Hirth 3202

From Wikipedia, the free encyclopedia
Jump to navigation Jump to search

Template:Short description Script error: No such module "Unsubst". Template:Use British English

The Hirth 3202 and 3203 are a family of in-line twin cylinder, two stroke, carburetted aircraft engines, with optional fuel injection, designed for use on ultralight aircraft, especially two seat ultralight trainers, gyrocopters and small homebuilts. It is manufactured by Hirth of Germany.[1][2]

Development

The 3203 was developed as a replacement for the Hirth 2706 and as a competitor to the Script error: No such module "convert". Rotax 582. It replaced the 2706 in the Hirth line in May 2002. The engine is similar to the Rotax powerplant in being a two-cylinder in-line engine, with dual capacitor discharge ignition, although it is air-cooled, compared to the 582's liquid cooling. The 3202 was developed from the 3203 as a de-rated version to replace the Hirth 2704 and compete with the Script error: No such module "convert". Rotax 503. Both engines have the same bore, stroke, displacement, compression ratio, and weight as the Hirth engines they replace.[1][2]

Both the 3202 and 3203 use free air or fan cooling, with dual Bing 34 mm slide carburetors or optionally fuel injection. The cylinder walls are electrochemically coated with Nikasil. Standard starting is recoil start with electric start as an option. The reduction drive system available is the G-50 gearbox, with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1, with a cog-belt reduction drive optional.[1][2]

The engines run on a 50:1 pre-mix of unleaded 93 octane auto fuel and oil, or optionally oil injection.[1][2]

Variants

3202
Twin-cylinder in-line, two stroke, aircraft engine with a dual Bing 34mm slide carburetors or fuel injection. Produces Script error: No such module "convert". at 5500 rpm and has a factory rated TBO of 1200 hours. In production. Replaced the 2704 in production in May 2002.[1]
3203
Twin-cylinder in-line, two stroke, aircraft engine with dual Bing 34mm slide carburetors or fuel injection. Produces Script error: No such module "convert". at 6300 rpm and has a factory rated TBO of 1000 hours. In production. Replaced the 2706 in production in May 2002.[2]

Applications

3202

Script error: No such module "Template wrapper".Script error: No such module "Check for unknown parameters".

3203

Script error: No such module "Template wrapper".Script error: No such module "Check for unknown parameters".

Specifications (3203)

Data from Recreational Power Engineering[2]

General characteristics

  • Type: Twin cylinder, two-stroke, in-line, aircraft engine
  • Bore: Script error: No such module "convert".
  • Stroke: Script error: No such module "convert".
  • Displacement: 625 cc (38.1 cu in)
  • Length: Script error: No such module "convert".
  • Width: Script error: No such module "convert".
  • Height: Script error: No such module "convert".
  • Dry weight: Script error: No such module "convert".with free air cooling, Script error: No such module "convert". with fan cooling, including electric starter and exhaust. G-50 gearbox adds an additional Script error: No such module "convert".

Components

  • Fuel system: 2 X Bing 34mm slide type carburetors or fuel injection
  • Fuel type: unleaded 93 octane auto fuel
  • Oil system: 50:1 fuel/oil premix or oil injection
  • Cooling system: free air or fan
  • Reduction gear: G-50 gearbox with reduction ratios of 2.16:1, 2.29:1, 2.59:1, 3.16:1, or 3.65:1 or cog-belt

Performance

  • Power output: Script error: No such module "convert". at 5500 rpm
  • Compression ratio: 9.5:1

See also

References

<templatestyles src="Reflist/styles.css" />

  1. a b c d e Script error: No such module "citation/CS1".
  2. a b c d e f Script error: No such module "citation/CS1".

Script error: No such module "Check for unknown parameters".

External links

Script error: No such module "Navbox".