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12-07-2011, 10:04 PM
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Join Date: May 2007
Location: Inver Grove Hgts, MN
Posts: 329
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AOA Probe on Piper Pitot Mast
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Mike Hilger
RV-6 N207AM w/G3X, 1,600 hours +
South St. Paul, MN (KSGS)
A&P, EAA Tech Counselor
We're all here because we're not all there...
Last edited by Ironflight : 12-08-2011 at 09:15 AM.
Reason: fixed formatting
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12-07-2011, 10:19 PM
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Join Date: Jun 2006
Location: 8I3
Posts: 3,562
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Those Piper pitots are infinitely tunable to make them work well as a static source. If the airspeed reads high you just have to cut the bottom steeper to increase static pressure, which will lower indicated airspeed. And vise-versa. The tube you have here approximates doing exactly the same thing.
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Bob Japundza CFI A&PIA
N9187P PA-24-260B Comanche, flying
N678X F1 Rocket, under const.
N244BJ RV-6 "victim of SNF tornado" 1200+ hrs, rebuilding
N8155F C150 flying
N7925P PA-24-250 Comanche, restoring
Not a thing I own is stock.
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12-08-2011, 11:54 AM
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Join Date: May 2007
Location: Inver Grove Hgts, MN
Posts: 329
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Quote:
Originally Posted by rocketbob
Those Piper pitots are infinitely tunable to make them work well as a static source.
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Sounds like I gave up too easily...
__________________
Mike Hilger
RV-6 N207AM w/G3X, 1,600 hours +
South St. Paul, MN (KSGS)
A&P, EAA Tech Counselor
We're all here because we're not all there...
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12-08-2011, 12:18 PM
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Join Date: Jun 2006
Location: 8I3
Posts: 3,562
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Yep
Just think driving along on a summer day, hand out the window...what happens when you change the AOA of your hand... 
__________________
Please don't PM me! Email only!
Bob Japundza CFI A&PIA
N9187P PA-24-260B Comanche, flying
N678X F1 Rocket, under const.
N244BJ RV-6 "victim of SNF tornado" 1200+ hrs, rebuilding
N8155F C150 flying
N7925P PA-24-250 Comanche, restoring
Not a thing I own is stock.
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12-08-2011, 04:56 PM
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Forum Peruser
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Join Date: Jan 2005
Location: Austinville, Alabama
Posts: 2,455
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Huh? Total Pressure, Static Pressure and Velocity Pressure
Quote:
Originally Posted by rocketbob
... cut the bottom steeper to increase static pressure...
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There is a difference between "pressure measured by the static port" and "static pressure." Rocketbob, I think in your rush you meant to say "by cutting the bottom at a steeper angle, the pressure measured by the static port increases."
The Pitot port measures TOTAL Pressure and the STATIC port measures STATIC Pressure. Subtract Static Pressure from Total Pressure and you get Velocity Pressure. (An Air Speed Indicator converts this Velocity Pressure measurement into a number (knots or MPH) which our brain understands.)
By cutting the bottom of the Piper mast at a steeper angle, the static port will measure not only the Static Pressure but also some fraction of the Velocity Pressure. The Static Pressure reading is higher, but the Static Pressure surrounding the aircraft is the same. The measurement of Static Pressure should be the same all around the aircraft as long as the Static port is not measuring any of the pressure caused by the airflow (velocity pressure). That's one way measurement errors occur.
As Mike, the original poster, indicated, another port for Static Pressure for other instruments such as Altimeter should be used, as the pressure measured by his new tube in the Static Port is now measuring more than just Static Pressure.
The AOA probe shown by Mike, Mel and others works by measuring the angle at which the Pitot port measures more Static Pressure than Total Pressure AND the "Static" port measures more Total Pressure than "Static" Pressure, not necessarily "absolute" but certainly "relatively." The two ports reverse roles as AOA is increased. By bending the probe slightly into the airflow, the tubing probe Mike made measures more Total Pressure when the aircraft is near a stalled airflow condition. (In the above, "Static" implies Static plus some fraction of Total pressure, as decribed in the paragraph above.)
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Don Hull
RV-7 Wings
KDCU Pryor Field
Pilots'n Paws Pilot
N79599/ADS-B In and Out...and I like it!
?Certainly, travel is more than the seeing of sights;
it is a change that goes on, deep and permanent, in the ideas of living." Miriam Beard
Last edited by rv7boy : 12-08-2011 at 06:07 PM.
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12-08-2011, 05:58 PM
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Join Date: Jan 2005
Location: Austinville, Alabama
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One question for Mike (rvsxer):
Will you be able to bend the tubing without removing the mast from the wing? I'm thinking you might have to make some fine adjustments, and it may be hard to do while it's on the airplane. I do note your tubing is aluminum so it may be easier than I first thought. The Lift Reserve Indicator mast uses an adjustable mount which appears to be easy to adjust. Its ports are at 90 degrees to each other; that means both ports will be moved when it is adjusted.
Keep us posted on how well this works. I'm interested because I bought a used Piper mast and hadn't thought about using it for an AOA probe until I saw yours.
__________________
Don Hull
RV-7 Wings
KDCU Pryor Field
Pilots'n Paws Pilot
N79599/ADS-B In and Out...and I like it!
?Certainly, travel is more than the seeing of sights;
it is a change that goes on, deep and permanent, in the ideas of living." Miriam Beard
Last edited by rv7boy : 12-08-2011 at 06:02 PM.
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04-26-2013, 11:41 AM
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Join Date: Nov 2006
Location: Savannah, GA
Posts: 1,029
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I hope thread necromancy isn't frowned upon...
I'm at work so I can't view the pictures right now, but has anyone tried doing this (making AOA work) without adding additional tubing? Now that my wings are here I probably need to make a decision soon on a pitot system, and using an old heated Piper blade seems like a wonderful solution--at least, much better than shelling out $550 for the Dynon probe and mount.
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