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-   -   ge90-115b flat rated? (https://www.pprune.org/tech-log/555903-ge90-115b-flat-rated.html)

MaxFL360 4th Feb 2015 08:12

ge90-115b flat rated?
 
Is the ge90-115b flat rated to say 90000lb of thrust or is it capable of actually producing 115000lb of thrust assuming no limitations with high OATs.

Cheers

Goldenrivett 4th Feb 2015 08:21

There is a marvellous new invention called a search engine. e.g Google.
The GE90 Engine Family | Engines | Commercial | GE Aviation

barit1 4th Feb 2015 16:02

Perhaps a review of the meaning of flat rated thrust will help. I don't need to spell it out - someone's already done it:And yes, gas turbine engines are capable of more thrust on a cold day (surprise, surprise), but will encounter turbine temp or RPM or other limitations in hot day conditions. The -115B produces 115K# up to a corner point (30C I think) but it's cut back above that corner point.

DaveReidUK 4th Feb 2015 16:33

Yes, rated at 115,540 lb for takeoff up to 30C.

stilton 5th Feb 2015 03:08

Isn't that nice, Dave had the commonsense and civility to just give an answer.


Grivet could take note.

agg_karan 5th Feb 2015 05:32

Can someone provide a LINK to a document stating flat rating is ISA + 15 for these engines?

DaveReidUK 5th Feb 2015 06:47

http://rgl.faa.gov/Regulatory_and_Guidance_library/rgMakeModel.nsf/0/491573d6cdf5ee3986257c89006e56d4/$FILE/E00049EN_Rev_18.pdf

KBPsen 5th Feb 2015 18:35


Originally Posted by stilton
Grivet could take note.

On the other hand, when people want others to answer questions they themselves could find the answer to in less time than it takes to write the question, is that not just laziness or pretend helplessness? Is that something you would want to reward?

DaveReidUK 5th Feb 2015 20:24

Except that the link provided in post #2 doesn't actually answer the OP's question about flat-rating.

MaxFL360 6th Feb 2015 02:46

so would i be correct in saying that the 115b is flat rated to 115000 lb/thrust although it theoretically is capable of much more if no limit was placed up to ISA+15?

Im assuming this is to protect the engine from unnecessary wear as the 300ER would never require more thrust than this amount?

Gysbreght 6th Feb 2015 10:04


Originally Posted by MaxFL360
so would i be correct in saying that the 115b is flat rated to 115000 lb/thrust although it theoretically is capable of much more if no limit was placed up to ISA+15?

That would be correct if the only limits to consider were gas temperatures and rotational speeds. There are other limits such as loads on bearings, shaft torques, carcass pressures that may impose an absolute limit on the allowable thrust.

barit1 6th Feb 2015 13:46

The 777-200LR uses the same -115B engine.

Its nonstop ferry range from KORD for example can take it to ANY international airport in the world, with one exception: Perth, WA.

Now tell me, once more, why you want more thrust?


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