M14PEngines-List Digest Archive

Mon 04/10/06


Total Messages Posted: 8



Today's Message Index:
----------------------
 
     1. 12:28 AM - Manifold Pressure (Scott Aldrich)
     2. 08:38 AM - Re: Manifold Pressure (A. Dennis Savarese)
     3. 08:50 AM - Re: Manifold Pressure (Ted Waltman)
     4. 08:53 AM - Re: Manifold Pressure (Scott Aldrich)
     5. 08:58 AM - Re: Manifold Pressure (A. Dennis Savarese)
     6. 09:02 AM - Re: Manifold Pressure (A. Dennis Savarese)
     7. 09:27 AM - Re: Manifold Pressure (Scott Aldrich)
     8. 10:31 AM - Re: Manifold Pressure (A. Dennis Savarese)
 
 
 


Message 1


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    Time: 12:28:44 AM PST US
    From: "Scott Aldrich" <s-aldrich@comcast.net>
    Subject: Manifold Pressure
    Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 2


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    Time: 08:38:22 AM PST US
    From: "A. Dennis Savarese" <dsavarese@elmore.rr.com>
    Subject: Re: Manifold Pressure
    Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 3


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    Time: 08:50:31 AM PST US
    From: "Ted Waltman" <tedwaltman@i1ci.com>
    Subject: Manifold Pressure
    Dennis, This whole debate started with a couple of us comparing MP on our M-14 engines. Yesterday, at roughly std temp--or maybe a few degrees warmer--I saw 26.1" at takeoff at 4,965'. A standard engine on a Swift was showing about 22" at takeoff (at 1,921 prop rpm or 2,919 engine rpm). We were both at roughly 25" before engine start. So, I'm not seeing the 736mm, or 28.97", you indicate below. Perhaps my gauge is a bit off? Ted _____ From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott <mailto:s-aldrich@comcast.net> Aldrich Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 4


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    Time: 08:53:14 AM PST US
    From: "Scott Aldrich" <s-aldrich@comcast.net>
    Subject: Manifold Pressure
    That is about what I was thinking we should see roughly 29 inches. With no real charts (that I know of or can understand) I am wondering when the supercharger starts to loss it effectiveness in giving the approx. 5 inch. Scott _____ From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich <mailto:s-aldrich@comcast.net> Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 5


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    Time: 08:58:17 AM PST US
    From: "A. Dennis Savarese" <dsavarese@elmore.rr.com>
    Subject: Re: Manifold Pressure
    Most likely the gauge is off, just like I know mine is. We're at 200' MSL here at our airport. So our MP gauges should read pretty close to 760 mm on a standard day. I can tell you this. Mine surely does not. It reads low by about 30-40 mm compared to the other 4 Yaks in our hangar. The numbers should be just about right I think. I used this site, http://www.digitaldutch.com/atmoscalc/, to get the standard atmospheric pressure at 5000'. The rest of the data came from the engine manual and basic calculations. Dennis ----- Original Message ----- From: Ted Waltman To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 10:50 AM Subject: RE: M14PEngines-List: Manifold Pressure Dennis, This whole debate started with a couple of us comparing MP on our M-14 engines. Yesterday, at roughly std temp--or maybe a few degrees warmer--I saw 26.1" at takeoff at 4,965'. A standard engine on a Swift was showing about 22" at takeoff (at 1,921 prop rpm or 2,919 engine rpm). We were both at roughly 25" before engine start. So, I'm not seeing the 736mm, or 28.97", you indicate below. Perhaps my gauge is a bit off? Ted From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM To: m14pengines-list@matronics.com Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 6


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    Time: 09:02:30 AM PST US
    From: "A. Dennis Savarese" <dsavarese@elmore.rr.com>
    Subject: Re: Manifold Pressure
    The super charger drop is basically linear, assuming 100% power. It never really loses its "effectiveness". It will always boost above atmospheric pressure, as long as it's turning. -) It just starts off higher (+5" approximately). Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 10:53 AM Subject: RE: M14PEngines-List: Manifold Pressure That is about what I was thinking we should see roughly 29 inches. With no real charts (that I know of or can understand) I am wondering when the supercharger starts to loss it effectiveness in giving the approx. 5 inch. Scott From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM To: m14pengines-list@matronics.com Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 7


