Author Topic: main spar of the Fw190 (Read 2837 times)

Crumpp · « **Reply #90 on:** February 09, 2006, 07:44:21 PM »

Quote

We do not weld anything that is structural in a spar. Thats why fasteners are used. Hell, about the only thing we ever weld are the original weld joints in specific original fairings joints and such. As for annealing a weld, like an engine mount (Steel), we gas weld the piece allowing it to self anneal in the process.

Are you working on any FW-190's?

Bodhi · « **Reply #91 on:** February 09, 2006, 08:39:27 PM »

Have in the past, doing American stuff now. A little bit ago, I did a feasibility study on a couple of projects (190's) that are not in the country for a buyer. Both airframes are fairly complete, newly found, with good history. You'll probably hear of them in a few months or so.

Crumpp · « **Reply #92 on:** February 09, 2006, 11:17:24 PM »

Well then you should know how the mainspar is constructed.

Bodhi · « **Reply #93 on:** February 10, 2006, 11:55:27 AM »

It is multiple pieces connected together to form a solid one piece spar that is not designed to come apart. Like I said from the beginning.