aircraft diesel engine

A number of manufacturers built diesel aero engines in the 1920s and 1930s; the best known were the Packard air-cooled radial, and the Junkers Jumo 205, which was moderately successful, but proved unsuitable for combat use in World War II. The Blohm & Voss BV 138 trimotor maritime patrol flying boat, however, was powered with the more developed Junkers Jumo 207 powerplant, and was more successful with its trio of diesel Jumo 207s conferring upwards of a maximum 2,100 km (1,300 mile) combat radius upon the nearly 300 examples of the BV 138 built during World War II.

The first successful diesel engine developed specifically for aircraft was the Packard DR-980 radial diesel of 1928–1929, which was laid out in the familiar air-cooled radial format similar to Wright and Pratt & Whitney designs, and was contemporary with the Beardmore Tornado used in the R101 airship. The use of a diesel had been specified for its low fire risk fuel. The first successful flight of a diesel powered aircraft was made on September 18, 1928, in a Stinson model SM-1DX Detroiter registration number X7654.{{cite book|url=https://books.google.com/books?id=veQDAAAAMBAJ&q=Popular+Mechanics+1931+curtiss&pg=PA456 |title=Mystery Engine Promises|publisher=Popular Mechanics|date=September 1931|volume=56|access-date=2012-09-22|page=456}} Around 1936 the heavier but less thirsty diesel engines were preferred over gasoline engines when flight time was over only 6–7 hours.Odel, Axel. "[http://www.e-pages.dk/ingarkiv/4818/?page=13 Teknikken i luftfartens tjeneste]" page 18-20 Ingeniøren, 2 May 1936. Accessed: 28 December 2014.

File:Jumo205 cutview 02.jpg opposed-piston engine, sectioned]]

Entering service in the early 1930s, the two-stroke Junkers Jumo 205 opposed-piston engine was much more widely used than previous aero diesels. It was moderately successful in its use in the Blohm & Voss Ha 139 and even more so in airship use. In Britain Napier & Son license-built the larger Junkers Jumo 204 as the Napier Culverin, but it did not see production use in this form. A Daimler-Benz diesel engine was also used in Zeppelins, including the ill-fated LZ 129 Hindenburg. This engine proved unsuitable in military applications and subsequent German aircraft engine development concentrated on gasoline and jet engines.

The Soviet World War II-era four-engine strategic bomber Petlyakov Pe-8 was built with Charomskiy ACh-30 diesel engines; but just after the war's end, both its diesels, and gasoline-fueled Mikulin inline V12 engines for surviving Pe-8 airframes were replaced with Shvetsov-designed radial gasoline engines because of efficiency concerns. The Yermolaev Yer-2 long-range medium bomber was also built with Charomskiy diesel engines.

Other manufacturers also experimented with diesel engines in this period, such as the French Bloch (later Dassault Aviation), whose MB203 bomber prototype used Clerget diesels of radial design. The Royal Aircraft Establishment developed an experimental compression ignition (diesel) version of the Rolls-Royce Condor in 1932, flying it in a Hawker Horsley for test purposes.{{cite web|url=http://www.flightglobal.com/pdfarchive/view/1932/1932%20-%201172.html |title=rolls-royce condor | 1932 | 1172 | Flight Archive |publisher=Flightglobal.com |date=1932-11-17 |access-date=2012-09-22 | page=1094}}

Interest in diesel engines in the postwar period was sporadic. The lower power-to-weight ratio of diesels, particularly compared to turboprop engines, weighed against the diesel engine. With fuel available cheaply and most research interest in turboprops and jets for high-speed airliners, diesel-powered aircraft virtually disappeared. The stagnation of the general aviation market in the 1990s saw a massive decline in the development of any new aircraft engine types.

Napier & Son in Britain had developed the Napier Culverin, a derivative of the Junkers Jumo 205, before World War II, and took up aero diesel engines again in the 1950s. The British Air Ministry supported the development of the {{cvt|3000|hp|kW|order=flip}} Napier Nomad, a combination of piston and turboprop engines, which was exceptionally efficient in terms of brake specific fuel consumption, but judged too bulky and complex and canceled in 1955.

Several factors have emerged to change this equation.McLanahan, J. Craig. “Diesel Aircraft Engines: A Delayed Promise from the 1930's.” SAE Transactions, vol. 108, 1999, pp. 1103–1112. First, a number of new manufacturers of general aviation aircraft developing new designs have emerged. Second, in Europe in particular, avgas has become very expensive. Third, in several (particularly remote) locations, avgas is harder to obtain than diesel fuel. Finally, automotive diesel technologies have improved greatly in recent years, offering higher power-to-weight ratios more suitable for aircraft application.

