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Bob Kuykendall
Bob Kuykendall
Bob Kuykendall
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Mass balance bellcrank drive
0:13
7 лет назад
Horizontal upper skin
1:16
9 лет назад
HP-24 Flaperon Actuation
0:10
10 лет назад
100 4278
0:26
10 лет назад
HP-24 First Wing Join
0:15
10 лет назад
100_2814.MOV
0:26
13 лет назад
coupon2.02x.013.MOV
1:34
14 лет назад
coupon1.27x.013.MOV
0:45
14 лет назад
Push pull tube compression test
3:17
14 лет назад
RV-8 first takeoff
0:52
15 лет назад
VID00079
5:37
15 лет назад
VID00079
5:37
15 лет назад
VID00081
4:11
15 лет назад
VID00085
1:13
15 лет назад
VID00083
1:14
15 лет назад
Carabiner Strength Test
2:35
17 лет назад
Carabiner Gate Open Strength
1:16
17 лет назад
Комментарии
@johnlidstone5791
@johnlidstone5791 10 месяцев назад
Hi, what size rivets were they please? 3/16" ? Great video, straight to the point.
@kelvinmpatterson
@kelvinmpatterson Год назад
What about pulling from under angle
@ultimajp
@ultimajp 2 года назад
how is this project coming along ? Im curious how 5400 is acceptable. Would love more information on this project!!
@BobKuykendall
@BobKuykendall 2 года назад
We'll be flying the first set of wings at the Reno Air Races in September. There are regular updates on the Vans Air Force forums.
@ultimajp
@ultimajp 2 года назад
@@BobKuykendall Awesome I will be there. I look forward to meeting you all. I am the new owner of 577AZ the LS1 swapped RV7. Looking for every opportunity to make that thing stronger and lighter.
@davebrittain9216
@davebrittain9216 2 года назад
Good video! Pretty impressive the shear strength on them!
@cloudstreets1396
@cloudstreets1396 3 года назад
Automatic control hookups? Is this kit still being produced?
@BobKuykendall
@BobKuykendall 3 года назад
Yes, automatic connection for all controls. We still offer the HP-24, but are transitioning to the HP-26 which will only be available with electric sustainer or self-launch systems.
@cloudstreets1396
@cloudstreets1396 3 года назад
@@BobKuykendall - when will the HP-26 be available?
@BobKuykendall
@BobKuykendall 3 года назад
@@cloudstreets1396 Basically, when I get around to it.
@Dee-im7ug
@Dee-im7ug 3 года назад
Have you obtained any results with your camera settup?
@BobKuykendall
@BobKuykendall 3 года назад
Yes, indeed! The battery quit about three hours into a 4.5 hour flight, but we edited this montage from the footage: ru-vid.com/video/%D0%B2%D0%B8%D0%B4%D0%B5%D0%BE-vNWcQ8EcGKk.html. I just added the link to the description. Thanks for asking!
@GrantOakes
@GrantOakes 3 года назад
What was the laminate schedule? It looks like 1 layer of bidirectional CF cloth, a foam (Divinycell?) and another layer of bidirectional CF. What weight cloth and foam type and thickness was used?
@BobKuykendall
@BobKuykendall 3 года назад
It's about like most similarly-sized sailplanes.
@GrantOakes
@GrantOakes 3 года назад
@@BobKuykendall That doesn't answer my question. Is it a trade secrete? I'm curious if it's a 5.7oz or 8oz satin, twill or plain weave and what type of foam and thickness was used. The answers would be most helpful with my powered aircraft project.
@BobKuykendall
@BobKuykendall 3 года назад
@@GrantOakes It's not exactly secret, but I'd rather not get into specifics here. For your powered aircraft you'll almost certainly want a more robust lamination schedule based on sound engineering principles. There's a lot of great content on composite design on homebuiltairplanes.com, and many engineers on the forums with a far more comprehensive understanding than mine. I'd recommend starting here: www.homebuiltairplanes.com/forums/forums/composites.8/
@alfonzmuller294
@alfonzmuller294 4 года назад
what is your guess about 4140 solid rivets would they survive till 3k force or higher ?
@mahpts3211
@mahpts3211 4 года назад
شغل رائع من خبرة فذة
@pranavarora7933
@pranavarora7933 5 лет назад
And how do you put the two skins together?! Rivets? Glue?
@johnkerr99
@johnkerr99 5 лет назад
Great demo -- quick and to the point. Thank you!
