Suprised you lot have let the 787/Rolls delay go uncommented
Suprised you lot have let the 787/Rolls delay go uncommented
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DJC

Original Poster:

23,563 posts

259 months

Monday 30th August 2010
quotequote all
Thought Eric would have been all over this by now.

If folks do with to comment, be warned there are a few people who work for Rolls and at Derby on the board!

M-J-B

15,377 posts

273 months

Monday 30th August 2010
quotequote all
Is it the airframe or powerplant that is late?

hurstg01

3,133 posts

266 months

Monday 30th August 2010
quotequote all
BBC News said:
Boeing said the setback was due to the availability of a Rolls-Royce engine needed for the final phases of flight testing.
BBC News said:
A spokesman for Rolls-Royce said: "We have been informed by Boeing that the currently planned dates for Trent 1000 engine deliveries will now not support their latest flight test programme requirements.

"We are working closely with Boeing to expedite delivery in support of their programme schedule.
So Boeing rejigged their test flight programme requirements, shifting the goalposts and make RR sound in the press that they are at fault, and RR [very PR aware] said they are doing all they can to keep up with the new schedule?

M-J-B

15,377 posts

273 months

Monday 30th August 2010
quotequote all
hurstg01 said:
BBC News said:
Boeing said the setback was due to the availability of a Rolls-Royce engine needed for the final phases of flight testing.
BBC News said:
A spokesman for Rolls-Royce said: "We have been informed by Boeing that the currently planned dates for Trent 1000 engine deliveries will now not support their latest flight test programme requirements.

"We are working closely with Boeing to expedite delivery in support of their programme schedule.
So Boeing rejigged their test flight programme requirements, shifting the goalposts and make RR sound in the press that they are at fault, and RR [very PR aware] said they are doing all they can to keep up with the new schedule?
I was hoping that it was the Americans fault.

Why blame yourself when you can blame others rolleyes

havoc

32,643 posts

258 months

Monday 30th August 2010
quotequote all
This is Boeing - the masters at blaming others (and making others seem worse than they are - Airbus FBW issues vs 737 rudder hard-over, anyone?!?).

Chrisgr31

14,212 posts

278 months

Monday 30th August 2010
quotequote all
M-J-B said:
hurstg01 said:
BBC News said:
Boeing said the setback was due to the availability of a Rolls-Royce engine needed for the final phases of flight testing.
BBC News said:
A spokesman for Rolls-Royce said: "We have been informed by Boeing that the currently planned dates for Trent 1000 engine deliveries will now not support their latest flight test programme requirements.

"We are working closely with Boeing to expedite delivery in support of their programme schedule.
So Boeing rejigged their test flight programme requirements, shifting the goalposts and make RR sound in the press that they are at fault, and RR [very PR aware] said they are doing all they can to keep up with the new schedule?
I was hoping that it was the Americans fault.

Why blame yourself when you can blame others rolleyes
It did appear from the news reports on this that it wasnt Rolls Royces fault but Boeings. Mind you as the aircraft is very late (2 years is it) it does seem slightly surprising the engine isnt ready to go. Although I guess there was no point working on the engine until it became clear that Boeing werent going to can the project!

TimJMS

2,584 posts

274 months

Monday 30th August 2010
quotequote all
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.

hurstg01

3,133 posts

266 months

Monday 30th August 2010
quotequote all
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
You can

smile


TimJMS

2,584 posts

274 months

Monday 30th August 2010
quotequote all
Cheers - does rather point to RR being the culprits though.

Mojocvh

16,837 posts

285 months

Monday 30th August 2010
quotequote all
More than likely some smoke and mirrors from both companies.

Airbus expo on the dreamliner, some imteresting points ref powerplant.

http://www.flightglobal.com/blogs/flightblogger/20...

no where near the full document, in fact they are being very kind to boeing.

http://www.planebusiness.com/buzz/airbus2.pdf

Edited by Mojocvh on Monday 30th August 18:42

pikeyboy

2,349 posts

237 months

Tuesday 31st August 2010
quotequote all
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
Just heard from an ex work mate very close to the Trent 1000 dev team that they had a failure due to oil pooling in a shaft during several dry cranks of a Trent 1000 engine. The engine was subsequently started and run up to full power when the pooled oil ignited, the ensuing fire destroyed the engine allowing the turbine and compressor to seperate. Head scratching time regarding oil drainage and air sealing of bearing chambers.

Somewhatfoolish

4,977 posts

209 months

Wednesday 1st September 2010
quotequote all
Mojocvh said:
More than likely some smoke and mirrors from both companies.

Airbus expo on the dreamliner, some imteresting points ref powerplant.

http://www.flightglobal.com/blogs/flightblogger/20...

no where near the full document, in fact they are being very kind to boeing.

http://www.planebusiness.com/buzz/airbus2.pdf

Edited by Mojocvh on Monday 30th August 18:42
Bloody hell!

S3_Graham

12,835 posts

222 months

Wednesday 1st September 2010
quotequote all
DJC said:
Thought Eric would have been all over this by now.

