Blade insert connected in the lamination of a blade determining a double shear joint between insert and lamination. The insert is made up of two defined parts, head ( 2 ), designed to screw the insert to another structure ( 2′ ), and the body ( 3 ) that determines a cylindrical or conical shape with an internal conical cavity. In an embodiment, the insert is designed to be joined to the lamination ( 1 ) of the blade with adhesive means ( 4 ). In another embodiment, the insert is embedded in the blade lamination with an inner part ( 5 ) stuck to the body ( 3 ) of the insert.
1. A blade insert coupled in a solid lamination located in a top or bottom center part of the aerodynamic part of a blade, wherein:
the insert is made of a head ( 2 ), comprising a metal fitting head equipped with a through-hole that is not embedded in the lamination ( 1 ) designed to screw the insert to an identical insert on another structure ( 1 ′, 2 ′, 3 ′), and a body ( 3 ) for joining to the lamination ( 1 ) that determines a cylindrical or conical shape with an internal conical cavity, and
the joint between the insert and lamination ( 1 ) is carried out with an adhesive, chemical double sheathed joint ( 4 ), on the outer and/or inner surface of the insert's body ( 3 ).
2. The blade insert of claim 1 , wherein the body of the insert is embedded in the blade's ( 1 ) lamination and at least one inner part ( 5 ) is stuck to the inner part of the insert's body ( 3 ).
3. The blade insert of claim 2 , wherein the shape of the inner part ( 5 ) determines two sections, one conical ( 5 . 1 ), stuck with adhesive ( 4 ) to the surface of the insert body's conical inner cavity ( 3 ), and another cylindrical cavity ( 5 . 2 ) and chamfered.
4. The blade insert of claim 2 , wherein in the manufacturing of the inner part ( 5 ), fiberglass is used due to its rigidity and provides a high resistance joint between the laminate and the insert.
5. The blade insert of claim 2 , wherein in the manufacturing of the inner part ( 5 ), foam or wood is used due to its lightness and not very rigid material and provides a low resistance joint.
6. The blade insert of claim 1 , wherein the insert consists of a body ( 3 ) and a head ( 2 ) for screwing the insert to another structure ( 1 ′, 2 ′, 3 ′), including on said joint an auxiliary metal fitting ( 10 ) that determines at least one non-threaded through-hole ( 11 ) and at least one anchor bolt ( 9 , 9 ′) per structure to be joined.
7. The blade insert of claim 6 , wherein the anchor bolt ( 9 ) determines an inner anti-clockwise thread ( 13 ), an outer clockwise thread ( 14 ), and a fastening head ( 12 ) on the end of the bolt ( 9 ) around which a nut ( 15 ) is screwed.
8. The blade insert of claim 6 , wherein the nut ( 15 ) to screw onto the bolt ( 9 ) of the insert presents a clockwise thread.
9. A method for placing an insert inside a blade lamination, wherein the joint between the insert and the lamination ( 1 ), so that the insert is embedded, comprising:
using a mould ( 7 ) with a corrugated surface so that the lamination ( 1 ) adapts to the insert's cylindrically shaped body ( 3 );
laminating a series of composite material layers on said surface including fiberglass or carbon fiber;
placing the inserts, which the inner parts ( 5 ) have been previously stuck to, on the lamination ( 1 );
placing a plurality of separators ( 6 ) between the inserts; and
laminating additional composite layers on the inserts and separators ( 6 ).
10. The method for placing said insert inside said blade lamination according to claim 9 , wherein the preimpregnation lamination process is used, the material being previously impregnated with resin.
11. The method for placing the insert inside the blade lamination according to claim 9 , wherein the dry fabric lamination process is used, followed by a resin infusion.
12. A blade insert coupled in a solid lamination located in a top or bottom center part of the aerodynamic part of a blade, wherein:
the insert is made of a head ( 2 ), designed to screw the insert to another structure ( 1 ′, 2 ′, 3 ′), and a body ( 3 ) for joining to the lamination ( 1 ) that determines a cylindrical or conical shape with an internal conical cavity, and
the joint between the insert and lamination ( 1 ) is carried out with an adhesive, chemical double sheathed joint ( 4 ), on the outer and/or inner surface of the insert's body ( 3 ),
and wherein the insert is totally embedded in the lamination ( 1 ) consisting of a body ( 3 ) and a head ( 2 ) for screwing the insert to another structure ( 1 ′, 2 ′, 3 ′), including on said joint an auxiliary metal fitting ( 10 ) that determines at least one non-threaded through-hole ( 11 ) and at least one anchor bolt ( 9 , 9 ′) per structure to be joined.