Fluid coupling

Patent metadata

Field	Value
Publication number	US-11808388-B2
Application number	US-202016804462-A
Country	US
Kind code	B2
Filing date	Feb 28, 2020
Priority date	Mar 1, 2019
Publication date	Nov 7, 2023
Grant date	Nov 7, 2023

Abstract

A fluid coupling includes a body including a plurality of segments and one or more links connecting the segments in a substantially annular configuration. At least one of the one or more links may be adjustable to modify a diameter of the body. The body may have a substantially U-shaped a cross-section with a first tapered portion, a second tapered portion, a first planar portion, a second planar portion, and/or a third planar portion. The body may include a first rounded corned and a second rounded corner. The first planar portion may be disposed substantially between the first tapered portion and the first rounded corner, the second planar portion may be disposed substantially between the first rounded corner and the second rounded corner, and/or the third planar portion may be disposed substantially between the second rounded corner and the second tapered portion.

First claim

What is claimed is:

1. A fluid coupling, comprising:
a body including a plurality of segments including a first segment and a second segment, each of the segments having opposite ends and an ear offset from each end by an end length extending from the end along a circumference of the body;
a plurality of links connecting the segments in a substantially annular configuration with an interior diameter and an exterior diameter, a first of the links having a first end coupled to a first ear of the first segment and a second end coupled to a second ear of the second segment, the first link defining a concave curvature between the first and second ends, the concave curvature disposed outside of the interior diameter and facing an interior of the annular configuration, the first link spanning a first end length of the first segment, a circumferential gap between the first segment and the second segment, and a second end length of the second segment;
wherein at least one of the plurality of links is adjustable to modify a diameter of the body; and
the body has a substantially U-shaped cross-section with a first tapered portion, a second tapered portion, a first planar portion, a second planar portion, and a third planar portion.

2. The fluid coupling of claim 1 , wherein the body includes a first rounded corner and a second rounded corner.

3. The fluid coupling of claim 2 , wherein the first planar portion is disposed substantially between the first tapered portion and the first rounded corner;
the second planar portion is disposed substantially between the first rounded corner and the second rounded corner; and
the third planar portion is disposed substantially between the second rounded corner and the second tapered portion.

4. The fluid coupling of claim 2 , wherein a radius of the first rounded corner is greater than about 0.05 inches.

5. The fluid coupling of claim 2 , wherein the body includes a third rounded corner and a fourth rounded corner.

6. The fluid coupling of claim 5 , wherein a radius of the third rounded corner is at least 40% smaller than a radius of the first rounded corner.

7. The fluid coupling of claim 1 , wherein the first planar portion and the third planar portion are shorter than the second planar portion.

8. The fluid coupling of claim 7 , wherein the first planar portion and the third planar portion are shorter than the first tapered portion and the second tapered portion.

9. The fluid coupling of claim 1 , wherein the first tapered portion is disposed at an angle of about 15 degrees to about 25 degrees.

10. The fluid coupling of claim 9 , wherein the angle is about 19 degrees.

11. The fluid coupling of claim 1 , wherein the second planar portion is at least twice as long as the first planar portion.

12. The fluid coupling of claim 1 , wherein the body include a recess formed, at least in part, by the first tapered portion, the second tapered portion, the first planar portion, the second planar portion, and the third planar portion; and
the recess is configured to at least partially receive and retain a first flange of a first fluid conduit and a second flange of a second fluid conduit.

13. The fluid coupling of claim 1 , wherein the body is configured to at least partially receive and retain AS1985 joints.

14. The fluid coupling of claim 1 , wherein the body and the plurality of links are configured to apply a clamping force to corresponding mating surfaces of flanges of fluid conduits; and
said corresponding mating surfaces are radially offset from outer edges of said flanges.

15. An aircraft bleed air system, comprising:
a first fluid conduit including a first flange;
a second fluid conduit including a second flange; and
a fluid coupling retaining the first flange and the second flange, the fluid coupling comprising:
a body including a plurality of segments including a first segment and a second segment each of the segments having opposite ends and an ear offset from each end by an end length extending from the end along a circumference of the body;
a plurality of links connecting the segments in a substantially annular configuration with an interior diameter and an exterior diameter, a first of the links having a first end coupled to a first ear of the first segment and a second end coupled to a second ear of the second segment, the first link defining a concave curvature between the first and second ends, the concave curvature disposed outside of the interior diameter and facing an interior of the annular configuration, the first link spanning a first end length of the first segment, a circumferential gap between the first segment and the second segment, and a second end length of the second segment;
wherein at least one of the plurality of links is adjustable to modify a diameter of the body and clamp the body onto the first flange and the second flange; and
a cross-section of the body is substantially U-shaped with a first tapered portion, a second tapered portion, a first planar portion, a second planar portion, and a third planar portion.

16. The aircraft bleed air system of claim 15 , wherein the first planar portion is disposed substantially between the first tapered portion and a first rounded corner;
the second planar portion is disposed substantially between the first rounded corner and a second rounded corner; and
the third planar portion is disposed substantially between the second rounded corner and the second tapered portion.

17. The aircraft bleed air system of claim 16 , wherein the first fluid conduit and the second fluid conduit are rigid metal ducts; and
the first fluid conduit, the second fluid conduit, and the fluid coupling are configured for fluid pressures of at least 750 psig and at least 15,000 in-lbs of bending torque.

18. The aircraft bleed air system of claim 16 , wherein the plurality of segments includes three segments and the plurality links includes three links connecting the three segments together.

19. The aircraft bleed air system of claim 15 , wherein the plurality of links include at least two curved links; and
the concave surfaces of the curved links are configured to receive respective tabs of the first flange and/or the second flange.

20. The aircraft bleed air system of claim 15 , wherein the first flange and the second flange include corresponding mating surfaces that are radially offset from ends of the first flange and the second flange; and
the fluid coupling applies a clamping force to the first flange and the second flange at or about the corresponding mating surfaces.

Assignees

• Eaton Intelligent Power Ltd

Inventors

• Emrick Benjamin
• Matthews emmanuel
• Murray Jonathan D

Classifications

• F16L23/10 Primary

  with a pivoting or swinging pin · CPC title

• F16L23/08

  connection by tangentially arranged pin and nut · CPC title