Sealing and shimming of structural joints

Abstract

A method of producing a sealed structural joint between two components (23, 24) and such a sealed joint are provided. The method includes the steps of applying a layer of sealant (27) to the first component (23), applying liquid shim (28) to the second component (24), inserting an intermediate layer (29) between the sealant (27) and the liquid shim (28), the intermediate layer (29) having a series of raised structural features (31) to engage the first component (23). The features (31) are positioned to allow the sealant (27) to extend across the joint between the raised features (31) to form a continuous seal. The joint is then closed and cure of the liquid shim (28) and sealant (27) takes place to solidify the shim (28) to the desired thickness within the joint.

Claims

1. A method of producing a sealed structural joint between first and second components, the method includes: determining that the sealed structural joint requires a liquid shim, wherein the sealed structural joint is between the first and second components, applying a layer of sealant to a faying surface of the first component, applying the liquid shim to a faying surface of the second component, inserting an intermediate layer between the faying surface of the first component and the liquid shim, wherein the intermediate layer is formed with a series of raised structural features thereacross whereby upon joint closure to engage the faying surface of at least the first component, wherein the series of raised structural features are positioned to allow sealant from the layer of sealant to extend across the joint between said raised features and form a continuous seal across the joint, closing the joint to achieve a desired separation of the faying surfaces, and curing at least the liquid shim to solidify the shim to a desired thickness within the joint.

2. The method according to claim 1, in which the intermediate layer is formed as a continuous layer to prevent either the sealant or the liquid shim passing therethrough.

3. The method according to claim 1, in which the intermediate layer is formed as a permeable layer to allow at least one of the sealant and the liquid shim to pass therethrough.

4. The method according to claim 1, in which the intermediate layer is formed as a mesh.

5. The method according to claim 1, in which the intermediate layer is formed as a corrugated layer.

6. The method according to claim 1, in which the intermediate layer is formed of a flat sheet with said series of raised structural features formed on either side of the flat sheet.

7. The method according to claim 1, in which dimensions of the raised structural features of the intermediate layer, measured across the joint, are determined in dependence upon a cross sectional area of a fastener intended to pass through the joint.

8. The method according to claim 1, including cleaning or drilling the joint.

9. The method according to claim 1, including disassembling the joint for inspection and wherein the step of applying a layer of sealant to the faying surface of the first component is carried out after the disassembly of the joint for inspection.

10. A method to join first and second components including: determining a desired thickness for a shim to be inserted between the first and second components; applying a layer of sealant to a first faying surface of the first component, applying liquid shim to a second faying surface of the second component, inserting an intermediate layer between the layer of sealant and the liquid, wherein a first surface of the intermediate layer includes projections facing the layer of sealant; closing a gap between the first and second components while the layer of sealant, the liquid shim and the intermediate layer are between the first and second components; squeezing the layer of sealant between the intermediate layer and the first faying surface by closing the gap, wherein the squeezing distributes sealant in the layer of sealant between the projections of the first surface of the intermediate layer, across the first faying surface and thereby forms a seal between the intermediate layer and the first component; and curing the liquid shim to solidify the shim to the desired thickness after closing the gap and squeezing the layer of sealant.

11. The method of claim 10 further comprising preventing mixing of the layer of sealant and the liquid shim by the insertion of the intermediate layer.

12. The method of claim 10 wherein the projections on the first surface of the intermediate layer are dimples with flat tops distributed across an entire area of the first surface which faces the first component, and the method further comprises abutting the flat tops of the dimples against the first flaying surface as a result of the closure of the gap.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The present invention will now be described, by way of example only, with reference to the following drawings in which:

(2) FIG. 1a is a sectional view of a joint pre-assembled, according to the prior art;

(3) FIG. 1b shows the same joint with release film applied;

(4) FIG. 1c shows the same joint with release film and liquid shim applied;

(5) FIG. 1d shows the same joint drilled off;

(6) FIG. 1e shows the same joint finally assembled;

(7) FIG. 2a is a sectional view of a joint with sealant and liquid shim applied, according to the invention;

(8) FIG. 2b shows the same joint with an intermediate layer inserted into the joint;

(9) FIG. 2c shows the same joint closed;

(10) FIG. 3 shows a first intermediate layer according to the invention, and

(11) FIG. 4 shows a second corrugated intermediate layer according to the invention

(12) FIG. 5 is a side part sectional view of a sealed structural joint according to the invention.

DESCRIPTION OF PREFERRED EMBODIMENT

(13) With reference to FIG. 1, a joint assembled according to the prior art is shown. This method of joint assembly is current in aircraft production and requires the joint to be disassembled at least twice before final assembly.

