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MikeyC
Joined: 24 Jan 2017 Posts: 21 Location: 1GA0
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Posted: Wed Oct 07, 2020 4:35 pm Post subject: "Beefing Up" |
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I’ve built in a couple of hard points to accommodate an over-the-shoulder angle for the safety harness and a couple to allow removal of the seat back. The technique is similar to the one used to install the engine mounts. The main difference is that the engine mounts transfer load directly to the embedded unidirectional glass. What that means to me, an amateur builder, is that my mods need to be conservative - in terms of structural integrity. Because these mods were important to me, I paid the penalty of a slight weight hit in order to beef that structure up. My advice would be to build the plane exactly as it was designed. If there’s a standard feature you just can’t live with, seek the advice of an experienced builder before even contemplating a change.
Best, Mike Cowan Pulsar Series 2.5
On Wed, Oct 7, 2020 at 12:50 PM Yellowhammer <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)> wrote:
Quote: | --> Pulsar-List message posted by: "Yellowhammer" <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)>
Greetings Folks,
Read an ad for a Pulsar Kit number 1 for sale and it said it had a beefed up fuselage. Was just curious as to how folks are beefing up their fuselages or if anyone has beefed up other parts of their planes.
If so, what did you do to make it stronger?
Thanks,
Yellowhammer
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498687#498687
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errer" target="_blank">http://wiki.matronics.com
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| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
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Yellowhammer
Joined: 21 Mar 2018 Posts: 101 Location: Franklinton, Louisiana
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Posted: Mon Oct 12, 2020 6:25 am Post subject: Re: |
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Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
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_________________ J.M. Oyler "Clyde" |
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gregsmi
Joined: 01 Jan 2011 Posts: 268 Location: Topeka, KS
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Posted: Mon Oct 12, 2020 7:14 am Post subject: "Beefing Up" |
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If you follow the build manuals the Pulsar seems very strong for the type of flying it was designed for. Beefing up or adding extra glass will add significant weight which will reduce load capacity. It will not change the design weight limitations. When I was building, I would call the factory and was always told deviations in one area always had consequences in another area. Mark would have to do analysis to ferret out the proposed changes, emphasizing that the plane is a system and changes in any area have compound affects in other areas. In some cases, adding more glass to a layup just adds weight because the structure you are glassing to has not change.
We do not have the designer for that support today so be very careful about any deviations. After 1500 hours of Pulsar flying, over 24 years, I am not disappointed in the aircraft.
Greg
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bernard.wilder2(at)gmail. Guest
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Posted: Mon Oct 12, 2020 7:45 am Post subject: "Beefing Up" |
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I doubled the rear brackets where the landing gear attaches to the lower fire wall. When building, some other owners had them crack or fail.
I attached angle aluminum supports to the bottom of the rear engine mount where the nose gear shock absorber attaches to the bottom of the mount. This is the element that transverses the engine compartment. Some had bent when the nose wheel was used as part of the landing gear.
I closed off about 60% of the front cowl openings. I faired in the closure. Too much air comes in the original openings that were designed to provide air to the two radiators used with the 481. One chap had an oil leak and the oil exited the front left cowl opening. Also the rear of the top cowl puffed up due to the pressure under the cowl from the large openings. Further, the increased pressure under the cowl fools the carbs into thinking they are at a lower altitude then they really are. Never had a cooling problem while significantly reducing the drag.
I filleted the horizontal stab to the fuselage. Yes,, it is no longer removable by just pulling the two pins and disconnecting the push rod, but who cares ? ? ? ? ? ME ! ! ! ! ! When I moth balled my girl I had to get out the dremel again and cut the fillet away. No problem.
I doubled the uniweave glass in the bed mount side supports. Just on general principles.
I put three extra attach screws on the rear of the top cowl where it attaches to the fuselage. Because p[eople were reporting that the top of the cowl raised up when in the air. (( Due to too much air pressure under the cowl, again, from too large openings in the front cowl.))
