TeamGrumman-List Digest Archive

Thu 02/04/10


Total Messages Posted: 5



Today's Message Index:
----------------------
 
     1. 11:50 AM - Fw: AC voltage at aircraft bus at approx. 1000rpm (teamgrumman@aol.com)
     2. 02:48 PM - Re: Fw: AC voltage at aircraft bus at approx. 	1000rpm (FLYaDIVE)
     3. 07:56 PM - Re: Fw: AC voltage at aircraft bus at approx. 1000rpm (teamgrumman@AOL.COM)
     4. 08:50 PM - Re: Fw: AC voltage at aircraft bus at approx. 1000rpm (Gil Alexander)
     5. 09:56 PM - Anouncement (923te)
 
 
 


Message 1


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    Time: 11:50:30 AM PST US
    Subject: Fwd: AC voltage at aircraft bus at approx. 1000rpm
    From: teamgrumman@aol.com
    Here is the ripple on a PP alternator. Even with a Zeftronics regulator and a Garmin audio panel, the noise comes through. -----Original Message----- From: Keith Wannamaker <keith@wannamaker.org> Sent: Thu, Feb 4, 2010 10:51 am Subject: Fwd: AC voltage at aircraft bus at approx. 1000rpm Gary, here is an oscope on my bus with the plane-power. I'm a bit like a hog looking at a wristwatch with the readout. I'm not sure if it is sayi ng 1/2 volt AC top to bottom or 1/8 volt top to bottom. The plane power guy claims that 1/8 volt ac is within spec, but I sent him the picture an d am waiting to hear back. Keith


    Message 2


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    Time: 02:48:02 PM PST US
    Subject: Re: Fwd: AC voltage at aircraft bus at approx. 1000rpm
    From: FLYaDIVE <flyadive@gmail.com>
    Keith & Gary: Looking at your picture ... In the lower right corner the screen reads 0.2 V/Div. That means between EACH large Tic it is 0.2 V. SO ... Your Peak reading is about (again looking at the picture) 0.24 Volts and the Peak to Peak (P-P) is 0.28 Volts. As for what is acceptable... That may be determined by the manufacture or the FAA. I do not know. BUT! When I do a very simple but ACCURATE test using a DMM (Digital Multi Meter) I look for 0.4 to 0.5 V AC at the BATTERY to determine if a diode is bad. For the little voltage you are seeing I would put a 0.001 uF Ceramic Cap in parallel with a 50,000 uF (or more) Electrolytic Cap and the NEG side of the Cap goes to GROUND, POS side to POS Battery AND/OR - Put a large electrolytic Cap from the 'S' terminal of the VR to Ground. If you have that little noise (0.48 V P-P) the caps will remove it. Barry On Thu, Feb 4, 2010 at 2:48 PM, <teamgrumman@aol.com> wrote: > Here is the ripple on a PP alternator. Even with a Zeftronics regulator > and a Garmin audio panel, the noise comes through. > > > -----Original Message----- > From: Keith Wannamaker <keith@wannamaker.org> > To: Gary Vogt <teamgrumman@aol.com> > Sent: Thu, Feb 4, 2010 10:51 am > Subject: Fwd: AC voltage at aircraft bus at approx. 1000rpm > > Gary, here is an oscope on my bus with the plane-power. I'm a bit like a > hog looking at a wristwatch with the readout. I'm not sure if it is saying > 1/2 volt AC top to bottom or 1/8 volt top to bottom. The plane power guy > claims that 1/8 volt ac is within spec, but I sent him the picture and am > waiting to hear back. > > Keith > >


    Message 3


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    Time: 07:56:44 PM PST US
    Subject: Re: Fwd: AC voltage at aircraft bus at approx. 1000rpm
    From: teamgrumman@AOL.COM
    The whole point is not to patch together something that should work withou t a "FIX." It says right on the alternator and the associated paperwork that no noise filter is required. It's kind of like wearing a glove when you buy a pen that leaks. -----Original Message----- From: FLYaDIVE <flyadive@gmail.com> Sent: Thu, Feb 4, 2010 2:47 pm Subject: Re: TeamGrumman-List: Fwd: AC voltage at aircraft bus at approx. 1000rpm Keith & Gary: Looking at your picture ... In the lower right corner the screen reads 0.2 V/Div. That means between EACH large Tic it is 0.2 V. SO ... Your Peak reading is about (again looking at the picture) 0.24 Volt s and the Peak to Peak (P-P) is 0.28 Volts. As for what is acceptable... That may be determined by the manufacture or the FAA. I do not know. BUT! When I do a very simple but ACCURATE test using a DMM (Digital Multi Meter) I look for 0.4 to 0.5 V AC at the BATTE RY to determine if a diode is bad. For the little voltage you are seeing I would put a 0.001 uF Ceramic Cap in parallel with a 50,000 uF (or more) Electrolytic Cap and the NEG side of the Cap goes to GROUND, POS side to POS Battery AND/OR - Put a large electrolytic Cap from the 'S' terminal of the VR to Ground. If you have that little noise (0.48 V P-P) the caps will remove it. Barry On Thu, Feb 4, 2010 at 2:48 PM, <teamgrumman@aol.com> wrote: Here is the ripple on a PP alternator. Even with a Zeftronics regulator and a Garmin audio panel, the noise comes through. -----Original Message----- From: Keith Wannamaker <keith@wannamaker.org> Sent: Thu, Feb 4, 2010 10:51 am Subject: Fwd: AC voltage at aircraft bus at approx. 1000rpm Gary, here is an oscope on my bus with the plane-power. I'm a bit like a hog looking at a wristwatch with the readout. I'm not sure if it is sayi ng 1/2 volt AC top to bottom or 1/8 volt top to bottom. The plane power guy claims that 1/8 volt ac is within spec, but I sent him the picture an d am waiting to hear back. Keith ======================== =========== ======================== =========== ======================== =========== ======================== ===========


