Fish joint device having an improved mechanical hold

Patent metadata

Field	Value
Publication number	US-9738373-B2
Application number	US-201213979939-A
Country	US
Kind code	B2
Filing date	Jan 17, 2012
Priority date	Jan 17, 2011
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

The invention relates to a fish joint device intended to attach securely first and second structural elements of an aircraft to one another, having two fishplates positioned either side of the structural elements, and attached to them by a set of fishplate through fastenings. According to the invention, the fish joint device includes at least one intermediate fish joint plate which is positioned between one of said fishplates and said structural elements which said intermediate plate partly covers, and which is attached to these elements by a set of intermediate plate through fastenings which includes the set of fishplate through fastenings.

First claim

The invention claimed is:

1. A fish joint device configured to securely attach first and second structural elements of an aircraft to one another, the fish joint device comprising:
a first fishplate disposed on either side of the first and second structural elements;
a second fishplate disposed on a side of the first and second structural elements opposite the first fishplate, the second fishplate including a first attachment branch, a second attachment branch, and a third attachment branch;
a set of through fastenings configured to attach the first and second fishplates to the first and second structural elements, the second fishplate being attached to the first and second structural elements by the first and second attachment branches, respectively, and to a third structural element by the third attachment branch; and
at least one intermediate fish joint plate disposed between and in contact with one of the first or second fishplates and the first and second structural elements, respectively, wherein the intermediate fish joint plate at least partly covers and is attached to the first and second structural elements by at least some of the through fastenings,
wherein the at least one intermediate fish joint plate has a flexural rigidity greater than the first or second fishplate located on a same side as the at least one intermediate fish joint plate, relative to the first and second structural elements, and
wherein the first and second fishplates and the at least one intermediate fish joint plate are configured to transmit forces experienced by the first and second structural elements into the first and second fishplates and the at least one intermediate fish joint plate.

2. The fish joint device according to claim 1 , wherein at least 50% of the through fastenings passing through the at least one intermediate fish joint plate also pass through the first or second fishplate on the same side of the first and second structural elements as the at least one intermediate fish joint plate.

3. The fish joint device according to claim 2 , wherein the through fastenings passing through the at least one intermediate fish joint plate are distributed in several rows which extend in parallel to a joining direction of the first and second structural elements, each of which has a same number of the through fastenings.

4. The fish joint device according to claim 1 , wherein each fishplate and each of the at least one intermediate fish joint plate is dimensioned and configured to transmit, between the first and second structural elements, a level of forces greater than or equal to 50% of a reference level equal to a quotient of a predefined maximum level of forces, divided by a number of fishplates and intermediate fish joint plate(s) of the fish joint device.

5. The fish joint device according to claim 1 , wherein the at least one intermediate fish joint plate comprises at least two intermediate fish joint plates, at least one second intermediate fish joint plate being disposed between the first or second fishplate and a first intermediate fish joint plate which is in contact with the first and second structural elements, the at least one second intermediate fish joint plate having a rigidity less than or equal to that of the first intermediate fish joint plate.

6. The fish joint device according to claim 1 , wherein the at least one intermediate fish joint plate comprises a local thickness of between 50% and 80% of a combined local thickness of the first or second fishplate and each of the at least one intermediate fish joint plate between the first or second fishplate and the first and second structural elements.

7. The fish joint device according to claim 6 , wherein the at least one intermediate fish joint plate in contact with the first and second structural elements has a local thickness strictly greater than a local thickness of the first or second fishplate.

8. The fish joint device according to claim 6 , wherein the first or second fishplate on a same side of the first and second structural elements as the at least one intermediate fish joint plate has a local thickness of between 20% and 50% of the combined local thickness of the first or second fishplate and each of the at least one intermediate fish joint plate.

9. The fish joint device according to claim 1 , wherein the first or second fishplates comprises a metal material, wherein another of the first or second fishplates comprises a metal material or a composite material, and wherein each of the at least one intermediate fish joint plate comprises a composite material.

10. An aircraft structure comprising an aircraft wing surface including a wing surface element, forming the first structural element, a fuselage box including a lower panel, forming the second structural element, and the fish joint device according to claim 1 to securely attach the wing surface element and the lower panel of the fuselage box.

11. The fish joint device according to claim 1 , wherein more than 66% of the through fastenings passing through the intermediate fish joint plates also pass through the first or second fishplate on a same side of the first and second structural elements as the at least one intermediate fish joint plate.

12. The fish joint device according to claim 1 , wherein more than 75% of the through fastenings passing through the intermediate fish joint plates also pass through the first or second fishplate on a same side of the first and second structural elements as the at least one intermediate fish joint plate.

13. The fish joint device according to claim 1 , wherein 100% of the through fastenings passing through the intermediate fish joint plates also pass through the first or second fishplate on a same side of the first and second structural elements as the at least one intermediate fish joint plate.

14. The fish joint device according to claim 1 , wherein each fishplate and each of the at least one intermediate fish joint plate is dimensioned and configured to transmit, between the first and second structural elements, a level of forces greater than or equal to 100% of a reference level equal to a quotient of a predefined maximum level of forces, divided by a number of fishplates and intermediate fish joint plate(s) of the fish joint device.

15. The fish joint device according to claim 1 , wherein each fishplate and each of the at least one intermediate fish joint plate is dimensioned and configured to transmit, between the first and second structural elements, a level of forces greater than or equal to 150% of a reference level equal to a quotient of a predefined maximum level of forces, divided by a number of fishplates and intermediate fish joint plate(s) of the fish joint device.

16. A method for fishplating first and second structural elements of an aircraft together, the method comprising:
providing a fish joint device comprising:
a first fishplate disposed on either side of the first and second structural elements;
a second fishplate disposed on a side of the first and second structural elements opposite the first fishplate, the second fishplate including a first attachment branch, a second attachment branch, and a third attachment branch;
a set of through fastenings configured to attach the first and second fishplates to the first and second structural elements, the second fishplate being attached to the first and second structural elements by the first and second attachment branches, respectively, and to a third structural element by the third attachment branch; and
at least one intermediate fish joint plate disposed between and in contact with o

Assignees

• Guillemaut Julien
• Gallant Guillaume
• Airbus Operations Sas

Inventors

• Guillemaut Julien
• Gallant Guillaume

Classifications

• Y10T403/74

  Cross-Sectional Technologies · mapped topic

• B64C1/26 Primary

  Attaching the wing or tail units or stabilising surfaces · CPC title

• F16B5/02

  by means of fastening members using screw-thread ({F16B5/0004 takes precedence}; construction of screw-threaded connections F16B25/00 - F16B39/00) · CPC title