Lobed tubular piece made of a composite with unidirectional fibers

Patent metadata

Field	Value
Publication number	US-11472133-B2
Application number	US-202016785979-A
Country	US
Kind code	B2
Filing date	Feb 10, 2020
Priority date	Aug 10, 2017
Publication date	Oct 18, 2022
Grant date	Oct 18, 2022

Abstract

A method for manufacturing a fibrous tubular structure including lobes, in which fibers are draped/deposited on a mandrel having a shape corresponding to that of the fibrous structure, includes draping/deposition carried out such that at least one group of fibers has a same orientation with respect to the axis (A) of said fibrous structure, then, the fibers having been draped over an angular sector less than the total periphery of the mandrel, one of the ends of the fibrous structure is separated from the mandrel in order to allow the continuation of the draping on the same mandrel.

First claim

What is claimed is:

1. A method for manufacturing a tubular fibrous structure with lobes, the method comprising:
drape-molding/depositing fibers on a mandrel having a shape corresponding to that of the tubular fibrous structure, the drape-molding/depositing being performed so that at least one group of fibers has a same orientation with respect to a longitudinal axis (A) of said tubular fibrous structure,
wherein fibers from the at least one group of fibers are drape-molded/deposited over an angular sector smaller than a total periphery of the mandrel to form a discrete segment of fibers on the angular sector, an end of the fibrous structure being separated from the mandrel in order to enable further drape-molding on the mandrel and formation of the tubular fibrous structure with lobes.

2. The method according to claim 1 , wherein a circumference of the mandrel corresponds to a shape of a portion of a fibrous structure comprising an area of revolution and an area forming at least two lobes.

3. The method according to claim 1 , wherein the mandrel has a reduced shape corresponding, or fitting, to that of a portion of a final piece over a predetermined angular sector.

4. The method for manufacturing according to claim 1 , wherein prior to drape-molding/depositing the fibers on the mandrel, a separation film is wound on the mandrel.

5. The method for manufacturing according to claim 4 , wherein the separation film is separated from the mandrel at a same time as the tubular fibrous structure on which the separation film is supported.

6. The method for manufacturing according to claim 1 further comprising:
impregnating the fibers by a matrix in the form of a unidirectional ribbon of fibers before the drape-molding/depositing; and
after final winding of the fibers onto a tubular shape, curing by polymerization, or in the case of ceramic matrices by sintering or densification.

7. The method for according to claim 6 , wherein the impregnation with the matrix occurs after the drape-molding/depositing over the tubular shape,
wherein fibers embedded in a preform are in a resin adapted to be cured by polymerization.

8. The method for manufacturing according to claim 6 , wherein a material forming the matrix is an organic matrix or a ceramic matrix.

9. The method for manufacturing according to claim 1 , wherein a composite piece obtained from the tubular fibrous structure has an open portion, in which an angular sector is missing.

10. The method for manufacturing according to claim 1 , further comprising separating the end of the fibrous structure from the mandrel and drape-molding/depositing another group of fibers onto the mandrel.

11. The method for manufacturing according to claim 1 , further comprising drape-molding/depositing fibers from the at least one group of fibers to form at least one of the lobes of the tubular fibrous structure.

Assignees

• Safran Nacelles

Inventors

• Desjoyeaux Bertrand
• Silva De Vasconcellos Davi
• Provost Benjamin

Classifications

• B29B11/16

  comprising fillers or reinforcement {(non-woven fabrics per se D04H1/00, D04H3/00)} · CPC title

• C04B35/76

  Fibres, filaments, whiskers, platelets, or the like · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• C04B35/80

  Fibres, filaments, whiskers, platelets, or the like · CPC title

• F02K1/44

  Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction (F02K1/40 takes precedence) · CPC title