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Turbomeca Arriel

The Turbomeca Arriel is a series of French turboshaft engines that first ran in 1974.[1] Delivering 650 to 1,000 hp (480 to 750 kW), over 12,000 Arriel engines have been produced from 1978 to 2018, logging more than 50 million flight hours for 40 helicopter applications. In June 2018, 1,000 Arriel 2D were in service, powering H125 and H130 single-engine helicopters, having logged one million flight hours since 2011. After endurance tests and fleet data analysis, their TBO increased by 25% to 5,000 hours and mandatory inspection rose to 15 years with no hourly limit, lowering maintenance costs.[2]

Arriel
Cutaway of a Turbomeca Arriel
Type Turboshaft
National origin France
Manufacturer Turbomeca
Safran Helicopter Engines
First run 1974
Major applications Agusta A109
Eurocopter MH-65 Dolphin
Sikorsky S-76
Harbin Z-9
Harbin Z-19
Number built 10,000

The Liming WZ-8 (turboshaft) and Liming WJ-9 (turboprop) are the designations for Turbomeca Arriel production in China. In 2021 Safran opened a production facility in Grand Prairie, Texas for production of Arriel 2E engines, which had previously only been produced in France.[3]

Applications edit

Specifications (Arriel 1) edit

Data from FAA Type Certificate Data Sheet.[4]

General characteristics

  • Type: Turboshaft engine
  • Length: 112.2 cm (44.2 in)
  • Diameter: 60 cm (24 in)
  • Dry weight: 111 kg (245 lb)

Components

Performance

See also edit

Related lists

References edit

  1. ^ Gunston 1989, p.170.
  2. ^ Mark Huber (June 27, 2018). "Safran Boosts Arriel 2D TBO by 25 Percent". AIN online.
  3. ^ O'Connor, Kate (19 October 2021). "Safran Opens Arriel 2E Assembly Line In U.S." AVweb. Retrieved 20 October 2021.
  4. ^ FAA Type Certificate Data Sheet Retrieved: 2 November 2008
  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. p. 166.

External links edit

  • Turbomeca Arriel official site

turbomeca, arriel, series, french, turboshaft, engines, that, first, 1974, delivering, over, arriel, engines, have, been, produced, from, 1978, 2018, logging, more, than, million, flight, hours, helicopter, applications, june, 2018, arriel, were, service, powe. The Turbomeca Arriel is a series of French turboshaft engines that first ran in 1974 1 Delivering 650 to 1 000 hp 480 to 750 kW over 12 000 Arriel engines have been produced from 1978 to 2018 logging more than 50 million flight hours for 40 helicopter applications In June 2018 1 000 Arriel 2D were in service powering H125 and H130 single engine helicopters having logged one million flight hours since 2011 After endurance tests and fleet data analysis their TBO increased by 25 to 5 000 hours and mandatory inspection rose to 15 years with no hourly limit lowering maintenance costs 2 ArrielCutaway of a Turbomeca ArrielType TurboshaftNational origin FranceManufacturer Turbomeca Safran Helicopter EnginesFirst run 1974Major applications Agusta A109 Eurocopter MH 65 Dolphin Sikorsky S 76 Harbin Z 9 Harbin Z 19Number built 10 000The Liming WZ 8 turboshaft and Liming WJ 9 turboprop are the designations for Turbomeca Arriel production in China In 2021 Safran opened a production facility in Grand Prairie Texas for production of Arriel 2E engines which had previously only been produced in France 3 Contents 1 Applications 2 Specifications Arriel 1 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 References 5 External linksApplications editAgustaWestland AW109 Eurocopter AS365 Dauphin Eurocopter AS565 Panther Eurocopter MH 65 Dolphin Eurocopter EC130 Eurocopter EC145 Eurocopter EC155 Eurocopter AS350 Ecureuil Harbin Z 9 Harbin Z 19 Kopter AW09 MBB Kawasaki BK 117 Sikorsky S 76Specifications Arriel 1 editData from FAA Type Certificate Data Sheet 4 General characteristics Type Turboshaft engine Length 112 2 cm 44 2 in Diameter 60 cm 24 in Dry weight 111 kg 245 lb Components Compressor Single stage axial plus single stage centrifugal Combustors Annular combustion chamber Turbine Single stage power turbine two stage gas generator turbine Fuel type Jet A1Performance Maximum power output 681 shp 508 kW Overall pressure ratio 8 1 Turbine inlet temperature 840 C 1 540 F Power to weight ratio 5 kilowatts per kilogram 3 0 hp lb approxSee also editRelated lists List of aircraft enginesReferences edit Gunston 1989 p 170 Mark Huber June 27 2018 Safran Boosts Arriel 2D TBO by 25 Percent AIN online O Connor Kate 19 October 2021 Safran Opens Arriel 2E Assembly Line In U S AVweb Retrieved 20 October 2021 FAA Type Certificate Data Sheet Retrieved 2 November 2008 Gunston Bill 1986 World Encyclopedia of Aero Engines Wellingborough Patrick Stephens p 166 External links edit nbsp Wikimedia Commons has media related to Turbomeca Arriel Turbomeca Arriel official site Retrieved from https en wikipedia org w index php title Turbomeca Arriel amp oldid 1195160441, wikipedia, wiki, book, books, library,

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