I often put an extra layer of glass on joints that looked crucially structural. Did I add weight ? ? ? Sure,, but not much. Besides I was on a diet and lost weight personally so I figured I came out even..
My bird survived a 325 MPH dive with no damage other than a little paint peeled off the leading edges here and there. I obviously don't regret the extra weight and strength that came with the weight. But what really saved me was that my control surfaces were well balanced and I got no flutter.
On your second flight you want to carefully but aggressively check for flutter.
Good Luck.
Bernie Wilder
XP 390XP
On Mon, Oct 12, 2020 at 10:29 AM Yellowhammer <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)> wrote:
Quote: | --> Pulsar-List message posted by: "Yellowhammer" <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)>
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752
===========
ar-List" rel="noreferrer" target="_blank">http://www.matronics.com/Navigator?Pulsar-List
===========
FORUMS -
eferrer" target="_blank">http://forums.matronics.com
===========
WIKI -
errer" target="_blank">http://wiki.matronics.com
===========
b Site -
-Matt Dralle, List Admin.
rel="noreferrer" target="_blank">http://www.matronics.com/contribution
===========
|
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
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DiscoverPulsar
Joined: 24 Jan 2019 Posts: 10
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Posted: Mon Oct 12, 2020 9:01 am Post subject: "Beefing Up" |
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Hi Clyde,
I was looking for my notes before responding but could not find them yet. I do recall taking them when I decided to sell my wood wing XP project and purchase the Pulsar II. I recall that each time horsepower was increased there were structural additions. With the upgrade from the 582 to the 912 it seems that additional layer or layers of fiberglass were laid into the mold of the upper fuselage and there was additional unidirectional to be placed in the roll bar behind the cockpit lip and of course the bed mount uni. The spars were upgraded with different caps and fiberglass and then to complete fiberglass and then different thickness of caps over the years. The fuel tank move to the wings was actually a good thing from a structural requirement of the wings and eventually brought with it the “red” foam ribs that were more fuel “proof” than the blue. The wing skins went from a light fiberglass covered wood to complete fiberglass and the vertical spar went from attaching to the fuselage top only to extending through the fuselage top all the way to the floor. Also, I think additional plies were added to where the vertical attached to the top of the fuselage when it was determined that the starting torque of the 912 was so much more than the 582 that the vertical stab was countering the torque so much that cracking was occurring there on the fuselage top. That’s all from memory of some 20+ years ago. so I may have said some things not quite correct.... I’ll keep looking for notes and post what I can find.
Best regards,
Your Fellow Pulsar Enthusiast,
Ned
On Oct 12, 2020, at 9:29 AM, Yellowhammer <coyler(at)sthpk-12.net> wrote:
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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DiscoverPulsar
Joined: 24 Jan 2019 Posts: 10
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Posted: Mon Oct 12, 2020 9:06 am Post subject: "Beefing Up" |
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One thing I meant to mention is that the original Pulsar design was done by an aerospace structural engineer by the name of Mark Brown. My Dad worked at AeroCommander with Mark in Norman, OK many years ago before Mark moved to San Antonio. Mark has an excellent reputation for certified structural engineering so when you think you have found an area that needs “beefed up” it is a good idea to do as you have here and ask the group about it. Sometimes beefing up something has unintended consequences that defeat the design.
