Tool and method for inspecting the quality of assemblies of structural elements of aircraft

Patent metadata

Field	Value
Publication number	US-11053026-B2
Application number	US-201916251865-A
Country	US
Kind code	B2
Filing date	Jan 18, 2019
Priority date	Jan 30, 2018
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

A device and an inspection method for inspecting screw and nut assemblies in an aircraft, comprising a mechanical tool and a digital human-machine interface. The mechanical tool comprises a housing comprising a bearing surface defining a reference plane, a support beam mounted to be translationally mobile inside the housing, a linear encoder configured to measure, in use, a distance between the reference plane and a bottom face of the mobile support beam. The digital human-machine interface comprises a central unit, a display screen, an application and a database in which are stored validity ranges or standardized distances relating to types of assembly, the application and the database being loaded and operational in the central unit.

First claim

The invention claimed is:

1. A tool for inspecting a quality of assemblies of structural elements of an aircraft by means of fixing sets, each of which have a nut screwed onto a screw, the tool comprising a mechanical device and an electronic device connected to one another,
the mechanical device comprising:
a housing comprising a bearing surface defining a reference plane, said surface being configured to, in use, be pressed onto a contact face of a structural element of an assembly to be inspected against which the nut screwed onto the screw bears;
a support beam mounted to be translationally mobile inside the housing, said support beam comprising a bottom face configured to, in use, be pressed onto a free end of the screw;
a linear encoder configured to measure, in use, a distance between the reference plane and the bottom face of the mobile support beam;

the electronic device comprising:
a central unit having a database, a display screen and a human-machine interface,
the database comprising characteristics of each of a plurality of different assemblies of structural elements existing in the aircraft, characteristics of an assembly comprising at least dimensions and references of the screw and of the nut of the fixing set, a total thickness of the assembled structural elements and the dimensions and references of a washer inserted between the contact face and the nut in the case where the assembly contains such a washer, a first and a second value recommended for the screw-nut combination of the fixing set in the case where the fixing set does not comprise a washer,
and the first and the second value delimiting, respectively, a first and a second range of validity to which the measurement made on the assembly by means of the mechanical device must be compared to inspect the quality of said assembly, and

wherein the central unit is configured, in use, to execute a program for implementing a method for inspecting the quality of an assembly of structural elements from the measurement of the distance between the reference plane and the bottom face of the mobile support beam, the program invoking the database.

2. The tool according to claim 1 , wherein the electronic device is a touch tablet or a smart phone.

3. The tool according to claim 1 , further comprising a shell for receiving and protecting the electronic device, and straps fixed to the shell and configured to be placed around a forearm of an operator.

4. The tool according to claim 1 , wherein the mechanical device has a planar bottom face forming the bearing surface of the mechanical device.

5. The tool according to claim 1 , wherein the mechanical device comprises three feet each having a bottom end, the bottom ends of the three feet forming the bearing surface of the mechanical device.

6. A method for inspecting a quality of an assembly of structural elements of aircraft by means of a fixing set having a nut screwed onto a screw, said method being implemented by means of a tool according to claim 1 , comprising the following successive steps:
an identification step in which an operator identifies the assembly of structural elements that he wants to inspect and enters, via the human-machine interface, parameters relating to characteristics of the assembly;
a determination step, in which the central unit determines, as a function of the parameters entered by the operator and of data from the database, two values linked to the assembly identified in the preceding step;
a positioning step, in which the operator places the mechanical device in such a way as to grip the nut of the assembly, with the bearing surface of the mechanical device pressed against the contact face and the planar surface of the support beam pressed against the free end of the screw;
a measurement step, in which the linear encoder measures a distance between the bottom face of the support beam and the reference plane;
a first comparison step, in which the central unit compares the measurement with a first validity range delimited by a first value determined in the determination step;
a second comparison step, in which the central unit compares the measurement with a second validity range delimited by a second value determined in the determination step;
a step of determination of the quality of the assembly, in which the central unit determines that the quality of the assembly is correct if, cumulatively, the measurement lies within the first validity range and within the second validity range or, otherwise, that the quality of the assembly is incorrect if the measurement is outside of at least one of the two validity ranges.

7. The method according to claim 6 , wherein the central unit controls an activation of a visual or audible alarm when the inspected quality of the assembly is incorrect.

Assignees

• Airbus Operations Sas

Inventors

• Martres Jean-Luc

Classifications

• G01B5/061 Primary

  height gauges · 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

• B64F5/60 Primary

  Testing or inspecting aircraft components or systems · CPC title

• G01B5/02

  for measuring length, width or thickness (G01B5/004, G01B5/08 take precedence) · CPC title

• G01B5/0025

  Measuring of vehicle parts (G01B5/003 takes precedence) · CPC title