Analysis of Passenger Car Turbocharged Diesel Engines Performance When Tested at Altitude and of the Altitude Simulator Device UsedSource: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 008::page 81017Author:Broatch, Alberto
,
Bermúdez, Vicente
,
Serrano, José Ramón
,
Tabet, Roberto
,
Gómez, Javier
,
Bender, Stefan
DOI: 10.1115/1.4043395Publisher: American Society of Mechanical Engineers (ASME)
Abstract: According to current worldwide trends for homologation vehicles in real driving conditions is forced to test the engines in altitude and in highly dynamic driving cycles in order to approach nowadays and next future emissions standard. Up to now, there were two main options to perform this type of tests: round-robin tests of the whole vehicle or hypobaric chambers, both with high costs and low repeatability. In this paper a new device is described, which can emulate ambient conditions at whatever altitude between sea level and 5000 m high. Even it can be used to emulate ambient conditions at sea level when test bench is placed up to 2000 m high. The main advantages of the altitude simulation equipment are as follows: dynamic emulation of all the psychrometric variables affecting the vehicles during round-robin tests; lower space usage and low-energy consumption. The altitude simulator (AS) has been validated comparing with results from a hypobaric chamber at different altitudes. Previously a research about the dispersion in the measurements of both testing devices has been done for assessing the results of the comparison experiment. Final conclusion resulted in the same operating performance and emissions of the studied engine with both types of testing equipment for altitude simulation.
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contributor author | Broatch, Alberto | |
contributor author | Bermúdez, Vicente | |
contributor author | Serrano, José Ramón | |
contributor author | Tabet, Roberto | |
contributor author | Gómez, Javier | |
contributor author | Bender, Stefan | |
date accessioned | 2019-09-18T09:07:37Z | |
date available | 2019-09-18T09:07:37Z | |
date copyright | 4/25/2019 12:00:00 AM | |
date issued | 2019 | |
identifier issn | 0742-4795 | |
identifier other | gtp_141_08_081017 | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4259171 | |
description abstract | According to current worldwide trends for homologation vehicles in real driving conditions is forced to test the engines in altitude and in highly dynamic driving cycles in order to approach nowadays and next future emissions standard. Up to now, there were two main options to perform this type of tests: round-robin tests of the whole vehicle or hypobaric chambers, both with high costs and low repeatability. In this paper a new device is described, which can emulate ambient conditions at whatever altitude between sea level and 5000 m high. Even it can be used to emulate ambient conditions at sea level when test bench is placed up to 2000 m high. The main advantages of the altitude simulation equipment are as follows: dynamic emulation of all the psychrometric variables affecting the vehicles during round-robin tests; lower space usage and low-energy consumption. The altitude simulator (AS) has been validated comparing with results from a hypobaric chamber at different altitudes. Previously a research about the dispersion in the measurements of both testing devices has been done for assessing the results of the comparison experiment. Final conclusion resulted in the same operating performance and emissions of the studied engine with both types of testing equipment for altitude simulation. | |
publisher | American Society of Mechanical Engineers (ASME) | |
title | Analysis of Passenger Car Turbocharged Diesel Engines Performance When Tested at Altitude and of the Altitude Simulator Device Used | |
type | Journal Paper | |
journal volume | 141 | |
journal issue | 8 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4043395 | |
journal fristpage | 81017 | |
journal lastpage | 081017-9 | |
tree | Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 008 | |
contenttype | Fulltext |