PW100TS engine family is a direct derivative from the PW100 turboprop engine, incorporating the latest advanced technologies in the drive to exceed our customer’s expectations in performance, reliability, durability, fuel consumption and environmental friendliness. The PW100TS will leverage the widely acclaimed low fuel consumption and environmental friendliness of the PW100 turboprop engine. The PW100 is a three-shaft, two-spool engine. Low pressure and high pressure compressors are powered independently by cooled turbine stages. A third shaft couples the power turbine to the helicopter rotor system through a direct drive output shaft. The latest technology materials and engine control features result in a family of engines that will achieve impressive maintenance intervals, high dispatch reliability and provide the pilot and maintenance crew with easy engine operation and maintenance.
Two-spool, two-stage centrifugal compressors
- All rotors integrally bladed
- Each driven independently by low pressure and high pressure compressor turbines
- No variable geometry
- Easy electric start – no APU required