HKP 15 - Agusta A109LUHS (2002-    )

Helicopter Sweden

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HKP 15 (# 15236) at airshow, Såtenäs, Sweden 2009. Photo Lars Henriksson, www.avrosys.nu
 

Power Plant

Both versions of HKP 15 are powered by two Turbomeca Arrius 2K2 turboshaft engines each. The manufacturer states the following particulars. See also www.turbomeca.com :

One Engine Operative (OEI)
- OEI 2,5 minutes: 590 kW / 791 shp
- OEI continuous: 534 kW / 716 shp

All Engines Operative (AEO)
- Take off 534 kW / 716 shp
- Max. continuous 454 kW / 609 shp

Length 973 mm / 38.3 in
Width 538 mm / 21.9 in
Height 638 mm / 25.1 in

Power output shaft speed 6000 rpm

Clean burning – extremely low combustion number

Very low scheduled maintenance – less than 1 minute per running hour

Two wholly replaceable modules – gas generator module and reduction gear box module

Long TBO period (3000 hours)

The engine electronic control unit

- improves overall safety and reduces pilot work load
- indicates operational parameters
- drives engine life safety to its TBO limits
- signals maintenance actions on automatic engine overrun display
- OEI training function
- N1 control optimizes engine life

(shp = Shaft Horse Power, TBO = Time Between Overhaul)
 

 
Principal drawing of the Turbomeca Arrius 2K2 turboshaft helicopter engine
Principal drawing of the Turbomeca Arrius 2K2 engine
 
 
 
HKP 15 (# 15236) at airshow, Såtenäs, Sweden 2009. Photo Lars Henriksson, www.avrosys.nu
The Turbomeca Arrius 2K2 engine
 
 
 

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© Lars Henriksson

Updated: 2010-07-14

 

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