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Wikipedia / General Electric CF34

The General Electric CF34 is a civilian high-bypass turbofan developed by GE Aviation 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/C909. There are 7,500 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 high pressure (HP) compressor driven by a 2-stage 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 and , were derived from the CFM56 engine family, 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 for the variant.

On wing times can reach 14,000 hours, an overhaul costs over $1.5 million and a set of LLPss $2.1 million for a 25,000 cycle life. In 1995, GE invested $200 million to develop the -8C derivative for the CRJ700.

In a 2020 solicitation by the US Air Force called the B-52 Commercial Engine Replacement Program, GE had proposed updating the Boeing B-52 Stratofortress with CF34-10 engines. In September 2021, the Rolls-Royce F130 was selected instead of the GE proposal.

Applications

CF34-1A

CF34-3

CF34-3A

CF34-3B

CF34-8

CF34-8C

CF34-8E

CF34-10

CF34-10A

CF34-10E

Specifications

CF34-3

CF34-8C

CF34-8E

CF34-10A

CF34-10E

Application

CL600/CRJ200

CRJ700/900/1000

E170/175

C909

E190/195

Length

Diameter

Dry weight

Fan

Compressor

14 stages, 14:1

10 HP stages

3 + 9 stages

Turbine

4 + 2 stages

4 LP + 1 HP stage

Thrust (SL)

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)

CF34 Engine Comparison

See also

References