PW1100G in depth start-up sequence
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Joined: Jul 2017
Posts: 94
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From: Europe
PW1100G in depth start-up sequence
Hi all
So the PW1100G has this "cooling" period during startup. During this phase, N2 is kept below 10% and the fan is not moving at all. I've been wondering the following:
- How is the N2 maintained? Is the starter valve modulated, not a simple on/off valve?
- Why does the fan remain stationary? Is it just a matter of internal friction vs low N2 not producing enough force to spin it, or is there some mechanism in place to hold it?
So the PW1100G has this "cooling" period during startup. During this phase, N2 is kept below 10% and the fan is not moving at all. I've been wondering the following:
- How is the N2 maintained? Is the starter valve modulated, not a simple on/off valve?
- Why does the fan remain stationary? Is it just a matter of internal friction vs low N2 not producing enough force to spin it, or is there some mechanism in place to hold it?



Joined: Jul 2013
Aviation Qualifications: Non-Aircrew
Posts: 5,682
Likes: 3,347
From: Everett, WA
I don't know about the PW1000G, but the LEAP uses "pulse width modulation" to control N2 - i.e. the starter air valve is rapidly opened and closed to maintain the desired N2 speed.
I'd be very surprised is there any physical mechanism to prevent N1 rotation - first off the failure modes are outright nasty, and there is no need to keep the fan from rotating.
I'd be very surprised is there any physical mechanism to prevent N1 rotation - first off the failure modes are outright nasty, and there is no need to keep the fan from rotating.

Joined: May 2015
Posts: 1
Likes: 0
From: near EDDV
Why does the fan remain stationary? Is it just a matter of internal friction vs low N2 not producing enough force to spin it, or is there some mechanism in place to hold it?



Joined: Jul 2013
Aviation Qualifications: Non-Aircrew
Posts: 5,682
Likes: 3,347
From: Everett, WA
Back during the GE90 development, one of the GE engineers showed me an analysis he'd done of how much oil cooling would be required for a gearbox capable of driving the fan on a 100,000 lbs. thrust class engine. Suffice to say the oil cooler would have had to be massive
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