Quoting KarelXWB (Reply 69): I'm not sure where you are getting the 4k lbf from, the Advance thrust range is 75 - 105 klbf. |
I attributed your quote above to the Advance but you were referring to the XWB, my bad.
Quoting KarelXWB (Reply 69): The Advance engine will be heavier, it's designed for a 777 sized aircraft, and would also require more structural support (wing / landing gear etc). It would easily add weight to the 787-10ER. |
I am sure it would add weight but 5t in engines and strengthening is a lot.
I have a hard time picturing four 777-sized engines on an A380neo. Its hard to imagine that the engine could be ideal for both an aircraft that requires ~75k X 4 as well as one that would need ~100 X 2. Its hard to believe there wouldn't be a compromise somewhere.
Quoting KarelXWB (Reply 69): This is weird: the A351 has more design range than the 777-9 and most of the 777X on order are for the latter one. |
I have the A351 as a ~8000nm bird and the 779 as 'greater than 8200nm'. I agree its a weird quote from him but if it was nearly anyone else I would disregard but Sir Tim Clark is not one to mince words.
Quoting KarelXWB (Reply 69): I did some research, this "10-hour" quote dates from 2011 and was based on the original design of the A350-1000 (which had even less range than today's 777-300ER): |
I have him saying it in 2012 after the re-design as well.
Quote: He said the competing jet proposed by Airbus, the A350-1000, will have its own market niche but "doesn't quite stack up" against Boeing's so-called 777X update, planned for the end of the decade....Clark said the delivery timetable of the Airbus jet is questionable. He also predicted that the 777X will outperform it.
"They're different airplanes," he said. The 777X "has greater legs, greater range, greater lift."
The specifications offered by Airbus for the A350 show that the plane will adequately cover up to 10-hour flights, Clark said. That currently encompasses 80 percent of the Emirates route network, he said, but the airline plans to shift more "into the 13-to-18 hour mission range." "That's, frankly, where it doesn't quite stack up," Clark said. |
http://seattletimes.com/html/busines...echnology/2017651815_boeing03.html
Maybe it is a dated quote in the article or maybe he is going to pack more people in then Airbus estimates or maybe he was referencing its performance before the redesign, I don't know. If he still feels that way then it is hard to see him being interested in a simple stretch A350-1100 in my opinion.
I do, and Boeing is in deep do-do if they need 115k out of it.
Quoting BoeingVista (Reply 71): A) It is not a given that GE and RR can come to the same SFC level given their radically different approach to engine design (2 shaft v 3) at every level of technology. |
And
GE is multiple generations into a carbon fan and starting more advanced ceramic work for higher temperatures which
RR is not up to speed on. There are tradeoffs but I feel pretty confident that as they are being produced in similar time periods that the results will also be similar. If
RR could have beaten the GE9x then I think Boeing would have given them at least a chance when they were deciding on engines. I can't see them saying that they purposely want the worse engine.
Quoting BoeingVista (Reply 71): B) It not really the engines fault here, the 777-9 is 20t+ heavier and here comes our old friend physics again. |
Don't get me wrong, I think Airbus and
RR can do it, I just don't think it would be cheap, it will sacrifice production slots that can already be sold at solid margin, and ultimately isn't the best use of resources in the near term. They would need to launch immediately and I have been saying all along that if this 400 seat market is big enough (not sure it is) then there will be time post 2020 to launch it not unlike the 77W vs the 77E.
...and I clearly had an issue with his conclusion which is what I am mentioning above.
tortugamon