Aircraft diesel engine

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Thielert Centurion aircraft diesel engine.

The aircraft diesel engine or aero diesel has not been widely used as an aircraft engine. Diesel engines were used in airships and were tried in aircraft in the late 1920s and 1930s, but never widely used. Their main advantages are their excellent specific fuel consumption and the somewhat higher density of their fuel, but these have been outweighed by a combination of inherent disadvantages compared to gasoline-fueled or turboprop engines. The ever-rising cost of avgas and doubts about its future availability[according to whom?] have spurred a resurgence in aircraft diesel engine production in recent years.[when?]


Early diesel aircraft[edit]

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 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-IDX "Detroiter," registration number X7654 (presently owned by Greg Herrick, and based near Minneapolis, Minnesota).[1] Around 1936 the heavier but less thirsty diesel engines were only preferred over gasoline engines when flight time was over 6–7 hours.[2]

Jumo 205 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 later in the production run diesels were replaced with 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.[3]

Postwar development[edit]

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 near-death 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 3,000 hp (2,200 kW) 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.

Modern developments[edit]

Several factors have emerged to change this equation. 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.[4]



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".[5]

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.[6] 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.

Modern (21st century) aircraft diesel engine manufacturers[edit]


The first manufacturer to produce a certified design for the general aviation market was Thielert, located in the small town of Lichtenstein in the German state of Saxony. They produce four-stroke, liquid-cooled, geared, turbo-diesel aircraft engines based on Mercedes automotive designs which will run on both diesel and jet aviation fuel (Jet A-1). Their first engine, a 1.7 litres (100 in3), 135 hp (101 kW) four-cylinder (based on the 1.7 turbo diesel Mercedes A-class power unit), was first certified in 2002. It is certified for retrofitting to Cessna 172s and Piper Cherokees which were originally equipped with the 160 hp (120 kW) Lycoming O-320 320 cubic inches (5.2 l) Avgas engine. Although the weight of the 135 hp (101 kW) Thielert Centurion 1.7 at around 136 kilograms (300 lb) is similar to that of the 160 hp (120 kW) Lycoming O-320, its displacement is less than a third of that of the Lycoming. It however achieves maximum power at 2300 prop rpm (3900 crank rpm) as opposed to 2700 for the petrol Lycoming.

Thielert users included Austrian aircraft firm Diamond Aircraft Industries, which offered its single-engine Diamond DA40-TDI Star with a Thielert Centurion 1.7' engine, and also the DA42 (formerly known as Twin Star) with two. The twin-Thielert engined DA42 offered low fuel consumption with a high fuel efficiency of 15.1 L/h (3.3 imp gal/h; 4.0 gal/h). Several hundred Thielert-powered airplanes are flying. There was also a certified a 4.0-litre (240 cu in), V8, 310 hp (230 kW) version available from 2005 although this engine has not been certified for installation in any airframes. Apex aircraft, formerly Robin, also offered an aircraft (Ecoflyer) with the Thielert engine.

In May 2008, Thielert went bankrupt. Although Bruno M. Kubler, Thielert's insolvency administrator, 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.


SMA Engines, located in Bourges, 150 km south of Paris have designed a four-stroke, air-cooled, turbo-diesel aircraft engine from the ground up, the SR305-230. SMA's engineering team came from Renault Sport (Formula 1). The four cylinder 230 hp (170 kW), 305 cubic inch (5.0 liter) jet fuel engine first obtained European certification in April 2001, followed by US FAA certification in July 2002. It is now certified as retrofit on several Cessna 182 models in Europe and the USA, and Maule is working toward certification of the M-9-230.

SMA develops a 330-400 hp six cylinder version, the SR460.[7] 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 400 to 800 horsepower 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).[8]

United States[edit]

Interest in diesel aircraft in the United States has been more limited, due to its lower fuel taxes. However, doubt about the future availability of avgas has raised awareness of diesel alternatives. In March 2008 the Indus Aviation team led by Aldo Sibi (Director Of Production, Chief Mechanic and Head of Research and Development) prototyped the world's first diesel powered Light Sport Aircraft, N211GD. This airplane was built and flown in 30 days. This novel aircraft, although a prototype, sparked huge interest in alternative fuels in the industry. Mr. Sibi and his team also championed no less than 70 modifications and improvements. After the diesel project Mr. Sibi and his team took Indus to the next level, developing the Primary Trainer. This was an attractive low cost trainer that competed very well with the high-end imports from overseas.

