messiach
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@GriffinsRule @Thunder.Storm
I gather PAF is to stick with RD93. This i a twitter Q&A session with some insider source.
You are aware these turbines are twin spool eg RD-series 3 , WS13/e/j with 2 X L-H compressor-turbines.
This is pretty much standard for this range. Most chinese effort is based on russian designs and this goes for WS engines aswell eg. the fan-Lp compressor-turbine assembly for WS series 10, 13 incld. bypass duct has been tested on russian RD engines with russian assistance. Technically they are modified russian turbines. Power to thrust ratio is a nonlinear relationship but my estimate is 105kn.
You can quote me.
I gather PAF is to stick with RD93. This i a twitter Q&A session with some insider source.
You are aware these turbines are twin spool eg RD-series 3 , WS13/e/j with 2 X L-H compressor-turbines.
This is pretty much standard for this range. Most chinese effort is based on russian designs and this goes for WS engines aswell eg. the fan-Lp compressor-turbine assembly for WS series 10, 13 incld. bypass duct has been tested on russian RD engines with russian assistance. Technically they are modified russian turbines. Power to thrust ratio is a nonlinear relationship but my estimate is 105kn.
You can quote me.
Here is a pdf member @messiach she mentioned somewhere that engine thrust 105 kn for bl3.