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Charles'&Rick's UltraCruisers
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Hummel UltraCruiser
Plans # 527

S. Steve Adkins
EAA 9221

Technical Adviser: Dale Johnson
Technical Advice: Chris Bobka
Technical Counselor: Peter Denny

Created: 15 January 2009
Updated: 14 May 2010


Hoping my UltraCruiser will look this nice ... good head room!
Credits: Photo from Dan Johnson 
       
News Break:
Charles and Rick fly two new UltraCruisers:  http://cwsnyder2001.blogspot.com/ ...  Building Ends, Flying to Begin!
Steve Adkins (website author) completes wing panel: http://quid.us/hummel/final_riveting.html  ... (OK, my success pales in comparison)

Note:
I am reorganizing this website.  A "Navigation Matrix" table is immediately below.   Page down for about 50 construction image and use the navigation links for specific topics.
Eventually, nearly all the images below will be moved onto appropriate pages and be accessable via the Navigation Matrix.



Navigation Matrix
Data

Parts Finder Spreadsheet
- Sort by Sheet
- Sort by Assembly

Material Testing 

Changes Made 

Goofs and remedy 

Damaged UC 



Tools

Rivet Workstation
Video: 20 rivets in 4 minutes 
Rib Construction


Built-Up Rib Construction
Squeeze Riveting 
Nose Rib Support Fixture 

Wing construction

Spar
- Taper Pins

Vacuum Forming
-  My Nose Skins  
-  Charles Snyder - Horiz Stab
      Page down 2/3rds
      Video and still images
-   Charles - Video Only



Wing Panel Assembly
- Fixture Supports Nose Ribs 
- Bottom Skins 
- Wing Stand

Removing Dimples in Skin
- The problem  
- Tools  
- Removal Process  

Ailerons
-  Aileron Mock up  



Engines
Cordless Drill Starter ... why flip props?




Email Contact: [   ]

   S. Steve Adkins ...     

The original Hummel Bird was designed for a 5-foot, 7-inch pilot weighing 160 pounds.  

The UltraCruiser?  6 foot, 4 inches and 225 pounds.        

        


Parts Finder Spreadsheet
While on a month trip to So. California, I used spare time review the UltraCruiser plans.  During this time, I created a spreadsheet listing every part contained on the 19 sheets.

Summary:
-  There are about 660 parts
-  About 1/3 are unique or only two like parts
-  The rest are duplicate parts such as rib parts
WARNING: Do not rely on this list.  Use your Official drawings to determine the parts and correct materials required to build your aircraft.

Website Editorial Policy & Copyright Notice
These pages are presented here are for the use, education and enjoyment of those interested in homebuilding.   No claim is made for the accuracy of materials presented. Content and/or policy opinions expressed within these pages are solely those of the author. They DO NOT necessarily reflect the position of any other person nor organization. Responsibility for accuracy in referred and hyperlinked materials rests entirely with the applicable author and no remuneration is made.
Copyright © 2008, by S. Steve Adkins, all rights reserved. 
Links to Spreadsheet
- Sort by Sheet
- Sort by Assembly



... Left-click on most photos for full-size and more-complete image ...

                                                  


Click on Photo for larger and complete photo
New webpage has been created:


Progress: 7 July 2009
Skins were formed using vacuum technique described by Charles Snyder.  
Page down for photos and movie.  
Charles suggests using a 2-inch pipe.  I used 1-7/8ths inch plastic drain pipe from my scrap pile.  
I will add a webpage showing my process.  Vacuum forming was the easiest and most satisfying task so far.
See my vacuum forming process.

Also, be sure to visit my webpage: Nose Rib Support Fixture which solves a pesky problem.




Progress: 22 June 2009
I delayed riveting the second upper skin until the D-Cell is complete.

Larger Image:   med   large


 

Status: 2/15/2009 - Outer Wing Panel - 5 ribs complete, 2 to go


  

Current Status: 2-19-2009 all ribs in place except for one nose rib
(Viewers with sharp eyes will notice that one rib is a formed rib and not a truss built-up rib.)
This rib is what you get from Hummel Aviation ... isn't it a beauty!  Notice the largest lightening hole is "squared" at the bottom front..
I purchased this rib for comparison and review with EAA Chapter 25.  
I have been building using very precise hole location ... as a result, I was able to correctly mount the rib as their pre-drilled holes matched with mine!