If folks do with to comment, be warned there are a few people who work for Rolls and at Derby on the board!
have you had a hand in this one also mate?

Mojocvh

16,837 posts

285 months

Wednesday 1st September 2010
quotequote all
pikeyboy said:
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
Just heard from an ex work mate very close to the Trent 1000 dev team that they had a failure due to oil pooling in a shaft during several dry cranks of a Trent 1000 engine. The engine was subsequently started and run up to full power when the pooled oil ignited, the ensuing fire destroyed the engine allowing the turbine and compressor to seperate. Head scratching time regarding oil drainage and air sealing of bearing chambers.
Is your mate getting a little confused with a titanium fires scratchchin

pikeyboy

2,349 posts

237 months

Wednesday 1st September 2010
quotequote all
Mojocvh said:
pikeyboy said:
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
Just heard from an ex work mate very close to the Trent 1000 dev team that they had a failure due to oil pooling in a shaft during several dry cranks of a Trent 1000 engine. The engine was subsequently started and run up to full power when the pooled oil ignited, the ensuing fire destroyed the engine allowing the turbine and compressor to seperate. Head scratching time regarding oil drainage and air sealing of bearing chambers.
Is your mate getting a little confused with a titanium fires scratchchin
nope. without going into detail the bearing chambers seal with air which during cranking prior to starting is not at sufficent pressure to seal the bearing chambers. This allows oil to leak past the seal fins and into areas where it can pool, in this case the IP shaft which is used for starting the Trent 1000. Upon start up this pooled oil can lead to a flash fire. A titianium fire is also a messy business and I've seen the results of them during development engine testing, however it wasnt the cause of this failure.

anonymous-user

77 months

Wednesday 1st September 2010
quotequote all
pikeyboy said:
Mojocvh said:
pikeyboy said:
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
Just heard from an ex work mate very close to the Trent 1000 dev team that they had a failure due to oil pooling in a shaft during several dry cranks of a Trent 1000 engine. The engine was subsequently started and run up to full power when the pooled oil ignited, the ensuing fire destroyed the engine allowing the turbine and compressor to seperate. Head scratching time regarding oil drainage and air sealing of bearing chambers.
Is your mate getting a little confused with a titanium fires scratchchin
nope. without going into detail the bearing chambers seal with air which during cranking prior to starting is not at sufficent pressure to seal the bearing chambers. This allows oil to leak past the seal fins and into areas where it can pool, in this case the IP shaft which is used for starting the Trent 1000. Upon start up this pooled oil can lead to a flash fire. A titianium fire is also a messy business and I've seen the results of them during development engine testing, however it wasnt the cause of this failure.
Was the issue also that the Trent failure resulted in uncontained blade separation?

pikeyboy

2,349 posts

237 months

Wednesday 1st September 2010
quotequote all
el stovey said:
pikeyboy said:
Mojocvh said:
pikeyboy said:
TimJMS said:
Can we have a link? The only info I can find is a link to an unconfined engine failure that additionally managed to damage the test facility at Derby.
Just heard from an ex work mate very close to the Trent 1000 dev team that they had a failure due to oil pooling in a shaft during several dry cranks of a Trent 1000 engine. The engine was subsequently started and run up to full power when the pooled oil ignited, the ensuing fire destroyed the engine allowing the turbine and compressor to seperate. Head scratching time regarding oil drainage and air sealing of bearing chambers.
Is your mate getting a little confused with a titanium fires scratchchin
nope. without going into detail the bearing chambers seal with air which during cranking prior to starting is not at sufficent pressure to seal the bearing chambers. This allows oil to leak past the seal fins and into areas where it can pool, in this case the IP shaft which is used for starting the Trent 1000. Upon start up this pooled oil can lead to a flash fire. A titianium fire is also a messy business and I've seen the results of them during development engine testing, however it wasnt the cause of this failure.
Was the issue also that the Trent failure resulted in uncontained blade separation?
yes as far as I'm aware as it was the compressor and turbine that parted company, blades being uncontained was the least of their worries though. its also worth pointing out that the engines are only designed to be able to containa fan blade off event. Disks failures can not be contained and there are some good pics around of a plane with a turbine disk wedged in the toilet of the aircraft.

DJC

Original Poster:

23,563 posts

259 months

Thursday 2nd September 2010
quotequote all
S3_Graham said:
DJC said:
Thought Eric would have been all over this by now.

If folks do with to comment, be warned there are a few people who work for Rolls and at Derby on the board!
have you had a hand in this one also mate?
Possibly in the employment of my previous company.

havoc

32,643 posts

258 months

Thursday 2nd September 2010
quotequote all
pikeyboy said:
Disks failures can not be contained and there are some good pics around of a plane with a turbine disk wedged in the toilet of the aircraft.
yikes THAT probably hurt!

Mojocvh

16,837 posts

285 months

Friday 3rd September 2010
quotequote all
Hmm a fan spinner came off a cfm(??) fitted to a 737 a year or so ago.
They had damage up to the front cabin door on the same side AND unbelievably, damage to the fuselage on the other side that was non penetration ie the FOD had gone forwards and AROUND the fuselage...................