Ultralight Airplane Workshop
Ultralight Airplane Workshop
  • Видео 173
  • Просмотров 517 244
Aluminum Flange Setter Tool
There is a way to set a 90 degree flange in an aluminum sheet part and get it almost perfect every time without guessing. Use a Flange Setter tool. Let's make and use one in this video.
Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders""
www.ultralightairplaneworkshop.com/design-copy
Links:
RUclips Channel: ruclips.net/channel/UCuC7MVr2bBUQ-9xQbg0v82Q
Patreon: www.patreon.com/ultralight_airplane_workshop
Discord: discord.gg/eTd9ruZpFj
Twitter: Designer1032
Website: www.UltralightAirplaneWorkshop.com
FAA AC 103-7: www.faa.gov/documentLibrary/media/Advisory_Circular/AC_103-7.pdf
Disclaimer: If you use any of the information ...
Просмотров: 2 057

Видео

Whipple Tree Analysis and Fabrication
Просмотров 9014 месяца назад
For testing the Truss Style Nose Rib for the UWS-4 Ultralight airplane, a Whipple Tree is to be used. A Whipple Tree spreads a single load into multiple individual loads. The design of the Whipple Tree allows the individual loads to be customized for the item being load tested. This video covers the analysis to design a Whipple Tree and then the fabrication of a Whipple Tree. Link to the Ultral...
Truss Nose Rib Test: Part C
Просмотров 5334 месяца назад
In this video of a design for a truss style nose rib for the UWS-4, the rib is formed with hydroforming using rubber. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/channel/UCuC7MVr2bBUQ-9xQbg0v82Q Patreon: www.patreon.com/ultralight_airplane_wo...
Truss Nose Rib Test: Part B
Просмотров 3914 месяца назад
It is time to get out into the shop and start making sawdust and aluminum chips for the aluminum truss style nose rib of the UWS-4. In this video the template for cutting out the rib is fabricated and then the aluminum rib is cut out. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy...
UWS-4 Aero Design: Forward CG, Part 13b
Просмотров 4195 месяцев назад
In this video we switch from the most aft CG to the most forward CG to determine the tail size for the UWS-4 Ultralight Airplane. Which ever is biggest wins. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/channel/UCuC7MVr2bBUQ-9xQbg0v82Q Patreon...
UWS-4 Aero Design: Pitch Stability, Part 13 a
Просмотров 4146 месяцев назад
In this video we will take a look at the Pitch Stability of the UWS-4 Ultralight Airplane. This is the next section in the book we are using to aid in the design of the UWS-4, "Simplified Aircraft Design for Homebuilders". Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUcl...
Truss Nose Rib Test: Part A
Просмотров 6087 месяцев назад
Since we did some testing on a cantilever style nose rib, lets try a truss style nose rib. In this video the design of the truss style nose rib for an ultralight airplane is discussed. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/channel/UCuC7...
UWS-4 Aero Design: Weight and CG Estimation, Part 12 C
Просмотров 4647 месяцев назад
In this video the estimated position of the the Center of Gravity (CG) of the UWS-4 Ultralight Airplane is estimated using the software tool OpenVSP. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/channel/UCuC7MVr2bBUQ-9xQbg0v82Q Patreon: www.pa...
UWS-4 Aero Design: Weight Estimation Part 12 B
Просмотров 3517 месяцев назад
With Part B if the little video series on the UWS-4 Ultralight Weight Estimation we modify the Aero Commander weight estimation rules for aluminum airplanes in order to more accurately estimate aluminum ultralight weights. We then get the first estimate of the empty weight of the UWS-4. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuil...
UWS-4 Aero Design: Weight Estimation Part 12 A
Просмотров 4757 месяцев назад
