REFLECTOR: Hydraulic Pump Leak..fluid levels
Alex Balic
alex157 at direcway.com
Tue Dec 14 09:22:55 CST 2004
Just as a rough guess (not being at the aircraft this morning) but if the
main cyl is 1.5" diameter, and the rod is .375 diameter, then the difference
would be 25% in both volume and power calculations- with a (another guess)
stroke length of 18" this would be a difference of 4.4 oz of fluid- the
nose cylinder probably adds another oz or so.
-----Original Message-----
From: reflector-bounces at tvbf.org [mailto:reflector-bounces at tvbf.org]On
Behalf Of Al Gietzen
Sent: Tuesday, December 14, 2004 12:34 AM
To: alex157 at direcway.com; 'Velocity Aircraft Owners and Builders list'
Subject: RE: REFLECTOR: Hydraulic Pump Leak..fluid levels
Subject: RE: REFLECTOR: Hydraulic Pump Leak..fluid levels
You would think that, but remember that when the cylinders are extended,
the
fluid volume is the volume of the cylinder bore x stroke, when the
cylinders
are retracted, the fluid volume is the volume of the cylinder bore x
stroke
minus the volume of the rod(s) - so there is a significant volume
difference- this type of difference is also taken into account in the
calculations of cylinder power, since on the out stroke, you get full
power,
but on the return stroke, you do not, since you must subtract the rod end
area from the total piston area.
All true. The difference is about 6%.
Al
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