    

Height from table: Adkins Truss Built-Up Rib on left and Hummel Aviation Formed Rib on the right
(Tilt of spar on table adds 1/16 inch measurement which should be 9 and 22/32nds or 11/16ths)




I will be starting a spreadsheet with the actual
weight of parts as they are built.
To date:
Nose rib and mid rib =  6 ounces
(and they transfer 100 pounds of lift to the spar at 4.5 Gs)
Spar with fittings   =  6 pounds approximate (no bolts yet)
Lightening holes in spar web saved = 7.4 ounces both spars


Jim T. , Yahoo! Groups Sponsor reports:
A truss-built rib (nose and mid rib) at 5.94 ounces, or 8.395lbs for a set

Mike, Hummel Aviation, reports a set of formed rib at  9 pounds, 2 ounces
So the updated truss ribs are about 13 ounces lighter than the laser-cut formed ribs.

100 Years of progress
My first two ribs: UltraCruiser and 1903 Wright Flyer
(The Wright Flyer was funded by the State of Minnesota)

Better view of the rib with flanging die
Circle hole flanging die "turned" by Dale Johnson 
Modified nose rib per suggestion by
Peter Denny (Sonex builder).
 
Bill Batzloff also came to the same conclusion.
An additional change was made to the rivet pattern ... see below.

Built-up Nose Rib for the WWII Spitfire!

These two photos are from the March 2008
issue of Air & Space 

Note: For comparison, I have included photos of a built-up rib for the WWII Spitfire shown in the March 2008 issue of Air & Space magazine.   Compare the Spitfire photos to the photos below.

y
Spitfire Mid-Rib and wing structure
If formed ribs are so great, why aren't they used here? I know why.
(By the way, I understand that Hummel makes a great set of formed ribs.)

     Back Issues/Reprint Policy 


Rivet Station ... rivet squeezer clamped in vice
Note: see below for a new holding fixture.  

Reaching a difficult rivet
Rail section holds angle brace while allowing total freedom for placement

Improved squeeze rivet work station ... shown with nose rib.
Two tubes hold the squeezer vs. clamping in the vise.
This allows rotation of the squeezer.  
The left or right tube is selected
based on required
space for your hand during the squeeze operation.
Note: Mounting board is from a busted Ice Boat plank.
Huge aircraft bolt replaces railroad track.

Squeeze rivet work station - close view
Vice, squeezer, yoke and support angle can all be positioned to reach
difficult locations while ensuring that the squeezer is perpendicular.
Here the change to the rivet pattern can be seen.  The
lower flange is made longer to allow the rivets to be longitudinal
rather than perpendicular.  Also, the formed piece has a 
simplified corner at the lower and upper -rear corners
allowing for a straight cut with your tin snips.

Squeezer shown with a mid-rib

A "no space" plans desk ... workbench to the right (not shown).
Fast and inexpensive to build ... light weight, easy to move.

Insert sides filed flat for tight riveting ...
Note: if the squeezer inserts lean against
the assembly,
 the rivet will be driven crooked (bad) and may split (worse) .
(both top insert and bottom insert have flat sides cut and polished)

.020 aluminum sheet (4x8 foot) ready for cutting ... no that isn't a mirror


Cutting guide is clamped (not absolutely necessary)

Inexpensive cutter ... make 20 strokes, bend and brake off piece./

As the groove gets deep enough, the cutting stroke makes a different sound.

Spar web, cap and fittings ... temporary assembly.
Note: Basement assembly workshop. Hopefully, I'll
lose 20 pounds running up and down stairs between
the basement workshop and the garage.


Note:

The wing shown here is the right-outer wing panel.

The total wing consists of a center section and two outer wing panels.

Each outer panel is a little about 9 feet.

The center section is a little about 7 feet.

Total wings span is 25 feet.