On Oct 12, 2020, at 11:57 AM, N3300P <n3300p(at)gmail.com> wrote:
Hi Clyde,
I was looking for my notes before responding but could not find them yet. I do recall taking them when I decided to sell my wood wing XP project and purchase the Pulsar II. I recall that each time horsepower was increased there were structural additions. With the upgrade from the 582 to the 912 it seems that additional layer or layers of fiberglass were laid into the mold of the upper fuselage and there was additional unidirectional to be placed in the roll bar behind the cockpit lip and of course the bed mount uni. The spars were upgraded with different caps and fiberglass and then to complete fiberglass and then different thickness of caps over the years. The fuel tank move to the wings was actually a good thing from a structural requirement of the wings and eventually brought with it the “red” foam ribs that were more fuel “proof” than the blue. The wing skins went from a light fiberglass covered wood to complete fiberglass and the vertical spar went from attaching to the fuselage top only to extending through the fuselage top all the way to the floor. Also, I think additional plies were added to where the vertical attached to the top of the fuselage when it was determined that the starting torque of the 912 was so much more than the 582 that the vertical stab was countering the torque so much that cracking was occurring there on the fuselage top. That’s all from memory of some 20+ years ago. so I may have said some things not quite correct.... I’ll keep looking for notes and post what I can find.
Best regards,
Your Fellow Pulsar Enthusiast,
Ned
On Oct 12, 2020, at 9:29 AM, Yellowhammer <coyler(at)sthpk-12.net> wrote:
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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MikeyC
Joined: 24 Jan 2017 Posts: 21 Location: 1GA0
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Posted: Mon Oct 12, 2020 9:20 am Post subject: "Beefing Up" |
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Clyde,
Fleetwide experience has highlighted the need for attention to the nosegear fork assy. There’s consensus agreement on that (not a factor for taildraggers).
Some builders have beefed up the vertical stab spar. Others have added plies to the main gear near the axle attach area. If you have blue foam ribs, you may want to replace those. The kit-supplied exhaust left a lot to be desired. Offhand, I can’t think of anything else.
That said, there are lots of Pulsars flying around with none of those mods. As the builder, it’s your call. I would emphasize, though, that nearly any modification is going to add weight - the enemy of performance. I think your plan to stick with the baseline design is sound. You’ll likely have opportunities to “fix” problems as they arise.
My 2 cents.
MikeyC
On Mon, Oct 12, 2020 at 10:29 AM Yellowhammer <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)> wrote:
Quote: | --> Pulsar-List message posted by: "Yellowhammer" <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)>
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752
===========
ar-List" rel="noreferrer" target="_blank">http://www.matronics.com/Navigator?Pulsar-List
===========
FORUMS -
eferrer" target="_blank">http://forums.matronics.com
===========
WIKI -
errer" target="_blank">http://wiki.matronics.com
===========
b Site -
-Matt Dralle, List Admin.
rel="noreferrer" target="_blank">http://www.matronics.com/contribution
===========
|
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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_________________ Mike Cowan |
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Yellowhammer
Joined: 21 Mar 2018 Posts: 101 Location: Franklinton, Louisiana
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Posted: Mon Oct 12, 2020 10:48 am Post subject: Re: Nose Gear Fork |
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In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
I appreciate all the feedback on my "beefed up " questions.
So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
I wonder if I should convert it to a single seat because of how small the cockpit is?
I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
I am building away as hard and steady as I can.
Wont be long now.
Thanks,
Clyde
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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_________________ J.M. Oyler "Clyde" |
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Yellowhammer
Joined: 21 Mar 2018 Posts: 101 Location: Franklinton, Louisiana
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Posted: Mon Oct 12, 2020 10:48 am Post subject: Re: Nose Gear Fork |
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In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
I appreciate all the feedback on my "beefed up " questions.
So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
I wonder if I should convert it to a single seat because of how small the cockpit is?
I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
I am building away as hard and steady as I can.
Wont be long now.
