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Re:

3 messages picture_as_pdf Source PDF
J
jeffrey E. Aug 15, 2015 9:30 PM
To
Larry Visoski

Up to about 28,000 feet the aircraft is limited by indicated air speed (Vne), so say you can do 350 kias at ground level, you can do that all the way up to 28,000 too. Above that the limit is by Mach number (Mmo), as you continue to climb your indicated air speed and your ground speed now decline as your Mach number remains constant.

However, even though you are slowing down you engines are burning less and less fuel, part of this is from the decreased IAS, but part is from the cold air. Colder air gives greater charge weight, it can be compressed more and the engines get greater thermodynamic efficiency.

Eventually you reach the lowest clean IAS for your current weight, and that's as high as you are going. It doesn't make any difference how much power you could add, you still can't climb because to do so you would need to slow down or break up, and to slow down you'd have to start deploying high lift devices which increase drag and reduce efficiency. This is what's called the coffin corner, your engines are probably running near max power, you are near or at max speed and you are just above the stall.

L
Larry Visoski Aug 15, 2015 9:54 PM
To
jeffrey E.

Jeffrey

Great email description of coffin corner, weight and altitude vs performance.

Below Are comments from Cyrus supervisor at PBI Gulfstream:

-Both left and right (cockpit and cabin) packs can feed the cabin silencer through some interconnect valves.

-If you turn the right pack or right bleed air off in flight there is a cross-over duct and check valve that will open and allow the left air/pack to supply air to both cockpit and cabin.

The ADC does also the turbine bypass valve on both ACM's to open but that's at 42k feet

-The left and right pack inlet valves go into high flow mode from 25 pounds per min to 26.5 PPM at 13k feet

-They jump again to 28 PPM to the packs at 23k feet

-So the ACM turbine bypass valves and the pack inlet valves are both altitude controlled but only the turbine bypass valve gets it altitude position from the ADC. The other has a built in aneroid on the side of the valve and senses the atmospheric pressure in the boiler room in flight.

-Larry,

Honestly I doubt the bleed is your problem but only way to tell that I can think of is to turn them off one at a time in flight. And see if the problem changes.

Best is to turn both off at altitude but that is not a flight I'm going on!

Cyrus

Sent from my iPhone

J
jeffrey E. Aug 16, 2015 3:26 AM
To
Larry Visoski

im looking for something that dumps overboard

1419 files from the DOJ Epstein case media release. All files are public records from justice.gov.

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