Honeywell HTF7000

The Honeywell HTF7000 is a turbofan engine for medium-sized business aircraft of the U.S. company Honeywell Aerospace.

Development

When the engine is a two-shaft engine which was first developed under the name of AS907 with a power range of the core engine from 17.8 to 40.0 kN. It was admitted by the FAA in June 2002 and was renamed in 2003 in HTF7000. His first assignment was in January 2005 at the Bombardier Challenger 300

The engine is equipped with a FADEC, Blisks and a reverse thrust system. It has four axial compressor stages, including two stators with variable geometry, a single radial compressor, a cooled combustion chamber, a two-stage high pressure as well as a three-stage low pressure turbine which drives a fan.

Versions

Specifications

  • Thrust: 28.89 to 33.33 kN
  • Bypass ratio: 4.4:1
  • Overall pressure ratio: 28,2:1
  • Brass Diameter: 0.87 m
  • Length: 2,347 m
  • Dry weight: 618.7 kg
Embraer Legacy 450 Embraer Legacy 500
398060
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