We are now at the point in Dan Raymer's book "Simplified Aircraft Design for Homebuilders" book that we can make the first estimate of the weight of the UWS-4 Ultralight Airplane. In this case will choose to use some equations for the weight estimation of the wing, horizontal tail and vertical tail. In this video we will take a look at these equations to try to understand them because we will m...
UWS-4 Aero Design: Revision Part 2
Просмотров 6967 месяцев назад
This is the continuation of the UWS-4 Ultralight Airplane revision that was started in Part 1. In this Part 2 I'll talk about changes to the wing planform and airfoil and possible enhancements to the fuselage changes discussed in Part 1. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-c...
Cantilever Rib Portion Test: Part C
Просмотров 5798 месяцев назад
Since we've done some testing for parts of a cantilever nose rib, it is time to test a full cantilever nose rib. Can this rib handle the 3.8g load of 75 lbs and then the extra 1.5 load factor? Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/chann...
UWS-4 Aero Design: Revision Part 1
Просмотров 1,8 тыс.9 месяцев назад
After a lot of consideration and an informative trip to Oshkosh, it was time to make some aerodynamic design changes to the UWS-4 ultralight airplane. In part 1 we talk about changes to the landing gear, tail and cockpit area of the ultralight. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/d...
Airventure 2023 Highlights
Просмотров 37110 месяцев назад
Here is a video of the Ultralight Airplane Workshop version of a visit to Airventure 2023, Oshkosh, WI. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.net/channel/UCuC7MVr2bBUQ-9xQbg0v82Q Patreon: www.patreon.com/ultralight_airplane_workshop Discord...
Tour of Camp Scholller, Airventure 2023, Oshkosh WI
Просмотров 2,6 тыс.10 месяцев назад
If you have never visited Camp Scholler at Airventure then you may not have a good idea of how big it is and how many people camp there during the week of Airventure. Here is a tour of Camp Scholler. Link to the Ultralight Airplane Workshop's books web page, including "Simplified Aircraft Design for Homebuilders"" www.ultralightairplaneworkshop.com/design-copy Links: RUclips Channel: ruclips.ne...
Road trip to Airventure 2023, Oshkosh, WI.
Просмотров 8810 месяцев назад
Road trip to Airventure 2023, Oshkosh, WI.
Cantilever Rib Portion Testing: Part B
Просмотров 1 тыс.Год назад
Cantilever Rib Portion Testing: Part B
Can an AI design an Ultralight Airplane?
Просмотров 1,2 тыс.Год назад
Can an AI design an Ultralight Airplane?
X-plane 12: Airfoil Maker
Просмотров 2,5 тыс.Год назад
X-plane 12: Airfoil Maker
UWS-4: Touch Panel, Part 3
Просмотров 254Год назад
UWS-4: Touch Panel, Part 3
UWS-4: Instrument Panel Thoughts, Part2
Просмотров 188Год назад
UWS-4: Instrument Panel Thoughts, Part2
UWS-4: Instrument Display, Part 1
Просмотров 418Год назад
UWS-4: Instrument Display, Part 1
From Selig Airfoil to Rib Template
Просмотров 895Год назад
From Selig Airfoil to Rib Template
Does an Ultralight Airplane need a parachute?
Просмотров 1,5 тыс.Год назад
Does an Ultralight Airplane need a parachute?
Cantilever Rib Portion Testing: Part A
Просмотров 948Год назад
Cantilever Rib Portion Testing: Part A
UWS-4 Struct Design: Rib Skin Rivet Locations , Part 2a
Просмотров 913Год назад
UWS-4 Struct Design: Rib Skin Rivet Locations , Part 2a
Wing Skin/Flat Panel Compression Limit
Просмотров 2,4 тыс.Год назад
Wing Skin/Flat Panel Compression Limit
UWS-4 Struct Design: Ribs Part 1, Ultra Cruiser Ribs
Просмотров 3,2 тыс.Год назад
UWS-4 Struct Design: Ribs Part 1, Ultra Cruiser Ribs
Aluminum Wing Skin/Rib Rivet Load Test
Просмотров 2,8 тыс.Год назад
Aluminum Wing Skin/Rib Rivet Load Test
UWS-4 Aero Design: Part 11d, Wing Chordwise Lift Distribution (V1.1)
Просмотров 1,7 тыс.Год назад
UWS-4 Aero Design: Part 11d, Wing Chordwise Lift Distribution (V1.1)

Комментарии

  • @LightAndSportyGuy
    @LightAndSportyGuy День назад

    Thank you!!!!!

