Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

BMW 6012

From Wikipedia, the free encyclopedia
1960s German turboshaft aircraft engine
6012
BMW 6012 engine on display at theDeutsches Museum
TypeTurboshaft
National originGermany
ManufacturerBMW
First runc.1960
Major applicationsDornier Do 32

TheBMW 6012 (laterMTU 6012) was a Germanturboshaft andgas generator engine. Designed in the late-1950s byBMW the engine powered theDornier Do 32 helicopter and was also used as anauxiliary power unit (APU).

Variants

[edit]
6012A
Basic version.[1]
6012B 1
De-rated version.[1]
6012B 2
Version designed to produce 19 kW (25 shp) continuously to 7,000 m (23,000 ft).[1]
6012L
Gas generator version with additional gear-driven compressor.[1]

Applications

[edit]

Specifications (6012A)

[edit]

Data fromJane's All the World's Aircraft 1965-66.[1]

General characteristics

  • Type: Turboshaft
  • Length: 700 mm (28 in)
  • Diameter: 380 mm (15 in)
  • Dry weight: 45 kilograms (99 lb)

Components

  • Compressor: Single-stage radial
  • Combustors: Annular (disc shaped)
  • Turbine: Single-stage radial
  • Fuel type:Jet fuel
  • Oil system: Dry sump, gear-type pumps

Performance

  • Maximum power output: 75 kW (100 shp)
  • Overall pressure ratio: 3:1
  • Fuel consumption: 57 kg (125 lb) per hour at maximum power

See also

[edit]

Comparable engines

Related lists

References

[edit]
Wikimedia Commons has media related toBMW 6012.
Notes
  1. ^abcdeTaylor 1965, p. 462.
  2. ^www.deutsches-museum.de - Dornier Do 32 Retrieved: 18 January 2021
  • Taylor, John W.R.Jane's All the World's Aircraft 1965-66., Great Missenden, Sampson Low, Marston and Company Ltd, 1965.
Piston engines
Turbojets
Turbofans
Turboprops
Turboshafts
Rockets
Aeroderivatives
Retrieved from "https://en.wikipedia.org/w/index.php?title=BMW_6012&oldid=1211565875"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp