Pratt
& Whitney Canada PW100
|
| The
Engine |
|
Specifications |
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| The
PW100 is a family of turboprop engines designed to power 30
to 70 seat regional transport aircraft. The family concept of
powerplant and gearbox allows a continuum of engines to meet a range
of performance requirements.
Work began on the PW100 in the late 1970s. |
|
 | Two-spool turboprop |
| Compressor: low- and high-pressure single-stage
centrifugal compressors |
| Turbine: low- and high-pressure single-stage
axial turbines |
| Power: two-stage axial "free"
turbines |
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| Models |
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Used
by |
| |
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| PW118: 1,800 hp (1340 kW) |
| PW120: 1,800 hp (1340 kW) |
| PW120A: 2,000 hp (1491 kW) |
| PW150A: 4,573 hp (3410 kW) |
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| Related
Pages |
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