@rashmiranjannayak3251
@rashmiranjannayak3251 5 лет назад
nice experiment, may I, know what is the thickness of carbon fiber there in experiment ?
@BobKuykendall
@BobKuykendall 5 лет назад
Sorry, that's proprietary. I can say that the cross-section is basically an I-beam, and that the spar caps are made of Graphlite pultruded strips. Get a copy of the Marske wing spar guide for details.
@antonioranaldi3455
@antonioranaldi3455 4 года назад
@@Lawiah0 you know the number?
@Bull761
@Bull761 4 года назад
@@BobKuykendall great product, and Marske makes the application simple. good job - why for an RV?
@hpaircraft2187
@hpaircraft2187 4 года назад
@@Bull761 RVs have a lot of potential for performance improvement from a laminar airfoil on a wing with more aspect ratio and a more effective spanwise lift distribution.
@Bull761
@Bull761 4 года назад
@@hpaircraft2187 I built an RV-4, still have it, great versatile aeroplane. For a high altitude special I can understand, for a sport/XC aircraft we already cruise so far above optimum Cl that the benefit would be small I think.
@danieljohnson327
@danieljohnson327 5 лет назад
cool
@522alien
@522alien 5 лет назад
can u make same experiment with the weld ?
@jaredbixenman7397
@jaredbixenman7397 6 лет назад
Great video, thanks for posting!
@antonioranaldi3455
@antonioranaldi3455 6 лет назад
you many layers​ of carbon fiber and what kind of resin?
@duby149
@duby149 6 лет назад
Wow I had no idea rivets was so strong, I was planning to use them to mount a computer monitor to my aluminum window frame but I was scared it wasn't going to be strong enough.
@thetribal697
@thetribal697 2 года назад
I build a gate out of rivets without welding.....riddle me that
@TeemarkConvair
@TeemarkConvair 6 лет назад
and did you see the "artifacting" alongside the epoxied mount? when in high speed it seems to show the surface actually changing. quite an interesting video. thanks
@BloomingtonFPV
@BloomingtonFPV 6 лет назад
Is the top side of this the top side of the eventual wing?
@BobKuykendall
@BobKuykendall 6 лет назад
The top side of this part is actually inside the wing. We do the same process for the upper wing skin, then install the wing spar and control system, then we glue this part on to close the wing.
@2Phast4Rocket
@2Phast4Rocket 6 лет назад
Wow, I hope you can take out some of the carbon and reduce the weight even more.
@BobKuykendall
@BobKuykendall 6 лет назад
The wing spar weight is already basically inconsequential. The entire internal structure of the wing is about 22 lbs.
@billtrue3017
@billtrue3017 6 лет назад
Sorfy just got near the end much better
@billtrue3017
@billtrue3017 6 лет назад
Why wet layup and not vacume bagging!
@BobKuykendall
@BobKuykendall 6 лет назад
It is vacuum bagged; the camera ran out of battery before we got it drawn down.
@BobKuykendall
@BobKuykendall 7 лет назад
We pointed the camera at the middle mounting point because what we were expecting was a shear failure of the bond between that Garolite mounting pad and the carbon fiber shear web. That bond turned out to be much more robust than we expected, and the actual failure turned out to be a shear rupture between the two inboard pads. And even that failure came at a substantially higher load than we'd expected according to handbook values for vacuum bagged carbon fiber.
@prash007more
@prash007more 7 лет назад
will you please mention the thickness of both the material you have used for test
@MatHelm
@MatHelm 6 лет назад
Prashant More You mistake their bragging for sharing..
@fire67bird
@fire67bird 7 лет назад
Thanks for sharing. I did a quick test of cheap hardware store pop rivets and it was ridiculously low.
@AdmiralUmptDumpt
@AdmiralUmptDumpt 8 лет назад
How is galvanic corrosion prevented between the carbon and the aluminum?
@cloudstreets1396
@cloudstreets1396 7 лет назад
Through the TLAR process, prior to molding, galvanic corrosion is completely prevented.
@BobKuykendall
@BobKuykendall 6 лет назад
There is no direct contact between any steel or aluminum parts and the carbon fiber. Anywhere they come close there is an insulating layer of fiberglass.
