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Sichuan Hongying Dongli Keji Youxian Gongsi HF150 Turbofan Engine

By Sichuan Hongying Dongli Keji Youxian Gongsi ↗

The Sinohawk Power HF150 is a single-rotor turbofan engine for unmanned aircraft and other flying platforms. Its fan, centrifugal compressor and axial-flow turbine deliver a maximum thrust of 160 daN. The engine weighs 25 kg, measures 250 mm in diameter by 760 mm long, and supports electric motor and pyrotechnic starting.

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HF150 turbofan engine with metal housing and mounting brackets on a blue background
HF150 turbofan engine with metal housing and mounting brackets on a blue background
Model and typeHF150 turbofan engineProduct detail page
ApplicationUnmanned aircraft and other flying platformsApplication stated by the manufacturer
Starting methodsElectric motor and pyrotechnic startingSupported methods
Physical architectureSingle-rotor turbofan with a single-stage fan, single-stage centrifugal compressor and axial-flow turbine
Maximum thrust160 daN
Specific fuel consumption1.03 kg/daN·hAt maximum rotational speed.

Product overview

The Sinohawk Power HF150 is a turbofan propulsion engine for unmanned aircraft and other flying platforms. Its single-rotor arrangement combines a single-stage fan, a single-stage centrifugal compressor and an axial-flow turbine in a compact structure intended for integration into aircraft. The engine weighs 25 kg, measures 250 mm in diameter and is 760 mm long. It supports electric motor and pyrotechnic starting. Maximum thrust is 160 daN, maximum rotational speed is 54900 rpm and air mass flow is 4.50 kg/s.

At maximum rotational speed, the HF150 has a specific fuel consumption of 1.03 kg/daN·h and a volumetric fuel consumption of 3.43 L/min. Its exhaust temperature is 650 °C. The maximum starting altitude is 4000 m, while the maximum flight altitude is 12000 m. Maximum flight speed is Mach 0.8, and the operating temperature range extends from -40 to 55 °C. The engine has a maintenance interval of 25 hours, alongside these stated temperature, altitude and speed limits.

Specifications

SpecificationValue & conditions
Model and typeHF150 turbofan engineProduct detail page
ApplicationUnmanned aircraft and other flying platformsApplication stated by the manufacturer
Starting methodsElectric motor and pyrotechnic startingSupported methods
Physical architectureSingle-rotor turbofan with a single-stage fan, single-stage centrifugal compressor and axial-flow turbine
Maximum thrust160 daN
Specific fuel consumption1.03 kg/daN·hAt maximum rotational speed.
Fuel consumption3.43 L/minAt maximum rotational speed.
Weight25 kg
Diameter250 mm
Length760 mm
Maximum rotational speed54900 rpm
Air mass flow4.50 kg/s
Exhaust temperature650 °C
Maximum starting altitude4000 m
Maximum flight altitude12000 m
Maximum flight speedMach 0.8
Operating temperature range-40 to 55 °C
Maintenance interval25 h
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