Granted Patent B2

US 12,729,792 · App. 18/823,120 · Granted Sep 8, 2026

Inventor: Steffen Wiegand (Hamburg, DE)

Assignee: Airbus Operations GmbH

F16L39/005

Abstract

Claims (68)

1 . A support for coaxial flanges of a double-coaxial coupling, the support comprising a circular support structure;

wherein the circular support structure comprises:

a primary mounting zone for attaching a primary flange for connecting a primary outer tube;

a secondary mounting zone for attaching a secondary flange for connecting a secondary inner tube coaxial to the primary outer tube;

wherein the primary mounting zone and the secondary mounting zone are spaced apart from each other in a radial direction for centering the primary flange and the secondary flange in a radially spaced coaxial manner;

wherein the primary mounting zone comprises an outer circumferential connection region with at least three mounting points for attaching the primary flange;

wherein the secondary mounting zone comprises an inner circumferential connection region with at least three mounting points for attaching the secondary flange;

wherein a thermal path within the circular support structure between a mounting point of the primary mounting zone and an adjacent spaced apart mounting point of the secondary mounting zone is longer than the distance between the two points;

wherein the circular support structure comprises a U-shaped profile in an axial cross-section thereof,

wherein legs of the U-shaped profile comprise sleeve structures;

wherein an apex of the U-shaped profile comprises a ring structure,

wherein the primary mounting zone and the secondary mounting zone are provided by a plurality of at least three brackets, each bracket providing one of the at least three mounting points of the primary mounting zone and one of the at least three mounting points of the secondary mounting zone; and

wherein the support further comprises a circumferential connector providing a common mount for the plurality of at least three brackets.

2 . The support according to claim 1 , wherein the primary mounting zone is configured as a circumferential primary mounting zone; and

wherein the secondary mounting zone is configured as a circumferential secondary mounting zone.

3 . The support according to claim 2 , wherein, for an axially oriented fluid flow, the circular support structure comprises axially oriented passages between the circumferential primary mounting zone and the circumferential secondary mounting zone.

4 . The support according to claim 1 , wherein the circular support structure is preloadable by a force acting between the mounting point of the primary mounting zone and the mounting point of the secondary mounting zone.

5 . The support according to claim 1 ,

wherein the U-shaped profile is open to one of the at least three mounting points of the primary mounting zone and one of the at least three mounting points of the secondary mounting zone; and

wherein the U-shaped profile provides for stiffness between the one of the at least three mounting points of the primary mounting zone and the one of the at least three mounting points of the secondary mounting zone in an axial and radial direction.

6 . A coupling comprising:

a primary flange;

a secondary flange;

a support for coaxial flanges of a double-coaxial coupling, the support comprising a circular support structure;

wherein the circular support structure comprises:

a primary mounting zone for attaching a primary flange for connecting a primary outer tube;

a secondary mounting zone for attaching a secondary flange for connecting a secondary inner tube coaxial to the primary outer tube;

wherein the primary mounting zone and the secondary mounting zone are spaced apart from each other in a radial direction for centering the primary flange and the secondary flange in a radially spaced coaxial manner;

wherein the primary mounting zone comprises an outer circumferential connection region with at least three mounting points for attaching the primary flange;

wherein the secondary mounting zone comprises an inner circumferential connection region with at least three mounting points for attaching the secondary flange;

wherein a thermal path within the circular support structure between a mounting point of the primary mounting zone and an adjacent spaced apart mounting point of the secondary mounting zone is longer than the distance between the two points;

wherein the circular support structure comprises a U-shaped profile in an axial cross-section thereof,

wherein legs of the U-shaped profile comprise sleeve structures; and

wherein an apex of the U-shaped profile comprises a ring structure;

wherein the support rigidly connects the primary flange and the secondary flange and centers the secondary flange and the primary flange in a radially spaced coaxial manner; and

wherein the primary flange and the secondary flange respectively each comprises an axially facing flange side for a sealingly-tight coupling connection to a respective counterpart.

7 . The coupling according to claim 6 , wherein the axially facing flange side of the primary flange is configured for a sealingly-tight abutment to an axially facing flange side of a primary flange of an adjoining coupling; and

wherein the axially facing flange side of the secondary flange is configured for a sealingly-tight abutment to an axially facing flange side of a secondary flange of the adjoining coupling.

8 . The coupling according to claim 6 , wherein the primary flange comprises at least one fastening area for receiving an axially clamping force of a flange fastening structure for pressing the axially facing flange side of the primary flange to an abutting axially facing primary flange side of the adjoining coupling; and

wherein the circular support structure is configured to transfer the axially clamping force to the secondary flange for pressing the axially facing flange side of the secondary flange to an abutting axially facing secondary flange side of the adjoining coupling.

9 . A double-coaxial conduit comprising:

a double-coaxial tube arrangement comprising:

a primary outer tube; and

a secondary inner tube; and

at least one coupling according to claim 8 ;

wherein a circumferential portion of one end of the primary outer tube is sealingly attached to the primary flange of the coupling;

wherein a circumferential portion of one end of the secondary inner tube is sealingly attached to the secondary flange of the coupling; and

wherein a circular support structure comprises axially oriented passages between an inner side of the primary outer tube and an outer side of the secondary inner tube.

10 . The conduit according to claim 9 , further comprising a second coupling according to claim 8 attached to the other end of the double-coaxial tube arrangement.

11 . A double-coaxial tubing system comprising:

at least two double-coaxial conduits according to claim 9 ; and

at least one fastening structure;

wherein the fastening structure provides a clamping force by pressing adjacent primary flanges of the at least two double-coaxial conduits against each other.

12 . An aircraft comprising:

a fluid reservoir storing a fluid;

at least one load configured for operating with the fluid; and

a double-coaxial tubing system of claim 11 ;

wherein the double-coaxial tubing system is configured to supply the fluid from the fluid reservoir to the at least one load.

13 . A method for providing a support for coaxial flanges of a double-coaxial coupling, comprising:

providing a circular support structure;

providing, at the circular support structure, a primary mounting zone for attaching a primary flange for connecting a primary outer tube;

providing, at the circular support structure, a secondary mounting zone for attaching a secondary flange for connecting a secondary inner tube coaxial to the primary outer tube;

wherein the primary mounting zone and the secondary mounting zone are spaced apart from each other in a radial direction for centering the primary flange and the secondary flange in a radially spaced coaxial manner;

wherein the primary mounting zone provides an outer circumferential connection region with at least three mounting points for attaching the primary flange;

wherein the secondary mounting zone provides an inner circumferential connection region with at least three mounting points for attaching the secondary flange;

wherein a thermal path within the circular support structure between a mounting point of the primary mounting zone and an adjacent spaced apart mounting point of the secondary mounting zone is longer than the distance between the two points;

wherein the primary mounting zone and the secondary mounting zone are provided by a plurality of at least three brackets, each bracket providing one of the at least three mounting points of the primary mounting zone and one of the at least three mounting points of the secondary mounting zone; and

wherein the support further comprises a circumferential connector providing a common mount for the plurality of at least three brackets.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (17)