@TorontoDrivingVideos
@TorontoDrivingVideos 9 лет назад
Hi there can you tell me if you have any pics of your rig you made here? How much capacity is the load cell? Where did you buy the readout/loadcell? What are you using to pull? I can't see the top/puller arrangement in any of the videos. Thank you for you help. Watched all of them and enjoyed :)
@douglasanderson1276
@douglasanderson1276 7 лет назад
EBay all the way
@raulgonzalezcruz3862
@raulgonzalezcruz3862 9 лет назад
super !
@Rusiputki
@Rusiputki 10 лет назад
Rivets are very underrated.I use them pretty much all the time to hold pieces together. You can make anything with the help of L shape metal to connect joints.
@thenande
@thenande 10 лет назад
Hi, thanks for your test. Would stainless steel pop rivets be stronger than the tested rivets? Anyone else who knows please feel free to answer please, thanks a lot.
@sablatnic8030
@sablatnic8030 10 лет назад
Most impressive! And watch your fingers! ;-)
@thecrazynebraskan
@thecrazynebraskan 10 лет назад
What application is the push/pull tube used for? Also, I have another question.... I am a Drafting/Design student and I need to design a step stool. I want to use 3003 1/2" OD aluminum tube for the frame. The frame will be made up of two equal size/shape tubes, each will be bent 4 times to provide mounting areas for steps. The height of the top step will be 16", the bottom step is 8". The two steps themselves will be high density polyethylene plastic, bolted to the tubes. Do you think 3003 alloy 1/2" OD aluminum tube will suffice for my step stool? Any advice will help. Thanks!
@sanjeetkamboj2141
@sanjeetkamboj2141 10 лет назад
nice
@dberm22
@dberm22 12 лет назад
That sounded rude...didn't mean to be. Just saying that you shouldn't second guess your results.
@dberm22
@dberm22 12 лет назад
Just what i was looking for! Thanks!
@dberm22
@dberm22 12 лет назад
If you know anything about mechanics of materials, you would know that the failure makes sense. The cross sectional area around the hole seems to be roughly the same size as the total cross sectional area in the middle. Also, since the hole is there, small failures can be catastrophic to that area. Also, with the sudden drop in strength, that is quite common in almost all materials, but usually not THAT great of a drop. Great video, though! It definitely assures me on the strength of epoxy.
@sieczkadotcom
@sieczkadotcom 12 лет назад
I'm just trying to understand the physics here. Would a lead fall on a clove hitched sling, say if I put a carabiner at the end of the sling, break? I can easily exert 1200lbs when falling. I'm 200lbs x 9.8mp/s (close to 2000lbs). Is that right?
@petethewrist
@petethewrist 12 лет назад
Great i was surprised. now can you pleas do some high tensile nuts and bolts cheers Pete
@BobKuykendall
@BobKuykendall 13 лет назад
The PSI to pound force calculation _is_ dependent on the size of cylinder used. The force equals the effective piston area times the pressure.
@wb5mgr
@wb5mgr 13 лет назад
Is the psi to pound force calculation constant or it depends on the size cylinder you use.
@Crazylimes99
@Crazylimes99 13 лет назад
i didnt see anything happen....
@kodisilver
@kodisilver 14 лет назад
awesome
@BatmanProject777
@BatmanProject777 14 лет назад
Kind of funny to see these tests performed with high tech machinery, gear made by extremely thorough and professional companies, etc...then the read out is placed on a humble cardboard box. I'm not saying i trust these results any less, just a little odd ;)
@acrazedmaniac
@acrazedmaniac 14 лет назад
never, never, run webbing around bare cable!!! its called hot knifing. And , never put your fingers around a loaded webb or pins like you did! I have personally 'broke' over 200 test pulls like this, testing my stitch patterns and webbing strength. nice job showing stuff.
@dogdogee
@dogdogee 15 лет назад
so it is just round 5,5 kN that is really low :( nice to see one should use carabiners :)
@zihyer
@zihyer 15 лет назад
I second that idea... please more webbing, bolts, hangers, quicklinks, coldshuts, etc. Thanks for the vids!
@MetaView7
@MetaView7 15 лет назад
congratulations on your 1st flight
@BobKuykendall
@BobKuykendall 16 лет назад
RobNoone87, thanks for watching! The point of this test was to determine how climbing gear performs under unusual circumstances. Plenty of tests have shown how slings, chocks, and stoppers perform in "real situations;" it alomst invariably performs to its rated specification. The point of my tests were (and still are) to explore the sort of situations, no less real, that climbers occasionally must resort to under desperate circumstances. Thanks, Bob "BoKu" K.
@thebksfriend
@thebksfriend 16 лет назад
lol