(14) Looking at FIG. 1a, first and second components 1, 2 are assembled together and a gap 3 between faying surfaces 4, 5 of the components is measured or a decision gauge used.

(15) In FIG. 1b, the joint is disassembled for the first time and release film 6 is applied to the faying surface 4 of component 1, in order to prevent adhesion of liquid shim to the faying surface 4.

(16) In FIG. 1c, liquid shim 7 is applied to faying surface 5 of component 2 by injection into the joint or by butter and paste application. Once the liquid shim has cured, the joint is disassembled to inspect for porosity in the shim 7; the shim is then repaired as necessary and the joint re-assembled.

(17) In FIG. 1d, the assembly 1, 2, 6, 7 is drilled off to form apertures 9, 10 through the joint to receive fasteners. The joint is then disassembled for the second time for cleaning and de-burring and for the release film 6 to be removed. The joint is then inspected for porosity and other defects in the shim 7; the shim is then repaired as necessary.

(18) Finally, in FIG. 1e, final assembly of the joint takes place: interfay sealant 10 is applied and fasteners 11, 12 are installed.

(19) The method of the invention is able to remove at least one if not both disassembly steps from the above process and thereby markedly to reduce overall process time and at the same time reduce the potential for process errors.

(20) Referring to FIGS. 2a to 2c, an example process according to the invention is described. FIG. 2a shows components 23, 24 having faying surfaces 25, 26. Initially, the structural designer has here decided that the structure interfaces will require shimming and set the design dimensions for the joint accordingly. No measurement of the joint gap between faying surfaces 25, 26 will therefore be necessary. Next, appropriate cleaning and pre-treatment of the faying surfaces 25, 26 is carried out. Onto faying surface 25 is applied a standard sealant 27 and onto faying surface 26 is applied two-part epoxy liquid shim 28.

(21) Next, with reference to FIG. 2b and FIG. 3, an intermediate layer 29 is inserted between components 23, 24 as shown. The intermediate layer 29 comprises a flat sheet 30 having a regular series of raised structural features in the form of raised dimples 31 distributed across the sheet. The raised dimples 31 each have a flat top 32 and a height not exceeding 200 m.

(22) It will be observed from FIG. 3 that a continuous matrix of sealant 37 applied to the intermediate layer 29 between the dimples 31 will extend both horizontally and vertically of the layer 29. A sealed joint may therefore be created such that no leak path can form across the joint face between the intermediate layer 29 and the faying surface 25, using the method of the invention.

(23) The dimples 31 must be sized so that each flat top, which will be in contact with the faying surface 25 of the first component 23, will have a small enough surface area so that, once an aperture 33 is drilled through the component assembly 23, 24 for fastener insertion through the joint, an even distribution of compression load from the first component 23 through the intermediate layer 29 to the second component 24 is possible around the entire fastener aperture 33. If the surface area of the dimples 31 is too large, there is a greater risk that the loading is not evenly transferred.

(24) FIG. 2c shows the joint assembled for curing of the liquid shim 28 and sealant 27 to take place in situ. No further disassembly of the joint is necessary.

(25) FIG. 4 shows a corrugated intermediate layer 41. The layer is corrugated in two directions with peaks 42 of the double corrugation forming the raised structural features.

(26) FIG. 5 shows a sealed structural joint 50, according to the invention with various features exaggerated, for clarity. The joint 50 is formed between a first component in the form of a wing skin 51 and a second component in the form of a rib foot 52. The joint is sealed with sealant 57 and is packed with cured liquid shim 58. The joint is secured with fasteners 53.

(27) A joint formed as in FIG. 5, according to the invention, is ideally suited for the connection of rib feet to a wing skin. Such a joint must be dimensionally extremely precise as the relatively flexible wing skin is being drawn into contact with a structurally stiff rib. Any dimensional error attributable to component misalignment in the joint will distort the wing skin from its design profile and upset the aerodynamics of the aircraft. Additionally, the joint must normally be sealed as the wing box is in almost all cases a fuel tank and fuel leakage past the joint to the wing exterior must be prevented. Lightning strike is another risk to be avoided through adequate sealing. Such sealed structural joints on aircraft also occur in the fuselage.

(28) The embodiments described herein are respective non-limiting examples of how the present technology, and aspects of the present technology, may be implemented. Any feature described in relation to any one embodiment may be used alone, or in combination with other features described, and may also be used in combination with one or more features of any other of the embodiments, or any combination of any other of the embodiments. Furthermore, equivalents and modifications not described above may also be employed without departing from the scope of the invention, which is defined by the accompanying claims.

(29) The word or as used herein is to be taken to mean and/or unless explicitly stated otherwise.