MiTasol
Captain
Thank you both for those diagrams.
Am I correct that the PS system has three rows of inlet guide vanes with only the first being variable (and the other two locked and rotating with the centrifugal wheel while the Russian only had one set of inlet guide vanes.
EDIT - I have just read the USAAF report and realise I have misinterpreted the PS system - the PS system on the 12Z is downstream of the comprssor, not upstream as I was envisaging.
Nice photo. That distributor on the RH cylinder head - is it fuel injection or pneumatic starting?
Is there an on line manual for that engine?
Am I correct that the PS system has three rows of inlet guide vanes with only the first being variable (and the other two locked and rotating with the centrifugal wheel while the Russian only had one set of inlet guide vanes.
EDIT - I have just read the USAAF report and realise I have misinterpreted the PS system - the PS system on the 12Z is downstream of the comprssor, not upstream as I was envisaging.
For the 12Z, I have these curves too.
And a personal pic of the (big) 12Z Turbomeca supercharger, with well-known twin inlet, but single outlet :
Nice photo. That distributor on the RH cylinder head - is it fuel injection or pneumatic starting?
Is there an on line manual for that engine?
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