Sliding connection between the floor structure and the hull structure of an aircraft

Patent metadata

Field	Value
Publication number	US-9764816-B2
Application number	US-201514724080-A
Country	US
Kind code	B2
Filing date	May 28, 2015
Priority date	May 30, 2014
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

Abstract

An aircraft structure part comprising a floor structure, a hull structure, and a connecting element. The connecting element comprises a rod attached, at its first end, to one of the hull and the floor; an attachment element, attached to the other of the hull and the floor, and provided with an opening in which the second end of the rod is slidably mounted; and an endstop attached to the rod so as to engage with the attachment element, to limit the sliding amplitude of the rod in the opening. When the connection between the floor and the hull is loaded in tension, the endstop makes it possible to comply with the standards for withstanding acceleration towards the aircraft front. When the connection is loaded in compression, the rod slides freely in the opening, which limits the constraints of withstanding compressive stresses, reducing the weight of the connecting element.

First claim

The invention claimed is:

1. An aircraft structure part comprising:
a floor structure portion,
a hull structure portion, and
a connecting element, wherein the connecting element comprises:
a rod having a longitudinal axis fixed, at a first end, relative to one of the hull structure portion and the floor structure portion;
an attachment element, attached to an other of the hull structure portion and the floor structure portion, and provided with an opening in which a second end of the rod is mounted such that the rod can slide within the attachment element along the longitudinal axis when the first end of the rod is fixed; and
an endstop element attached to the rod, arranged so as to engage with the attachment element when the hull structure portion tends to move away from the floor structure portion, so as to limit the sliding amplitude of the rod in the opening.

2. The structure part according to claim 1 , wherein the rod is attached, at its first end, to the hull structure portion, and wherein the attachment element is attached to the floor structure portion.

3. The structure part according to claim 2 , wherein the attachment element is attached to an external rail of the floor structure portion.

4. The structure part according to claim 2 , wherein the rod is attached to a frame and a skin of the hull structure portion.

5. The structure part according to claim 1 , wherein the endstop element is a nut screwed around the rod.

6. The structure part according to claim 1 , wherein the endstop element has a rectangular cross section, in a plane orthogonal to the longitudinal axis of the rod.

7. The structure part according to claim 1 , wherein the attachment element comprises a recess in which is created the opening and which receives the endstop element, the endstop element being guided in translation within the recess when the rod slides through the opening.

8. The structure part according to claim 7 , wherein the recess has an internal wall with a U-shaped cross section.

9. The structure part according to claim 7 , wherein a coating made of elastomeric material, attached to internal sidewalls of the recess or to external sidewalls of the endstop element.

10. The structure part according to claim 7 , wherein a coating made of elastomeric material extends in a plane orthogonal to the longitudinal axis of the rod, on an internal wall of the recess which surrounds the opening.

11. The structure part according to claim 1 , wherein the attachment element extends in its entirety between the first end of the rod and the endstop element.

12. The structure part according to claim 1 , wherein the rod is inserted, at its first end, into an opening created in an intermediate component attached to one among the hull structure portion and the floor structure portion, the rod being held secured to the intermediate component by two nuts positioned around the rod on either side of said opening in the intermediate component.

13. The structure part according to claim 1 , wherein the first end of the rod is pressed against the bottom of an indentation in an intermediate component, by a clip extending transversely to the rod, the clip being attached on either side of the rod to one of the hull structure portion and the floor structure portion.

14. The structure part according to claim 1 , wherein the first end of the rod is pressed against an internal face of an orifice created in an intermediate component, by a clip extending transversely to the rod, the clip being attached on just one side of the rod to one of the hull structure portion and the floor structure portion.

Assignees

• Airbus Operations Sas

Inventors

• Dazet Francis
• Antypas Jerome
• Bel Laurent
• Delorme Philippe
• Brisbart Raphael

Classifications

• B64C1/18

  Floors · CPC title

• C09J5/00

  Adhesive processes in general; Adhesive processes not provided for elsewhere, e.g. relating to primers · CPC title

• Y10T29/49623

  Static structure, e.g., a building component · CPC title

• B64C1/062 Primary

  specially adapted to absorb crash loads · CPC title

• B64C1/069 Primary

  Joining arrangements therefor · CPC title