Radome with ceramic matrix composite

Patent metadata

Field	Value
Publication number	US-11901619-B2
Application number	US-202117553238-A
Country	US
Kind code	B2
Filing date	Dec 16, 2021
Priority date	Dec 16, 2021
Publication date	Feb 13, 2024
Grant date	Feb 13, 2024

Abstract

In a first example, a radome includes a shell including a ceramic matrix composite, the shell forming a first hole at a forward end of the shell and a second hole at an aft end of the shell. The radome also includes a fluid impervious coating on the shell. In a second example, a vehicle includes a main body, the radome, and an attachment assembly that couples the radome to the main body. In a third example, a method includes forming a shell comprising a ceramic matrix composite using a wet layup process, applying a fluid impervious coating onto the shell, and curing the shell and the fluid impervious coating.

First claim

What is claimed is:

1. A radome comprising:
a shell comprising a ceramic matrix composite, the shell forming a first hole at a forward end of the shell and a second hole at an aft end of the shell;
a fluid impervious coating on the shell;
an annular component configured to be attached to a vehicle at the aft end of the shell via a first fastener received through a third hole of the annular component; and
a bipod component comprising:
a joint that is attached via a second fastener to the shell forward of the annular component;
a first leg extending aft from the joint, wherein the first leg is adjoined to the annular component; and
a second leg extending aft from the joint, wherein the second leg is adjoined to the annular component.

2. The radome of claim 1 , wherein the shell comprises an inner surface and an outer surface, and wherein the fluid impervious coating covers an entirety of the outer surface.

3. The radome of claim 1 , wherein the first hole is smaller than the second hole.

4. The radome of claim 1 , further comprising a tip that forms a fluid tight seal with the shell over the first hole.

5. The radome of claim 4 , wherein the tip comprises a ceramic material.

6. The radome of claim 4 , further comprising a fastening assembly that mechanically fastens the tip to the shell.

7. The radome of claim 6 , wherein the fastening assembly comprises:
a bushing that conforms to an inner surface of the shell, wherein the bushing is configured to receive an aft end of the tip; and
a third fastener configured to mate with the aft end of the tip to hold the tip against the shell over the first hole.

8. The radome of claim 7 , further comprising a spring element between the third fastener and the bushing, wherein the spring element is configured to receive the aft end of the tip.

9. The radome of claim 8 , wherein the spring element is configured to maintain a preload on the tip during thermal expansion of the shell or during thermal contraction of the shell.

10. The radome of claim 1 , wherein the first hole and the second hole are aligned on an axis, and wherein the bipod component is more flexible perpendicular to the axis than parallel to the axis.

11. The radome of claim 1 , further comprising a fastening assembly comprising a spring element that is configured to maintain a preload on the shell and the bipod component during thermal expansion of the shell or during thermal contraction of the shell.

12. A vehicle comprising:
a main body;
a radome comprising:
a shell comprising a ceramic matrix composite, the shell forming a first hole at a forward end of the shell and a second hole at an aft end of the shell;
a fluid impervious coating on the shell;
an annular component configured to be attached to the vehicle at the aft end of the shell via a first fastener received through a third hole of the annular component; and
a bipod component comprising:
a joint that is attached via a second fastener to the shell forward of the annular component;
a first leg extending aft from the joint, wherein the first leg is adjoined to the annular component; and
a second leg extending aft from the joint, wherein the second leg is adjoined to the annular component.

13. The vehicle of claim 12 , further comprising a metallic gasket that forms a fluid impervious seal between the radome and the main body.

14. The radome of claim 1 , wherein the annular component comprises a first surface that faces aft, wherein the first surface is configured to be attached to and contact a second surface of the vehicle that faces forward.

15. The radome of claim 1 , wherein the ceramic matrix composite comprises ceramic fibers reinforced in a ceramic matrix.

16. The radome of claim 1 , wherein the third hole is between the first leg and the second leg.

17. The vehicle of claim 12 , wherein the ceramic matrix composite comprises ceramic fibers reinforced in a ceramic matrix.

18. The vehicle of claim 12 , wherein the annular component comprises a first surface that faces aft, wherein the first surface is configured to be attached to and contact a second surface of the vehicle that faces forward.

19. The vehicle of claim 12 , wherein the first hole is between the first leg and the second leg.

20. The vehicle of claim 12 , wherein the first hole and the second hole are aligned on an axis, and wherein the bipod component is more flexible perpendicular to the axis than parallel to the axis.

Assignees

• Boeing Co

Inventors

• Best Michael J
• Dichiara Robert A
• Muench Brian L
• Heng Vann
• Embler Jonathan D
• Pinney Thomas R
• O'Brien Holly M

Classifications

• H01Q1/42 Primary

  Housings not intimately mechanically associated with radiating elements, e.g. radome · CPC title

• H01Q1/281

  Nose antennas · CPC title