Analysis of the applicability of a common rail pump for an aircraft engine

The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by el...
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Autor*in:	Rafał SOCHACZEWSKI [verfasserIn] Marcin SZLACHETKA [verfasserIn] Mirosław WENDEKER [verfasserIn] Paweł KARPIŃSKI [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2019

Schlagwörter:	diesel engine two-stroke opposing piston fuel pump common rail

Übergeordnetes Werk:	In: Combustion Engines - Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020, 179(2019), 4, Seite 192-197
Übergeordnetes Werk:	volume:179 ; year:2019 ; number:4 ; pages:192-197

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc Journal toc

DOI / URN:	10.19206/CE-2019-432

Katalog-ID:	DOAJ067706681

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allfields	10.19206/CE-2019-432 doi (DE-627)DOAJ067706681 (DE-599)DOAJdb4276641c8d400a97e75018c71125ac DE-627 ger DE-627 rakwb eng Rafał SOCHACZEWSKI verfasserin aut Analysis of the applicability of a common rail pump for an aircraft engine 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine. diesel engine two-stroke opposing piston fuel pump common rail Technology T Marcin SZLACHETKA verfasserin aut Mirosław WENDEKER verfasserin aut Paweł KARPIŃSKI verfasserin aut In Combustion Engines Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020 179(2019), 4, Seite 192-197 (DE-627)786309784 (DE-600)2771766-5 26581442 nnns volume:179 year:2019 number:4 pages:192-197 https://doi.org/10.19206/CE-2019-432 kostenfrei https://doaj.org/article/db4276641c8d400a97e75018c71125ac kostenfrei http://www.journalssystem.com/cen/,116195,0,2.html kostenfrei https://doaj.org/toc/2300-9896 Journal toc kostenfrei https://doaj.org/toc/2658-1442 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 179 2019 4 192-197
spelling	10.19206/CE-2019-432 doi (DE-627)DOAJ067706681 (DE-599)DOAJdb4276641c8d400a97e75018c71125ac DE-627 ger DE-627 rakwb eng Rafał SOCHACZEWSKI verfasserin aut Analysis of the applicability of a common rail pump for an aircraft engine 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine. diesel engine two-stroke opposing piston fuel pump common rail Technology T Marcin SZLACHETKA verfasserin aut Mirosław WENDEKER verfasserin aut Paweł KARPIŃSKI verfasserin aut In Combustion Engines Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020 179(2019), 4, Seite 192-197 (DE-627)786309784 (DE-600)2771766-5 26581442 nnns volume:179 year:2019 number:4 pages:192-197 https://doi.org/10.19206/CE-2019-432 kostenfrei https://doaj.org/article/db4276641c8d400a97e75018c71125ac kostenfrei http://www.journalssystem.com/cen/,116195,0,2.html kostenfrei https://doaj.org/toc/2300-9896 Journal toc kostenfrei https://doaj.org/toc/2658-1442 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 179 2019 4 192-197
allfields_unstemmed	10.19206/CE-2019-432 doi (DE-627)DOAJ067706681 (DE-599)DOAJdb4276641c8d400a97e75018c71125ac DE-627 ger DE-627 rakwb eng Rafał SOCHACZEWSKI verfasserin aut Analysis of the applicability of a common rail pump for an aircraft engine 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine. diesel engine two-stroke opposing piston fuel pump common rail Technology T Marcin SZLACHETKA verfasserin aut Mirosław WENDEKER verfasserin aut Paweł KARPIŃSKI verfasserin aut In Combustion Engines Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020 179(2019), 4, Seite 192-197 (DE-627)786309784 (DE-600)2771766-5 26581442 nnns volume:179 year:2019 number:4 pages:192-197 https://doi.org/10.19206/CE-2019-432 kostenfrei https://doaj.org/article/db4276641c8d400a97e75018c71125ac kostenfrei http://www.journalssystem.com/cen/,116195,0,2.html kostenfrei https://doaj.org/toc/2300-9896 Journal toc kostenfrei https://doaj.org/toc/2658-1442 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 179 2019 4 192-197
allfieldsGer	10.19206/CE-2019-432 doi (DE-627)DOAJ067706681 (DE-599)DOAJdb4276641c8d400a97e75018c71125ac DE-627 ger DE-627 rakwb eng Rafał SOCHACZEWSKI verfasserin aut Analysis of the applicability of a common rail pump for an aircraft engine 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine. diesel engine two-stroke opposing piston fuel pump common rail Technology T Marcin SZLACHETKA verfasserin aut Mirosław WENDEKER verfasserin aut Paweł KARPIŃSKI verfasserin aut In Combustion Engines Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020 179(2019), 4, Seite 192-197 (DE-627)786309784 (DE-600)2771766-5 26581442 nnns volume:179 year:2019 number:4 pages:192-197 https://doi.org/10.19206/CE-2019-432 kostenfrei https://doaj.org/article/db4276641c8d400a97e75018c71125ac kostenfrei http://www.journalssystem.com/cen/,116195,0,2.html kostenfrei https://doaj.org/toc/2300-9896 Journal toc kostenfrei https://doaj.org/toc/2658-1442 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 179 2019 4 192-197
