Английская Википедия:General Electric CF34
Шаблон:Short description Шаблон:More citations needed
Шаблон:Infobox Aircraft EngineThe General Electric CF34 is a civilian high-bypass turbofan developed by GE Aircraft Engines from its TF34 military engine. The CF34 is used on a number of business and regional jets, including the Bombardier CRJ series, the Embraer E-Jets, and Comac ARJ21.[1][2] In 2012, there were 5,600 engines in service.
Design and development
The original engine contained a single stage fan driven by a 4-stage low pressure (LP) turbine, supercharging a 14-stage HP compressor driven by a 2-stage high pressure (HP) turbine, with an annular combustor. Later higher thrust versions of the CF34 feature an advanced technology core, with only 10 HP compressor stages. Latest variants, the Шаблон:Nowrap and Шаблон:Nowrap, were derived from the CFM56 engine family,Шаблон:Citation needed and have a radically different HP spool, containing a 9-stage compressor driven by a single stage turbine. The LP spool has 3 core booster stages behind the fan. Static thrust is Шаблон:Convert for the Шаблон:Nowrap variant.
On wing times can reach 14,000 hours, an overhaul costs over $1.5 million and a set of LLPs $2.1 million for a 25,000 cycle life.[3] In 1995, GE invested $200 million to develop the -8C derivative for the CRJ700.[4]
GE had proposed updating the Boeing B-52 Stratofortress with CF34-10 engines, [5] but the Rolls-Royce F130 was selected in September 2021[6] instead.
Applications
- CF34-1A
- CF34-3A
- CF34-3A1
- CF34-3A2
- CF34-3B
- CF34-3B1
- CF34-3B
- CF34-8C1
- CF34-8C5
- CF34-8C5A1
- CF34-8C5A2
- CF34-8C5B1
- CF34-8E
- CF34-10A
- CF34-10E
Specifications
CF34-3[8] | CF34-8C[9] | CF34-8E[10] | CF34-10A[11] | CF34-10E[12] | |
---|---|---|---|---|---|
Application | CL600/CRJ200 | CRJ700/900/1000 | E170/175 | ARJ21 | E190/195 |
Length | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert |
Diameter | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert |
Dry weight | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert |
Fan | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | ||
Compressor | 14 Шаблон:Abbr stages, 14:1 | 10 HP stages | 3 Шаблон:Abbr + 9 Шаблон:Abbr stages | ||
Turbine | 4 Шаблон:Abbr + 2 Шаблон:Abbr stages | 4 LP + 1 HP stage | |||
Thrust (SL) | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert |
Thrust/weight | 5.52:1 | 5.7-6:1 | 5.6:1 | 5.1:1 | 5.2:1 |
OPR (max. power) | 21:1 | 28-28.5:1 | 28.5:1 | 29:1 | |
Bypass ratio | 6.2:1 | 5:1 | 5.4:1 | ||
SFC (Cruise) | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert | Шаблон:Convert |
See also
References
External links
Шаблон:GE aeroengines Шаблон:USAF gas turbine engines
- ↑ The CF34 at aviationpros.com
- ↑ GE's CF34-3 Engines Celebrate 20 Years of Regional Jet Service at aviationpros.com
- ↑ Шаблон:Cite news
- ↑ Шаблон:Cite magazine
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web
- ↑ Шаблон:Cite web