![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#26
|
|||
|
|||
![]()
I agree with Bob ... the numbers seem very low. However I have little doubt
that a production airplane will have less rivets than most homebuilts. In general homebuilt airplanes tend to be quite complex in their construction ... there are more bits in the firewall of an RV-6 than an entire C-150 fuselage (OK maybe a little exageration but not too far wrong). There are several reasons for this: (a) Designers of homebuilts don't have access to production tooling such as guerin presses to make firewalls in a single piece. Consequently they use more, simpler to make pieces, which need more rivets. (b) In general designers of homebuilt airplanes are not as focused on refining the product for production ... if you work for C, B or P etc then you need to design lean for production. You also have the facilities, budget and extensive test programs to help refine the design. The big companies in some cases design unconservatively and then beaf up the structure where it fails. Homebuilt designers in general design conservatively and cannot afford for a part to fail during test. (c) Few homebuilts are subject to extensive structural analysis and consequently the designers has no idea what the margins are re rivet shear and inter-rivet buckling etc so they have no choice but to stick to the typical minimum rivet spacings. I think it would be safe to say that you could not produce many homebuilts economically .. they are simply over built and their crudeness, whilst good for homebuilders is not suited for volume production .... the number of rivets is a huge cost driver WRT to cost of production since the labour in any airplane will be the most significant single cost in its production. That is why stir friction welding is being used in the Eclipse business jet. There are some exceptions to my generalisation re homebuilts being more complex that factory produced airplanes. The MM-I for example is an elegantly simple airplane with a minimum number of bits - but then Dave Long was a Piper design engineer. The T-18 is also a very simple airplane ... of course John Thorp also had a background in the design of airplanes for production. I think it all comes down to the designers background. "Bob K." wrote in message oups.com... Earlier, Brian Sponcil wrote: ...I recall the builders telling me that their RV kits have around 10,000 rivets. Compared to a Piper Comanche at 3,714 and a Warrior at 1,785 that's a heck of a lot of rivets. I've seen various RVs, Cherokees, and Comanches. I've kitted rivets for HP-series sailplane kits. And I just plain do not belive those numbers for the Warrior and Comanche. Not for relatively conventional riveted aluminum airplanes with few composite components and no metal-to-metal bonding. Until it's demonstrated otherwise, I propose that someone has cooked the books on this one to make for a good story. Consider the Warrior wing: Let's guess that the rib spacing is a relatively lean 12" OC. Let's guess that the rivet spacing is an equally lean 2". The span of the metal stuff (minus fiberglass tips) is probably about 32". Taking the fuselage out probably leaves room for at least 14 ribs on a side. The wing area of 170 ft^2 over the span of 35' yields an average chord of about 58". Since the skins are riveted top and bottom, I think that there are going to be about 58 rivets per wing rib. So that yields at least 58*30 skin-to-rib rivets, and that's 1740. Admittedly, that's a pretty rough estimate, and disregards the (probably negative) contribution of the flaps and ailerons to the rivet count. But it's a start. When you factor in the rivets between the spar and the skin, between the ribs and the spars, and for the many inspection panel rings, stringers, and other local additions, you see you can easily exceed the stated rivet count for the wings alone. And you've still got an entire fuselage and set of tail surfaces to go. And also the extremely close-pitched rivets around the baseball-stitched fuel tanks, and other miscellanea. I'll change my mind if, when I next see a warrior, I see fewer than 28 wing ribs or greater rivet spacing than 2". But until then, I'm not convinced. Thanks, and best regards to all Bob K. http://www.hpaircraft.com |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
"C-175 SoCal Beware" Original Poster Replies | Bill Berle | Home Built | 3 | July 8th 04 07:01 AM |
Poppers Revisted and the Return of the Teenie Two | Veeduber | Home Built | 0 | March 29th 04 09:57 AM |
Patching Baffling, 3/32 C-Sunk Rivets, 1100 Aluminum? | jls | Home Built | 3 | February 3rd 04 12:15 AM |
Bonded aluminum aircraft structures | asennad | Home Built | 9 | December 31st 03 02:58 PM |
Dimpling and riveting pressures | Max Krippler | Home Built | 5 | November 11th 03 08:03 PM |