Experimental engine manufacturers[edit]

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.[9] Examples include:

  • Bourke engine, designed by Russell Bourke, of Petaluma, CA, is an opposed rigidly connected twin cylinder design using the detonation principle.[10]
  • Diesel Air Limited, a British company developing a 100 hp (75 kW) 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.[11]
  • Powerplant Developments, a British company developing a 100 hp (75 kW) opposed-piston engine called the Gemini 100 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 a three-cylinder (therefore six-piston) 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.[12]
  • Wilksch Airmotive, a British company developing/producing a 120 hp (89 kW) three-cylinder (WAM-120) two-stroke diesel and working on a four-cylinder 160 hp (120 kW) 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. 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 125 knots (232 km/h) TAS at 6,000 ft (1,800 m) on 15 litre/hr of jet A1 fuel. A Rutan LongEz canard-pusher (G-LEZE) has also flown with the WAM120 engine with test flights showing a TAS of 160 kn (300 km/h) at 11,000 ft (3,400 m) and 22ltrs per hour. At economy cruise of 125 knots (232 km/h) at 2,000 ft (610 m) the fuel consumption is 12 ltrs/hr giving a range of 1,890 nautical miles (3,500 km); see [1]
  • Raptor Turbo Diesel LLC, an American company currently developing the Raptor 105 diesel engine. It is a four-stroke inline turbo charged engine. Formerly Vulcan Aircraft Engines (until September 2007).[13]
  • DeltaHawk Engines, an American company currently developing three V-4 designs of 160, 180 and 200 horsepower (150 kW), 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.[14] 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.[14][15] 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)
  • Eco-Motors, a company with sites in Germany and France, which developed an 100 hp (75 kW) aircraft engine based on a small turbocharged automotive diesel.[16][17]
  • GAP Diesel Engine, a NASA development.[18]
  • The Zoche aero-diesels company in 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.[19] A Zoche engine has run successfully in wind tunnel tests,[20] but Zoche seem barely closer to production than they were a decade ago.
  • Weslake Engine, another UK based company, announced in May 2014 that they finished prototype of a 2-stroke.[21]

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.

Teos/Austro Engine AE440[edit]

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.[22] The powerplant is a liquid-cooled, dry sump lubricated 4.6-liter 90° V8 engine with a 1800 bar common rail direct injection, fully machined aluminum blocks, titanium connecting rods, steel pistons and liners, one turbocharger per cylinder bank.[23]

With an air/air intercooler, it weighs 197 kg (dry) without gearbox and the 330 kW (440 hp) installed powerpack weighs 249 kg.[22] Its brake specific fuel consumption is 200 g/kW.h.[24] 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.[22]

See also[edit]


  1. ^ Mystery Engine Promises. 56. Popular Mechanics. September 1931. p. 456. Retrieved 2012-09-22. 
  2. ^ Odel, Axel. "Teknikken i luftfartens tjeneste" page 18-20 Ingeniøren, 2 May 1936. Accessed: 28 December 2014.
  3. ^ "rolls-royce condor | 1932 | 1172 | Flight Archive". 1932-11-17. p. 1094. Retrieved 2012-09-22. 
  4. ^ Vassilios Pachidis. Clean Sky Technology Evaluator Environmental Performance Assessment of Rotorcraft , page 36. Cranfield University, 20 October 2015.
  5. ^ Shute, Nevil (1954). Slide Rule. London: Heinemann. pp. 98–99. 
  6. ^ Leasor, James (1957). The Millionth Chance: The story of the R101. London: Hamish Hamilton. p. 78. 
  7. ^ "The innovation by SMA, the SR460" (Press release). Safran SMA. 3 September 2015. 
  8. ^ "SMA Debuts Its High Power Density Engine". AviationPros. 13 October 2016. 
  9. ^ "W W W . D I E S E L A I R . C O M - The Diesel Air Newsletter - Home". Retrieved 2012-09-22. 
  10. ^ "Bourke Engine". 2007-04-24. Retrieved 2012-09-22. 
  11. ^ "Diesel Air Limited". Archived from the original on 2006-04-04. Retrieved 2012-09-22. 
  12. ^ "Gemini Engine". Retrieved 2012-09-22. 
  13. ^ "". Retrieved 2012-09-22. 
  14. ^ a b "DeltaHawk Diesel Engines". 2008-08-14. Retrieved 2012-09-22. 
  15. ^ Created: August 10, 2009 (2009-08-10). "DeltaHawk Diesel-Powered SR20 Announced". Retrieved 2012-09-22. 
  16. ^ "Home". Retrieved 2012-09-22. 
  17. ^ "Diesel Design by EcoMotors". Businessweek. 2008-03-21. Retrieved 2012-09-22. 
  18. ^ "NASA - Small Aircraft Propulsion: The Future Is Here". 2008-05-20. Retrieved 2012-09-22. 
  19. ^ "Zoche brochure" (PDF). Retrieved 2012-09-22. 
  20. ^ "zoche aero-diesels testbench video". Retrieved 2012-09-22. 
  21. ^ "News Page Weslake". Retrieved 2014-07-05. 
  22. ^ a b c "Final Report Summary - HIPE AE 440 (Diesel Powerpack for a Light Helicopter Demonstrator)". CORDIS. European Commission. 19 Feb 2016. 
  23. ^ "Airbus Helicopters starts flight tests with high-compression piston engine" (Press release). Airbus Helicopter. November 10, 2015. 
  24. ^ "Jet A-1 Aircraft Engine". Teos Powertrain Engineering. 

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