Certified diesel-powered light planes are currently available, and a number of companies are developing new engine and aircraft designs for the purpose. Many of these run on readily available jet fuel (kerosene), or on conventional automotive diesel.

Simulations indicate lower maximum payload due to the heavier engine, but also longer range at medium payload.Vassilios Pachidis. [http://www.aerodays2015.com/wp-content/uploads/sites/20/1D-Vassilis-Pachidis.pdf Clean Sky Technology Evaluator Environmental Performance Assessment of Rotorcraft] {{Webarchive|url=https://web.archive.org/web/20160127134349/http://www.aerodays2015.com/wp-content/uploads/sites/20/1D-Vassilis-Pachidis.pdf |date=2016-01-27 }} , page 36. Cranfield University, 20 October 2015.

File:Beardmore Tornado diesel engine from R101.JPG ]]

The zeppelins LZ 129 Hindenburg and LZ 130 Graf Zeppelin II were propelled by reversible diesel engines. The direction of operation was changed by shifting gears on the camshaft. From full power forward, the engines could be brought to a stop, changed over, and brought to full power in reverse in less than 60 seconds.

Nevil Shute Norway wrote that the demonstration flight of the airship R100 was changed from India to Canada, "when she got petrol engines, because it was thought that a flight to the tropics with petrol on board would be too hazardous. It is curious after over twenty years to recall how afraid everyone was of petrol in those days (c. 1929), because since then aeroplanes with petrol engines have done innumerable hours of flying in the tropics, and they don't burst into flames on every flight. I think the truth is that everyone was diesel-minded in those days; it seemed as if the diesel engine for aeroplanes was only just around the corner, with the promise of great fuel economy".{{cite book

|title=Slide Rule

|last=Shute |first=Nevil

|author-link=Nevil Shute

|year=1954

|publisher=Heinemann |location=London

|ref=Shute, Slide Rule

|pages=98–99

}}

Hence, the ill-fated diesel-engined R101 — which crashed in 1930 — was to fly to India, though her diesel engines had petrol starter engines, and there had only been time to replace one with a diesel starter engine.{{cite book |last=Leasor |first=James |year=2001 |orig-year=1957 |title=The Millionth Chance: The Story of the R.101 |place=London |publisher=Stratus Books |page=78 |isbn=978-0-7551-0048-4}} The R101 used the Beardmore Tornado aero diesel engine, with two of the five engines reversible by an adjustment to the camshaft. This engine was developed from an engine used in railcars.

Continental Motors, Inc. subsidiary Technify Motors GmbH of Sankt Egidien, Germany, is the new TC holder of the Thielert TAE 110 certified by the EASA on 8 March 2001, a 4-cylinder, four stroke {{cvt|1689|cm3|in3}} engine with common rail direct injection, turbocharger, 1:1.4138 reduction gearbox and FADEC producing {{cvt|81|kW}} at takeoff at 3675 rpm and {{cvt|66|kW}} continuously at 3400 rpm for {{cvt|141|kg}}.{{citation |url= https://www.easa.europa.eu/system/files/dfu/EASA-TCDS-E.019_Technify_Motors_GmbH_TAE110_series_engines-01-19082013.pdf |title= Type Certificate Data Sheets No. E.019 |publisher= EASA |date= 19 August 2013 |access-date= 7 August 2017 |archive-date= 7 August 2017 |archive-url= https://web.archive.org/web/20170807152250/https://www.easa.europa.eu/system/files/dfu/EASA-TCDS-E.019_Technify_Motors_GmbH_TAE110_series_engines-01-19082013.pdf |url-status= dead }}

The TAE 125-01, certified 3 May 2002, is the same with a 1:1.689 gearbox, weighs {{cvt|134|kg}} and outputs {{cvt|99|kW}} maximum at 3900 rpm, like the later {{cvt|1991|cm3|in3}} TAE 125-02-99 certified on 14 August 2006, then the TAE 125-02-114 on 6 March 2007 for {{cvt|114|kW}} at 3900 rpm, and the TAE 125-02-125 outputting {{cvt|125|kW}} at 3400 rpm for {{cvt|156|kg}}.{{citation |url= https://www.easa.europa.eu/sites/default/files/dfu/E.055%20TCDS_TAE125_issue_13_0.pdf |title= Type Certificate Data Sheets No. E.055 |publisher= EASA |date= 22 July 2020 |access-date= 8 October 2020 |archive-date= 11 August 2021 |archive-url= https://web.archive.org/web/20210811163857/https://www.easa.europa.eu/sites/default/files/dfu/E.055%20TCDS_TAE125_issue_13_0.pdf |url-status= dead }}

