Method for producing a releasable seal with a sealing compound and use of adhesive strips for carrying out the method
Disclosed is a method for producing a releasable seal with a sealing compound between two fairing parts, in particular between two fairing parts for the wing-fuselage fillet of aircraft, including the steps of applying adhesive strips to respectively opposite edges, of the fairing parts and outer surfaces adjacent to them of the fairing parts; filling a sealing joint extending between the opposite edges with the sealing compound; and removing the adhesive strips after the curing of the sealing compound. This makes it possible to provide a re-releasable seal with a sealing compound which is curable or cures on its own in air between two fairing parts without the use of release agents. Also disclosed is the use of adhesive strips for carrying out this method.
1. A method for producing a releasable seal with a sealing compound between two fairing parts, the method comprising the steps of:
applying adhesive strips to respectively opposite facing edges of the fairing parts and outer surfaces adjacent to the opposite facing edges of the fairing parts,
filling a sealing joint extending between the opposite edges with the sealing compound and
removing the adhesive strips after the curing of the sealing compound, wherein the adhesive strips are pulled out from the sealing joint generally at right angles with respect to the outer surfaces of the fairing parts.
2. The method according to claim 1 , wherein the adhesive strips are firstly applied along the edges of the fairing parts and subsequently placed onto the outer surfaces of the fairing parts.
3. The method according to claim 1 , wherein the adhesive strips are respectively applied to the outer surfaces of the fairing parts on both sides in the region of the sealing joint in a width that corresponds to at least twice a material thickness of the fairing parts.
4. The method according to claim 1 , wherein the two fairing parts are fairing parts for the wing-fuselage fillet of aircraft.
5. The method according to claim 1 , wherein upper sides of the adhesive strips have anti-adhesive properties, in order largely to avoid the sealing compound sticking to the upper sides of the adhesive strips.
6. The method according to claim 1 , wherein the adhesive strips have a relatively low flexibility that permits bending while providing sufficient intrinsic stiffness so as to prevent the strips from being draped, said sufficient intrinsic stiffness facilitating pulling removal of said strips from said sealing joint without leaving any non-adhesive remnants of said strips.
7. The method according to claim 1 , wherein the adhesive strips have a low material thickness.
8. The method according to claim 7 , wherein the adhesive strips have a material thickness that is less than about 0.5 mm.
9. The method according to claim 1 , wherein the adhesive strips have a width of up to about 50 mm.
10. The method according to claim 1 , wherein the adhesive strips have a width of up to about 25 mm.