Pratt & Whitney Canada PW300
The Pratt & Whitney Canada PW300 is a family of turbofan engines in the thrust range of 20 to 35 kN, which have been developed specifically for business aircraft. The basic structure consists of a single stage fan, powered by a three-stage low-pressure turbine, a single-stage and four-stage axial centrifugal high pressure compressor driven by a two-stage high pressure turbine, and an annular combustion chamber. Some versions have a non -mixing nozzle, but the PW306 and PW308 close the action mixer for the exhaust jet with a. The engines are controlled by a FADEC system.
Is used the PW300 among others, the Learjet 60, Cessna Citation Sovereign, Gulfstream G200, Hawker 1000, Dassault Falcon 7X, Fairchild Dornier 328JET and White Knight Two.
The PW307 has been specially developed for the three- turbine arrangement of the Dassault Falcon 7X. It was approved by the Canadian Aviation Authority in March 2005.