The Centurion 4.0 is a four stroke {{cvt|3996|cm3|in3}} 8-cylinder, with common rail, 2 turbochargers, 1:1.689 reduction gearbox, propeller governor and FADEC weighting {{cvt|286|kg}} and certified on 26 September 2007 for up to {{cvt|257|kW}} maximum, {{cvt|243|kW}} continuous at 3900 rpm.{{citation |url= https://www.easa.europa.eu/system/files/dfu/EASA%20E.014%20TCDS%20Technify%20Motors%20GmbH_%20Centurion%204.0_issue%2006_2015.18.09_1.0.pdf |title= Type Certificate Data Sheets No. E.014 |publisher= EASA |date= 20 June 2017 |access-date= 7 August 2017 |archive-date= 24 September 2017 |archive-url= https://web.archive.org/web/20170924124534/http://www.easa.europa.eu/system/files/dfu/EASA%20E.014%20TCDS%20Technify%20Motors%20GmbH_%20Centurion%204.0_issue%2006_2015.18.09_1.0.pdf |url-status= dead }} The centurion 4.0 V8 has not been certified for installation in any airframes.

EASA certified on 20 June 2017, the Centurion 3.0 is a {{cvt|2987|cm3|in3}} four stroke V6, also with common rail, turbocharger, Electronic Engine Control Unit (EECU) and 1 : 1.66 reduction gearbox, weighting {{cvt|265|kg}} and outputting 221 kW (300 HP) at take-off, 202 kW (272 HP) continuously, both at 2340 propeller RPM.{{citation |url= https://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20E104_Centurion3_Issue01.pdf |title= Type Certificate Data Sheets No. E.104 |publisher= EASA |date= 18 Sep 2015 |access-date= 7 August 2017 |archive-date= 7 August 2017 |archive-url= https://web.archive.org/web/20170807192959/https://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20E104_Centurion3_Issue01.pdf |url-status= dead }}

Thielert, based in German Lichtenstein, Saxony was the original TC holder of the 1.7 based on the Mercedes A-class turbo diesel, running on diesel and jet A-1 fuel. It was certified for retrofitting to Cessna 172s and Piper Cherokees, replacing the {{cvt|160|hp}} Lycoming O-320 {{cvt|320|in3|L|order=flip}} Avgas engine.

The {{cvt|134|kg}} of the {{cvt|99|kW}} 1.7 engine is similar to the O-320 but its displacement is less than a third and it achieves maximum power at 2300 prop RPM instead of 2700.

Austrian aircraft manufacturer Diamond Aircraft Industries offered its single-engine Diamond DA40-TDI Star with the 1.7 engine, and the Diamond DA42 Twin Star with two, offering a low fuel consumption of {{cvt|15.1|L/h|gal/h}}.

Robin Aircraft also offered a DR400 Ecoflyer with the Thielert engine.

In May 2008, Thielert went bankrupt and although Thielert's insolvency administrator, Bruno M. Kubler, was able to announce in January 2009 that the company was "in the black and working to capacity," by then Cessna had dropped plans to install Thielert engines in some models, and Diamond Aircraft has now developed its own in-house diesel engine: the Austro Engine E4.

Several hundred Thielert-powered airplanes are flying.

SMA Engines, located in Bourges, France, have designed the SMA SR305-230: a direct drive four-stroke, air and oil-cooled, turbo-diesel of four horizontally opposed cylinders displacing {{cvt|4988|cm3|in3}} with an electronically controlled mechanical pump fuel injection, it obtained EASA certification on 20 April 2001 for {{cvt|169|kW}} at 2200 rpm, weighting {{cvt|195|kg}}.

A {{cvt|194|kW}} SR305-260 was certified in February 2019.{{cite web |url= https://www.easa.europa.eu/sites/default/files/dfu/E.076%20TCDS%20Issue%208.pdf |title= Type Certificate Data Sheets No. E.076 |date= 15 February 2019 |publisher= EASA |access-date= 6 March 2019 |archive-date= 18 January 2021 |archive-url= https://web.archive.org/web/20210118214954/https://www.easa.europa.eu/sites/default/files/dfu/E.076%20TCDS%20Issue%208.pdf |url-status= dead }}

The SR305-230 obtained US FAA certification in July 2002. It is now certified as retrofit on several Cessna 182 models in Europe and the US, and Maule is working toward certification of the M-9-230. SMA's engineering team came from Renault Sport (Formula 1) and designed it from the ground up.