End view of fittings
Fittings machined by Dale Johnson

Three-quarter view of end fittings
End Polishing, more hole drilling and deburring remain to be done

Top view of first trial assembly mating rib to spar.

Photo by Dan Johnson



Review of wing assembly
Note: circle-hole flanging dies "turned" by Dale Johnson.

Too much effort vs. using a flanging hand tool?
(Not when some one else volunteers to make them!)

Front view ... note ribs for 1903 Wright Flyer on wall above
100 years and a significant change in technology!



 Take a look at Mr. Fujita's wing with formed ribs:
also
 His complete gallery at the Hummel website:

Edge view ... note spar web vertical stiffeners

Another edge view


3M polishing wheel ... source Avery Tools (SKU 3753)
.... 6" 3M SCOTCH-BRITE DEBURRING WHEEL
Available from several aviation suppliers.
This is the wheel recommended for RV builders.

Photo on left show the grove created to smooth edges on aluminum
This is totally SUPERIOR  to any other method of deburring an edge.


More on this later ... see preliminary discussion to the right ----->

<------ Hole drilling guide or Index Bar                                                  


I have tried a number of methods to create an accurate hole guide.

In matched hole tooling, it doesn't matter if the guide is imperfect
.... as long as it is placed correctly on matching parts.
But, I wanted a guide that was perfect so that it can be flipped and flopped and still drill a matching pattern.

In my scrap pile, I discovered an aluminum bar bought at a Control Data employee sale
over 30 years ago.  Aluminum was being sold at scrap prices.  This bar is from a super computer chassis.  It is straight, relatively thick and had accurately drilled holes at  one-half inch intervals.  The holes were tapped for 6-32 machine screws.  These threads nicely capture the silver or the small Cleco which fits a #41 or 3/32nd drill bit.

The holes are #35 drill in size.  I have drilled out every over hole and inserted
brass tubing which is then press fitted by pounding an awl into the tubing
followed by pounding on the end of the tube with an 1/8 inch drift punch.  This produces a hole that fits the smaller #41 drill for 3/32nd rivets.  I may drill out the other holes to fit a #31 drill.

Work bench, plans table, shelving and tool stands.  
Table saw and compound cross-cut saw under work bench.

Small belt sander to the left, bench drill press  (center left) and band saw (far right)
Shelving holds drill accessories, battery chargers, hand drill stand, misc tools.

I hope to buy a house with a three-car garage and walkout basement workshop.
You haven't built an airplane until the project has been moved at least once!
More coming ..............................

Log:
Site Updated : January 16, 2009
Primary effort has been purchase of aviation metal-working tools and changing basement and garage shops over to metal working shops.  Also, investigating material sources and purchasing enough material to build one wing panel; and, as you can see below building one wing panel.  Also, considerable effort building jigs for the nose-rib and mid-rib.  A form block and drilling guide was made for the formed nose piece (yes, the built-up ribs have a formed piece).  Several hole drilling guides have been built.  Much effort here and many discards (you know the drill).

Last entry made early 2008:
Bought plans and some tools during December.  Started building January 2008.  
Have built one full rib (nose and mid rib) using the built-up design ... total weight = 6 ounces

February 2009
Built second spar web.  Five ribs are finished, two to go ... then I start skining the wing panel.  Charles Snyder also recommends completing the total spar web at this time working on a flat table with bend that matches the dihedral and the drill press mounted at work table height.

See photo: Wing Spar Drilling Jig  from the Charle's and Rick's UltraCruiser Blog
 Photo: Dan Johnson  



Address of this Webpage:   http://quid.us/hummel/
Copyright © 2008, by S. Steve Adkins, all rights reserved. 

Disclaimer: Website Editorial Policy & Copyright Notice
These pages are presented here are for the use, education and enjoyment of those interested in the world aircraft homebuilding.   No claim is made for the accuracy of materials presented. Content and/or policy opinions expressed within these pages are solely those of the author. They DO NOT necessarily reflect the position of any other person nor organization. Responsibility for accuracy in referred and hyperlinked materials rests entirely with the applicable author and no remuneration is made.