KELPkid From United States, joined Nov 2005, 3561 posts, RR: 3 Reply 2, posted (1 year 11 months 2 weeks 2 hours ago) and read 676 times:
Quoting Cdekoe (Reply 1): The uninstalled weight of the PW610F on the Eclipse (excluding pumps, starter-generator and fire detection equipment) will be just under 270 pounds.
Didn't that throw the program off for a couple of years when they decided to switch engines from the Williams FX-22, because the PWC engine was actually heavier than the Williams engine (hard as that is to believe...)?
Rulebooks and regulations are made from paper...and they do a poor job at preventing metal from contacting rock-Ernest G
Dw747400 From United States, joined Aug 2001, 873 posts, RR: 1 Reply 3, posted (1 year 11 months 2 weeks 1 hour ago) and read 663 times:
Quoting KELPkid (Reply 2): because the PWC engine was actually heavier than the Williams engine (hard as that is to believe...)?
All sort of things had to be changed. The additional weight and thrust required a beefier structure, and those PW610s are very thirsty compared to the proposed Williams.
Mlglaw From United States, joined Feb 2006, 53 posts, RR: 0 Reply 4, posted (1 year 11 months 1 week 6 days 13 hours ago) and read 608 times:
Thanks to cdekoe's response and link; I see that the Eclipse engine PW610F is listed at 270 lbs and rated with 900 lbs of thrust, better than a 3 to 1 ratio. What is the ratio of the B777 engines (weight to thrust) and the proposed B787?