Thanks,
Clyde
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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_________________ J.M. Oyler "Clyde" |
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Yellowhammer
Joined: 21 Mar 2018 Posts: 101 Location: Franklinton, Louisiana
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Posted: Mon Oct 12, 2020 11:14 am Post subject: Re: |
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DiscoverPulsar wrote: | Hi Clyde,
I was looking for my notes before responding but could not find them yet. I do recall taking them when I decided to sell my wood wing XP project and purchase the Pulsar II. I recall that each time horsepower was increased there were structural additions. With the upgrade from the 582 to the 912 it seems that additional layer or layers of fiberglass were laid into the mold of the upper fuselage and there was additional unidirectional to be placed in the roll bar behind the cockpit lip and of course the bed mount uni. The spars were upgraded with different caps and fiberglass and then to complete fiberglass and then different thickness of caps over the years. The fuel tank move to the wings was actually a good thing from a structural requirement of the wings and eventually brought with it the “red” foam ribs that were more fuel “proof” than the blue. The wing skins went from a light fiberglass covered wood to complete fiberglass and the vertical spar went from attaching to the fuselage top only to extending through the fuselage top all the way to the floor. Also, I think additional plies were added to where the vertical attached to the top of the fuselage when it was determined that the starting torque of the 912 was so much more than the 582 that the vertical stab was countering the torque so much that cracking was occurring there on the fuselage top. That’s all from memory of some 20+ years ago. so I may have said some things not quite correct.... I’ll keep looking for notes and post what I can find.
Best regards,
Your Fellow Pulsar Enthusiast,
Ned
On Oct 12, 2020, at 9:29 AM, Yellowhammer <coyler> wrote:
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752 |
THANK YOU FOR YOUR RESPONSE AND INPUT. IT IS VALUED AND APPREIATTED.
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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_________________ J.M. Oyler "Clyde" |
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Yellowhammer
Joined: 21 Mar 2018 Posts: 101 Location: Franklinton, Louisiana
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Posted: Mon Oct 12, 2020 11:22 am Post subject: Re: |
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MikeyC wrote: | Clyde,
Fleetwide experience has highlighted the need for attention to the nosegear fork assy. There’s consensus agreement on that (not a factor for taildraggers).
Some builders have beefed up the vertical stab spar. Others have added plies to the main gear near the axle attach area. If you have blue foam ribs, you may want to replace those. The kit-supplied exhaust left a lot to be desired. Offhand, I can’t think of anything else.
That said, there are lots of Pulsars flying around with none of those mods. As the builder, it’s your call. I would emphasize, though, that nearly any modification is going to add weight - the enemy of performance. I think your plan to stick with the baseline design is sound. You’ll likely have opportunities to “fix” problems as they arise.
My 2 cents.
MikeyC
On Mon, Oct 12, 2020 at 10:29 AM Yellowhammer <coyler> wrote:
Quote: | --> Pulsar-List message posted by: "Yellowhammer" <coyler>
Mike,
Thanks for your input. I am certainly building my by the book. I was just curious to learn what, if any, added areas of strength builders have used other than those already discussed.
With an aircraft that has been in service as long as the Pulsar has, I was wondering what, if any , areas were strengthened.
As I am progressing through my build, I keep finding certain places that could have some extra strength.
Thanks,
Yellowhammer "Clyde"
--------
J.M. Oyler "Clyde"
Mikey,
I have already installed my blue foam ribs. I will not have fuel in the wings so will it still be an issue??
Thanks
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498752#498752
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ar-List" rel="noreferrer" target="_blank">http://www.matronics.com/Navigator?Pulsar-List
===========
FORUMS -
eferrer" target="_blank">http://forums.matronics.com
===========
WIKI -
errer" target="_blank">http://wiki.matronics.com
===========
b Site -
-Matt Dralle, List Admin.
rel="noreferrer" target="_blank">http://www.matronics.com/contribution
===========
|
|
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
http://www.matronics.com/Navigator?Pulsar-List |
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_________________ J.M. Oyler "Clyde" |
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mortweaver
Joined: 25 Apr 2015 Posts: 22
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Posted: Mon Oct 12, 2020 4:52 pm Post subject: "Beefing Up" |
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I built a replacement nose wheel for a Pulsar XP after breaking the cast aluminum fork. It was a copy of the 4130 steel fork that Sky Star sold as an upgrade for Pulsar owners. After cutting out the parts and using a heavy vise secured to workbench. Bending of fork tangs was then completed. After TIG welding was finished, the fork was then professionally cleaned and powder coat finish applied. No special tools required. A saber saw was used to cut the flat steel parts out of steel sheet material ordered from Air Spruce. IF you are interested, I will look for the drawing I made that shows dimensions and material thickness.