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    Time: 09:27:18 AM PST US
    From: "Scott Aldrich" <s-aldrich@comcast.net>
    Subject: Manifold Pressure
    That brings up the question (at least for me) if you had a small leak in the MP line on a supercharged engine would that cause low indication due to pressure loss? Whereas on none turbo or supercharged a leak may cause higher indication due to less vacuum (because it is really vacuum and not "pressure" on a standard engine, i.e. MP usually drops slightly when takeoff power is applied). Too much thinking. Scott _____ From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:58 AM Subject: Re: M14PEngines-List: Manifold Pressure Most likely the gauge is off, just like I know mine is. We're at 200' MSL here at our airport. So our MP gauges should read pretty close to 760 mm on a standard day. I can tell you this. Mine surely does not. It reads low by about 30-40 mm compared to the other 4 Yaks in our hangar. The numbers should be just about right I think. I used this site, http://www.digitaldutch.com/atmoscalc/, to get the standard atmospheric pressure at 5000'. The rest of the data came from the engine manual and basic calculations. Dennis ----- Original Message ----- From: Ted Waltman <mailto:tedwaltman@i1ci.com> Sent: Monday, April 10, 2006 10:50 AM Subject: RE: M14PEngines-List: Manifold Pressure Dennis, This whole debate started with a couple of us comparing MP on our M-14 engines. Yesterday, at roughly std temp--or maybe a few degrees warmer--I saw 26.1" at takeoff at 4,965'. A standard engine on a Swift was showing about 22" at takeoff (at 1,921 prop rpm or 2,919 engine rpm). We were both at roughly 25" before engine start. So, I'm not seeing the 736mm, or 28.97", you indicate below. Perhaps my gauge is a bit off? Ted _____ From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich <mailto:s-aldrich@comcast.net> Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott


    Message 8


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    Time: 10:31:03 AM PST US
    From: "A. Dennis Savarese" <dsavarese@elmore.rr.com>
    Subject: Re: Manifold Pressure
    Yes, too much thinking for sure! -) Sounds about right to me. Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 11:07 AM Subject: RE: M14PEngines-List: Manifold Pressure That brings up the question (at least for me) if you had a small leak in the MP line on a supercharged engine would that cause low indication due to pressure loss? Whereas on none turbo or supercharged a leak may cause higher indication due to less vacuum (because it is really vacuum and not "pressure" on a standard engine, i.e. MP usually drops slightly when takeoff power is applied). Too much thinking. Scott From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:58 AM To: m14pengines-list@matronics.com Subject: Re: M14PEngines-List: Manifold Pressure Most likely the gauge is off, just like I know mine is. We're at 200' MSL here at our airport. So our MP gauges should read pretty close to 760 mm on a standard day. I can tell you this. Mine surely does not. It reads low by about 30-40 mm compared to the other 4 Yaks in our hangar. The numbers should be just about right I think. I used this site, http://www.digitaldutch.com/atmoscalc/, to get the standard atmospheric pressure at 5000'. The rest of the data came from the engine manual and basic calculations. Dennis ----- Original Message ----- From: Ted Waltman To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 10:50 AM Subject: RE: M14PEngines-List: Manifold Pressure Dennis, This whole debate started with a couple of us comparing MP on our M-14 engines. Yesterday, at roughly std temp--or maybe a few degrees warmer--I saw 26.1" at takeoff at 4,965'. A standard engine on a Swift was showing about 22" at takeoff (at 1,921 prop rpm or 2,919 engine rpm). We were both at roughly 25" before engine start. So, I'm not seeing the 736mm, or 28.97", you indicate below. Perhaps my gauge is a bit off? Ted From: owner-m14pengines-list-server@matronics.com [mailto:owner-m14pengines-list-server@matronics.com] On Behalf Of A. Dennis Savarese Sent: Monday, April 10, 2006 9:38 AM To: m14pengines-list@matronics.com Subject: Re: M14PEngines-List: Manifold Pressure Scott, On a standard day at sea level, barometric pressure in inches is 29.92" which equals 760 mm. At 100% the supercharger boosts the pressure (at sea level) to approximately 885 mm or 34.85", a factor of 1.165. At 5000' on a standard day the barometric pressure should be about 24.9 inches, or 632 mm. Given the supercharger boost factor, at 5000' with 100% rpm the manifold pressure should come up to about 736 mm. I'm sure if my numbers are wrong someone will definitely correct me. -) Dennis ----- Original Message ----- From: Scott Aldrich To: m14pengines-list@matronics.com Sent: Monday, April 10, 2006 2:27 AM Subject: M14PEngines-List: Manifold Pressure Wonder what to expect (roughly) for a take off Manifold Pressure on a standard day at a 5000' MSL airport with the standard M14P? Thanks, Scott




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