Joints of composite frames for optics support structure

Patent metadata

Field	Value
Publication number	US-11933350-B2
Application number	US-202217745501-A
Country	US
Kind code	B2
Filing date	May 16, 2022
Priority date	May 16, 2022
Publication date	Mar 19, 2024
Grant date	Mar 19, 2024

Abstract

A joint for a composite frame includes a first composite rod, a first shell abutting the first composite rod, a second shell abutting the first composite rod and disposed opposite the first shell relative to the first composite rod. The first and second shells are joined together such that composite rod is fixed therebetween. A method of forming joints of composite frame includes forming a composite frame by interconnecting a plurality of composite rods formed by an Automated Fiber Placement (AFP) manufacturing method around a mandrel, applying a first shell to the plurality of composite rods at a first location where composite rods are interconnected, applying a second shell at the first location opposite the first shell relative to the composite rods, and joining the first and second shells together with the composite rods at the first location disposed between the first and second shells.

First claim

The invention claimed is:

1. A joint for a composite frame, the joint comprising:
a first composite rod;
a second composite rod, wherein the first and second composite rods are interconnected at a first location;
wherein each of the first composite rod and the second composite rod comprises layers of a fiber-reinforced polymer-matrix composite material, and wherein layers of the first composite rod are separated by layers of the second composite rod at the first location;
a first shell abutting the first composite rod and the second composite rod;
a second shell abutting the first composite rod and the second composite rod, the second shell disposed opposite the first shell relative to the first composite rod and the second composite rod; and
wherein each of the first shell and the second shell comprises:
a first groove configured to accommodate the first composite rod;
a second groove configured to accommodate the second composite rod; and
a depression disposed at an intersection of the first groove and the second groove, the depression having a depth greater than each of the first groove and the second groove to accommodate the first composite rod and the second composite rods at the first location;

wherein the first and second shells are joined together such that the first and second composite rods are fixed therebetween at the first location.

2. The joint of claim 1 , wherein each of the first and second composite rods is a continuous composite rod extending beyond the first and second shells.

3. The joint of claim 1 , wherein the first composite rod is a continuous composite rod, and the second composite rod is a discontinuous composite rod having a terminal end disposed between the first and second shells.

4. The joint of claim 3 , wherein the second groove of each of the first and second shells is discontinuous to accommodate the terminal end, such that the first and second shells are joined around the terminal end.

5. The joint of claim 1 , and further comprising:
a third composite rod;
wherein the third composite rod is a continuous composite rod or a discontinuous composite rod having a terminal end disposed between the first and second shells or beyond the first and second shells; and
wherein the third composite rod, the first composite rod, and the second composite rod are interconnected at the first location such that layers of the first composite rod are separated by layers of the second composite rod and the third composite rod at the first location and within the depression.

6. The joint of claim 5 , wherein each of the first and second shells comprises:
a third groove configured to accommodate the third composite rod and wherein the depression has a depth to accommodate the third composite rod.

7. The joint of claim 6 , wherein the third composite rod is a discontinuous composite rod having a terminal end disposed between the first and second shells.

8. The joint of claim 7 , wherein the third groove of each of the first and second shells is discontinuous to accommodate the terminal end, such that the first and second shells are joined around the terminal end.

9. The joint of claim 1 , wherein the first and second shells are metal and are joined together with metallic fasteners.

10. The joint of claim 1 , wherein the first and second shells are thermoplastic materials and are joined together by at least one of welding, co-consolidation, and a metallic fastener.

11. The joint of claim 1 , wherein the first and second shells are thermoset materials and are joined together by at least one of an adhesive, co-curing, and a metallic fastener.

12. The joint of claim 1 , wherein each of the first and second shells includes a plurality of holes configured for connecting an optical device to the composite frame or for connecting the composite frame to another structure.

13. A composite frame for an optical device, the composite frame comprising a plurality of the joints of claim 1 .

Assignees

• Goodrich Corp

Inventors

• Gurvich Mark R
• Smith Brian J

Classifications

• F16B7/044 Primary

  for rods or tubes being in angled relationship · CPC title

• F16B7/0486

  forming an abutting connection of at least one tube · CPC title

• F16B7/0493

  forming a crossed-over connection · CPC title

• B29C65/562

  using extra joining elements, i.e. which are not integral with the parts to be joined (using plastic snap elements B29C65/58; using plastic rivets B29C65/601) · CPC title

• B29C70/382

  Automated fiber placement [AFP] · CPC title