SMA develops a {{cvt|330|-|400|hp|kW|order=flip}} six cylinder version, the SR460.{{cite press release |url= http://www.safran-aircraft-engines.com/fr/atom/807 |title= The innovation by SMA, the SR460 |date= 3 September 2015 |publisher= Safran SMA}} At AERO Friedrichshafen 2016, SMA debuted a high power density engine demonstrator: a 135 hp (100 kW), 38-cubic-inch (0.62 liter) single cylinder four-stroke for 215 hp (160 kW) per liter, scalable from {{cvt|400|to|800|hp|kW|order=flip}} and up to 1.5 hp/lb. (2.5 kW/kg) power density with a specific fuel consumption of 0.35 lb/hp/hr (210 g/kwh).{{cite news |url= http://www.aviationpros.com/article/12232319/sma-debuts-its-high-power-density-engine |title= SMA Debuts Its High Power Density Engine |date= 13 October 2016 |work= AviationPros}}

Austro Engine GmbH, based in Wiener Neustadt, Austria had the E4 engine certified by EASA on 28 January 2009. It is a 4-cylinder, 1991 cm³ four stroke engine with common rail direct injection, turbocharger, 1:1.69 reduction gearbox and an Electronic Engine Control Unit. It produces {{cvt|123.5|kW}} at Take-off and continuously, at 2300 propeller RPM for {{cvt|185|kg}}.

The same weight E4P was certified on 26 March 2015 for {{cvt|132|kW}} at Take-off at the same speed, and {{cvt|126|kW}} continuously at 2200 propeller RPM.{{citation |url= https://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20E200%20%20issue%2010_20161804_1.0.pdf |title= Type Certificate Data Sheets No.E.200 |publisher= EASA |date= 18 April 2016 |access-date= 7 August 2017 |archive-url= https://web.archive.org/web/20170924115103/http://www.easa.europa.eu/system/files/dfu/EASA%20TCDS%20E200%20%20issue%2010_20161804_1.0.pdf |archive-date= 24 September 2017 |url-status= dead }}

In 2011, Austro Engine was developing a {{cvt|280|hp|}} 6-cylinder in cooperation with Steyr Motors, based on their {{convert|3.2|L|in3}} block, to be used in the Diamond DA50.{{cite press release |publisher= STEYR MOTORS GmbH |title= STEYR MOTORS and Austro Engine form development partnership for {{cvt|280|hp|kW|order=flip}} 6-cylinder aircraft engine |url= http://www.steyr-motors.com/uploads/media/AustroEngine_STEYR_MOTORS_press_releaseEN__20110303.pdf |date= 3 March 2011}}

DieselJet s.r.l. of Castel Maggiore, Italy, had its TDA CR 1.9 8V EASA certified on 11 June 2010: a {{cvt|1.9|L|in3}} liquid cooled, 4 cylinder, 4 stroke, 8 valve engine, with a turbocharger and 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}}. The TDA CR 2.0 16V, certified 8 March 2016, is a {{cvt|2.0|L|in3}} 16 valve 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 }} In 2016, DieselJet was developing a {{cvt|240|kW}} TDA CR 3.0 24V.{{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= 2017-08-08 |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 }}

Continental Motors, Inc. of Mobile, Alabama, received on December 19, 2012, a type certification for its Continental CD-230 under the official TD-300-B designation: a turbocharged 4-stroke direct drive flat four air-cooled engine of {{cvt|4972|cm3|in3}}, with direct fuel injection and electronic control unit with a mechanical back-up, outputting continuously {{cvt|230|hp}} at 2200 RPM for 431 lb (195.5 kg) dry.{{cite web |url= http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/26f364649ebf047c86257ae8004fd4d8/$FILE/E00017AT_Rev_0.pdf |title= Type Certificate data sheet E00017AT Revision 0 |date= December 19, 2012 |publisher= FAA |access-date= August 9, 2017 |archive-url= https://web.archive.org/web/20170809212128/http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/26f364649ebf047c86257ae8004fd4d8/$FILE/E00017AT_Rev_0.pdf |archive-date= August 9, 2017 |url-status= dead }} It is developed from the SMA SR305-230.

