IP Library Granted Patent US 8,245,467
Granted Patent B2
US 8,245,467 · App. 12/619,597 · Granted Aug 21, 2012

Apparatus and method for joining building components

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 8,245,467
App. No.
12/619,597
Granted
Aug 21, 2012
Kind
B2
Abstract

A joint apparatus and method of assembly is disclosed for connecting building components such as panels, door jamb assemblies, windows and other structures. The apparatus includes an engagement structure with retaining elements that couple building components without the need for mechanical fasteners. The retaining element may contain serrations on which an adhesive is applied before a panel or other building component is secured to the joint apparatus. Other building components such as hinge assemblies include coupling members with a flange. The slots along a retaining element allows coupling members to snap fit into the joint apparatus once a flange is secured into the slots in order to lock the components.

Claims (13)

1. A joining apparatus to strengthen coupling and engage with building components, the apparatus comprising:

at least one connector that includes a curved surface;

at least one building component that includes at least one insert structure;

at least one channel that includes at least one retaining element and configured to receive the at least one insert structure;

at least one engagement structure disposed in said at least one channel such that the building components are securable in the at least one channel without the use of additional mechanical fasteners;

at least one projection extending from the at least one connector;

a rub strip having a rub curved surface and at least one structural extension for fastening with the at least one projection such that the rub strip is snap-fit fastenable for quick installation and disassembly; wherein the rub strip is at least 30% circuitous, in contact with the curved surface and reinforced by the at least one retaining element to enhance the ability of the rub strip to withstanding direct impact.

2. The apparatus of claim 1 further comprising a first retaining element, and a second retaining element that are configured to engage with the at least one insert structure of the building components having a planar surface.

3. The apparatus of claim 2 wherein the at least one engagement structure includes the first retaining element and the second retaining element and wherein the at least one-channel includes a first channel and a second channel; and the first channel comprises the first retaining element, the second retaining element, and adhesive on the first retaining element that provides rigidity to allow the first channel to secure the insert structure without a requirement of any flange.

4. The apparatus of claim 3 wherein the at least one insert structure comprises at least one of hinge assemblies, latches, and stops.

5. The apparatus of claim 1 wherein the at least one insert structure comprises a first and a second insert structure; and wherein at least one of the first and the second insert structure includes a jamb element.

6. The apparatus of claim 1 further comprising a hinge assembly that includes a coupling member that fits into the at least one engagement structure to secure the hinge assembly to the joining apparatus.

7. The apparatus of claim 5 wherein the jamb element includes at least one of the following: a door stop, a hinge assembly, and a latch assembly.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 7, 2010
From: LEWIS, MICHAEL S.; BRANSCOME, BRYAN A.; HABERSETZER, DEAN W.; MCINELLY, CHRIS G.
To: BOEING COMPANY, THE
Reel/Frame 023770/0095 →
Continuity (2)
Division 11395580 · Mar 31, 2006
Related Publication 20100095624A1 · Apr 22, 2010