PPRuNe Forums - View Single Post - De-rated power settings question
View Single Post
Old 21st Feb 2008, 13:12
  #34 (permalink)  
Chris Scott
 
Join Date: Jan 2008
Location: Blighty (Nth. Downs)
Age: 77
Posts: 2,107
Received 4 Likes on 4 Posts
Evolution of Flex-Thrust Performance Calculations

Quote from mutt:
Quote:
handbook of Perf A graphs
...I never had to use those charts for real...

I doubt any airline jet-pilot will ever have to use graphic charts again. Pity in a way, because, like any pictorial representation of a process - e.g., a systems diagram, or flow chart - they could be an aid to understanding and monitoring the "big picture". Just in case anyone is wondering, they were NOT runway-specific, so the first part of the process was to extract the runway details from an airfield list: Elevation; Slope; TORA; EMDA (ASDA); TODA; and any obstacles affecting the NTOFP (net T/O flight-path, after the end of the clearway). The graphs could be re-used indefinitely, being covered in sticky-back plastic, so we could use a sharp china-graph pencil - but fine ball-point was more practical.

Later. on the B707, we still used charts, but they combined runway, WAT and NTOFP considerations on to one chart, and were runway-specific. So the only remaining variables were QNH, OAT/Flex-Temp, W/C (wind-component, head or tail), and any permiissible contaminant. [You had to extract V-speeds elsewhere.]

TABLES are runway-specific; and incorporate V-speeds in the same 'box' for each temp, W/C, and resulting weight. The only corrections required are the QNH, and any permissible R/W contaminant. The trouble is that each weight is the RTOW for a specific OAT/Flex-Temp and W/C, and the speeds therefore assume you are at that weight. If you are lighter, the V1 is still valid, but the VR and V2 have to be calculated for the actual weight.** [If the quoted V1 is higher than (actual) VR, it must be reduced to VR.] And don't forget VMCG...

Quote from mutt:
Quote (from groundfloor):
The assumed temperature must not be lower than the flat-rating temperature
Why not?

Good question. It's always been so! I see that groundfloor correctly added "or the OAT", something I wrongly omitted in my post. But using a lower temperature shouldn't matter because, if you use TREF, you are already at Rated Thrust; so using a lower assumed temperature shouldn't make any difference. Equally, if you use something below OAT, I doubt that a modern engine would try to give you more than Rated Thrust. BUT I wouldn't want to try it out! In the old days, American jet engines COULD be "over-boosted" by opening the thrust levers too far. It was the job of the F/E (much-missed flight engineer) to pre-calculate the appropriate EPR, P7, (or whatever power indication applicable to the engine), and set the correct take-off thrust on the pilot's command.

Actually, using OAT or TREF as the assumed temperature is pointless - you might as well select Rated Thrust in the conventional manner. [The flat-rating concept did not apply, by the way, on the Conway-powered VC10. The first engine I operated with it was American - the JT3D on the B707.]

FE Hoppy has answered mutt's other point - I've never used de-rated thrust, so can't comment. Re graphs: yes, but practice makes (nearly) perfect, and a limiting take-off out of Entebbe (old R/W) or Nairobi used to concentrate the mind wonderfully... We always used to use the "thickness of the pencil" on the safe side. I don't think computers are capable of doing that!


** [Unless you are using optimised performance (capitalising on surplus runway length by using increased VR and V2 for a better climb gradient).]

Last edited by Chris Scott; 23rd Feb 2008 at 11:55. Reason: ** Optimised VR and V2. Typo. More typos. "Vref" corrected to read "Tref".
Chris Scott is offline