SMA SR305-230
| SR305-230 | |
|---|---|
| |
| Type | Four-cylinder four-stroke diesel aero engine |
| National origin | France |
| Manufacturer | SMA Engines |
| First run | 1998 (First flight) |
| Major applications | Cessna 182 |
| Number built | >50 |
| Developed into | Continental TD-300 |
The SMA SR305-230 is an air/oil-cooled, horizontally opposed, four-cylinder, four-stroke, diesel piston aircraft engine. The engine is manufactured by SMA Engines, and is currently the only product of this French company. The engine is offered as a conversion package for the Cessna 182.
Design
[edit]The SMA SR 305-230-1 is a four-cylinder, horizontally opposed turbocharged direct fuel injection diesel engine. The engine installation includes an electronic central processing unit (CPU) that continually calculates the proper fuel/air mixture. If this unit fails completely during flight, the mechanical backup position is selected and the pilot can control the fuel/air mixture as required to complete the flight.[citation needed]
Full-throttle operation at sea level is at 90 inches (3 bar) of manifold pressure. Unlike some aircraft engines, which recommend the maximum power setting be used only for five minutes during the initial takeoff stage, the SR 305 can be operated indefinitely at this setting, although normal cruise uses around 70 inches (2.3 bar) and economy cruise uses around 60 inches (2 bar) of manifold pressure.[citation needed]
The STC conversion on the Cessna 182 includes a new cowl, both to accommodate the different engine dimensions and to provide the required cooling airflow. Belly-mounted cowl flaps are still used, but less cooling airflow is directed over the cylinder barrels and more cooling airflow is directed into side-mounted oil coolers. About one-third of the engine cooling is provided by airflow over the cylinders; the remainder is provided by engine oil. The engine's oil distribution system routes a large oil flow to hot zones in the cylinder heads and upper cylinder barrels, carrying the heat away to the oil coolers.[1]
As of early 2008, SMA had provided over 50 conversion packages. (The installation is usually performed by other companies, not SMA.) Most of those conversions were performed in Europe, with less than a dozen having been performed in North America.[citation needed]
The cost of conversion may be justified in areas where aviation gasoline costs significantly more than jet fuel, and by the fact that the diesel fuel flow at cruise is about 10 gallons (38 litres) per hour, compared to about 13.5 gallons (51 litres) per hour with the original engine.[citation needed]
SMA expects 90 engines to be delivered in 2014, and is working on six-cylinder version called the SR460 which will have an output of 330 to 400 hp (246 to 298 kW).[2]
Applications
[edit]- SMA SR305-230: Cessna 182 (STC conversion)
- SMA SR305-260E: Diamond DA50[3]
- SMA SR305-230 ATLS GS-301 Batoor[4]
In July 2012, Cessna announced it would offer the Cessna 182 with this engine as a factory option, with deliveries expected by the second quarter of 2013. Cessna also stated at that time that the SMA engine would eventually replace the current avgas engine. The plan was abandoned and in 2023 the Cessna 182 was still being sold only with the Lycoming IO-540-AB1A5 gasoline engine.[5][6][7]
Specifications
[edit]
Data from EASA TCDS[8]
General characteristics
- Type: Four-cylinder, four-stroke diesel aircraft engine
- Displacement: 4,988 cm3 (304 cu in)
- Length: 834 mm (33 in)
- Width: 930 mm (37 in)
- Height: 750–784 mm (30–31 in)
- Dry weight: 195–207 kg (430–456 lb)
Components
- Fuel type: Jet fuel A/A-1
- Cooling system: Air/oil-cooled
- Reduction gear: Direct drive
Performance
- Power output: 169–194 kW (227–260 hp) at 2,200 rpm, producing 734–842 N⋅m (541–621 lb⋅ft) of torque, a 18.5-21.2 bar mean effective pressure
See also
[edit]Related development
Comparable engines
Related lists
References
[edit]- ^ Cessna Skylane Joins the Jet Set, Flying Magazine, Vol. 135, No. 5, May 2008, p. 74
- ^ Thurber, Matt. "AirVenture Report: 2014" AINonline, 1 September 2014. Accessed: 4 September 2014.
- ^ "DA50 Series - Preliminary Technical Specifications". Diamond Aircraft.
- ^ ATLS GS-301 Batoor - atls.com.pk Retrieved: 12 August 2022
- ^ "Cessna Unveils Jet A Engine For Skylane". Avweb.com. 22 July 2012. Archived from the original on 31 July 2023. Retrieved 11 October 2012.
- ^ Goyer, Robert (24 September 2012). "Cessna 182 JT-A - The future of the iconic 182 smells distinctly like kerosene". Flying. Archived from the original on 31 July 2023. Retrieved 31 July 2023.
- ^ Textron Aviation. "Cessna Skylane". cessna.txtav.comyear= 2023. Archived from the original on 24 March 2023. Retrieved 31 July 2023.
- ^ "Type Certificate Data Sheets No. E.076" (PDF). EASA. 15 February 2019. Archived from the original (PDF) on 18 January 2021. Retrieved 6 March 2019.
External links
[edit]