Bonding method

1. A method of manufacturing a component, the method comprising bonding a first component to a second component including:

locating the first component against the second component to form an interface between the components, a curable adhesive being provided at the interface;

locating a pressurisable, fluid-filled bladder against the first component such that the first component is sandwiched between the second component and the bladder;

locating a backing member against the bladder such that the bladder is sandwiched between the backing member and the first component;

pressurising the bladder such that a consolidating pressure is exerted by the bladder on the first component to conform the first component to the second component;

curing the adhesive while the first component is conformed to the second component by the consolidating pressure; and

locating a compliant layer between the fluid-filled bladder and the first component, the compliant layer carrying an arrangement of spaced, rigid protuberances which project from the side of the layer facing the first component, the protuberances including summits that are configured such that only the summits are in contact with the first component when the bladder is pressurized to concentrate the consolidating pressure exerted by the bladder on the first component at the locations of the protuberances.

2. The method according to claim 1 , wherein the bladder is pressurised by forcing further fluid into the bladder, expansion of the bladder being constrained by the backing member.

3. The method according to claim 1 , wherein the bladder is pressurised by forcing the backing member against the bladder to squeeze the bladder between the backing member and the first component.

4. The method according to claim 1 , wherein one or more supports extend from the compliant layer to the backing member to hold the compliant layer in position.

5. The method according to claim 1 , wherein the method further includes locating a mould release layer and/or a puncture protection sheet on the first component between the first component and the bladder.

6. The method according to claim 1 , wherein the method further includes locating one or more heating mats adjacent the components, and heating the components during the curing of the adhesive using the mats.

7. The method according to claim 1 , wherein the first component is an acoustic liner or an abradable liner, and the second component is a gas turbine engine fan casing.

8. A method of manufacturing a gas turbine engine comprising manufacturing one or more components using the method according to claim 1 .

9. A method of bonding a first component to a second component, the method comprising:

locating the first component against the second component to form an interface between the components, a curable adhesive being provided at the interface;

locating a pressurisable, fluid-filled bladder against the first component such that the first component is sandwiched between the second component and the bladder;

locating a backing member against the bladder such that the bladder is sandwiched between the backing member and the first component;

pressurising the bladder such that a consolidating pressure is exerted by the bladder on the first component to conform the first component to the second component;

curing the adhesive while the first component is conformed to the second component by the consolidating pressure; and

supporting a weight of a compliant layer between the fluid-filled bladder and the first component with one or more telescoping supports that extend from the compliant layer to the backing member.