MAN Turbo 6022

{{Infobox Aircraft Begin

|name= 6022

|image = File:Bückeburg Hubschraubermuseum 2011-by-RaBoe-41.jpg

|caption = MTU 6022 engine on display at the Hubschraubermuseum Bückeburg

}}

{{Infobox Aircraft Engine

|type= Turboshaft

|national origin = Germany

|manufacturer= MAN Turbo/MTU

|first run= 1962

|major applications= MBB Bo 105

|number built = 82

|program cost =

|unit cost =

|developed from =

|developed into =

|variants with their own articles =

}}

The MAN Turbo 6022 (also BMW 6022/MTU 6022) is a German gas turbine turboshaft engine for helicopter use. Designed in the early 1960s by BMW the engine powered the third prototype of the MBB Bo 105 on its maiden flight in December 1967.{{cite web |title=MTU-Museum Triebwerksgeschichte – gestern, heute und morgen |url=http://www.mtu.de/e-papers/MTU_ePaper/Marketing/MTU_Museum/epaper/ausgabe.pdf |website=mtu.de |publisher=MTU-Museum |access-date=23 March 2019 |location=München |page=19 |language=de |archive-date=4 March 2016 |archive-url=https://web.archive.org/web/20160304194848/http://www.mtu.de/e-papers/MTU_ePaper/Marketing/MTU_Museum/epaper/ausgabe.pdf |url-status=dead }}

Variants

;6022-A1

:Base variant. {{convert|217|shp|kW|disp=flip|abbr=on}} at 6,000 rpm.

;6022-A2

:{{convert|350|shp|kW|disp=flip|abbr=on}} at 6,000 rpm. Powered the third prototype Bo 105. Passed 100 hour type test in 1968.

;6022-A3

:{{convert|375|shp|kW|disp=flip|abbr=on}} at 6,000 rpm. Production engines for Bo 105 with strengthened reduction gear.

Applications

Dornier Aerodyne
MBB Bo 105 (third prototype)

Engines on display

Hubschraubermuseum Bückeburg

Specifications (6022-A3)

{{jetspecs

|ref=Jane's all the World's Aircraft 1972–73,{{cite book |title=Jane's all the World's Aircraft 1972–73 |editor1-last=Taylor |editor1-first=John W.R. |year=1972 |publisher=Sampson Low, Marston & Co. Ltd |location=London |isbn=0-354-00109-4 |page=671}} Aircraft engines of the World 1970{{cite book |last=Wilkinson |first=Paul H. |title=Aircraft engines of the World 1970 |year=1970 |publisher=Paul H. Wilkinson |location=Washington D.C. |edition=21st |page=195 }}

|type=Turboshaft

|length={{cvt|1062|mm}}

|diameter=~{{cvt|400|mm}} casing diameter

Width: {{cvt|429|mm}}
Height: {{cvt|670|mm}}

|weight={{convert|90|kg|lb|0|abbr=on}} (minus reduction gear and starter motor)

|compressor=Two-stage centrifugal

|combustion=Single tube

|turbine=Three-stage axial

|fueltype=Jet fuel

|oilsystem=pressure spray at {{cvt|44|psi|bar|order=flip}} with return scavenge

|power={{convert|375|shp|kW|order=flip|abbr=on}}

|thrust=

|compression=6.4:1

|bypass=

|aircon={{cvt|1.9|kg/s|lb/s}}

|turbinetemp=JPT {{cvt|590|C|K|order=flip}}

|fuelcon=

|specfuelcon= {{cvt|0.74|lb/hph|kg/kWh|order=flip}}

|power/weight={{cvt|1.89|shp/lb|kW/kg|order=flip}}

|thrust/weight=

}}

References

Category:1960s turboshaft engines