CraffsjDaos-Coroer DRAG/ANTI-DRAG WIRE ALIGNMENT AND DRILLING GUIDE By Chuck Larsrn, EAA Designee Dim-tor Photos by Marian Cavadias, KAA Staff Photographer
Bauken Noack of the EAA Aviation Foundation Shop staff fabricated this ingenious device to align and drill the mounting and passage holes for the drag/ anti-drag wires in aircraft wings. This particular one was made to drill the holes on Aero Sport and Aero II aircraft, but the dimensions can be changed to suit
nearly any project. The device consists of four parts. A 6 foot length of 7/8" O.D. square (round won't work) tubing and 3 "stands" for marking and drilling the holes. Each stand consists of a 7/8" I.D. square tubing mount with a locking device, a 4" mast and a head through which the pivot or drill bit extends. By extending the mast to 6 or more inches, the device could accommodate most current wing designs.
Photo "A" — The complete alignment and drilling tool.
Photo A illustrates the completed guide tool. The
pivot points shown on the outer masts are bolts ground
Photo "B" — Drilling the mounting holes in a wing for an Aero II.
to a point to be used in marking and holding the device while drilling. A fork with an appropriate size "nut" attachment can be screwed onto the bolt when one end of the drag/anti-drag wires are mounted on an existing interior mounting plate. Photo B illustrates drilling the mounting holes in a wing for an Aero II. You will note the stand at the far end of the picture is placed in the position in which that hole will be drilled while the hole is drilled in the position shown in the foreground. The device will then be turned around for drilling of the other mounting hole. An angle drill is illustrated in this photo, but, as you can see, a standard drill would work as well in this application.
Photo C shows the drilling of holes through the compression ribs by placing the t h i r d mast in the center and the outer mast in the previously drilled mounting holes. This makes it possible to drill a small diameter, perfectly aligned hole for the drag/anti-drag wire as it passes through that rib. This device allows for a very high degree of accuracy in accomplishing this delicate procedure which can safely offer very little leeway in its accuracy. Bauken's answer for accurately completing this procedure, which is required on nearly every airplane, will help builders to produce a higher level of craftsmanship in their project. This tool is one every Chapter or group of builders should add to their inventory. Photo "C" — Drilling holes through a compression rib. 12 NOVEMBER 1982
Satellite Infrared. Internet Access via Cirrus. Satellite Visual ... across the airplane spectrum and may be particularly applicable to homebuilt airplanes that don't ...
Jan 22, 1997 - tance of designing for low drag, and the ability to estimate drag, can hardly be ... projected configuration size and cost, and thus on the decision to ...... 5-11, comparing the drag on a modern airfoil to that of a single wire.
Engine cooling is a popular topic in homebuilt circles. ... More total flow translates into more drag on the airframe. In other words .... the engine and oil cooler.
Jan 22, 1997 - The subject of drag didn't arise in our use of panel methods to examine ... accurately with high confidence levels3 (especially for unusual ... Fluid Mechanics: This viewpoint emphasizes the drag resulting from ...... bial zero thickne
on Jim Frost's Stits Playboy, and the wing rack arrangement shown in the picture of L. R. Eaves' Cougar. (SA 2-59 page 14). If you have any questions regard-.
Jan 22, 1997 - Here we illustrate the problem by defining drag from several viewpoints. .... as the X-29 minimize this penalty by defining a device schedule to ...... The fuselage mid-section cross-sectional area had been reduced ...... Stuart, Willi
maneuvering affect stall speed but not the stall AOA. Using a landing pattern ex- ample, we compared the stall protection of an AOA-based fi- nal approach with ...
flight. However, why pay the full price when you can get a discount. Let's look into this idea a bit .... assembly of some parts. ... A poor job of rigging could saddle.
of wing systems at subsonic speed are reported. Recent theoretical and ..... Drag, NASA Technical Paper 3598, Ames Research Center. [3]. Spreiter J.R., Sacks ...
silicone stopped all leakage. The concept of .... built to be a drop-in replacement for the silicone baffle seal material. ... Plenum Top: plug, mold and finished part.
Jun 10, 2005 - total bulk momentum transfer charges plus host in this case is found to be ... This same approach has been used previously 2,3 in treatments of ...
INTRODUCTION. Now that ... cargo or passenger craft, is not practi- cal for the ..... berances, air leaks, gaps, grooves or steps in the ... course reduce. At any rate ...
INTRODUCTION. Now that ... cargo or passenger craft, is not practi- cal for the ..... berances, air leaks, gaps, grooves or steps in the ... course reduce. At any rate ...
of some photographs of the air flow round wings and propellers. These pictures were taken in a wind tunnel at Cambridge University*, and the streamlines were ...
thrust he can afford to purchase and the total drag of the product of his labors. .... tury English to make it fit a Lycoming engine. At the ..... prevention measures may be pretty elementary. As speeds ..... Standard equipment on the new Model.
Blue Drag http://www.youtube.com/user/AladinChorizo. Music by Fletcher Allen. As arranged & performed by AladinChorizo n= A o= E p= C q= G h = 100. 441. &.
Reducing Induced Drag...A French Approach. By G. Limbach, EAA 6911. 56 E. Oaks Rd., St. Paul, Minn. WHILE MY French is not good enough to translate ...
Jan 22, 1997 - The best success has been achieved for air- foils, and even ... Drag: An Introduction 5 - 3 ...... It is known as LAMDES, and the user's manual.Missing:
Mutopia-2004/10/21-465. This music is part of the Mutopia project: http://www.MutopiaProject.org/. It has been typeset and placed in the public domain by Daniel ...