    Message 4


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    Time: 08:50:53 PM PST US
    From: Gil Alexander <gilalex@earthlink.net>
    Subject: Re: Fwd: AC voltage at aircraft bus at approx. 1000rpm
    Gary, At 5 mS/div on the scope... could you be seeing some 60 Hz pickup? - which would be just over 3 divisions. Is the noise frequency proportional to RPM? How long was the ground lead to your probe? gil A At 08:55 PM 2/4/2010, teamgrumman@aol.com wrote: >The whole point is not to patch together something that should work >without a "FIX." It says right on the alternator and the associated >paperwork that no noise filter is required. > >It's kind of like wearing a glove when you buy a pen that leaks. > > >-----Original Message----- >From: FLYaDIVE <flyadive@gmail.com> >To: teamgrumman-list@matronics.com >Sent: Thu, Feb 4, 2010 2:47 pm >Subject: Re: TeamGrumman-List: Fwd: AC voltage at aircraft bus at >approx. 1000rpm > >Keith & Gary: > >Looking at your picture ... In the lower right corner the screen >reads 0.2 V/Div. >That means between EACH large Tic it is 0.2 V. >SO ... Your Peak reading is about (again looking at the picture) >0.24 Volts and the Peak to Peak (P-P) is 0.28 Volts. >As for what is acceptable... That may be determined by the >manufacture or the FAA. I do not know. BUT! When I do a very >simple but ACCURATE test using a DMM (Digital Multi Meter) I look >for 0.4 to 0.5 V AC at the BATTERY to determine if a diode is bad. > >For the little voltage you are seeing I would put a 0.001 uF Ceramic >Cap in parallel with a 50,000 uF (or more) Electrolytic Cap and the >NEG side of the Cap goes to GROUND, POS side to POS Battery > >AND/OR - Put a large electrolytic Cap from the 'S' terminal of the >VR to Ground. > >If you have that little noise (0.48 V P-P) the caps will remove it. > >Barry > > >On Thu, Feb 4, 2010 at 2:48 PM, ><<mailto:teamgrumman@aol.com>teamgrumman@aol.com> wrote: >Here is the ripple on a PP alternator. Even with a Zeftronics >regulator and a Garmin audio panel, the noise comes through. > > >-----Original Message----- >From: Keith Wannamaker <<mailto:keith@wannamaker.org>keith@wannamaker.org> >To: Gary Vogt <<mailto:teamgrumman@aol.com>teamgrumman@aol.com> >Sent: Thu, Feb 4, 2010 10:51 am >Subject: Fwd: AC voltage at aircraft bus at approx. 1000rpm > >Gary, here is an oscope on my bus with the plane-power. I'm a bit >like a hog looking at a wristwatch with the readout. I'm not sure >if it is saying 1/2 volt AC top to bottom or 1/8 volt top to >bottom. The plane power guy claims that 1/8 volt ac is within spec, >but I sent him the picture and am waiting to hear back. > >Keith > > >=================================== >ator?TeamGrumman-List">http://www.matronics.com/Navigator?TeamGrumman-List >=================================== >ttp://forums.matronics.com >=================================== >ibution">http://www.matronics.com/contribution >=================================== > >


    Message 5


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    Time: 09:56:43 PM PST US
    From: "923te" <923te@att.net>
    Subject: Anouncement
    Grumman Gang, MT Propeller has received Supplemental Type Certificate for installing their MTV-18-B/183-59b propeller assembly with 2700 RPM controller on all models of Grumman Tigers. This STC was initiated through a cooperative of 2 Grumman gangers and the MT distributor Jim Ayers with Less Drag Products. This STC uses the latest, most efficient blade design. Pictures and more information are available at links below. The MT propeller is an electrically controlled constant speed prop. It has both an automatic mode and a manual mode. In the auto mode you simply dial in the desired RPM and the controller will hold that RPM. In the manual mode the pilot must hold the RPM thru a momentary switch. It works great and really makes a whole new airplane out of the Tiger. As an introductory special, we have been able to arrange that the first 10 props can be sold at a 10% discount. The current price of the prop is $12,480. The discounted price for the first ten purchasers is $11,232. The prop is shipped disassembled from Germany to Less Drag Products, Inc. in Southern California for $360 so the total cost is $11,592 plus freight to you, or you can fly in to Less Drag Products at OXNARD airport and fly home faster. This special group purchase price ends March 15 and MT is raising prices on April 1, so if you want to go faster and climb better, now is the time to do it. Website links that you should check out: http://www.mt-propeller.com/en/entw/stcusa/grumman.htm http://www.mt-propeller.com/en/entw/electric.htm Here are MT Data and manual links: http://www.mt-propeller.com/pdf/datsheet/mtv-18.pdf The Design Limit for the MT prop is 300HP at 2800RPM Manual: http://www.mt-propeller.com/pdf/manuals/e-118.pdf Email me Ned Thomas at 923te@att.net to hold a place in the group purchase. Contact Jim Ayers for more details on the prop at 805-795-5377 8am to 8pm PST.




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