# DieselJet > Mediated Wiki article. Canonical URL: https://mediated.wiki/source/DieselJet > Markdown URL: https://mediated.wiki/source/DieselJet.md > Source: https://en.wikipedia.org/wiki/DieselJet > Source revision: 1201588117 > License: Creative Commons Attribution-ShareAlike 4.0 International (https://creativecommons.org/licenses/by-sa/4.0/) {{Short description|Italian aircraft engine manufacturer}} {{Third-party|date=January 2018}} '''DieselJet''' s.r.l. is an [aircraft engine](/source/aircraft_engine) manufacturer based in [Castel Maggiore](/source/Castel_Maggiore), Italy. It was established in 2003 and grown in partnership with the [University of Bologna](/source/University_of_Bologna), [Forlì Airport](/source/Forl%C3%AC_Airport) ISAERS and Centro Ricerche [FIAT](/source/FIAT) (CRF). [Lycoming Engines](/source/Lycoming_Engines) licensed its TDA engines in 2009–2010. [Metatron S.p.A.](/source/Metatron_S.p.A.), an [automotive industry](/source/automotive_industry) group field manufacturing [Compressed natural gas](/source/Compressed_natural_gas) and [Liquefied petroleum gas](/source/Liquefied_petroleum_gas) systems, own it since 2011.{{cite web |url= http://dieseljet.com/wp-content/uploads/2013/01/DJ-HD-A-3500002-WEB-Site_Mar_2016.pdf |title= Brochure |publisher= DieselJet |date= March 2016 |access-date= 2017-08-09 |archive-date= 2017-02-15 |archive-url= https://web.archive.org/web/20170215093600/http://dieseljet.com/wp-content/uploads/2013/01/DJ-HD-A-3500002-WEB-Site_Mar_2016.pdf |url-status= dead }} == Products == The TDA CR 1.9 8V EASA was certified on 11 June 2010 : a 1.9 L liquid cooled, 4 cylinder, 4 stroke, 8 valves engine, with a turbocharger and [Common Rail](/source/Common_Rail) injection, a 1:0.644 reduction gearbox and dual FADEC, it produces 118 kW (160 hp) at take-off and 107 kW (146 hp) continuously at 2450 propeller RPM for {{cvt|205|kg}}. It made its [maiden flight](/source/maiden_flight) on 17 January 2005 with an [IAI Heron](/source/IAI_Heron) UAV. It powered the [Alenia Aermacchi Sky-Y](/source/Alenia_Aermacchi_Sky-Y) UAV demonstrator on its 20 June 2007 first flight{{cite web |url= http://dieseljet.com/history/ |title= History |publisher= DieselJet |access-date= 2017-08-09 |archive-date= 2017-08-20 |archive-url= https://web.archive.org/web/20170820142545/http://dieseljet.com/history/ |url-status= dead }} Its 82mm bore and 90.4mm stroke lead to a 1910 cm3 displacement, it have a 16.0 compression ratio and a 1600 bar common rail and the manufacturer announces {{cvt|190|kg}}, 121 kW / 165 hp maximum and 110 kW continuously till an 8000 ft [critical altitude](/source/critical_altitude) and a {{cvt|225|g/kWh|lb/hph}} [fuel consumption](/source/Brake_specific_fuel_consumption).{{cite web |url= http://dieseljet.com/wp-content/uploads/Brochure_TDA_CR_1.9_8V_web.pdf |title= The 1.9 liter 8V Diesel engine |publisher= DieselJet |access-date= 2017-08-09 |archive-date= 2017-08-20 |archive-url= https://web.archive.org/web/20170820142407/http://dieseljet.com/wp-content/uploads/Brochure_TDA_CR_1.9_8V_web.pdf |url-status= dead }} It is based on the 1.9 [JTD engine](/source/JTD_engine). thumb|DieselJet TDA CR 2.0 16V engineThe TDA CR 2.0 16V, certified 8 March 2016, is a 2.0 L 16 valves engine with a 1:0.607 reduction ratio and a similar configuration, producing 142 kW (193 hp) continuous and 160 kW (217.5 hp) at take-off at 2306 propeller RPM for {{cvt|219|kg}}.{{citation |url= https://www.easa.europa.eu/system/files/dfu/E.079%20TCDS_issue03_20160803_1.0.pdf |title= Type Certificate Data Sheets No. E.079 |publisher= EASA |date= 8 March 2016 }} It powered the IAI Super Heron first flight in 2012 and aims for a 1,500 hours [MTBF](/source/MTBF), a 1,000 hours [Time between overhaul](/source/Time_between_overhaul) initially then 2,000 in service for a €25,000 Cost and a 2,000 hours initial service life then 4,000. The 1955 cm3 engine has cylinders bores of 83 mm and 90.4 mm strokes, a 16.0:1 [compression ratio](/source/compression_ratio) for a {{cvt|210|g/kWh|lb/hph}} min. [brake specific fuel consumption](/source/brake_specific_fuel_consumption), its manufacturer claims {{cvt|205|kg}}, a 8,700 ft critical altitude and operability till 35,000 ft.{{cite web |url= http://dieseljet.com/wp-content/uploads/Brochure_TDA_CR_2.0_16V_web.pdf |title= The 2.0 liter 16V Diesel engine |publisher= DieselJet |access-date= 2017-08-09 |archive-date= 2017-08-20 |archive-url= https://web.archive.org/web/20170820132310/http://dieseljet.com/wp-content/uploads/Brochure_TDA_CR_2.0_16V_web.pdf |url-status= dead }} A [light-sport aircraft](/source/light-sport_aircraft) gasoline engine GA 1.4 8V was in development in 2014-2016. Based on the [Fiat FIRE engine](/source/Fiat_FIRE_engine) with a 2.54:1 reduction gearbox, it has four cylinders of 72mm bore and 84mm stroke for 1368 cm3, a 11:1 compression ratio and generates {{cvt|115|hp}} at {{#expr:6250/2.54round0}} propeller rpm for {{cvt|85|kg}} and a {{cvt|215|g/hph|g/kWh}} fuel consumption.{{cite web |url= http://dieseljet.com/project/1-4/ |title= GA 1.4 8V |publisher= DieselJet |access-date= 2017-08-09 |archive-date= 2017-08-20 |archive-url= https://web.archive.org/web/20170820132630/http://dieseljet.com/project/1-4/ |url-status= dead }} In 2016, DieselJet was developing a {{cvt|240|kW}} TDA CR 3.0 24V. == References == {{reflist}} == External links == * {{official website|http://dieseljet.com/}} Category:Aircraft engine manufacturers of Italy Category:Aircraft diesel engines --- Adapted from the Wikipedia article [DieselJet](https://en.wikipedia.org/wiki/DieselJet) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/DieselJet?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.