I was just wondering how the cooling air gets to the turbine blades...
Does anybody know?|||I studied the RB-211 when flying 747 airplanes fitted with these engines -
I do recall instructor mentioning the hollow turbine blades and cooling air -
If I recall well, was air bled from the compressors (maybe N2) -
Likely to be controlled by the electronic FCU -
Source was probably from the AFC "air flow control" - (N2, bleeds and IGV)
I do not recall exactly, slept most of the time in the powerplant class -
RR loves to make simple things complicated -
I prefer CF6 and JT9D motors anyway...!
Next time I shall go in my cellar, dust off my old 747 RR manuals -
If you know, why ask...?
Forner examiner and instructor, I can dig "gee wizz" questions too -|||Why are you asking questions that you already have the answers to?
Are you related to Caretaker by chance?
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