Shrouded pipe

Patent metadata

Field	Value
Publication number	US-11143349-B2
Application number	US-201715600146-A
Country	US
Kind code	B2
Filing date	May 19, 2017
Priority date	May 20, 2016
Publication date	Oct 12, 2021
Grant date	Oct 12, 2021

Abstract

A shrouded pipe formed from inner and outer pipe sections, the inner pipe section having an outwardly projecting flange joining the outer pipe section, and the outer pipe section having an inwardly projecting flange joining the inner pipe section, an annular volume between the inner and outer pipe sections providing a secondary fluid path. The flanges control axial position of the inner pipe section. By providing one flange which extends radially outwardly and one which extends radially inwardly, assembly is possible of the shrouded pipe by inserting the inner pipe section into the outer pipe section, without modification of the outer pipe section or inner pipe section. The first and second flanges ensure no unwanted contact between the inner and outer pipe sections and, therefore, prevent damage to the primary fluid path. The first and second flanges ensure good load distribution between the inner and outer pipe sections.

First claim

The invention claimed is:

1. A shrouded pipe assembly comprising:
an inner pipe section comprising a primary fluid path;
a first flange that is directly attached to and projects radially outwardly from a first end of the inner pipe section;
an outer pipe section enclosing the inner pipe section;
a second flange that is directly attached to and projects radially inwardly from a second end of the outer pipe section;
wherein the first end of the inner pipe section is at an opposite end of the shrouded pipe assembly from the second end of the outer pipe section;
wherein the first flange is joined to a first end of the outer pipe section, such that the first flange is directly attached to both the inner pipe section, at the first end of the inner pipe section, and the outer pipe section, at the first end of the outer pipe section, to define a first radial gap between the inner and outer pipe sections at a first end of the shrouded pipe assembly;
wherein the second flange is joined to a second end of the inner pipe section, such that the second flange is directly attached to both the inner pipe section, at the second end of the inner pipe section, and the outer pipe section, at the second end of the outer pipe section, to define a second radial gap between the inner and outer pipe sections at a second end of the shrouded pipe assembly;
wherein an annular volume extends from the first radial gap to the second radial gap, between the inner and outer pipe sections, to provide a secondary fluid path;
wherein the second flange is a continuous annular flange extending radially inwardly from the outer pipe section to have an inner diameter that is a same as, or smaller than, an inner diameter of the inner pipe section; and
wherein the first flange has an inner diameter that is a same as, or smaller than, the inner diameter of the inner pipe section.

2. The shrouded pipe assembly of claim 1 , wherein the inner and outer pipe sections are curved, such that the inner and outer pipe sections share a common curved longitudinal axis.

3. The shrouded pipe assembly of claim 1 , wherein the first flange and the inner pipe section are cast as a single inner pipe member and/or the second flange and the outer pipe section are cast as a single outer pipe member.

4. The shrouded pipe assembly of claim 3 , wherein the first flange extends radially away from the inner pipe section to have a diameter that is a same as, or greater than, a diameter of the outer pipe section, such that the inner pipe section is insertable through the outer pipe section only via the first end of the outer pipe section.

5. The shrouded pipe assembly of claim 1 , wherein the first flange is joined to the first end of the outer pipe section by a first circumferential joint and the second flange is joined to the second end of the inner pipe section by a second circumferential joint.

6. The shrouded pipe assembly of claim 5 , wherein the first and/or second circumferential joints comprise circumferential weld seams.

7. The shrouded pipe assembly of claim 1 , wherein the first flange and/or the second flange comprise one or more openings arranged to permit fluid flow from the secondary fluid path.

8. An aircraft fuel system comprising a shrouded pipe assembly according to claim 1 .

9. The aircraft fuel system according to claim 8 , wherein the primary fluid path is arranged to carry fuel and the secondary fluid path is arranged to provide one or more of: a fluid path for leaked fuel from the primary fluid path; a fluid path flowing in an opposite direction to the primary fluid path; and a fluid path for increasing or reducing heat exchange to or from the primary fluid path.

10. The aircraft fuel system according to claim 8 , wherein the first flange is joined to the first end of the outer pipe section by a first circumferential joint, the second flange is joined to the second end of the inner pipe section by a second circumferential joint, and the first and second circumferential joints comprise circumferential weld seams.

11. The aircraft fuel system according to claim 8 , wherein the inner and outer pipe sections are curved, such that the inner and outer pipe sections share a common curved longitudinal axis.

12. An aircraft fuel system comprising a pair of shrouded pipe assemblies according to claim 1 , wherein the first flange or second flange of one of the pair of the shrouded pipe assemblies extends between the secondary fluid path of that shrouded pipe assembly and the secondary fluid path of the other of the pair of shrouded pipe assemblies.

13. The aircraft fuel system according to claim 12 , wherein the pair of shrouded pipe assemblies are connected together by fasteners passing through first fastening projections extending radially outwardly from the first flange of one of the pair of shrouded pipe assemblies and through second fastening projections extending radially outwardly from the second flange of the other of the pair of shrouded pipe assemblies.

14. The aircraft fuel system according to claim 12 , wherein the first flange is joined to the first end of the outer pipe section by a first circumferential joint, the second flange is joined to the second end of the inner pipe section by a second circumferential joint, and the first and second circumferential joints comprise circumferential weld seams.

15. A method for producing a shrouded pipe assembly, the method comprising:
providing an inner pipe section, which comprises a primary fluid path, and a first flange, which is directly attached to and projects radially outwardly from a first end of the inner pipe section;
providing an outer pipe section and a second flange, which is directly attached to and projects radially inwardly from a second end of the outer pipe section;
enclosing the inner pipe section within the outer pipe section;
joining the first flange to the outer pipe section at a first end of the outer pipe section, such that the first flange is directly attached to both the inner pipe section, at the first end of the inner pipe section, and the outer pipe section, at the first end of the outer pipe section, to define a first radial gap between the inner and outer pipe sections at a first end of the shrouded pipe assembly; and
joining the second flange to the inner pipe section at a second end of the inner pipe section, such that the second flange is directly attached to both the inner pipe section, at the second end of the inner pipe section, and the outer pipe section, at the second end of the outer pipe section, to define a second radial gap between the inner and outer pipe sections at a second end of the shrouded pipe assembly;
wherein the first end of the inner pipe section is at an opposite end of the shrouded pipe assembly from the second end of the outer pipe section;
wherein an annular volume extends from the first radial gap to the second radial gap, between the inner and outer pipe sections to provide a secondary fluid path;
wherein the second flange is a continuous annular flange extending radially inwardly from the outer pipe section to have an inner diameter that is a same as, or smaller than, an inner diameter of the inner pipe section; and
wherein the first flange has an inner diameter that is a same as, or smaller than, the inner diameter of the inner pipe section.

16. The method according to claim 15 , wherein the inner pipe section and outer pipe section are curved such that the inner and outer pipe sections have a common curved longitudinal axis.

17. The method according to claim 15 , wherein enclosing the inner pipe section wit

Assignees

• Airbus Operations Gmbh

Inventors

• Rappitsch Michael
• Rauch Konrad
• Döring Jens
• Friedewald-Witte Dirk

Classifications

• F16L9/18

  Double-walled pipes; Multi-channel pipes or pipe assemblies · CPC title

• B64D37/005

  Accessories not provided for in the groups B64D37/02 - B64D37/28 · CPC title

• F16L9/19

  Multi-channel pipes or pipe assemblies · CPC title

• F16L39/005 Primary

  for concentric pipes · CPC title