Pratt & Whitney Canada PW300
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The Pratt & Whitney Canada PW300 is a family of turbofan engines being developed specifically for business jet applications. The basic configuration is as follows: single stage fan, driven by a three-stage low pressure turbine, supercharging a four-stage axial/single stage centrifugal high pressure compressor, driven by a two stage high pressure turbine. An annular combustor is featured. Some versions have an unmixed exhaust, but the PW306 and PW308 include a forced mixer. A Full Authority Digital Engine Control (FADEC) system is incorporated.
Applications include the Learjet 60, Cessna Sovereign, Gulfstream G200, Hawker 1000, Dassault Falcon 7X and Fairchild-Dornier 328JET.
The PW307 is a new centre-line engine developed specifically for a tri-jet application on the Falcon 7X. The PW307 was certified by Transport Canada in March 2005.
| PW300 Leading Particulars | ||||||||
|---|---|---|---|---|---|---|---|---|
| PW305B | PW306A | PW307A | PW308C | |||||
| Thrust (lbf) | 5,258 | 6,400 | 6,100 | 7,000 | ||||
| Specific Fuel Consumption (lb/hr/lbf) | 0.391 | 0.394 | ? | ? | ||||
| Bypass Ratio | 4.3 | 4.5 | ? | ? | ||||
| Overall Pressure Ratio | 15.5 | 18.3 | ? | ? | ||||
| Overall Length (in) | 65.0 | 75.6 | ? | ? | ||||
| Approximate Fan Diameter (in) | 30.7 | 31.65 | 32.8 | 33.2 | ||||
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