Inspection methods and systems for detecting leaks in vacuum bag assemblies

• US 9,976,926 B2
• Filed: 05/25/2016
• Issued: 05/22/2018
• Est. Priority Date: 05/28/2015
• Status: Active Grant

• Current Assignee: Airbus Operations SL (Airbus SE)
• Original Assignee: Airbus Operations SL (Airbus SE)
• Inventors: Galera Crdoba, Georgina, Prez Pastor, Augusto, Jordn Carnicero, Francisco Javier, Miguez Charines, Yolanda, Gordo Arias, ngel Pablo, lvarez Anton, Laura
• Primary Examiner(s): Macchiarolo, Peter
• Assistant Examiner(s): Fuentes, Anthony W Megna
• Application Number:
  US15/164,203
• Publication Number:
  US 20160349139A1
• Time in Patent Office: 727 Days
• Field of Search: 73 407, 73 493
• CPC Class Codes: B29C 70/44 using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
• CPC Class Codes: B29C 70/544 Details of vacuum bags, e.g. materials or shape
• CPC Class Codes: G01M 3/20 using special tracer materials, e.g. dye, fluorescent material, radioactive material
• CPC Class Codes: G01M 3/227 for flexible or elastic containers
• CPC Class Codes: G01M 3/229 removably mounted in a test cell

Abstract

Inspection methods and systems for detecting leaks in a vacuum bag assembly used in the manufacture of a composite part based on spraying helium over the vacuum bag and detecting the helium drawn by the vacuum inside the vacuum bag through a leak. The inspection methods comprise creating a local helium atmosphere in a chamber over the vacuum bag assembly by zones, following a programmed zonal sequence, for a first leak detection test of each zone and a subsequent second leak detection test if the first test gives a positive result. The inspection systems comprise a helium spraying system and helium detecting equipment arranged to implement the inspection methods.

Claims

1. An inspection method for detecting leaks in a vacuum bag assembly used in the manufacture of a composite part, the method comprising spraying helium over the surface of the vacuum bag and using helium detecting equipment to detect helium dragged by the vacuum inside the vacuum bag through a leak, comprising the steps of:

creating a local helium atmosphere over the vacuum bag assembly by zones following a programmed zonal sequence for a first leak detection test of each zone;

the local helium atmosphere being created inside a chamber placed over each zone;

the first leak detection test giving a positive result when the helium inside the vacuum bag detected by the helium detecting equipment exceeds a predetermined first threshold;

due to the first leak detection test giving a positive result in a particular zone, creating a new local helium atmosphere over the zone for a second leak detection test;

the second leak detection test giving a positive result when the helium inside the vacuum bag detected by the helium detecting equipment exceeds a predetermined second threshold.

2. An inspection method according to claim 1, wherein the creation of the local helium atmosphere and the new local helium atmosphere over the zone comprises a first step of helium injection and a second step of helium exposure, a duration time of helium injection and a duration time of helium exposure being control variables of the inspection method with different values for the first and second leak detection tests.

3. An inspection method according to claim 2, wherein inspection of the zone further comprises a third step of helium removal, a duration time of helium removal being a control variable of the inspection method with different values for the first and second leak detection tests.

4. An inspection method according to claim 1, wherein a beginning of the inspection of a new zone requires a waiting time after finishing the inspection of the previous zone, the waiting time being a control variable of the inspection method with different values for the first and second leak detection tests.

5. An inspection method according to claim 1, wherein:

the vacuum bag assembly comprises a cured panel, a plurality of uncured stiffening stringers, curing tools for the uncured stiffening stringers with fastening clamps and the vacuum bag arranged directly over the composite part;

the vacuum bag is formed by joining individual bags for the uncured stiffening stringers and other bag pieces to cover the whole panel;

the zones of the vacuum bag assembly to be covered by a plurality of chambers are set so that, in a direction of the stiffening stringers, the zones have a predetermined length and in a direction transverse to the stiffening stringers comprise, for each stringer, the space occupied by its individual bag, the sealing tape of two contiguous individual bags being assigned to the zone of one of the individual bags so that the sealing tape is covered by one chamber.

6. An inspection method according to claim 5, wherein the composite part is a cover of an aircraft wing.

7. An inspection system for detecting leaks in a vacuum bag assembly used in the manufacture of a composite part comprising:

a helium spraying system configured to spray helium over the vacuum bag assembly, and helium detecting equipment configured to detect helium drawn by a vacuum inside the vacuum bag through a leak, the helium spraying system comprising an apparatus configured to create a local helium atmosphere over individual zones of the vacuum bag assembly so that the helium detecting equipment detects the helium drawn by the vacuum in the zone through a leak;

the apparatus including a chamber configured to be positionable over the individual zones for housing the local helium atmosphere and a helium injection apparatus in the chamber;

the helium spraying system being configured to carry out the inspection of the vacuum bag assembly by zones following a programmed zonal sequence, wherein;

the vacuum bag assembly comprises a cured panel, a plurality of uncured stiffening stringers, curing tools for the uncured stiffening stringers with fastening clamps and a vacuum bag arranged directly over the composite part;

the vacuum bag being formed by joining individual bags for the uncured stiffening stringers and other bag pieces to cover an entire panel of the composite part;

the zones of the vacuum bag assembly to be covered by a plurality of chambers being set so that in a direction of the stiffening stringers the zones have a predetermined length and in a direction transverse to the stiffening stringers the zones comprise, for each stringer, a space occupied by the stringer'"'"'s individual bag, the sealing tape of two contiguous individual bags being assigned to the zone of one of the stringers so that the sealing tape is covered by one chamber.

8. The inspection system according to claim 7, wherein the helium spraying system comprises a portal configured and arranged to be displaced over the vacuum bag assembly in the direction of the stiffening stringers and a plurality of arms aligned with the stiffening stringers so that each arm positions a chamber over a zone of the vacuum bag assembly;

the arms having been connected to a helium bottle through pipes.

9. The inspection system according to claim 7, wherein the helium detecting equipment comprises a leak detector, regulated by a gas dosing valve, and two auxiliary pumps connected by hoses to a plurality of vacuum mold probes through hubs.