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DC-10 Tail Exhaust Design  
User currently offlineNwa320 From United States of America, joined Aug 2007, 70 posts, RR: 0
Posted (11 years 12 months 3 days 2 hours ago) and read 2251 times:

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Photo © Howard Chaloner


It says "note the original tail exhaust design on No. 2 engine." Did McDonnell Douglas change the exhaust design? If they did why?


Thanks

5 replies: All unread, jump to last
 
User currently offlineVC-10 From United Kingdom, joined Oct 1999, 3708 posts, RR: 34
Reply 1, posted (11 years 12 months 3 days 2 hours ago) and read 2235 times:
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They removed the Turbine Reverser to improve reliability & save weight

User currently offlineNwa320 From United States of America, joined Aug 2007, 70 posts, RR: 0
Reply 2, posted (11 years 12 months 3 days ago) and read 2215 times:

Thanks, VC-10  Big thumbs up

F I L L E R


User currently offlineBroke From United States of America, joined Apr 2002, 1322 posts, RR: 3
Reply 3, posted (11 years 12 months 2 days 6 hours ago) and read 2144 times:

All of the early 747's, DC-10's, and L-1011's had the capability to reverse both the fan air (cold stream) and the gas generator (hot stream) air. In all applications the system was terribly unreliable for the hot stream portion of the reverser. I worked at EAL and inoperative thrust reversers on the L-1011 in the early 1970's were a common occurrence, often after shedding parts of the hot stream deflectors on the runway.
For EAL operations into LGA, all 3 reversers have to be operative. This was an EAL requirement and not regulatory. Since most of our LGA-Florida operations were L-1011's, we have a lot of reverser related delay and cancellations at LGA.
A big problem with the design of the L-1011 reverser system was that the sensors indicating the status and operation of the system were all tied to the hot stream portion of the system; so converting to a cold stream only system required some major redesign and modification work in order to accomplish it.
In addition, if you look closely at the tail cone angle on the L-1011's through the early years of operation (1972 on), you will notice that the angle changes. The early tail cones were the 22 degree configuration, later they went to the 15 degree design. The reason was drag reduction, but not much of an improvement was ever actually seen.


User currently offlineGigneil From United States of America, joined Nov 2002, 16347 posts, RR: 85
Reply 4, posted (11 years 12 months 1 day 20 hours ago) and read 2089 times:

You can see the difference I think... one is straight and one is bubbled at the back.

N


User currently offlineNwa320 From United States of America, joined Aug 2007, 70 posts, RR: 0
Reply 5, posted (11 years 12 months 1 day 9 hours ago) and read 2089 times:

gigneil: Yes I can see the difference. The old one looks strange to me because I have never seen one like that at an airport.

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