Hybrid joint manufacturing

Patent metadata

Field	Value
Publication number	US-9909605-B2
Application number	US-201314437402-A
Country	US
Kind code	B2
Filing date	Oct 21, 2013
Priority date	Oct 22, 2012
Publication date	Mar 6, 2018
Grant date	Mar 6, 2018

Abstract

A method for forming a joint between a fiber reinforced composite component and a metallic component and a joint are provided. The metallic component and the composite component each define a joint surface for mating with the joint surface of the other to join the two components together and the composite component defines a free surface opposed to the joint surface thereof. The joint surface of the metallic component defines an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface. The method includes the steps of pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate through the fiber reinforcing material, and modifying the effective cross sectional shape of the pin heads whereby to increase the constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component.

First claim

The invention claimed is:

1. A method of forming a joint between a fibre reinforced composite component and a metallic component, the metallic component and the composite component each defining a joint surface for mating with the joint surface of the other to join the two components together and the composite component defining a free surface opposed to the joint surface thereof, the joint surface of the metallic component defining an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface, the method including:
pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate the fibre reinforced composite component; and
modifying the effective cross sectional shape of the pin heads whereby to increase a constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component,
wherein modifying the effective cross sectional shape of the pin heads comprises attaching a retaining feature to the pins, the retaining feature being shaped to engage the composite component to prevent withdrawal of the pins therefrom, and
wherein the method further includes forming the pins so as not to fully penetrate the composite component, upon assembly, and forming the pin heads with one of an internal and an external taper and forming the retaining feature with the other of the internal and external taper whereby, upon assembly of the metallic component and composite component together, axial engagement of the pins with the retaining feature will occur and the tapers will force one of the pin head and the retaining feature to expand radially of the pin and interfere with the composite component.

2. The method as in claim 1 , further including adhering the retaining feature to the pins.

3. The method as in claim 1 , further including forming the pins and the retaining feature whereby, upon assembling the metallic component and composite component together, an interference fit will occur between the pins and the retaining feature.

4. The method as in claim 1 , wherein the retaining feature is metallic, and wherein the method further includes welding the retaining feature to each pin head after assembly of the metallic component and composite component together.

5. The method as in claim 1 , further including forming the pins with a hollow to receive the retaining feature therein and forming each retaining feature with at least one protrusion to engage at least one pin in the hollow thereof.

6. The method as in claim 1 , further including forming the retaining feature with an external taper shaped to compress an area of the composite component surrounding an aperture formed therein by passage of the pin therethrough, upon assembly of the metallic component and composite component together.

7. The method as in claim 1 , wherein increasing the constraint applied to the composite component applies a residual compressive stress to the composite component.

8. The method as in claim 1 , wherein the composite component comprises a layup of fibre plies which is interspersed with a plastics matrix material and wherein, subsequent to carrying out the method, the layup is cured.

9. A method of forming a joint between a fibre reinforced composite component and a metallic component, the metallic component and the composite component each defining a joint surface for mating with the joint surface of the other to join the two components together and the composite component defining a free surface opposed to the joint surface thereof, the joint surface of the metallic component defining an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface, the method including:
pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate the fibre reinforced composite component;
modifying the effective cross sectional shape of the pin heads whereby to increase a constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component; and
forming the pins and retaining feature whereby, upon assembling the metallic component and composite component together, an interference fit will occur between the pins and retaining feature,
wherein modifying the effective cross sectional shape of the pin heads comprises attaching a retaining feature to the pins, the retaining feature being shaped to engage the composite component to prevent withdrawal of the pins therefrom, and
wherein the retaining feature comprises at least one of a metallic mesh and a covering layer, and the method further includes forming the pins with pointed pin heads and forcing the pins through at least one of the metallic mesh and the covering layer, upon assembly of the metallic component to the composite component, whereby to cause the said interference fit to occur.

10. The method as in claim 9 , wherein the pin heads are formed as arrowheads and wherein at least one of the metallic mesh and the covering layer is caused to pass into interlocking engagement with the pins behind the arrowheads, upon assembly of the metallic component and composite component together.

11. The method as in claim 9 , further including adhering the retaining feature to the pins.

12. The method as in claim 9 , wherein the retaining feature is metallic, and wherein the method further includes welding the retaining feature to each pin head after assembly of the metallic component and composite component together.

13. The method as in claim 9 , further including forming the pins with a hollow to receive the retaining feature therein and forming each retaining feature with at least one protrusion to engage at least one pin in the hollow thereof.

14. The method as in claim 9 , further including forming the retaining feature with an external taper shaped to compress an area of the composite component surrounding an aperture formed therein by passage of the pin therethrough, upon assembly of the metallic component and composite component together.

15. A method of forming a joint between a fibre reinforced composite component and a metallic component, the metallic component and the composite component each defining a joint surface for mating with the joint surface of the other to join the two components together and the composite component defining a free surface opposed to the joint surface thereof, the joint surface of the metallic component defining an array of pins extending therefrom with each pin defining a pin head at an end distal from the joint surface, the method including:
pressing together the joint surfaces of the two components whereby to cause the array of pins to penetrate the fibre reinforced composite component; and
modifying the effective cross sectional shape of the pin heads whereby to increase a constraint applied to the composite component against peeling of the composite component from the joint surface of the metallic component,
wherein modifying the effective cross sectional shape of the pin heads comprises attaching a retaining feature to the pins, the retaining feature being shaped to engage the composite component to prevent withdrawal of the pins therefrom, and
wherein the method further includes fitting the pins with temporary shaped pin head attachments to aid assembly of the metallic component to the composite component and removing the pin head attachments after the assembly and prior to fitting the retaining feature to the pins.

16. The method as in claim 15 , fu

Assignees

• Bae Systems Plc

Inventors

• Baker David
• Rezai Amir
• Wescott Andrew David
• Graham Daniel Peter

Classifications

• B29C66/742

  to metals or their alloys · CPC title

• B29C66/8432

  Machines for making separate joints at the same time mounted in parallel or in series · CPC title

• B29C66/81429

  comprising a single tooth · CPC title

• B29C65/606

  the rivets being integral with one of the parts to be joined, i.e. staking · CPC title

• Y10T29/49938

  Radially expanding part in cavity, aperture, or hollow body · CPC title