PRC VCE and low bypass engines (fighters, tactical jets, UAVs, others)

Alfa_Particle

Senior Member
Registered Member
The 2 stage LPT is bizarre though. I'd expect the WS-21 to be a 3-7-1-1. In fact even the RD-33 family it's related to never had a 2 stage LPT configuration.
 

taxiya

Brigadier
Registered Member
The 2 stage LPT is bizarre though. I'd expect the WS-21 to be a 3-7-1-1. In fact even the RD-33 family it's related to never had a 2 stage LPT configuration.
How so? In many (such as F-404) low bypass turbofan, the bypass happens (air flow split) between LPC and HPC. This makes the LPC nearly equal to Fan. In F-404 there are 3 stages of Fan/LPC, in other words 1 Fan stage + 2 LPC stages. WS-21 has the same configuration of F-404 family. RD-33 is different, it does have 1 Fan + 3 LPC or 4 fan/LPC stages. The confusion of counting stages is caused by whether fan and LPC are counted separately or combined.
 
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Nx4eu

Junior Member
Registered Member
How so? In many (such as F-404) low bypass turbofan, the bypass happens (air flow split) between LPC and HPC. This makes the LPC nearly equal to Fan. In F-404 there are 3 stages of Fan/LPC, in other words 1 Fan stage + 2 LPC stages, or 3 Fan/LPC stages. WS-21 has the same configuration of F-404 family. RD-33 is different, it does have 1 Fan + 3 LPC. The confusion of counting stages is caused by the fact that LPC is doing nearly the same work as Fan.
Bro is talking about how the engine has three turbine stages. A high pressure one and 2 low pressure ones. Which is odd, because both WS-13 and RD-33 only have two turbine stages, 1 high and 1 low.. HPT drives the HPC, LPT drives both the fan and the LPC. The WS-21 seems to have chosen the path to draw more energy out of the core stream to power the Fan and LPC's.

Both the WS-13/RD-33 have 4 LPC stages while the WS-21 only has 3. What could be the thought process and benefits of adding the second LPT stage?
 
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taxiya

Brigadier
Registered Member
Bro is talking about how the engine has three turbine stages. A high pressure one and 2 low pressure ones. Which is odd, because both WS-13 and RD-33 only have two turbine stages, 1 high and 1 low.. Why are you talking about the compressors?
oops. My mistake looking at LPT but thinking of LPC.

But 2 low pressure turbine isn't unusual. And why should WS-21 be considred to be related to RD-33? P.S. I don't buy the rumor that WS-21 is somehow improved version of RD-33 derivatives.
 
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Alfa_Particle

Senior Member
Registered Member
Bro is talking about how the engine has three turbine stages. A high pressure one and 2 low pressure ones. Which is odd, because both WS-13 and RD-33 only have two turbine stages, 1 high and 1 low.. HPT drives the HPC, LPT drives both the fan and the LPC. The WS-21 seems to have chosen the path to draw more energy out of the core stream to power the Fan and LPC's.

Both the WS-13/RD-33 have 4 LPC stages while the WS-21 only has 3. What could be the thought process and benefits of adding the second LPT stage?
Thank you. Confused how this mistake was made not once, but twice...

Tbh, there's a non-zero chance this is just a non-descript model of no significance and just a placeholder. A 3-7-1-2 configuration genuinely makes no sense for a F414-class engine, considering how this engine supposedly is derived from both the RD-33 and F404, both of which only has one LPT stage. As @Nx4eu said, an addition of an LPT stage while going from a 4 to 3 stage LPC is very odd, again, considering the size.
 

latenlazy

Brigadier
Bro is talking about how the engine has three turbine stages. A high pressure one and 2 low pressure ones. Which is odd, because both WS-13 and RD-33 only have two turbine stages, 1 high and 1 low.. HPT drives the HPC, LPT drives both the fan and the LPC. The WS-21 seems to have chosen the path to draw more energy out of the core stream to power the Fan and LPC's.

Both the WS-13/RD-33 have 4 LPC stages while the WS-21 only has 3. What could be the thought process and benefits of adding the second LPT stage?
Thank you. Confused how this mistake was made not once, but twice...

Tbh, there's a non-zero chance this is just a non-descript model of no significance and just a placeholder. A 3-7-1-2 configuration genuinely makes no sense for a F414-class engine, considering how this engine supposedly is derived from both the RD-33 and F404, both of which only has one LPT stage. As @Nx4eu said, an addition of an LPT stage while going from a 4 to 3 stage LPC is very odd, again, considering the size.
It’s probably related to bypass ratio. Larger fan. F110 and F135 both have to 2 LPT. F119, EJ200 and F414 all have 1 LPT.
 
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