  • @margaritamednikova3931
    @margaritamednikova3931 День назад

    Thank you for these videos very much!

  • @toxaq
    @toxaq 6 дней назад

    If you cut a hole in the base plate under the 'R' you could have a bar run down to a foot pedal. With a little extra geometry, that could also power the compression for the bend. Much like a shrinker/stretcher in automotive body work.

  • @JeffCurtisIflyHG
    @JeffCurtisIflyHG 7 дней назад

    So, given how much time you have spent forming this style rib, do you think this is still faster than building the rib similar to multipart Ultracruiser rib?

  • @JeffCurtisIflyHG
    @JeffCurtisIflyHG 7 дней назад

    I'm loving your content, I'm interested in developing an ultralight myself. I want to replace a wood and fabric wing design with aluminum and fabric. Have you read "Sheet Metal Building Basics" from the EAA store? If not you should, lots of great information well presented. In this video you mentioned using 1/8" rivets through 0.016" skin. This is too large a rivet for the skin thickness. Chapter 19.4 states that the rivet diameter to thickness ratio should be no greater than 5.5, otherwise the expanding rivet will locally distort and buckle the sheet. For 0.016" sheet the largest diameter rivet that can be used is 1/16". See Table 2 on page 19-4. I have not been able to find 1/16" pull rivets so it will be necessary to use solid rivets. One other comment. A downside of starting with a large sheet, bending it, and cutting out lightening holes is that it results in the most scrap so it adds considerable cost (the need to buy more raw material for the same end result). While I agree that the 5 piece nose requires making more parts and using more rivets to assemble them, the parts start as straight rectangles that then get bent into shape so there is much less scrap from the raw materials. If solid rivets are used they are cheaper, lighter, and stronger than pulled rivets, but they do require different tools and learning the techniques to install them. If your ultralight is going to be primarily aluminum then the one time cost of the tools will be small compared to the number of rivet you will need to set so using solid rivets where ever possible will ultimately cost less, be stronger, and weigh less.

  • @MalfiWing
    @MalfiWing 7 дней назад

    Very cool! Thank you for sharing this. My experience with hydro-forming is that, yes, different thicknesses will definitely have different springback angles. For a given alloy and heat-treat, thinner metal is springier and needs to be over-bent more, while thicker metal is less springy and will come closer to just staying where you bent it. This makes sense if you think about it; When you bend something thick, the stresses that you put on the outer and inner surfaces are much higher (i.e. more yielding will happen) than when you bent something thin, if you think of it in terms of "beam height". Anyways... I'm a huge fan (currently also developing my own ultralight), please keep up the great work!

    • @MalfiWing
      @MalfiWing 7 дней назад

      Oh, and: The bend radius will also impact the springback. Again, think about stresses in beam-bending: A sharper radius will cause higher stresses and more yielding (so, less springback) than a wider radius (which would therefore need to be over-bent more).

  • @tanyawingfield9981
    @tanyawingfield9981 8 дней назад

    I wonder if you stuck something like a ring sizing mandrel on the outside or " feeder" side, it would take a flat slat and begin the curve on a consistent basis.

  • @jonnupe1645
    @jonnupe1645 9 дней назад

    Thank you

  • @jonnupe1645
    @jonnupe1645 9 дней назад

    Thank you

  • @pulsarspacetime
    @pulsarspacetime 11 дней назад

    Thank you for all work and dedication. Highly appreciated !!

  • @TukaihaHithlec
    @TukaihaHithlec 26 дней назад

    7:29 I’m noticing that the laminar airfoil also appears to reverse its curves near the trailing edge so that the reuniting streams have a closer angle once they rejoin, probably inducing lower drag, perhaps similar to the effect winglets have.

  • @ghostflight73
    @ghostflight73 Месяц назад

    Usually fly in and camp with plane, this year driving our "other rv" and have a decent solar set up, think we can live without air. I know the generators just scream, even in the just till 10PM areas, so thinking of our 32' rv parking in no genie area? Thoughts, think that would be a mistake? Sure would enjoy not hearing genies, thoughts?

