Hirth HM 508

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

Template:Short description

The Hirth HM 508 was an air-cooled, eight-cylinder, 60° cylinder bank angle inverted-V aircraft engine built in Germany in the 1930s.[1] It had a bore and stroke of 105 mm × 115 mm (4.1 in × 4.5 in) and developed 210 kW (280 hp) at 3,000 rpm.

Variants

HM 8U
HM 508A
HM 508B
HM 508C
Template:Cvt[2]
HM 508D
Template:Cvt at 3000 rpm[3]
HM 508E
Template:Cvt
HM 508F
HM 508G
HM 508H
Template:Cvt, low fuel consumption variant, with centrifugal supercharger geared at 3.86:1 crankshaft speed for long-range record breaking aircraft.

Applications

Specifications (HM 508D)

Data from Flugzeug-Typenbuch. Handbuch der deutschen Luftfahrt- und Zubehör-Industrie 1944,[4] Jane's fighting aircraft of World War II,[3] Jane's all the World's Aircraft 1938[5]

General characteristics

Template:Cvt wet, equipped

Components

  • Valvetrain: 1 inlet and 1 exhaust under-valve per cylinder driven by pushrods and rockers
  • Supercharger: Centrifugal supercharger geared at 4.47:1 crankshaft speed
  • Fuel system: 2x Pallas-Zenith 65 VAH2 carbutettors
  • Fuel type: 87 Octane gasoline
  • Oil system: Pressure system for crankshaft, pistons and reduction gear at Template:Cvt: splash lubrication for camshaft and supercharger
  • Cooling system: Air-cooled
  • 1x Double Bosch magneto

Performance

  • Power output:

See also

Comparable engines

Related lists

References

Template:Sister project

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

  1. Script error: No such module "citation/CS1".
  2. Script error: No such module "citation/CS1".
  3. a b Script error: No such module "citation/CS1".
  4. Script error: No such module "citation/CS1".
  5. Script error: No such module "citation/CS1".

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

Template:Hirth aeroengines