allfieldsSound	10.19206/CE-2019-432 doi (DE-627)DOAJ067706681 (DE-599)DOAJdb4276641c8d400a97e75018c71125ac DE-627 ger DE-627 rakwb eng Rafał SOCHACZEWSKI verfasserin aut Analysis of the applicability of a common rail pump for an aircraft engine 2019 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine. diesel engine two-stroke opposing piston fuel pump common rail Technology T Marcin SZLACHETKA verfasserin aut Mirosław WENDEKER verfasserin aut Paweł KARPIŃSKI verfasserin aut In Combustion Engines Polskie Towarzystwo Naukowe Silników Spalinowych/Polish Scientific Society of Combustion Engines, 2020 179(2019), 4, Seite 192-197 (DE-627)786309784 (DE-600)2771766-5 26581442 nnns volume:179 year:2019 number:4 pages:192-197 https://doi.org/10.19206/CE-2019-432 kostenfrei https://doaj.org/article/db4276641c8d400a97e75018c71125ac kostenfrei http://www.journalssystem.com/cen/,116195,0,2.html kostenfrei https://doaj.org/toc/2300-9896 Journal toc kostenfrei https://doaj.org/toc/2658-1442 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 179 2019 4 192-197
language	English
source	In Combustion Engines 179(2019), 4, Seite 192-197 volume:179 year:2019 number:4 pages:192-197
sourceStr	In Combustion Engines 179(2019), 4, Seite 192-197 volume:179 year:2019 number:4 pages:192-197
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	diesel engine two-stroke opposing piston fuel pump common rail Technology T
isfreeaccess_bool	true
container_title	Combustion Engines
authorswithroles_txt_mv	Rafał SOCHACZEWSKI @@aut@@ Marcin SZLACHETKA @@aut@@ Mirosław WENDEKER @@aut@@ Paweł KARPIŃSKI @@aut@@
publishDateDaySort_date	2019-01-01T00:00:00Z
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author	Rafał SOCHACZEWSKI
spellingShingle	Rafał SOCHACZEWSKI misc diesel engine misc two-stroke misc opposing piston misc fuel pump misc common rail misc Technology misc T Analysis of the applicability of a common rail pump for an aircraft engine
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topic_title	Analysis of the applicability of a common rail pump for an aircraft engine diesel engine two-stroke opposing piston fuel pump common rail
topic	misc diesel engine misc two-stroke misc opposing piston misc fuel pump misc common rail misc Technology misc T
topic_unstemmed	misc diesel engine misc two-stroke misc opposing piston misc fuel pump misc common rail misc Technology misc T
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title	Analysis of the applicability of a common rail pump for an aircraft engine
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title_full	Analysis of the applicability of a common rail pump for an aircraft engine
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author_browse	Rafał SOCHACZEWSKI Marcin SZLACHETKA Mirosław WENDEKER Paweł KARPIŃSKI
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title_sort	analysis of the applicability of a common rail pump for an aircraft engine
title_auth	Analysis of the applicability of a common rail pump for an aircraft engine
abstract	The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine.
abstractGer	The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine.
abstract_unstemmed	The paper presents an analysis of the possibility of using a common rail pump to supply an aircraft compression-ignition engine. It is an engine with a two-stroke cycle, three cylinders, opposing pistons and 100 kW power. Its each combustion chamber is supply by one or two injectors controlled by electromagnetic valves. In order to assess the possibility of using a common rail pump, four high-pressure pumps were tested on a bench. They are piston pumps differing in the number and geometry of their pumping sections. The analysis included the pumping output, the torque on the pump drive shaft and the power needed to drive the pump. The weight and overall dimensions of the pump were also considered, including the arrangement of the pumping sections and the way the drive is transmitted. The research allowed to optimize the engine power supply system depending on fuel demand and the way the pump is mounted on the engine.
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title_short	Analysis of the applicability of a common rail pump for an aircraft engine
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Analysis of the applicability of a common rail pump for an aircraft engine

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