    • @kenwilkerson1043
      @kenwilkerson1043 4 часа назад

      We're driving our 22' class B. It has 300W solar and an under-hood generator. We're planning on parking in the non-genny area. I don't know what's gonna be left when we get there on Thursday the 25th.

  • @StephenAnderson-db5gd
    @StephenAnderson-db5gd Месяц назад

    Unnecessary part's and labor.

  • @pavangc4881
    @pavangc4881 Месяц назад

    what are the design considerations required to design horizontal stabilizer in helicopter

  • @mckenziekeith7434
    @mckenziekeith7434 Месяц назад

    You could have used bondo instead of drywall once you had the fiberglass over the foam. (I think bondo will attack bare foam).

  • @mckenziekeith7434
    @mckenziekeith7434 Месяц назад

    For anyone watching, amine blush is water soluble. Use ample water and a mild abrasive (like a scotchbrite scrubbing pad) to remove it before sanding. Don't use alcohol or acetone or other solvents.

  • @perrycorn2789
    @perrycorn2789 Месяц назад

    When you talk about maintenance these 2 stroke engines can fail very easy and also you may have a new engine but there could be a flaw with the metal use in the engine and it fails . I have seen ultralight aircraft were the wing brackets had big scratches in the corners I fixed it and the brackets that hold the rudder peddles on had 3/16 pop rivets in 1/4 holes and it was loose had to fix that and a few other things . Been an engineer if you have to do maintenance have a full check list record the maintenance and always every few month contact the manafacture or some that has the same plane and ask of any problems they have come across . And the way I see it I’m going to build an ultralight and I’m putting a parachute so there is the protection should something go wrong

  • @TomHail
    @TomHail Месяц назад

    I take it this video was taken the Sunday before the start of the airshow, right? People are coming in looking for spots, first come, first served on that Sunday?

  • @flyingcatto404
    @flyingcatto404 2 месяца назад

    hi. by any chance, do you have forum or group for ultralight design maybe on discord or something? thanks in advance

  • @JeffCurtisIflyHG
    @JeffCurtisIflyHG 2 месяца назад

    Given then number of changes you want to make/have made, are you going to build a 2nd model or re-build the first model to verify the changes or just assume they will be good?

  • @samanthasaysmoon11
    @samanthasaysmoon11 2 месяца назад

    this rocks! i didnt know you could use safety wire for this purpose

  • @davidav8orpflanz561
    @davidav8orpflanz561 2 месяца назад

    Add a turnbuckle to the tension cable or easier adjustments, and relieving tension for storage.

  • @davidwebb4904
    @davidwebb4904 2 месяца назад

    As you have intent to paint, instead, in your glass smooth mould, paint two layers of gelcoat in your desired color, then a 90gsm cloth, then two 200gsm, then a core with built in flow channels, then two layers of 200gsm.

  • @rhemaislife
    @rhemaislife 2 месяца назад

    Thanks a lot man

  • @BorisCopeland
    @BorisCopeland 3 месяца назад

    Great job but can you explain permitted and not permitted

  • @abdbot2509
    @abdbot2509 3 месяца назад

    Excellent job, congratulations

  • @RA-gk5zg
    @RA-gk5zg 3 месяца назад

    I love your videos. Can you do a tutorial on XFLR5? I can't get that single CL vs Alpha plot to show and see the coordinates in the upper right corner.

  • @JasonDoan-yv3gm
    @JasonDoan-yv3gm 3 месяца назад

    Great work sir!

  • @cratersofthemoon
    @cratersofthemoon 4 месяца назад

    Boeing isn’t good enough to fly WO parachute! What make you special? Great show!

  • @iforce2d
    @iforce2d 4 месяца назад

    Again my comments keep disappearing, might be in your 'flagged for review' section.

  • @anthonyrstrawbridge
    @anthonyrstrawbridge 4 месяца назад

    Excellent work 👍🏻

  • @lemonyellow3117
    @lemonyellow3117 4 месяца назад

    I paid way too much for butyl tape on Amazon only to have it come alive while reinstalling the windows on my camper shell. What a mess I made. Now I plan to use it for vacuum bagging a surfboard so your video is very informative. I’m interested in using pvc pipe for sealing edges. I like that there are people like yourself who make videos of their whacky projects. Thanks man!

