Beam flange clamp, structural beam joint with beam flange clamps and method for forming a structural beam joint

Patent metadata

Field	Value
Publication number	US-9850931-B2
Application number	US-201514857298-A
Country	US
Kind code	B2
Filing date	Sep 17, 2015
Priority date	Sep 18, 2014
Publication date	Dec 26, 2017
Grant date	Dec 26, 2017

Abstract

A beam flange clamp includes a clamp body having a first vise jaw portion with a first gripping surface and a second vise jaw portion with a second gripping surface. The first gripping surface and the second gripping surface are oriented parallel to each other and are offset in height by a predetermined clamping distance. The clamp body further including a bolting portion protruding from the second vise jaw portion opposite of the first vise jaw portion, and at least one bolting hole is formed through the bolting portion.

First claim

The invention claimed is:

1. A structural beam joint, comprising:
a first structural beam comprising a web portion and at least one first flange portion;
a second structural beam comprising at least one second flange portion, wherein an axis of extension of the second structural beam is oriented at an angle relative to an axis of extension of the first structural beam, such that the first structural beam is oriented to intersect with the second structural beam;
at least one beam flange clamp comprising a clamp body having:
a first vise jaw portion with a first gripping surface;
a second vise jaw portion with a second gripping surface, wherein the first gripping surface and the second gripping surface are oriented parallel to each other and are offset in height by a predetermined clamping distance;
a bolting portion protruding from the second vise jaw portion, opposite the first vise jaw portion, and
at least one bolting hole formed through the bolting portion; and

at least one fastening pin or bolt inserted in the at least one bolting hole,
wherein the at least one first flange portion abuts the at least one second flange portion, and
wherein the at least one fastening pin or bolt is configured to tighten the clamp body to the web portion of the first structural beam, so that the clamp body sandwiches the at least one second flange portion between the at least one first flange portion and the first gripping surface of the clamp body.

2. The structural beam joint according to claim 1 , wherein the clamp body is substantially C-shaped, the first vise jaw portion and the second vise jaw portion forming respective legs of the C-shaped clamp body.

3. The structural beam joint according to claim 2 , wherein the clamp body is chamfered at at least one vertex of the C-shape and at a distal end of the first vise jaw portion.

4. The structural beam joint according to claim 1 , wherein a thickness of the bolting portion is smaller than a thickness of the second vise jaw portion.

5. The structural beam joint according to claim 1 , wherein the clamp body is integrally formed from one of a metal, a metal alloy and plastics.

6. The structural beam joint according to claim 1 , wherein the at least one fastening pin or bolt is configured to tighten the clamp body to the web portion of the first structural beam so that the first gripping surface presses the at least one second flange portion to the at least one first flange portion.

7. The structural beam joint according to claim 6 , wherein the first structural beam has an H-shaped cross-section, and wherein the second structural beam has an H-shaped or T-shaped cross-section.

8. The structural beam joint according to claim 6 , wherein the at least one beam flange clamp comprises four beam flange clamps,
wherein two of the four beam flange clamps clamp opposite sides of the second flange portion to respectively opposite sides of the web portion of the first structural beam.

9. The structural beam joint according to claim 6 , wherein the first structural beam has an H-shaped cross-section, or wherein the second structural beam has an H-shaped or T-shaped cross-section.

10. A method for forming a structural beam joint, the method comprising:
abutting a first flange portion of a first structural beam to a second flange portion of a second structural beam, the second structural beam having an axis of extension being angled with respect to the axis of extension of the first structural beam and intersecting with the first structural beam;
sandwiching the second flange portion between the first flange portion and a first gripping surface of a beam flange clamp, wherein the beam flange clamp comprises a clamp body having a first vise jaw portion, with the first gripping surface, and a second vise jaw portion, with a second gripping surface, the first gripping surface and the second gripping surface being oriented parallel to each other, and being offset in height by a predetermined clamping distance;
introducing a fastening pin or bolt in a bolting hole formed through a bolting portion protruding from the second vise jaw portion, opposite the first vise jaw portion, of the clamp body; and
tightening, using the fastening pin or bolt, the clamp body to the web portion of the first structural beam.

11. The method according to claim 10 , wherein the clamp body is substantially C-shaped, the first vise jaw portion and the second vise jaw portion forming respective legs of the C-shaped clamp body.

12. The method according to claim 10 , comprising:
repeating steps of sandwiching, introducing, and tightening for four beam flange clamps, wherein two of the four beam flange clamps clamp opposite sides of the second flange portion to respectively opposite sides of the web portion of the first structural beam.

13. An aircraft comprising:
a floor framework with interconnected structural beams, wherein the interconnected structural beams comprise a first structural beam, which comprises a web portion and at least one first flange portion, and a second structural beam, which comprises at least one second flange portion, and wherein the second structural beam has an axis of extension that is oriented at an angle relative to an axis of extension of the first structural beam, such that the second structural beam intersects with the first structural beam,
wherein the interconnected structural beams are interconnected with structural beam joints, each of the structural beam joints comprising:
at least one beam flange clamp comprising a clamp body, having:
a first vise jaw portion with a first gripping surface;
a second vise jaw portion with a second gripping surface, wherein the first gripping surface and the second gripping surface are oriented parallel to each other and are offset in height by a predetermined clamping distance;
a bolting portion protruding from the second vise jaw portion, opposite the first vise jaw portion, and
at least one bolting hole formed through the bolting portion; and

at least one fastening pin or bolt inserted in the at least one bolting hole,
wherein the at least one first flange portion abuts the at least one second flange portion, and
wherein the at least one fastening pin or bolt is configured to tighten the clamp body to the web portion of the first structural beam, so that the clamp body sandwiches the at least one second flange portion between the at least one first flange portion and the first dripping surface of the at least one beam flange.

Assignees

• Airbus Operations Gmbh

Inventors

• Westphal Stephan
• Richardson Busshoff Jan
• Rekert Christian
• Klotz Benjamin
• Roeschmann Marko
• Nalband-Abbasi Goulamhossein

Classifications

• F16B7/0493

  forming a crossed-over connection · CPC title

• B64C3/18

  Spars; Ribs; Stringers · CPC title

• F16B2/12 Primary

  using sliding jaws · CPC title

• F16B7/0486 Primary

  forming an abutting connection of at least one tube · CPC title

• B64C1/18

  Floors · CPC title