Method of brazing honeycomb and panel assemblies

Details Method of brazing honeycomb and panel assemblies Method of brazing honeycomb and panel assemblies

B - Operations, Transporting

23

K

113/83

B23K 31/02 (2006.01)

Patent

CA 1167326

METHOD OF BRAZING HONEYCOMB AND PANEL ASSEMBLIES ABSTRACT OF THE DISCLOSURE . Rather than spray coat face sheets of honeycomb panels. with powder braze alloy or using foil strips of braze alloy between honey- comb core and face sheets, individual ribbon segment of brazing foil are positioned between succesive honeycomb cell vertices or nodes. The arrangement is such that several such ribbon segments will lie essentially in parallel plants, to each other and normal to the planes of the top and bottom panel sheets when these panel sheets are positioned to sandwich the honeycomb cells therebetween. Heat can then be applied to melt the ribbon . segments resulting in a flow of the brazing material-into the ' nodes as well as the contact line joints made between the top and '' bottom of the cell walls with the top and bottom panel sheets. ,' Excess brazing material on the panel surfaces covering the open cell portions free of joints is thereby virtually eliminated and desirable ductility and elongation characteristics of the resulting structure are retained.

399928

Affiliated with

Also associated with

Rating

Method of brazing honeycomb and panel assemblies does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of brazing honeycomb and panel assemblies, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of brazing honeycomb and panel assemblies will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1313718