Granted Patent B2

US 12,370,737 · App. 18/253,369 · Granted Jul 29, 2025

Inventors: Daniel Perherin (Saint-Nazaire, FR); Daniel Boulze (Aussonne, FR); Nicolas Hallak (Colomiers, FR)

Assignee: AIRBUS ATLANTIC

B29C53/083B29C70/20B29D23/006F16L9/133F16L43/008B29K2071/00B29K2105/0881B29L2023/22B29L2031/243B29L2031/3076

Abstract

Claims (16)

1. A method of manufacturing a pipe intended to be mounted in a fluid circuit of an aircraft, the pipe comprising a tube and two connection ends, the tube being made of thermoplastic material and having a cylindrical shape, the tube defining an internal surface, intended to be in contact with the fluid, and an external surface opposite the internal surface, the manufacturing method, comprising:

a step of determining at least two portions to be reinforced of the tube,

a step of determining at least one portion to be bent, the portion to be bent being positioned between the at least two portions to be reinforced,

a step of positioning at least one reinforcement band extending longitudinally over the external surface of the at least two portions to be reinforced, the portion to be bent being free of the reinforcement band, then

a step of bending the portion to be bent.

2. The method of manufacturing according to claim 1 , wherein the reinforcement band comprises reinforcement fibers impregnated with a thermoplastic resin.

3. The method of manufacturing according to claim 2 , wherein the thermoplastic resin of the reinforcement band is identical to the thermoplastic material of the tube.

4. The method of manufacturing according to claim 3 , wherein the thermoplastic resin of the reinforcement band and the tube is polyaryletherketone.

5. The method of manufacturing according to claim 2 , wherein the reinforcement fibers are unidirectional fibers.

6. The method of manufacturing according to claim 1 , wherein, in a cross-sectional plane, the reinforcement band(s) extend over an angular range of between 28 and 58° at the periphery of the reinforced portion.

7. The method of manufacturing according to claim 1 , wherein the reinforced portion comprises at least three reinforcement bands distributed angularly over the external surface of the reinforced portion and positioned equidistant from each other.

8. The method of manufacturing according to claim 1 , wherein the reinforcement band has a thickness of between 0.1 and 0.4 mm.

9. A method of manufacturing a pipe for use on an aircraft, the pipe comprising a thermoplastic cylindrical tube section having two connection ends, the tube section having an internal surface and an external surface opposite the internal surface, the manufacturing method, comprising:

positioning one or more reinforcement bands over the external surface of the tube section at two spaced apart portions of the tube section to define two spaced apart portions of the tube section to be reinforced in a positioning step;

bending a portion of the tube section at a location between the two spaced apart portions of the tube section to be reinforced to define a bent section in a bending step; and

wherein the bent section is free of the one or more reinforcement bands and is formed after the positioning step.

Assignments (2)

Priority Claims (1)

Continuity (1)

References Cited (11)