Dave Weaver
Sent from my iPhone
Quote: | On Oct 12, 2020, at 1:57 PM, Yellowhammer <coyler(at)sthpk-12.net> wrote:
In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
I appreciate all the feedback on my "beefed up " questions.
So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
I wonder if I should convert it to a single seat because of how small the cockpit is?
I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
I am building away as hard and steady as I can.
Wont be long now.
Thanks,
Clyde
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498772#498772
|
| - The Matronics Pulsar-List Email Forum - | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
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ghf4986(at)gmail.com Guest
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Posted: Tue Oct 13, 2020 7:38 am Post subject: "Beefing Up" |
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Dave,
If you can find your files, I would like to make a copy for my files. I may need it someday!
Dennis Adams
Sent from an IPad
On Oct 12, 2020, at 6:54 PM, David Weaver <mortweaver(at)sbcglobal.net> wrote:
I built a replacement nose wheel for a Pulsar XP after breaking the cast aluminum fork. It was a copy of the 4130 steel fork that Sky Star sold as an upgrade for Pulsar owners. After cutting out the parts and using a heavy vise secured to workbench. Bending of fork tangs was then completed. After TIG welding was finished, the fork was then professionally cleaned and powder coat finish applied. No special tools required. A saber saw was used to cut the flat steel parts out of steel sheet material ordered from Air Spruce. IF you are interested, I will look for the drawing I made that shows dimensions and material thickness.
Dave Weaver
Sent from my iPhone
Quote: | On Oct 12, 2020, at 1:57 PM, Yellowhammer <coyler(at)sthpk-12.net> wrote:
In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
I appreciate all the feedback on my "beefed up " questions.
So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
I wonder if I should convert it to a single seat because of how small the cockpit is?
I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
I am building away as hard and steady as I can.
Wont be long now.
Thanks,
Clyde
--------
J.M. Oyler "Clyde"
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=498772#498772
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esalehto(at)yahoo.com Guest
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Posted: Tue Oct 13, 2020 8:31 am Post subject: "Beefing Up" |
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Hi,
Dave. it might be good idea to archive your drawings to the Pulsar group files.
-Esa
On Tuesday, October 13, 2020, 10:48:22 AM CDT, Dennis Adams <ghf4986(at)gmail.com> wrote:
--> Pulsar-List message posted by: Dennis Adams <ghf4986(at)gmail.com (ghf4986(at)gmail.com)>
Dave,
If you can find your files, I would like to make a copy for my files. I may need it someday!
Dennis Adams
Sent from an IPad
On Oct 12, 2020, at 6:54 PM, David Weaver <mortweaver(at)sbcglobal.net (mortweaver(at)sbcglobal.net)> wrote:
--> Pulsar-List message posted by: David Weaver <mortweaver(at)sbcglobal.net (mortweaver(at)sbcglobal.net)>
I built a replacement nose wheel for a Pulsar XP after breaking the cast aluminum fork. It was a copy of the 4130 steel fork that Sky Star sold as an upgrade for Pulsar owners. After cutting out the parts and using a heavy vise secured to workbench. Bending of fork tangs was then completed. After TIG welding was finished, the fork was then professionally cleaned and powder coat finish applied. No special tools required. A saber saw was used to cut the flat steel parts out of steel sheet material ordered from Air Spruce. IF you are interested, I will look for the drawing I made that shows dimensions and material thickness.
