GE Honda HF120
| HF118 | |
|---|---|
| |
| Type | Turbofan |
| National origin | Japan / United States |
| Manufacturer | GE Honda Aero Engines |
| First run | 2009[1] |
| Major applications | Honda HA-420 HondaJet |
The GE Honda HF120 is a small turbofan for the light business jet market, the first engine to be produced by GE Honda Aero Engines.
Development
Succeeding Honda's original HF118 prototype, the HF120 was undergoing testing in July 2008, with certification targeted for late 2009.[2] The first engines were produced at GE's factory, but in November 2014 production shifted to Burlington, North Carolina.[3] The U.S. Federal Aviation Administration (FAA) awarded Part 33 certification to the HF120 turbofan engine in December 2013, and production certification in 2015.[4]
Design
The engine has a wide-chord swept fan, two-stage low-pressure compressor and counter rotating high-pressure compressor based on a titanium impeller, for a 2,050 lbf (9.1 kN) takeoff thrust.[5] The HF120 engine’s components interact with greater efficiency by incorporating 3D aerodynamic design and its effusion-cooled combustor design emits few NOx, CO and HC. Noise levels are quieter than Stage 4 requirements.[6]
In May 2016 time between overhaul was 2,500 h and should mature to 5,000 h ; a midlife hot-section inspection isn't required and it should remain on wing 40% longer than other engines and have lower operating costs : Honda maintenance plan should run at $139 per engine per hour.[7]
Applications
The engine was announced as a retrofit to the Cessna CitationJet CJ1 by Sierra Industries,[8] in partnership with GE Honda, besides the Hondajet.[9]
Specifications
Data from Honda[10]
General characteristics
- Type: Turbofan engine
- Length: 44 inches (110 cm)
- Diameter: maximum: 21.2 inches (54 cm)
- Dry weight: 211.3 kg (466 lb) with basic accessories and optional equipment[11]
Components
- Compressor: One wide-chord fan, two axial low-pressure stages, one centrifugal high-pressure stage.
- Combustors: compact reverse flow
- Turbine: One axial high-pressure stage, two axial low-pressure stages.
Performance
- Maximum thrust: takeoff thrust: 2,050 lbf (9.1 kN)
- Overall pressure ratio: 24
- Bypass ratio: 2.9
- Specific fuel consumption: <0.7 lb/lbf/h (20 g/kN/s)
- Thrust-to-weight ratio: 4.4
See also
Related lists
References
- ^ "GE Honda's HF120 Engine Completes First Run Test" (Press release). GE Aviation. October 19, 2009.
- ^ "Engine Prototyping prepares GE Honda Aero Engines for certification tests" (Press release). GE Aviation Press Release. July 28, 2008.
- ^ Curt Epstein (12 November 2014). "GE Honda Transitions HF120 Production to N. Carolina". Aviation International News.
- ^ Chad Trautvetter (18 March 2015). "GE Honda Wins FAA Production Certificate for HF120 Engine". Aviation International News.
- ^ "GE Honda Aero Engines". Flight International. Archived from the original on August 11, 2011.
{{cite web}}: Unknown parameter|deadurl=ignored (|url-status=suggested) (help) - ^ "HF120 Engine". GE Honda Aero Engines.
- ^ Fred George (May 26, 2016). "GE Honda HF120-H1A Turbofans". Business & Commercial Aviation. Aviation Week.
- ^ Chad Trautvetter (18 September 2014). "Sierra Selects GE Honda HF120 for Sapphire CitationJet Upgrade Program". Aviation International News.
- ^ Dan Parsons (20 October 2014), "GE Honda launches Cessna jet engine retrofit programme", Flightglobal
- ^ "HF120 Turbofan Engine". Honda Worldwide. Retrieved September 29, 2017.
- ^ "TCDS No.: IM.E.054" (PDF). EASA. 20 April 2016.
External links
