2007 IEEE Vehicle Power and Propulsion Conference 2007
DOI: 10.1109/vppc.2007.4544184
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Modelling and Testing of a Turbo-generator System for Exhaust Gas Energy Recovery

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Cited by 19 publications
(5 citation statements)
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“…Moreover, as already mentioned, the exhaust gas turbine employed in a hybrid propulsion system should work under almost steady state conditions, which is why a torque/current control on the generator would allow the machine to operate at its best efficiency speed ratio, regardless of the power produced. The only turbine generator products present on the market or studied until now are composed of a radial turbine for turbocharging applications connected to an electric generator [30][31][32], and are designed exclusively to supply the vehicle's electric accessories, thus producing a very limited power output (i.e., 6 kW). Due to the lack of adequate products both in the literature and on the market, and according to the previous considerations, the authors assumed that in the compound engine, the turbine works with an almost constant speed ratio, regardless of the power produced, and hence with an almost constant efficiency η T .…”
Section: Separated Electric Compound Spark Ignition Enginementioning
confidence: 99%
“…Moreover, as already mentioned, the exhaust gas turbine employed in a hybrid propulsion system should work under almost steady state conditions, which is why a torque/current control on the generator would allow the machine to operate at its best efficiency speed ratio, regardless of the power produced. The only turbine generator products present on the market or studied until now are composed of a radial turbine for turbocharging applications connected to an electric generator [30][31][32], and are designed exclusively to supply the vehicle's electric accessories, thus producing a very limited power output (i.e., 6 kW). Due to the lack of adequate products both in the literature and on the market, and according to the previous considerations, the authors assumed that in the compound engine, the turbine works with an almost constant speed ratio, regardless of the power produced, and hence with an almost constant efficiency η T .…”
Section: Separated Electric Compound Spark Ignition Enginementioning
confidence: 99%
“…Therefore the bypass valve or emergency braking device installing is recommended. The parallel setting allows controlling the exhaust gas flow through the turbogenerator, controlling the power of the turbogenerator, performing maintenance on the operating unit, operating the power plant with the turbine generator switched off, and, in case of emergency, shutting off the exhaust gas supply to the turbogenerator, thereby reducing possible damage and cost of repairs, and also increasing the efficiency and productivity of the power plant [6][7][8] . This scheme also has a number of disadvantages, such as the increase in cost due to the need for high-temperature mass-size parameters, as well as the increase in the number of shutters, the design complexity and the increase in discharge resistance due to hydraulic losses.…”
Section: Disposition Of a Turbogenerator In The Exhaust Systemmentioning
confidence: 99%
“…A turbogenerator must produce from 5 to 10 kW of electric power with a specific fuel consumption reduction of at least 7% compared to the engine chosen. According to the research conducted, the recovery systems can convert up to 12-15% of the exhaust power [6][7][8]. Therefore, a ZMZ-409 engine with a capacity of 105 kW was selected, which will be used as a gas generator in testing the turbogenerator.…”
Section: Development Of the Simulation Model Of A Turbogeneratormentioning
confidence: 99%
“…This clarifies that the turbogenerator here considered, and the whole hybrid propulsion system shown in Figure 1, are not commercially available at the moment. The only commercially available products are composed of a radial turbine for turbocharging application connected to an electric generator [15][16][17] and are designed exclusively to supply the electric accessories of traditional vehicles, thus producing maximum output power within 6 kW. Given the lack of adequate references on the market, as indicated in the scientific literature, and in their preliminary studies, the authors considered a constant turbine thermomechanical efficiency η T,tm (i.e., the product of the total to static isentropic efficiency η t,s and the mechanical efficiency η m ), i.e., independent of the turbine speed and pressure ratio; more in detail, in their preliminary analysis, the authors considered two different levels of thermomechanical efficiency, namely 0.70 and 0.75.…”
Section: Introductionmentioning
confidence: 99%