RED Aircraft GmbH of Adenau, Germany, obtained EASA type certification on 19 December 2014 for its {{cvt|6134|cm3|in3}} RED A03 V12 four stroke, with common rail, turbocharger, 1:1.88 reduction gearbox and single lever FADEC/EECS, outputting 368 kW (500 hp) at take-off at 2127 propeller RPM and 338 kW (460 hp) at 1995 propeller RPM continuously for {{cvt|363|kg}} dry.{{cite web |url= http://www.easa.europa.eu/system/files/dfu/EASA_E_150_TCDS_REDA03_issue%2001_20141219_1.pdf |publisher= EASA |date= 19 December 2014 |title= Type-Certificate Data Sheet No. E.150 |access-date= 9 August 2017 |archive-url= https://web.archive.org/web/20160910092255/http://www.easa.europa.eu/system/files/dfu/EASA_E_150_TCDS_REDA03_issue%2001_20141219_1.pdf |archive-date= 10 September 2016 |url-status= dead |df= dmy-all }}

The RED A05 is a 3550cc V6 preliminary design, outputting {{cvt|300|hp}} at takeoff at 2127 propeller RPM and {{cvt|280|hp}} continuously at 1995 propeller RPM, with a {{cvt|210|g/kWh|lb/hph}} best brake specific fuel consumption.{{cite web |url= https://www.red-aircraft.com/wp-content/uploads/2012/07/RED-A051.pdf |title= RED A05 – V6 – 3550cc / 216 cu in |publisher= RED aircraft |date= Jul 2017 |access-date= 2017-08-09 |archive-url= https://web.archive.org/web/20170809172108/https://www.red-aircraft.com/wp-content/uploads/2012/07/RED-A051.pdf |archive-date= 2017-08-09 |url-status= dead }}

DeltaHawk Engines, Inc., an American company, is currently developing three V-4 designs of 160, 180 and {{cvt|200|hp|kW|order=flip}}, the latter two versions being turbocharged. Using a ported two-stroke design, they have also flown a prototype engine in a pusher configuration. Velocity aircraft are claiming delivery of non-certified engines since 2005 and hope to achieve certification early in 2011. DeltaHawk engines have a dry oil sump, so they can run in any orientation: upright, inverted or vertical shaft by changing the location of the oil scavenge port. They can also run counter-rotation for installation in twins to eliminate the critical engine issue.{{cite web|url= http://www.deltahawk.com/content/deltahawk-dh180a4 |title= DeltaHawk Diesel Engines}}{{cite press release |url= http://www.releasewire.com/press-releases/release-30381.htm |title= DeltaHawk Diesel-Powered SR20 Announced |publisher= DeltaHawk |date= August 10, 2009}}

A water-cooled DeltaHawk engine has been successfully fitted to a Rotorway helicopter, weighing the same as an air-cooled petrol engine of similar power and being capable of maintaining that power to 17,000 feet.Delta D2 Johnson, Pam. page 46 Pacific Wings. Accessed 2 January 2010

The 180 hp DeltaHawk DH180 received its FAA Type certification in May 2023, first deliveries are planned in 2024.{{cite press release |url= https://www.deltahawk.com/2023/05/18/faa-certification/ |title= DeltaHawk's jet-fueled piston engine receives FAA Certification |date= May 18, 2023 |publisher= DeltaHawk}}

A number of other manufacturers are currently developing experimental diesel engines, many using aircraft-specific designs rather than adapted automotive engines. Many are using two-stroke designs, with some opposed-piston layouts directly inspired by the original Junkers design.{{cite web |url= http://www.dieselair.com:80/ |archive-url= https://web.archive.org/web/20161023154609/http://www.dieselair.com/ |url-status= dead |archive-date= 2016-10-23 |title= Diesel Air Newsletter |publisher= DieselAir Research, Inc. }}{{failed verification|date=August 2017}}

Diesel Air Limited, Wilksch and Zoche have all had considerable problems bringing their prototype designs into production, with delays running into several years. The Diesel Air Limited-powered airship is no longer registered by the Civil Aviation Authority in the UK.

