Methods and systems for bonding

Patent metadata

Field	Value
Publication number	US-10245792-B2
Application number	US-201615568337-A
Country	US
Kind code	B2
Filing date	Apr 26, 2016
Priority date	Apr 29, 2015
Publication date	Apr 2, 2019
Grant date	Apr 2, 2019

Abstract

Methods and apparatus are described for improving fit checking at the bonding interface of a first component, such as a fan blade (1), and a second component, such as an edge guard (2) for the fan blade (1), to be bonded by adhesive. A bondline thickness profile over the area of the bonding interface is determined by interposing a compressible, flexible sensor layer between the components before they are bonded. The sensor layer contains an array of piezoelectric elements which indicate local bondline thickness by signalling pressure due to compression of the layer. The bondline thickness profile can be processed by a programmed control processor to produce an adhesive application schedule prescribing the shapes of pieces of adhesive film which, when applied over the bonding interface, will build up an adhesive layer corresponding in thickness to the bondline thickness. The sensor layer can be prepared as a kit of shaped panels or as a contoured preform (55) matching the form of the bonding interface.

First claim

The invention claimed is:

1. A bonding method for joining first and second components by adhesive bonding at a bonding interface defined by respective complementary bonding faces of the first and second components, the method comprising a pre-bonding fit check in which the components are arranged in an intended bonding position to check the closeness of fit between them over the bonding interface, and wherein the fit check comprises:
bringing the components together in the intended bonding position with a flexible, compressible spacing sensor layer between their bonding faces, thereby compressing the sensor layer to varying degrees according to the spacing between the faces at different regions of the bonding interface, and
sensing the degree of compression of the sensor layer at the different regions to obtain a bondline thickness profile for the bonding interface.

2. Bonding method according to claim 1 in which the sensor layer comprises an array of piezoelectric sensors.

3. Bonding method according to claim 1 in which the sensor layer is susceptible of resilient compression at least down to 20% of its rest condition thickness.

4. Bonding method according to claim 1 in which the thickness of the sensor layer is at least 0.5 mm and not more than 2 mm.

5. Bonding method according to claim 1 in which the sensor layer is recoverably compressible at least down to 0.2 mm thickness.

6. Bonding method according to claim 1 in which the sensor layer comprises a sensor sheet incorporating an array of pressure sensors and an extender layer laminated on one or both faces of the sensor sheet, the extender layer material being softer than that of the sensor sheet; and
optionally wherein the extender layer material constitutes at least 70% of the total sensor layer thickness.

7. Bonding method according to claim 1 in which the bonding interface is three-dimensionally shaped and the sensor layer is a sensor layer preform having a corresponding three-dimensional shape or a sensor layer preform kit comprising a set of shaped panels corresponding to respective correspondingly-shaped regions of the bonding interface.

8. Bonding method according to claim 1 comprising using a programmed control processor to determine an adhesive application schedule, representing the quantities of adhesive to be applied to the respective regions of the bonding interface, from the bondline thickness profile.

9. Bonding method according to claim 8 comprising using the control processor to control the amounts of adhesive applied at various regions of the bonding interface in dependence on the adhesive application schedule.

10. Bonding method according to claim 8 in which the adhesive is applied as a solid film of predetermined uniform thickness, and the adhesive application schedule determines an arrangement of pieces of the adhesive film for building up an adhesive layer corresponding in thickness to the bondline thickness profile.

11. Bonding method according to claim 10 in which the adhesive application schedule controls a cutter to cut a set of adhesive film pieces suitable to build up said adhesive layer.

12. Bonding method according to claim 10 comprising controlling an automated adhesive application guide in dependence on the adhesive application schedule to indicate on a said component the positions of application of adhesive film pieces to build up said adhesive layer.

13. Bonding method according to claim 1 in which the bonding interface is progressively curved in more than one plane.

14. Bonding method according to claim 1 in which the second component has a recess comprised in or constituting its bonding face and receiving a correspondingly projecting bonding face or bonding face portion of the first component.

15. Bonding method according to claim 1 in which the second component is a channel, cover or sheath having an interior recessed bonding face fitting onto a complementary outer edge bonding face of the first component.

16. Bonding method according to claim 1 in which one or both components is of fibre-reinforced composite.

17. Bonding method according to claim 1 in which the first component is a blade, vane or other aerofoil element and the second component is an edge cover or edge guard for it.

18. A fit check system for implementing a bonding method according to claim 7 and comprising:
the sensor layer preform or preform kit, and
a control processor programmed to determine a bondline thickness profile based on pressure data from the sensors of the sensor layer preform.

19. A fit check system according to claim 18 in which the control processor is programmed to determine an adhesive application schedule in dependence on the bondline thickness profile and optionally control any of a cutter to cut adhesive pieces, a positioning guide to indicate predetermined positions for adhesive pieces on a said component, or an automated adhesive applicator.

20. A fit check system according to claim 18 in which the sensor layer preform or preform kit is shaped to fit a blade edge.

Assignees

• Rolls Royce Plc

Inventors

• Collis Andrew
• Richmond Nolan

Classifications

• B29C66/1122

  Single lap to lap joints, i.e. overlap joints (B29C66/45, B29C66/472, B29C66/52272 take precedence) · CPC title

• B29C66/742

  to metals or their alloys · CPC title

• B29C66/301

  Three-dimensional joints, i.e. the joined area being substantially non-flat (B29C66/5223, B29C66/5224, B29C66/5225 take precedence) · CPC title

• F01D17/02

  Arrangement of sensing elements · CPC title

• B29C66/346

  Making joints having variable thicknesses in the joint area, e.g. by using jaws having an adapted configuration · CPC title