Chris, thanks for
the feedback and the work you did.
I sense a
contradiction in this statement;
[Our pumps come with
the lowest of three fixed TRV values. The set-point is 2,500 psi,
thus the statement "approximately
100-140 bar (1500-2000 psi) above
the system relief valve pressure" still holds true.]
I see two
interpretations.
1… The TRV “setpoint
is 2,500 psi”, presumably referenced to reservoir pressure, which is ambient
cabin pressure assuming the reservoir is well vented. Thus the TRV will limit
the output pressure to 2,500 psig max. In that case the graphs in the brochure
do not apply for our pumps above 2500 psi.
2… The TRV setpoint
is “(1500-2000 psi) above the system relief valve
pressure.” I interpret “system relief valve pressure” to be the setpoint of the
internal HPRV or LPRV located upstream of the check valves. These set points
are not specified in the brochure, but the performance graphs indicate that the
HPRV is at least 3,000 psi which would make the TRV setpoint 4,500 - 5,000
psig.
Perhaps you are
saying the TRV setpoint is 1,500 – 2,000 psi above the pressure switch
setpoint’s, but I was commenting on this quote from the brochure which says
something else.
“It is a fixed relief
valve with a pressure setting approximately 100-140 bar (1500-2000 psi) above
the system relief valve pressure.”
If the TRV setpoint
is lower than the HPRV and LPRV setpoints I see no need for the HPRV and LPRV.
What is their purpose?
I would like to know how much pressure it takes to keep the
wheels in the wells during a high speed high G pullup. If the relief valve
lifts and the gear comes out of the wells, it could literally blow the doors
off the airplane. If anybody with gauges does a gear test in the next few
months, please note the pressure just before the gear tightens up in the wells and let
me know. Five times that number should be about right.