Page 19 - AAA JANUARY - FEBRUARY 2018 Online Magazine
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engine fan can now rotate more slowly, while the low-pres-
         sure compressor and turbine can rotate much faster. The        Decoding Pure Power
         fewer number of compressor and turbine stages (six fewer                urePower Engines comprise
         stages)reduce engine weight and lower maintenance costs.                two engine families: the Pratt
         Compared to a conventional engine, a GTF powerplant has                 &  Whitney  Canada  PW800
         fewer stages and 2,000 fewer airfoils, while the fan drive    Pengine  family  designed
         gear system is designed to run for infinite life with no life   for  next  generation  large  business
         limited parts. Borescope capability at every engine stage      jets, and the PW1000G GTF engine
         allows a quick “look inside” for fast diagnostics.  While the   family. GTF engines power five plat-
         high bypass ratio fan is designed to prevent debris from
         entering the engine core, the externals have been designed     forms;  Airbus  A320neo  Family
         for quick removal and replacement.                             (PW1100G-JM), Bombardier C Series
                                                                        (PW1500G),  Mitsubishi  Regional
                                                                        Jet  (MRJ)  (PW1200G),  Irkut  MC-21
                                                                        (PW1400G-JM) and Embraer E-Jets
                                                                        E2  (PW  1900G,  PW1700G).  The
                                                                        PW1000G engine family are numbered
                                                                        based on model as follows. Since this
                                                                        is the first generation of GTF engines,
                                                                        the first number represents 1 or 1,000.
                                                                        The second number represents the
                                                                        airframer; 1- Airbus, 2 – Mitsubishi, 4 –
                                                                        Irkut, 5 - Bombardier and 7 – Embraer.
                                                                        The  thrust  class  of  the  engines  is
                                                                        denoted by the next two numbers: 24
                                                                        stands for 24,000 pounds of thrust.
                                                                        The letter ‘G’ at the end stands for GTF
                                                                        engine. Hence the PW1124G (24,000lbs
                                                                        thrust), PW1127G (27,000lbs thrust)
                                                                        and  PW1133G  (33,000lbs  thrust)
                                                                        engines, power the Airbus A319neo,
                                                                        A320neo and A321neo respectively.
                                                                        The MRJ70 and MRJ90 are powered
                                                                        by the 15,000lbs thrust PW1215G and
                                                                        17,000lbs  thrust  PW1217G  engines.
                                                                        Bombardier’s CSeries is powered by
                                                                        PW1521G engines with 21,000lbs of
                                                                        thrust for the CS100 and PW1524G
         Noise contours compared       Airbus A320neo  Airbus A320ceo
                                                MTOW: 73.5 t
                                       MTOW: 73.5 t
         A320neo vs. A320ceo                                            engines with 23,300lbs of thrust for
                                                         4 km
                                            ~-50%                       the CS300.
         The Airbus A320neo (new engine option) has an approximately   3.5 km
         50 percent reduced noise contour compared with the Airbus
         A320ceo (current engine option).
                                                         3 km
         The 85 dB(A) maximum noise level contours are shown for
         a takeoff with Lufthansa standard takeoff procedures and
         maximum takeoff weight (MTOW).                  2.5 km
         By comparison, a maximum noise level of 85 dB(A) is produced
         by a truck passing at a distance of five meters (16 feet) in city   2 km
         traffic.
                                                         1.5 km
                                                                 ©  01/2016
                                                         1 km
                                                                 Source: Airbus
                                                         0.5 km
                                                         0
                                      0.5 km  0  0.5 km  0.5 km  0  0.5 km
        ASIAN AIRLINES & AEROSPACE                                                             January/February 2018 | 19
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