Hybrid metallic/composite joint with enhanced strength

Patent metadata

Field	Value
Publication number	US-12092137-B2
Application number	US-202016997529-A
Country	US
Kind code	B2
Filing date	Aug 19, 2020
Priority date	Oct 5, 2016
Publication date	Sep 17, 2024
Grant date	Sep 17, 2024

Abstract

A metallic/composite joint includes a composite member and an insert located at least partially within the composite member. The composite member comprises a cylinder having an angled end extending along a centerline axis, an inner surface of the angled end oriented at a first angle relative to the centerline axis. The insert is located at least partially within the angled end and having an outer surface oriented at a second angle relative to the centerline axis. The first and second angles are oriented to reduce maximum shear stress in the composite member when the insert and composite member are in an installed position.

First claim

What is claimed is:

1. A metallic/composite joint comprising:
a composite member comprising a cylinder having a flared end extending along a centerline axis, an outer surface of the flared end oriented at a first angle relative to the centerline axis, wherein the outer surface of the flared end is a continuously formed surface;
a metallic member perimetrically surrounding the outer surface of the flared end and having an inner surface oriented at a second angle relative to the centerline axis, wherein the inner surface comprises a portion in which the second angle remains constant, and wherein the portion is proximate a terminus of the flared end; and
an insert located at least partially within the flared end and having an outer surface oriented at a third angle relative to the centerline axis,
wherein the portion of the inner surface of the metallic member and the outer surface of the composite member are separated by a first gap at a first location and are separated by a second gap at a second location, the first gap being greater than the second gap, the first location being spaced further axially inward from the terminus of the composite member at the flared end than the second location, and the second location being located further radially outward from the centerline axis and the cylinder than the first location, and the first gap and the second gap being measured in a direction substantially orthogonal to the centerline axis.

2. The metallic/composite joint of claim 1 , wherein the composite member comprises a fiber-reinforced polymer matrix composite.

3. The metallic/composite joint of claim 1 , wherein the first angle is greater than the second angle.

4. The metallic/composite joint of claim 3 , wherein the third angle is substantially equal to the first angle.

5. The metallic/composite joint of claim 3 , wherein the third angle is greater than the first angle.

6. The metallic/composite joint of claim 1 , wherein the first angle varies along an axial direction.

7. The metallic/composite joint of claim 1 , wherein the second angle varies along an axial direction.

8. The metallic/composite joint of claim 1 , wherein the first angle is substantially equal to the second angle and the third angle is greater than the first angle.

9. The metallic/composite joint of claim 1 , wherein the outer surface of the insert comprises a non-linear convex geometry.

10. The metallic/composite joint of claim 1 , wherein the composite member further comprises a plurality of fibers primarily oriented in a hoop direction .

11. A metallic/composite joint comprising:
a composite member comprising a cylinder having a flared end extending along a centerline axis, an inner surface of the flared end oriented at a first angle relative to the centerline axis, wherein the inner surface of the flared end is a continuously formed surface, and wherein an outer diameter of the flared end is greater than an outer diameter of the cylinder; and
an insert located at least partially within the flared end and having an outer surface oriented at a second angle relative to the centerline axis,
wherein the outer surface of the insert and the inner surface of the composite member are separated by a first gap at a first location and are separated by a second gap at a second location, the first location being spaced further axially inward from a terminus of the composite member at the flared end than the second location, and the second location being located further radially outward from the centerline axis and the cylinder than the first location, and the first gap and the second gap being measured in a direction substantially orthogonal to the centerline axis.

12. The metallic/composite joint of claim 11 , wherein the composite member comprises a fiber-reinforced polymer matrix composite.

13. The metallic/composite joint of claim 11 , wherein the second angle is greater than the first angle.

14. The metallic/composite joint of claim 13 , further comprising a metallic member perimetrically surrounding the flared end and having an inner surface oriented at a third angle relative to the centerline axis, wherein the third angle is substantially equal to the first angle.

15. The metallic/composite joint of claim 13 , further comprising a metallic member perimetrically surrounding the flared end and having an inner surface oriented at a third angle relative to the centerline axis, wherein the third angle is less than the first angle.

16. The metallic/composite joint of claim 11 , wherein the first angle varies along an axial direction.

17. The metallic/composite joint of claim 11 , wherein the second angle varies along an axial direction.

18. The metallic/composite joint of claim 11 , further comprising a metallic member perimetrically surrounding the flared end and having an inner surface oriented at a third angle relative to the centerline axis, wherein the first angle is substantially equal to the second angle and the third angle is less than the first angle.

19. The metallic/composite joint of claim 11 , wherein the outer surface of the insert comprises a non-linear convex geometry.

20. The metallic/composite joint of claim 11 , where the first gap is greater than the second gap.

Assignees

• Goodrich Corp

Inventors

• Gurvich Mark R
• Ganis Rony Giovanni
• Faustino Virginia H

Classifications

• F16C2220/40

  by deformation without removing material · CPC title

• F16C7/026 Primary

  made of fibre reinforced resin · CPC title

• B64C25/00

  Alighting gear (air-cushion alighting gear B60V3/08) · CPC title

• F16B11/002 Primary

  by pressing the elements together so as to obtain plastic deformation (shrinkage connections, force fits F16B4/00; pin-and-hole connections involving plastic deformation F16B17/00) · CPC title