  • @darrellmartin2234
    @darrellmartin2234 4 месяца назад

    You missed a great part of the ultralight flying in the mornings with all the ragwings in the air

  • @niio111
    @niio111 4 месяца назад

    Great info. Moving the reference point for aggregate moment along the wing seems harder than just adding each lift x arm for each station outboard of the calculation point.

  • @alexgustavsson5955
    @alexgustavsson5955 4 месяца назад

    Awesome video, can't wait for the load testing!

  • @pawlowskidog
    @pawlowskidog 4 месяца назад

    Carbon fiber will solve a lot of problems

  • @mmanzoor8667
    @mmanzoor8667 4 месяца назад

    Toooooo much pounds pounds pounds … not basics knowledge!

  • @Sivart4323
    @Sivart4323 4 месяца назад

    Why not just use the nichrome wire from the space heater you got the power cord from? Is there a benefit in using stainless wire I’m missing?

  • @raj61091
    @raj61091 4 месяца назад

    you deserve more views, excellent subject matter

  • @raj61091
    @raj61091 4 месяца назад

    Thankyou

  • @philipmorgan5050
    @philipmorgan5050 5 месяцев назад

    Too complicated for my dumbass, but you have a lot of smarts and I enjoyed.

  • @martinlitorell3834
    @martinlitorell3834 5 месяцев назад

    Dynamometer+ long spring would be good

  • @pedrosequeira4871
    @pedrosequeira4871 5 месяцев назад

    Your channel is awesome! I have been following your design process for a while and I am loving it. I am trying to follow this video but I can't seem to find JBlade anywhere, do you know if it's been deleted?

  • @bradhopper1108
    @bradhopper1108 5 месяцев назад

    Loved the vided, but one production suggestion, turn down your mic gain - you are overloading your preamp and distorting the audio a lot. Hard to listen to it.

  • @kenbradley5035
    @kenbradley5035 5 месяцев назад

    A lot of this video could be cut out to just one video also where is the comparison with the aluminium sheet which is the reason for me watching.

  • @hans-PeterSchneider
    @hans-PeterSchneider 5 месяцев назад

    Interesting video. If you intend to replace aluminum sheet metal you may have sufficient thickness of sandwich to eliminate some of the bulkheads including rivets. This gives you some reserve if you simply compare the sheets.

  • @trupinion512
    @trupinion512 5 месяцев назад

    You are a friggin'' genius! It is one thing to understand fluid dynamics but to explain it to a moron like me so I can understand it a rare talent. I am surprised you aren't teaching at Embry Riddle.

  • @gary24752
    @gary24752 5 месяцев назад

    What I have questions are how to make the power supply.

  • @nadeemkhouri4054
    @nadeemkhouri4054 6 месяцев назад

    How is the dynamic pressure lower on the top of the wing if the speed of the wind is higher up there

    • @Designer103
      @Designer103 6 месяцев назад

      Higher airspeed is lower pressure. It is Bernoulli's principle.

  • @petersantner2625
    @petersantner2625 6 месяцев назад

    Hi! i dont quite get how the geometry of an elyptical Wing functions. Specificale the "Edges" confuse me. Dos the Airfoil Linerely narrow down or does it just get ajusted to the resulting chordline?? And how would you support that structure? i guess you could bend Tube at the leading edge, but what would you use at the trailing edge? can you maybe use a tube as well and ignore the resulting radius at the end? Alos how does the tip narrow down and how would you build it?? I'd be very gratefull for an explaination!

    • @Designer103
      @Designer103 6 месяцев назад

      The elliptical geometry depends mostly on the chord. The chord of the wing has an elliptical distribution along the span of the wing. The leading edge or trailing edge can be straight or curved although at least on of them will be curved. Or you can approximate an elliptical profile with multiple trapezoids. You do not have to take the elliptical planform all the way to the tips. Even some of the later Spitfire airplanes had the tip trimmed off in order to make manufacturing a little easier. The tips do not provide enough lift to make much difference.