Wilksch Airmotive, a British company, is developing a {{cvt|120|hp|kW|order=flip}} three-cylinder two-stroke diesel (WAM-120) and is working on a four-cylinder {{cvt|160|hp|kW|order=flip}} design (WAM-160). In 2007 Wilksch claimed that they had completed multiple tests on the WAM-100 LSA in accordance with ASTM F 2538 – the WAM-100 LSA is a derated WAM-120. Wilksch originally showed a two-cylinder prototype alongside the three- and four-cylinder models. In April 2008 IndUS Aviation introduced the first diesel light-sport aircraft with a WAM 120 having flown 400 hours on a Thorp T211 in England for the past four years.{{cite news |url= http://eaa.org/news/2008/2008-04-12_indus.asp |archive-url= https://web.archive.org/web/20101214175035/http://eaa.org/news/2008/2008-04-12_indus.asp |url-status= dead |archive-date= 14 December 2010 |title= Diesel-Powered LSA Debuts at Sun 'n Fun |date= 11 April 2008 |publisher= EAA}}

By mid-2009, approximately 40 WAM-120 units had been sold, with around half currently flying. The British owner of a VANS RV-9A fitted with a WAM-120 reports getting {{cvt|125|kn|km/h}} TAS at {{cvt|6000|ft|m}} on 15 litre/hr of Jet A-1 fuel.

A Rutan LongEz canard-pusher (G-LEZE) has also flown with the WAM-120 engine with test flights showing a TAS of {{cvt|160|kn|km/h|order=flip}} at {{cvt|11000|ft|m|order=flip}} and 22 litre/hr. At economy cruise of {{cvt|125|kn|km/h|order=flip}} at {{cvt|2000|ft|m|order=flip}} the fuel consumption is {{cvt|12|L/h|USgal/h}}, giving a range of {{cvt|1890|nmi|km|order=flip}}.{{cite web |url= http://www.longezediesel.com/ |title= Longeze Diesel}}

GAP Diesel Engine is a NASA development.{{cite web |url= http://www.nasa.gov/centers/glenn/about/fs01grc.html |title= Small Aircraft Propulsion: The Future Is Here |publisher= NASA |date= Nov 22, 2004}}

With the branding Zoche aero-diesel, the company "Michael Zoche Antriebstechnik" in Munich/Germany has produced a prototype range of three radial air-cooled two-stroke diesel aero-engines, comprising a V-twin, a single-row cross-4 and a double-row cross-8.{{cite web |url= http://www.zoche.de/zoche_brochure.pdf |title= Brochure |publisher= Zoche }}

A Zoche engine has run successfully in wind tunnel tests.{{cite news |url= http://www.zoche.de/Zoche_video.html |title= Zoche aero-diesels testbench video |publisher= Zoche |date= Oct 14, 2015}} Zoche seem barely closer to production than they were a decade ago.

Andy Higgs' Advanced Component Engineering designed a step piston {{cvt|1,000|hp|kW|order=flip}} V12 weighing 665 lb /302 kg with the reduction gearbox to replace low-end, {{cvt|580|to|1200|hp|kW|order=flip}} PT6s like in the Cessna Caravan; a {{cvt|350|hp|kW|order=flip}}, 302 pounds/137 kg four-cylinder with a gearbox to reduce the prop RPM to 2300 from 5300; and a {{cvt|1.5|L|in3}} V4 weighing 103 pounds/47 kg and producing {{cvt|120|hp}}.{{cite news |url= http://www.ainonline.com/aviation-news/general-aviation/2016-11-08/ain-exclusive-higgs-diesel |work= AIN |title= Exclusive : The Higgs Diesel |author= Nigel Moll |date= November 8, 2016}} see http://www.higgs-diesel.com/higgs-diesel/falconfl200/ and http://www.higgs-diesel.com/higgs-diesel/hawkv4/ for the actual-engine pages ( sorry I don't know how to do the references properly, please fix if you know how ), & this is produced by Higgs-Diesel, so the "Advanced Component Engineering" in the title of this paragraph isn't identifying the actual company.

The {{cvt|1000|in3|L}} v12 can power generators, tanks, boats or blimps and v4 and v8 versions can be derived.{{cite news |url= http://www.heavy-fuel-engines.com/design-of-our-v12-heavy-fuel-engine-complete/ |title= Design of Our v12 Heavy Fuel Engine |author= Kevin Eldredge |date= March 6, 2016 |publisher= Advanced Component Engineering}}

The Bourke engine, designed by Russell Bourke, of Petaluma, CA, is an opposed rigidly connected twin cylinder design using the detonation principle.{{citation needed|date=August 2019}}

