|
enginehistory.org Aircraft Engine Historical Society Members' Bulletin Board
|
View previous topic :: View next topic |
Author |
Message |
jjuutinen
Joined: 13 Jul 2003 Posts: 180
|
Posted: Mon Oct 09, 2006 00:52 Post subject: Chrysler XI-2220 |
|
|
What were the cylinder dimensions of this engine, what was the boost for 2500 hp/3400 rpm and how much did weight? Except being a "wetliner", the cylinder construction (as per the drawing here) reminds me of the DB designs, i.e. liner screwed in the head and the liner pulled to the crankcase by large sized nuts over the liner. |
|
Back to top |
|
|
kmccutcheon
Joined: 13 Jul 2003 Posts: 298 Location: Huntsville, Alabama USA
|
|
Back to top |
|
|
jjuutinen
Joined: 13 Jul 2003 Posts: 180
|
Posted: Wed Oct 11, 2006 20:06 Post subject: |
|
|
Thanks, excellent! The most interesting piece of data concerns the SFC at full power, 0.54 lbs/hp/h. This is something that the R-2800 could only dream of at 2500 hp (the XI-2220 has some 30% lower sfc at TO power than the R-2800 B or C!). If we e.g. consider the USN combat radius definition, the Chrysler engine would have offered quite a considerable improvement in radius of action over the R-2800 in e.g. the F4U and the F6F. |
|
Back to top |
|
|
|
|
You cannot post new topics in this forum You cannot reply to topics in this forum You cannot edit your posts in this forum You cannot delete your posts in this forum You cannot vote in polls in this forum
|
Powered by phpBB © 2001, 2005 phpBB Group
|