IP Library Granted Patent US 9,817,923
Granted Patent B2
US 9,817,923 · App. 14/358,551 · Granted Nov 14, 2017

Part made from 3D woven composite material

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Quick Facts
Patent No.
US 9,817,923
App. No.
14/358,551
Granted
Nov 14, 2017
Kind
B2
Abstract

A method designing a part made of 3D woven composite material, performed by a computer, the method including: obtaining shape data representing an outside surface of the part; for each point of a set of points of the outside surface, determining a distance between the point and a projection of the point onto a target surface, the projection being along a predetermined projection direction; determining a structure of a 3D woven preform as a function of the determined distances; and obtaining projection data specifying a projection direction as a function of a position of a point on the outside surface of the part, wherein the projection direction that is used for at least some of the points of the set of points is determined during the determining a distance, as a function of the projection and as a function of the position of the point.

Claims (30)

1. A method of designing a part made of three-dimensional (3D) woven composite material, the design method being performed by a computer, the method comprising:

obtaining shape data representing an outside surface of the part;

selecting a set of points of the outside surface of the part;

for each point of the set of points of the outside surface of the part, obtaining projection data specifying a projection direction as a function of a position of the point along a height axis of the part;

for each point of the set of points of the outside surface of the part, determining whether a type of point is to be projected along a normal direction;

in response to the type of point being a point to be projected along the normal direction, projecting the point in the normal direction to the target surface;

otherwise, projecting the point along a direction as specified in a file;

for each point of the set of points of the outside surface of the part, determining a distance between the point and a projection of the point onto a target surface along the obtained projection direction, said determined distances forming a determined thickness field representing a thickness of the part; and

determining a structure of a 3D woven preform as a function of the determined distances and the determined type of point, comprising determining a number of layers and exit position of layers of the preform as a function of said target surface and said determined thickness field.

2. A design method according to claim 1 , wherein the projection data specify the projection direction as a function of the position of the point along the height axis of the part and depending on a position along a width axis of the part.

3. A design method according to claim 1 , wherein the target surface is a mean profile of the part.

4. A design method according to claim 1 , wherein the outside surface of the part includes a first face and a second face opposite to the first face, the set of points being a set of points of the first face and the target surface being the second face.

5. A design method according to claim 1 , wherein, for at least some of the points of the set of points, during the determining a distance, the projection direction that is used is a direction normal to the target surface.

6. A design method according to claim 1 , wherein the determining the structure of a 3D woven preform comprises:

calculating the target surface laid flat; and

determining the number of layers and exit positions for layers as a function of the calculated flat surface, as a function of the determined distances, and as a function of target weaving parameters.

7. A design method according to claim 1 , further comprising:

fabricating a prototype of the part; and

storing the projection data as a function of deformations observed in the prototype.

8. A non-transitory computer readable medium including a computer program including instructions for executing a design method according to claim 1 when executed by a computer.

9. A device for designing a part made out of three-dimensional (3D) woven composite material, the device comprising:

means for obtaining shape data representing an outside surface of the part;

means for selecting a set of points of the outside surface of the part;

means for obtaining, for each point of the set of points of the outside surface of the part, projection data specifying a projection direction as a function of a position of the point along a height axis of the part;

means for determining, for each point of the set of points of the outside surface of the part, whether a type of point is to be projected along a normal direction;

means for projecting the point in the normal direction to the target surface, in response to the type of point being a point to be projected along the normal direction;

means for projecting the point along a direction as specified in a file, if the point is not the type of point to be projected along the normal direction; and

structure determination means for determining a surface of a 3D woven preform as a function of the determined distances and the determined type of point, comprising determining a number of layers and exit positions of layers of the preform as a function of said target surface and said determined thickness field.

10. A design method according to claim 1 , wherein the target surface is a mean profile defined as center of circles inscribed in a volume of the part made of the 3D woven composite material.

11. A device according to claim 9 , wherein the target surface is a mean profile defined as center of circles inscribed in a volume of the part made of the 3D woven composite material.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 15, 2014
From: MARCHAL, YANN; MAHIEU, JEAN-NOEL
To: SNECMA
Reel/Frame 032904/0686 →