuel systems use a Fuel Delivery Module (FDM) with components to filter and pump gasoline at a specified pressure and flow rate from the fuel tank to the engine. The FDM uses a reservoir assembly to maintain a fuel supply at the pump inlet and support components such as pressure regulators and/or limiters, filters, level sensor, and the electrical and hydraulic connections that pass through the tank. Current systems predominantly use passive electrical components such as brush pumps and resistive fuel level sensors that are independently connected to a voltage supply and body control module, respectively. The high flow levels of these systems require high-power pumps that may operate continuously at maximum speed conditions. Some newer systems may employ a voltage controller to modulate the pump supply voltage to discrete speeds depending on projected engine demand, and provide some improvement in power consumption.
This document is applicable to commercial and military aircraft fuel quantity indication systems. It is intended to give guidance for system design and installation. It describes key areas to be considered in the design of a modern fuel system, and builds upon experiences gained in the industry in the last 10 years.
A flex fuel engine is capable of operating efficiently on any combination of gasoline and ethanol. However, an engine combustion strategy must adapt quickly to a change in ethanol concentration after a refueling event in order to achieve optimum engine combustion. Typical control systems rely on an exhaust gas oxygen sensor (lambda) to measure changes in oxygen concentration following combustion. This feedback control approach can take five to ten minutes to detect the fuel change and correct the combustion strategy. This relatively long lag time could result in suboptimal engine performance such as a loss of engine power, engine knocking, poor cold start performance, unburned hydrocarbons, and high pollutant emissions. To counter this shortcoming, an on-board flex fuel sensor (FFS) was developed to enable a feed-forward control strategy. The FFS may be installed inline between the fuel tank and fuel injector and measure the fuel prior to it reaching the injector. The FFS sensor estimates the concentration of ethanol in the fuel in real-time using a correlation based on permittivity, conductivity, and temperature of the fuel flowing through the sensor. The FFS is specifically designed for the Brazilian market and is calibrated to measure the anhydrous ethanol and hydrous ethanol contained in gasohol and alcohol respectively. The sensor can accurately estimate the total ethanol concentration (anhydrous plus hydrous) within +/− five volume percent for any combination of gasohol and alcohol. The sensor can operate with a fuel temperature range of −40°C to 95°C. In addition, the FFS provides diagnostic capability and is able to identify and report water contamination to the engine control module.
Four new 2-cylinder 4-stroke concepts are displayed as design and fitted in vehicles. These four different concepts comprise a Modular Concept V2- and W3-cylinder a MotoGP / Superbike concept with 2 and 3 cylinders, a narrow angle V-engine and a Building Block System Commuter CVT engine. Each engine concept is designed to meet the different requirements of the four segments. Specific analysis and simulation concerning 1D thermodynamics, vehicle simulation and delivered performance and tractive force was done for each concept. The concepts are compared in the aspects of uniform rotation, inertia forces and moments, and the effect on performance by the pulse effects of the manifolded intake and exhaust systems. The Modular Concept contains an OHC engine with a wide range of displacements and commonality of many parts. Good versatility is obtained as the concepts can be applied for sport- or custom bikes. Also an advanced EMS with additional features is applied and a heated 3-way catalyst and air/fuel sensors are integrated to fulfill the most stringent emission regulations after the year 2006. The MotoGP / Superbike Concept has an advanced transmission position, which allows to design a very compact motorcycle size comparable to much smaller displacement bikes. The application of a pneumatic valve train allows for aggressive valve timing and high engine output. The concept is compared to engines with higher number of cylinders in terms of race competitiveness. The narrow-angle V-engine is a sportive and compact engine with newly developed mass balancing. The Commuter is a medium output design with a continuously variable transmission, featuring an extremely space-saving design
The Beechcraft Starship 1 is a completely new and exceptionally advanced airplane in many of its fundamental aspects. The development of this aircraft has presented a unique opportunity to apply advanced avionics architectural concepts. The system that evolved consists of an integrated array of over 70 electronic line replaceable units (LRU), organized to provide unprecedented levels of functional capability, fault tolerance, and configurability, as well as on-board diagnostic aids, and other features designed to enhance the safety of flight. The digital data communication network achieves total and efficient connectivity among all subsystems, including those aircraft systems which have not traditionally been regarded as part of the “avionics.” This includes engine and fuel sensors as well as over 100 discrete signals originating with the many nonavionic subsystems which the pilot must monitor. The connectivity is accomplished through use of a dual-dual set of data concentrators. This significantly reduces the wiring and I/O provisions that are typical of currently available, commercial avionics systems.
Items per page:
50
1 – 34 of 34