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dfmoeller
Joined: 19 Jun 2006 Posts: 60 Location: Austin, TX
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Posted: Wed Feb 07, 2007 3:55 pm Post subject: A Few Questions for Scratchbuilders |
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Thank God for this forum!
I have two questions for the scratch-builders out there.
The First:
I am not clear on the meaning of one of the diagrams on the 601 XL rear wing
rib drawing 6W6. My question is this:
The detail diagram of the edge of the forming block on the spar side, says
to "file the top of the block 90 degrees to spar flange on 25 mm". A length
dimension of 214.9 mm is shown as the spar face length of the forming
blocks. The distance from X=0, Yu=147 to X=33.8, Yl=66.5 (as shown in the
curve point table) is 216.16 mm, implying that 1.2 to 1.3 mm should be
removed by the filing operation. Note: this is not the joggle, since the
joggle is clearly stated, in the blank forming diagram, to apply to both top
and bottom flanges. The filing is only done (per drawing) to the top
forming block edge.
Am I correct in executing the following steps in this order?
1. Sand edges of forming block to the curve table points.
2. Sand 1.2 mm off in the region shown perpendicular to the spar side edge
(should leave a spar side edge 214.9 mm long, but it leaves a flat top
surface far longer than 25 mm).
3. Apply 1/8" radius to forming block edge all around.
4. Sand 10 degree springback all around forming block (except rear channel
side which should be 13 degrees).
This will result in a forming block with a straight section abutting the
curve points.
The reason I'm being fussy about this 1.2 mm is that, this is exactly the
region in which the tolerance should be held to a mouse whisker.
Can some of you who've been through this step tell me if I'm interpreting
this correctly?
Second Issue:
The rear panel for the lockers is shown on the drawing as 498 mm length with
sides of 225 and 218 mm. What isn't shown clearly are the angles in which
these sides meet. I'm guessing that the top side is perpendicular to the
225 and 218 sides, but it could also be the case that this piece is cut
trapezoidally, or even the perpendicular side could be the bottom????.
Maybe I'm overlooking an obvious clue here; in case I am, please bear with
me.
Someone who has installed the lockers please clue me in on the correct way
to cut this piece.
I do appreciate the help in this forum!
Doug
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p.mulwitz(at)worldnet.att Guest
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Posted: Wed Feb 07, 2007 5:23 pm Post subject: A Few Questions for Scratchbuilders |
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The locker panel is almost rectangular, but actually a trapezoid
(almost?). This is because the wing tapers a little bit at that
point. I suggest you start with it cut as a rectangle and adjust the
few mm needed as you fit it in place. If you build it according to
the photo guide, the bottom skin will already be riveted in place,
and I suggest you fit the angle that meets the top skin before trying
to drill pilot holes in the rear panel.
One issue to watch here is the orientation of the flanges on the rear
ribs surrounding the locker. The drawings are a little vague
(wrong?) on this point. The proper way is to have the flanges on the
rear ribs on both sides of the locker facing away from the
locker. This gives you a smooth side wall on both the inboard and
outboard side of the locker. If you get this wrong, the rear panel
for the locker will need to be a considerably different size.
Good luck,
Paul
XL fuselage
At 03:52 PM 2/7/2007, you wrote:
Quote: | The rear panel for the lockers is shown on the drawing as 498 mm
length with sides of 225 and 218 mm. What isn't shown clearly are
the angles in which these sides meet. I'm guessing that the top
side is perpendicular to the 225 and 218 sides, but it could also be
the case that this piece is cut trapezoidally, or even the
perpendicular side could be the bottom????.
Maybe I'm overlooking an obvious clue here; in case I am, please bear with me.
Someone who has installed the lockers please clue me in on the
correct way to cut this piece.
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