Device positioning two aircraft pieces relative to one another, such as a crossbeam and a fuselage frame

Patent metadata

Field	Value
Publication number	US-10053234-B2
Application number	US-201514637770-A
Country	US
Kind code	B2
Filing date	Mar 4, 2015
Priority date	Mar 7, 2014
Publication date	Aug 21, 2018
Grant date	Aug 21, 2018

Abstract

A device for positioning a first piece relative to a second piece. The first piece comprises a free end with a first bore and the second piece comprises an engagement part with a second bore intended to come into correspondence with the first bore. The first and second bore are drilled to the definitive diameter thereof prior to the relative positioning thereof. The device comprises one or more positioning elements, which are able to position the first bore relative to the second bore along at least one of three geometric axes.

First claim

The invention claimed is:

1. An assembly comprising:
a first aircraft piece,
a second aircraft piece,
a device for positioning the first piece relative to the second piece,
the first piece comprising a free end provided with at least one first bore that is pre-drilled to a predetermined and definitive diameter, and
the second piece comprising an engagement part provided with at least one second bore intended to come into correspondence with said at least one first bore, said at least one second bore is pre-drilled to a predetermined and definitive diameter,
the device comprising at least one mechanical positioning element serving as a geometric reference in the event of a relative displacement of said at least one first and second bores to position said at least one first bore relative to said at least one second bore along at least one of a first, a second and a third geometric axis, wherein the first geometric axis is parallel to an axis of said at least first and second bores,
wherein the at least one positioning element comprises an element for centering the first piece relative to the second piece along the first axis;
wherein the centering element is arranged vertically offset in relation to the second bore and laterally aligned with the second bore;
wherein the centering element is a shoe, wherein an upper portion of the shoe forms a wedge in the vertical direction, wherein the shoe extends in the vertical direction with the upper portion of the shoe forming the wedge and an enlarged lower portion.

2. The assembly according to claim 1 , wherein said at least one positioning element is connected to one of the first and second pieces.

3. The assembly according to claim 1 , wherein said at least one positioning element is not arranged inside said at least one first and second bores.

4. The assembly according to claim 1 , wherein the centering element is arranged above the engagement part of the second piece.

5. The assembly according to claim 1 , wherein the centering element is arranged below the engagement part of the second piece.

6. The assembly according to claim 1 , wherein said assembly comprises a tool for positioning the first piece relative to the second piece.

7. The assembly according to claim 6 , wherein the positioning tool comprises first gripping members, which are able to be locked on one of the pieces, and second gripping members, which are able to be locked on the other piece, said first gripping members being displaceable relative to said second gripping members along said at least one geometric axis.

8. The assembly according to claim 7 , wherein the tool comprises a head provided with the first and second gripping members, the tool being configured to drive a movement of said first gripping members relative to said second gripping members along said at least one geometric axis.

9. The assembly according to claim 1 , wherein said at least one positioning element comprises a plurality of elements serving as geometric references arranged on the first piece and on the second piece and which are configured to be aligned with one another along at least one of the second geometric axis and the third geometric axis.

10. The assembly according to claim 1 , wherein said at least one positioning element comprises a plurality of elements serving as geometric references arranged on the first piece and on the second piece and which are configured to be aligned with one another along at least one of the second geometric axis and the third geometric axis and wherein at least one tool is able to bring the geometric reference or references of one piece in alignment with the geometric reference or references of the other piece along at least one of the second geometric axis and the third geometric axis.

11. The assembly according to claim 1 , wherein the first and the third geometric axis are arranged in a horizontal plane, and the second geometric axis is a vertical axis.

12. The assembly according to claim 1 , wherein the first piece is a crossbeam and the second piece is a frame.

13. The assembly according to claim 12 , wherein the crossbeam is configured to be fixed at two diametrically opposed points of the inner periphery of the frame by means of the two opposite ends of said crossbeam, of which one is the free, as yet unfixed end of the crossbeam and the other is the opposite end already fixed at a point of the frame.

14. The assembly according to claim 13 , further comprising a tool configured to compress the frame and which is able to exert a compressive force on the frame so as to bring toward one another the two diametrically opposed points of the inner periphery of the frame.

15. The assembly according to claim 12 , wherein the free end of the crossbeam comprises a clevis aligned in the longitudinal axis of the crossbeam, and the engagement part forms a tenon arranged on the inner periphery of the frame.

16. An assembly comprising:
a first aircraft piece,
a second aircraft piece,
a device for positioning the first piece relative to the second piece,
the first piece comprising a free end provided with at least one first bore that is pre-drilled to a predetermined and definitive diameter, and
the second piece comprising an engagement part provided with at least one second bore intended to come into correspondence with said at least one first bore, said at least one second bore is pre-drilled to a predetermined and definitive diameter,
the device comprising at least one mechanical positioning element serving as a geometric reference in the event of a relative displacement of said at least one first and second bores to position said at least one first bore relative to said at least one second bore along at least one of a first, a second and a third geometric axis, wherein the mechanical positioning element is a shoe, wherein an upper portion of the shoe forms a wedge in the vertical direction, wherein the shoe extends in the vertical direction with the upper portion of the shoe forming the wedge and an enlarged lower portion;
at least one active member arranged on one piece,
at least one passive member arranged on the other piece and which is able to cooperate with said at least one active member by transmission and reception of electromagnetic waves, wherein said at least one active member and said at least one passive member are located in said at least one first bore and said at least one second bore,
a closed-loop control system configured to control the electromagnetic waves transmitted and the displacement of at least one piece relative to the other depending on the waves received by said at least one passive member so as to bring said at least one active and passive member into geometric correspondence.

17. The assembly according to claim 16 , wherein the positioning device comprises a plurality of elements serving as geometric references arranged on the first piece and on the second piece and which are configured to be aligned with one another along at least one of the first geometric axis, the second geometric axis and the third geometric axis.

18. An aircraft comprising at least one assembly comprising:
a first aircraft piece,
a second aircraft piece,
a device for positioning the first piece relative to the second piece,
the first piece comprising a free end provided with at least one first bore that is pre-drilled to a predetermined and definitive diameter, and
the second piece comprising an engagement part provided with at least one second bore intended to come into correspondence with said at least one first bore,

Assignees

• Airbus Operations Sas
• Airbus Operations Sas

Inventors

• Durnad Yves
• Guering Bernard

Classifications

• B64C1/061

  Frames · CPC title

• B64F5/0009 Primary

  Operations & Transport · mapped topic

• B64C1/18

  Floors · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• Y10T29/49622

  Vehicular structural member making · CPC title