| 词条 | Turbomeca Makila | ||||||||||||||
| 释义 |
The Turbomeca Makila is a family of French turboshaft engines for helicopter use, first run in 1976 and flown in 1977.[1] Typical power output is around 1,300 kW (1,700 hp).[2] {{As of|2012}}, some 2,200 had been built.[2] Applications
Variants
Specifications (Makila 2A){{jetspecs|ref=Turbomeca.[3] |type=Free-turbine turboshaft |length={{convert|1836|mm|in|0|abbr=on}} |height={{convert|620|mm|in|0|abbr=on}} |diameter={{convert|498|mm|in|0|abbr=on}} |weight=278.9 kg (including FADEC) |compressor=3-stage axial flow LP, single-stage centrifugal flow HP |combustion=Annular |turbine=2-stage axial flow free turbine |fueltype= |oilsystem= |power=1,801kW (2,415 shp) |thrust= |compression= |aircon= |turbinetemp= |fuelcon= |specfuelcon= |power/weight= |thrust/weight= }} See also{{aircontent|see also= |related= |similar aircraft= |lists=
|similar engines= }} References{{Commons category}}
1. ^Flight International - Turbomeca Makila www.flightglobal.com Retrieved: 3 January 2012 2. ^1 SAFRAN - Turbomeca Makila {{webarchive|url=https://web.archive.org/web/20120120160909/http://www.turbomeca.com/english/our-products/helicopter-engines/makila-49/ |date=2012-01-20 }} www.turbomeca.com Retrieved: 3 January 2012 3. ^Turbomeca Makila - Manufacturer's data sheet. {{webarchive|url=https://web.archive.org/web/20120427115236/http://www.turbomeca.com/IMG/pdf/fiche_moteur_makila_1-_2.pdf |date=2012-04-27 }} www.turbomeca.com Retrieved: 3 January 2012
2 : Turbomeca aircraft engines|Turboshaft engines 1970–1979 |
||||||||||||||
| 随便看 |
|
开放百科全书收录14589846条英语、德语、日语等多语种百科知识，基本涵盖了大多数领域的百科知识，是一部内容自由、开放的电子版国际百科全书。