Dave Weaver
Sent from my iPhone
Quote: | In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
|
Quote: | I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
|
Quote: | Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
|
Quote: | I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
|
Quote: | My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
|
Quote: | I appreciate all the feedback on my "beefed up " questions.
|
Quote: | So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
|
Quote: | I wonder if I should convert it to a single seat because of how small the cockpit is?
|
Quote: | I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
|
Quote: | Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
|
Quote: | I am building away as hard and steady as I can.
|
Quote: | J.M. Oyler "Clyde"
|
Quote: | Read this topic online here:
|
<= the many List utilities such as List Un/Subscription,
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MikeyC
Joined: 24 Jan 2017 Posts: 21 Location: 1GA0
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Posted: Tue Oct 13, 2020 9:59 am Post subject: "Beefing Up" |
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David Weaver & J M Oyler:If you can't locate the drawing David made, I have one I can send. I made my nosegear fork using it as a reference and in consultation with Chuck Stroh. It was quite an undertaking, but worth the effort - as I have confidence it will not fail under normal loads.
Good luck, MikeyC
On Tue, Oct 13, 2020 at 11:41 AM Dennis Adams <ghf4986(at)gmail.com (ghf4986(at)gmail.com)> wrote:
Quote: | --> Pulsar-List message posted by: Dennis Adams <ghf4986(at)gmail.com (ghf4986(at)gmail.com)>
Dave,
If you can find your files, I would like to make a copy for my files. I may need it someday!
Dennis Adams
Sent from an IPad
On Oct 12, 2020, at 6:54 PM, David Weaver <mortweaver(at)sbcglobal.net (mortweaver(at)sbcglobal.net)> wrote:
--> Pulsar-List message posted by: David Weaver <mortweaver(at)sbcglobal.net (mortweaver(at)sbcglobal.net)>
I built a replacement nose wheel for a Pulsar XP after breaking the cast aluminum fork. It was a copy of the 4130 steel fork that Sky Star sold as an upgrade for Pulsar owners. After cutting out the parts and using a heavy vise secured to workbench. Bending of fork tangs was then completed. After TIG welding was finished, the fork was then professionally cleaned and powder coat finish applied. No special tools required. A saber saw was used to cut the flat steel parts out of steel sheet material ordered from Air Spruce. IF you are interested, I will look for the drawing I made that shows dimensions and material thickness.
Dave Weaver
Sent from my iPhone
> On Oct 12, 2020, at 1:57 PM, Yellowhammer <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)> wrote:
>
> --> Pulsar-List message posted by: "Yellowhammer" <coyler(at)sthpk-12.net (coyler(at)sthpk-12.net)>
>
> In regards to the nose wheel fork and strut. I have had a few issues. I dry fitted the fork onto the strut and I could not get it off. Due to the brass sleeve that was press fitted into the fork.
>
> I had to heat it up to get it off and even then the brass sleeve stayed on the strut. I then had to grind the sleeve off. When I had everything together it was so tight I couldn't even move the nose wheel. I am going to get another sleeve to press fit in the fork hole.
>
> Also, The fork itself looks like it was very poorly cast. I have found small pitting many areas I am certain it will cause a stress fracture at some point.
>
> I am about to start looking for an alternative and will most likely end up taking it to my machine shop and have them make my another one.
>
> My fork is made of aluminum. I wonder if anyone switched theirs to a steel version along with drilling lightening holes.
>
> I appreciate all the feedback on my "beefed up " questions.
>
> So far, I have not done any thing extra in the way of strengthening my plane I am planning on doing a few things others have done and that have been proven wise.
>
> I wonder if I should convert it to a single seat because of how small the cockpit is?
>
> I am 6 'feet tall and weigh around 200 pounds and each time I sit in it I cant even imagine a passenger being comfortable.
>
> Anyway, thanks for the insight as it is much appreciated. I know I will have some more questions before long.
>
> I am building away as hard and steady as I can.
>
> Wont be long now.
>
> Thanks,
> Clyde
>
> --------
> J.M. Oyler "Clyde"
>
>
>
>
> Read this topic online here:
>
> http://forums.matronics.com/viewtopic.php?p=498772#498772
>
>
>
>
>
>
>
>
>
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