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Contents

   



(Top)
 


1 Variants  





2 Applications  





3 Specifications (6012A)  



3.1  General characteristics  





3.2  Components  





3.3  Performance  







4 See also  





5 References  














BMW 6012






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From Wikipedia, the free encyclopedia
 


6012
BMW 6012 engine on display at the Deutsches Museum
Type Turboshaft
National origin Germany
Manufacturer BMW
First run c.1960
Major applications Dornier Do 32

The BMW 6012 (later MTU 6012) was a German turboshaft and gas generator engine. Designed in the late-1950s by BMW the engine powered the Dornier Do 32 helicopter and was also used as an auxiliary 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 from Jane's All the World's Aircraft 1965-66.[1]

General characteristics

Components

Performance

See also[edit]

Comparable engines

Related lists

References[edit]

Notes
  1. ^ a b c d e Taylor 1965, p. 462.
  • ^ www.deutsches-museum.de - Dornier Do 32 Retrieved: 18 January 2021

  • Retrieved from "https://en.wikipedia.org/w/index.php?title=BMW_6012&oldid=1211565875"

    Categories: 
    BMW aircraft engines
    1960s turboshaft engines
    Aircraft gas generator engines
    Hidden categories: 
    Articles with short description
    Short description matches Wikidata
    Commons category link from Wikidata
     



    This page was last edited on 3 March 2024, at 06:22 (UTC).

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