IP Library › Granted Patent US 8,597,763
Granted Patent B2
US 8,597,763 · App. 12/726,042 · Granted Dec 3, 2013

Element for sealing or reinforcing a cavity and method for introducing a penetrating element into such an element

Inventors: Marco Lehmann (Zurich, CH); Nicolas Brichet (Zurich, CH); Marcel Meister (Hochfelden, CH); Michael Koller (Dottingen, CH)
Assignee: Sika Technology AG
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Quick Facts
Patent No.
US 8,597,763
App. No.
12/726,042
Granted
Dec 3, 2013
Kind
B2
Abstract

In the case of an element for sealing or reinforcing a cavity of a structural element, in particular of a vehicle, the element comprises a base element a foamable part, and an opening for receiving a penetrating element. A wing is arranged on the base element, the opening is open at the side and an actuator which moves the wing when the penetrating element is introduced is arranged on the wing.

Claims (30)

1. An element for sealing or reinforcing a cavity of a structural element, the element comprising:

a base element;

a wing movably connected to the base element to form an opening for receiving a penetrating element:

a foamable element comprised of a foaming agent and arranged on the base element and the wing; and

an actuator protrusion connected to the wing;

wherein the actuator protrusion moves the wing from an open position to a closed position when the penetrating element is inserted into the opening.

2. A reinforcing system including the element according to claim 1 , wherein the wing is movably connected to the base element by a hinge.

3. A reinforcing system including the element according to claim 1 , wherein the wing is held in a closed position by the actuator protrusion, and/or additionally arranged on the base element is a locking device for locking the wing in the closed position.

4. A reinforcing system including the element according to claim 1 , wherein the wing is configured to enclose more than half the circumference of the penetrating element.

5. A reinforcing system including the element according to claim 1 , wherein the foamable element consists of foamable material that covers the entire base element.

6. A reinforcing system including the element according to claim 1 , wherein the foamable element consists of foamable material that partially covers the base element.

7. The reinforcing system according to claim 5 , wherein the foamable material is foamed thermally at a temperature of ≦160° C.

8. The element according to claim 1 , wherein the foaming agent consists of a single-component epoxy resin system.

9. The element according to claim 1 , wherein the foaming agent consists of a single-component polyurethane composition.

10. The element according to claim 1 , wherein the foaming agent consists of a two-component epoxy resin and polyurethane composition.

11. A reinforcing system including the element according to claim 1 , wherein at least one of the base element, the wing, and the actuator is constructed from a plastic, a metal, or a combination of plastic and metal.

12. A reinforcing system including the element according to claim 1 , wherein the base element has a fastening means for placing and fastening the penetrating element in a cavity.

13. A reinforced cavity of a structural component in a body and/or a frame of an air, water or land transport vehicles comprising the element of claim 1 .

14. A method for introducing a penetrating element into an element for sealing or reinforcing a cavity of a structural element, the method comprising:

providing an element for sealing or reinforcing a cavity of a structural element comprising:

a base element,

a wing movably connected to the base element to form an opening for receiving the penetrating element:

a foamable element comprised of a foaming agent and arranged on the base element and the wing, and

an actuator protrusion connected to the wing;

introducing the penetrating element into the opening; and

pressing the penetrating element against the actuator protrusion;

wherein pressing the penetrating element against the actuator protrusion causes the wing to move from an open position to a closed position.

15. The method according to claim 14 , further comprising enclosing more than half the circumference of the penetrating element with the wing.

16. The method according to claim 14 , further comprising holding the wing in a closed position by the actuator protrusion.

17. The method according to claim 14 , comprising providing the penetrating element as a tubular element.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 26, 2010
From: LEHMANN, MARCO; BRICHET, NICOLAS; MEISTER, MARCEL; KOLLER, MICHAEL
To: SIKA TECHNOLOGY AG
Reel/Frame 024149/0533 →
Priority Claims (1)
EP 09157281 · Apr 3, 2009 · regional
Continuity (1)
Related Publication 20100253004A1 · Oct 7, 2010