Diesel Air Limited is a British company developing a {{cvt|100|hp|kW|order=flip}} twin-cylinder (therefore four-piston), two-stroke opposed-piston engine inspired by the original Junkers design. Their engine has flown in test aircraft and airship installations. Unlike the Junkers, it is made for horizontal installation with a central output shaft for the geared cranks, the overall installed shape thereby approximately resembling a four-stroke flat-four engine.{{cite web |url= http://www.dair.co.uk/ |title= Diesel Air Limited |access-date= 2010-07-07 |archive-date= 2006-04-04 |archive-url= https://web.archive.org/web/20060404110036/http://www.dair.co.uk/ |url-status= dead }}

Powerplant Developments, a British company, is developing a {{cvt|100|and|120|hp|kW|order=flip}} opposed-piston engine called the Gemini 100/120 that resembles the Diesel Air Limited engine and uses the Junkers twin-crank principle, again for horizontal installation with a central output shaft for the geared cranks. However, the Gemini 100 is an engine. Like Diesel Air Limited, Powerplant Developments claim to be using Weslake Air Services for production. They have recently announced that Tecnam will test a prototype with the Gemini engine.{{cite web |url= http://www.geminidiesel.aero |title= Gemini Diesel }}

Superior Air Parts' subsidiary Gemini Diesel develops three cylinder two-stroke designs with six opposed pistons:

• a 100 hp (75 kW) weighing 159.5 lb (72.5 kg),
• a turbocharged 125 hp (118 kW) weighing 175 lb (72.5 kg), both measuring 23” wide × 16” high × 23” long (58 × 40 cm × 58 cm) and reaching {{cvt|.38|and|.378|lb/hp/h|g/kW/h}} BSFC, respectively;
• larger three cylinder (six piston) engines would produce 180-200 hp (134-149 kW) weighing 276 lb (125 kg) in 29” W × 16” H × 29” L (73 × 41.5 × 72.5 cm) and 300-360 HP (224-268 KW) turbocharged whilst weighing 386 lb (175 kg) within 29” W × 19” H × 37” L (73 × 47.5 × 95 cm)
• five cylinder (10 piston) engines would produce 450 hp (336 kW) whilst weighing 474 lb (215 kg) within 29” W × 22” H × 43 ” L (73 × 55 × 110 cm)
• six cylinder(12 piston) engines would attain 550 hp (410 kW) whilst weighing 551 pounds (250 kg in 29” W × 22” H × 48” L (73 × 55 × 122 cm), burning {{cvt|.386|to|.360|lb/hp/h|g/kW/h}}{{cite web |url= http://www.geminidiesel.aero/application/files/5014/2828/3029/GEMINI_GenInfoSht_LowRez.pdf |title= General Info Data Sheet |publisher= Gemini Diesel}} The 100 hp version will cost less than $25,000.{{cite web |url= https://eps.aero/wp-content/uploads/2016/07/Kitplanes-Article_EPS_201608.pdf |title= ENGINE THEORY: Diesel Engines |work= KITPLANES |date= August 2016}}

Weslake Engine, another UK based company, displayed its A80 lightweight diesel engine at Friedrichshafen Aero 2015.{{cite web |url= http://www.weslake.eu/news/news.html |title= News |publisher= Weslake |date= April 2015 |access-date= 2014-07-08 |archive-url= https://web.archive.org/web/20140714120803/http://www.weslake.eu/news/news.html |archive-date= 2014-07-14 |url-status= dead }}

Wisconsin-based Engineered Propulsion Systems develops its Graflight liquid-cooled V-8 engine with steel pistons and compacted graphite iron crankcase for better strength and durability than aluminium at similar weight, increasing time between overhauls to 3,000 hours. It is managed by a Bosch ECU and consumes Jet A, JP-8 or straight diesel for general aviation aircraft and small helicopters, military drones, small boats or troop carriers, and its low vibration allows the use of composite or aluminium airscrews.{{cite web |url= https://eps.aero/the-eps-engine |title= Engine Overview |date= 28 July 2023 |publisher= Engineered Propulsion Systems}}

At {{cvt|262|hp|kW|0|order=flip}}, 75% of the {{cvt|350|hp|kW|0|order=flip}} maximum power, it consumes {{cvt|{{#expr:63/5.54*6.79round0}}|lb/h|kg/h|order=flip}}, in comparison to the Continental TSIO-550-E, which burns {{cvt|{{#expr:114/6.08*5.87round0}}|lb/h|kg/h|order=flip}}{{cite web |url= https://eps.aero/the-eps-engine/fuel-consumption/ |title= Fuel Economy |date= 28 July 2023 |publisher= Engineered Propulsion Systems}}

