Method of measuring the thickness of a fiber texture wound onto an impregnation mandrel, and a winder machine implementing such a method

Patent metadata

Field	Value
Publication number	US-10345094-B2
Application number	US-201414786724-A
Country	US
Kind code	B2
Filing date	Apr 22, 2014
Priority date	Apr 26, 2013
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A method of measuring the thickness of a fiber texture wound on an impregnation mandrel for fabricating an annular structural part of a turbine engine out of composite material, the method including, prior to winding the fiber texture, acquiring a reference distance between an outside surface of the impregnation mandrel and a distance sensor positioned facing the outside surface of the impregnation mandrel, while winding the fiber texture, acquiring at least one real distance between the distance sensor and the outside surface of the fiber texture wound on the impregnation mandrel, and calculating the real thickness of the fiber texture wound on the impregnation mandrel by subtracting the real distance from the reference distance.

First claim

The invention claimed is:

1. A method of measuring a thickness of a fiber texture wound on an impregnation mandrel for fabricating an annular structural part of a turbine engine out of composite material, the method comprising:
prior to winding the fiber texture on the impregnation mandrel, acquiring a reference distance between an outside surface of the impregnation mandrel and a distance sensor positioned facing said outside surface of the impregnation mandrel;
while winding the fiber texture on the impregnation mandrel, acquiring at least one real distance between the distance sensor and the outside surface of the fiber texture wound on impregnation mandrel; and
calculating a real thickness of the fiber texture wound on the impregnation mandrel by subtracting the real distance from the reference distance,
wherein the real thickness of the fiber texture wound on the impregnation mandrel is calculated while taking account of the impregnation mandrel bending.

2. A method according to claim 1 , wherein the reference distance and the real distance are averages calculated from measurements taken by at least three distance sensors positioned facing the outside surface of the impregnation mandrel and in alignment along an axis parallel to an axis of rotation of the impregnation mandrel.

3. A method according to claim 1 , wherein the reference distance and the real distance comprise independent values obtained from measurements taken by at least three distance sensors positioned facing the outside surface the impregnation mandrel and in alignment along an axis parallel to an axis of rotation of the impregnation mandrel.

4. A method according to claim 1 , wherein the acquiring of at least one real distance comprises acquiring a plurality of real distances at different instants during the winding of the fiber texture on the impregnation mandrel.

5. A method according to claim 1 , wherein the reference distance is an average calculated for a plurality of distance values between the outside surface of the impregnation mandrel and the distance sensor as acquired over one complete revolution of the impregnation mandrel.

6. A method according to claim 1 , wherein the real thickness of the fiber texture is compared with a predetermined theoretical thickness value.

7. A winder machine for winding a fiber texture on an impregnation mandrel in order to fabricate an annular turbine engine part out of composite material, the machine comprising:
a takeup mandrel for storing a fiber texture, the takeup mandrel having a substantially horizontal axis of rotation;
an impregnation mandrel onto which superposed layers of the fiber texture stored on the takeup mandrel are to be wound, the impregnation mandrel having a substantially horizontal axis of rotation that is parallel to the axis of rotation of the takeup mandrel;
electric motors for driving each of the mandrels in rotation about its respective axis of rotation;
a control unit for controlling the electric motors for driving the mandrels in rotation;
at least one distance sensor positioned facing an outside surface of the impregnation mandrel;
a computer system for calculating a real thickness of the fiber texture wound on the impregnation mandrel by subtracting a real distance from a reference distance, wherein the reference distance is acquired, prior to winding the fiber texture on the impregnation mandrel, between the outside surface of the impregnation mandrel and the distance sensor positioned facing said outside surface of the impregnation mandrel and wherein, while winding the fiber texture on the impregnation mandrel, the real distance is acquired between the distance sensor and the outside surface of the fiber texture wound on impregnation mandrel, and
additional distance sensors positioned facing cheekplates of the impregnation mandrel in order to measure possible bending thereof.

8. A machine according to claim 7 , comprising three distance sensors positioned facing the outside surface of the impregnation mandrel and in alignment along an axis parallel to the axis of rotation of the impregnation mandrel.

9. A machine according to claim 7 , wherein the distance sensor is fastened on a retractable arm that is mounted on a stand.

10. A machine according to claim 7 , wherein the distance sensor is a laser sensor.

11. A method of measuring a thickness of a fiber texture wound on an impregnation mandrel for fabricating an annular structural part of a turbine engine out of composite material, the method comprising:
prior to winding the fiber texture on the impregnation mandrel, acquiring a reference distance between an outside surface of the impregnation mandrel and a distance sensor positioned facing said outside surface of the impregnation mandrel;
while winding the fiber texture on the impregnation mandrel, acquiring at least one real distance between the distance sensor and the outside surface of the fiber texture wound on impregnation mandrel; and
calculating a real thickness of the fiber texture wound on the impregnation mandrel by subtracting the real distance from the reference distance,
wherein the reference distance is an average calculated for a plurality of distance values between the outside surface of the impregnation mandrel and the distance sensor as acquired over one complete revolution of the impregnation mandrel.

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Corradini Sylvain
• Mathon Richard
• Durand Jean-François

Classifications

• B29K2101/00

  Use of unspecified macromolecular compounds as moulding material {(use of unspecified rubbers B29K2021/00)} · CPC title

• B29C45/0005

  using fibre reinforcements · CPC title

• B29L2022/00

  Hollow articles (tubular articles B29L2023/00; pneumatic tyres B29L2030/00) · CPC title

• B29K2105/10

  Cords, strands or rovings, e.g.} oriented {cords, strands or rovings · CPC title

• B29C53/8041

  Measuring, controlling or regulating (B29C53/665 takes precedence) · CPC title