Pratt & Whitney Canada PW500

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The Pratt & Whitney Canada PW500 is a family of twin-shaft turbofan engines in the 13.3 to 20 kN thrust range that have been specially developed for business aircraft.

construction

It contains a new core engine compared to the PW300 . The PW530 range contains a single-stage fan that is driven by a two-stage uncooled turbine with integral bladed rotor technology (blisk). In the high pressure system there is a two-stage axial compressor and a single-stage centrifugal compressor which is driven by a single-stage turbine and an annular combustion chamber . Although similar in configuration, the PW535 series has an additional T-stage attached to the low pressure shaft behind the fan to increase the overall pressure ratio and core throughput.

The more powerful PW545 series has (similar to the PW535) an additional BR booster stage to drive the larger fan (blisk) and a three-stage turbine. Compared to the PW300, this reduces fuel consumption by 10 to 15%.

The first test run of a PW500 took place on October 29, 1993, the first flight took place in late 1993 on a Boeing 720B . The engine was approved by the FAA on April 17, 1996. The EASA approval then took place on April 15, 1997.

The types PW535B, PW535E and PW545C are equipped with a FADEC system. In the Pratt and Whitney models, however, it is not called FADEC, but EEC (Electronic Engine Control).

Technical specifications

Type Thrust (kN) By-
pass ratio
at start
Total pressure
ratio
Fan diameter
(m)
Length (m) Dry
matter (kg)
Admission used at
PW530A 12.84 3.7: 1 13.3: 1 0.58 1.532 279.6 1997 Cessna Citation Bravo
PW535A 15.12 1.646 317 2000 Cessna Citation Ultra Encore
PW535B 15.12 1.646 318.4 2007 Cessna Citation Encore +
PW535E 14.95 1.697 317 2010 Embraer Phenom 300
PW545A 17.58 4.12: 1 11.7: 1 0.693 1.914 376.5 1998 Cessna Citation Excel
PW545B 18.32 4.1: 1 12.5: 1 0.693 1.914 376.5 2004 Cessna Citation XLS
PW545C 18.32 1.914 376.5 2009 Cessna Citation XLS +

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