Raptor Turbo Diesel LLC, an American company, is currently developing the Raptor 105 diesel engine. It is a four-stroke inline turbo charged engine. Formerly Vulcan Aircraft Engines (until September 2007).{{cite web |url= http://www.raptor-aircraft.com/engine.html |title= Raptor Diesel GT |publisher= Raptor Aircraft }}

ECO Motors developed the EM 80 and EM {{cvt|100|hp|kW|order=flip}} 4 stroke 4 cylinder diesel with FADEC based on a car engine for {{cvt|98|kg|lb}} dry but disappeared since 2008.{{cite web |url= https://www.experimentalaircraft.info/homebuilt-aircraft/aircraft-diesel-manufacturers.php |title= Aircraft Diesel Manufacturers |work= Experimental Aircraft Info}}

The FlyEco diesel is a three-cylinder, {{cvt|0.8|L|in3}} engine producing 80 HP / 58,8 kW up to 3,800 RPM and reduced by 1:1.50-1.79, derived from the Smart Car.{{cite web |url= http://www.flyeco.net/smart_diesel.html |title= Smart diesel engine |publisher= FlyEco}}

It powers the Siemens-FlyEco Magnus eFusion hybrid electric aircraft.{{cite news |url= https://www.avweb.com/avwebflash/news/Aero-Siemens-and-FlyEco-Show-Off-Hybrid-230712-1.html |title= Aero: Siemens And FlyEco Show Off Hybrid |author= Jason Baker |date= April 22, 2018 |work= AvWeb}}

File:Paris Air Show 2017 mecachrome AE440 front.jpg

Within the Green Rotorcraft European Clean Sky Joint Technology Initiative environmental research program started in 2011, an Airbus Helicopters H120 Colibri technology demonstrator equipped with a HIPE AE440 high-compression diesel engine, running on jet fuel, first flew on 6 November 2015. The powerplant is a liquid-cooled, dry sump lubricated {{cvt|4.6|L|in3|adj=on}} 90° V8 engine with {{cvt|1800|bar|psi}} common rail direct injection, fully machined aluminium blocks, titanium connecting rods, steel pistons and liners, one turbocharger per cylinder bank.{{cite press release |url= https://www.airbushelicopters.com/website/en/press/Airbus-Helicopters-starts-flight-tests-with-high-compression-engine-for-cleaner,-more-efficient-and-higher-performance-rotorcraft_1859.html |title= Airbus Helicopters starts flight tests with high-compression piston engine |publisher= Airbus Helicopter |date= November 10, 2015}}

With an air/air intercooler, it weighs {{cvt|197|kg|lb}} (dry) without gearbox and the {{cvt|330|kW|hp}} installed powerpack weighs {{cvt|249|kg|lb}}.{{cite web |url= http://cordis.europa.eu/result/rcn/177069_en.html |title= Final Report Summary – HIPE AE 440 (Diesel Powerpack for a Light Helicopter Demonstrator) |work= CORDIS |publisher= European Commission |date= 19 Feb 2016}} Its brake specific fuel consumption is 200 g/kW.h.{{cite web |url= http://www.teos-engineering.com/experience/jet-a1-aircraft-engine/ |title= Jet A-1 Aircraft Engine |publisher= Teos Powertrain Engineering}} It is manufactured by Teos Powertrain Engineering, a joint venture between Mecachrome and D2T (IFPEN group) for the mechanical design, engine main parts manufacturing, assembly and testing and Austro Engine for the dual channel FADEC and harness, fuel system, airworthiness.

• List of aircraft engines

{{Reflist}}

{{Commons category|Aircraft diesel engines}}

• {{cite web |url= http://www.oldengine.org/members/diesel/Duxford/avrange.htm |title= Diesel Engines in Aviation |work= Peter & Rita Forbes' Engine Webpages |publisher= Oldengine.org |access-date= 2008-08-17 |archive-date= 2008-09-16 |archive-url= https://web.archive.org/web/20080916133713/http://www.oldengine.org/members/diesel/Duxford/avrange.htm |url-status= dead }}
• {{cite magazine |url= http://www.flyingmag.com/aircraft/diesel-aircraft-engines-revolution |title= Diesel Aircraft Engines Revolution |author= Stephen Pope |date= October 28, 2013 |magazine= Flying Magazine}}
• {{cite web |url= https://www.experimentalaircraft.info/homebuilt-aircraft/aircraft-engines.php |publisher= Experimental Aircraft Info |title= Aircraft Diesel Engines}}

{{DEFAULTSORT:Aircraft diesel engine}}

Category:Aircraft engines

Category:Diesel engines