Assembly device for double-skinned aircraft fuel pipes

Patent metadata

Field	Value
Publication number	US-9546623-B2
Application number	US-201514598336-A
Country	US
Kind code	B2
Filing date	Jan 16, 2015
Priority date	Feb 5, 2014
Publication date	Jan 17, 2017
Grant date	Jan 17, 2017

Abstract

An assembly device between two sections of a double-skinned fuel pipe of an aircraft has a clamp for assembling the internal pipes, a coupling device for assembling the external pipes, a fitting extending between the ends of the external pipes of the first and second sections, with a shape complementary to the shape of an internal portion of the coupling device, and such that its section through any cutting plane perpendicular to the longitudinal axis common to the coupling device and the external pipes contains the smallest surface delimited by: a line corresponding to the intersection of the internal surface of the coupling device with this cutting plane and a straight line cutting said line at two points, this straight line being tangential to the orthogonal projection in this cutting plane, of the internal surface of the external pipes of the first or of the second section.

First claim

The invention claimed is:

1. An assembly device between a first section and a second section of a doubleskinned fuel pipe of an aircraft, said device comprising:
a clamp allowing one end of an internal pipe of the first section to be assembled with one end of an internal pipe of the second section;
a coupling device allowing one end of an external pipe of the first section to be assembled with one end of the external pipe of the second section; and
a fitting extending between the end of the external pipe of the first section and the end of the external pipe of the second section
and having a shape complementary to the shape of an internal portion of the coupling device,
wherein, when the first section and the second section of the fuel pipe are assembled by the assembly device, the section of the fitting through any cutting plane perpendicular to a longitudinal axis common to the coupling device, the external pipe of the first section and the external pipe of the second section contains the smallest surface delimited by:
a line corresponding to the intersection of the internal surface of the coupling device with the cutting plane and,
a straight line cutting said line at two points, the straight line being tangential to the orthogonal projection in the cutting plane, of the internal surface of the external pipe of the first section or of the external pipe of the second section.

2. The assembly device as claimed in claim 1 wherein the fitting has a first recess configured for containing at least part of a fixing integral with one of the internal pipes of the first section or of the second section.

3. The assembly device as claimed in claim 1 wherein the fitting has a second recess configured for containing part of said clamp.

4. The assembly device as claimed in claim 1 wherein the fitting is made of fluoro silicone.

5. The assembly device as claimed in claim 1 wherein the fitting is made of foam.

6. The assembly device as claimed in claim 5 wherein said foam is rigid polymethacrylimide foam.

7. A double-skinned fuel pipe of an aircraft comprising an assembly device comprising:
a clamp allowing one end of an internal pipe of the first section to be assembled with one end of an internal pipe of the second section;
a coupling device allowing one end of an external pipe of the first section to be assembled with one end of the external pipe of the second section; and
a fitting extending between the end of the external pipe of the first section and the end of the external pipe of the second section and having a shape complementary to the shape of an internal portion of the coupling device,
wherein, when the first section and the second section of the fuel pipe are assembled by the assembly device, the section of the fitting through any cutting plane perpendicular to a longitudinal axis common to the coupling device, the external pipe of the first section and the external pipe of the second section contains the smallest surface delimited by:
a line corresponding to the intersection of the internal surface of the coupling device with the cutting plane and,
a straight line cutting said line at two points, the straight line being tangential to the orthogonal projection in the cutting plane, of the internal surface of the external pipe of the first section or of the external pipe of the second section.

8. An aircraft having a double-skinned fuel pipe comprising an assembly device comprising:
a clamp allowing one end of an internal pipe of the first section to be assembled with one end of an internal pipe of the second section;
a coupling device allowing one end of an external pipe of the first section to be assembled with one end of the external pipe of the second section; and
a fitting extending between the end of the external pipe of the first section and the end of the external pipe of the second section and having a shape complementary to the shape of an internal portion of the coupling device,
wherein, when the first section and the second section of the fuel pipe are assembled by the assembly device, the section of the fitting through any cutting plane perpendicular to a longitudinal axis common to the coupling device, the external pipe of the first section and the external pipe of the second section contains the smallest surface delimited by:
a line corresponding to the intersection of the internal surface of the coupling device with the cutting plane and,
a straight line cutting said line at two points, the straight line being tangential to the orthogonal projection in the cutting plane, of the internal surface of the external pipe of the first section or of the external pipe of the second section.

Assignees

• Airbus Operations Sas

Inventors

• Fraysse Damien
• Gagnaire Thierry

Classifications

• B64D37/14

  Filling or emptying (transferring fuels to adjust aircraft trim B64C17/10) · CPC title

• F16L39/005

  for concentric pipes · CPC title

• B64D37/32

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• B64D37/005

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

• F16L39/00

  Joints or fittings for double-walled or multi-channel pipes or pipe assemblies {(quick-acting joints for double-walled or multi-channel pipes or pipe assemblies F16L37/56)} · CPC title