IP Library Granted Patent US 10,019,549
Granted Patent B2
US 10,019,549 · App. 14/863,871 · Granted Jul 10, 2018

Method of designing a common preform for providing preforms for turbine engine outlet guide vanes of different geometrical profiles and made out of composite material

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,019,549
App. No.
14/863,871
Granted
Jul 10, 2018
Kind
B2
Abstract

A method of designing a common preform for providing a plurality of preforms for turbine engine outlet guide vanes of different geometrical profiles and made out of composite material, the method including 3D geometrical modeling of the geometrical profiles of the different outlet guide vane preforms, flattening out each of the geometrical profiles of the different outlet guide vane preforms, superposing the geometrical profiles of the different flattened outlet guide vane preforms, and converging towards a single geometrical profile for an outlet guide vane preform common to all of the outlet guide vane preforms while guaranteeing identical positioning for the top and bottom regions of non-interlinking for all of the outlet guide vane preforms.

Claims (11)

1. A method for manufacturing a turbine engine outlet guide vane wheel comprising a plurality of outlet guide vanes made out of composite material, wherein the outlet guide vanes have different geometrical profiles, the method comprising:

designing a common outlet guide vane preform for outlet guide vane providing a plurality of preforms for outlet guide vanes of different geometrical profiles and made out of composite material, the designing being implemented on at least one machine having one or more processors executing machine-readable instructions from a tangible and non-transitory memory, the common preform being made from a single-piece woven fiber structure obtained by three-dimensional weaving, said fiber structure having first and second portions, each comprising a plurality of layers of yarns and each forming a fraction of the thickness of the fiber structure, the portions of the fiber structure being interlinked while leaving top and bottom regions of non-interlinking separating the first and second portions over respective fractions of the dimension of the fiber structure from opposite edges of the fiber structure, the designing comprising:

3D geometrical modeling, by one or more processors of the at least one machine, of the geometrical profiles of the different outlet guide vane preforms;

flattening, by one or more processors of the at least one machine, out each of the geometrical profiles of the different outlet guide vane preforms;

superposing, by one or more processors of the at least one machine, the geometrical profiles of the different flattened outlet guide vane preforms; and

converging, by one or more processors of the at least one machine, towards a single geometrical profile for an outlet guide vane preform common to all of the outlet guide vane preforms while guaranteeing identical positioning for the top and bottom regions of non-interlinking for all of the outlet guide vane preforms; and

manufacturing the plurality of the outlet guide vanes from said common outlet guide vane preform.

2. A method according to claim 1 , wherein the converging towards a single geometrical profile is performed by limiting the framing differences between the different geometrical profiles for outlet guide vane preforms.

3. A method according to claim 1 , wherein the converging towards a single geometrical profile is performed by limiting thickness differences between the different geometrical profiles for the outlet guide vane preforms.

4. A method according to claim 2 , wherein the framing differences between the different geometrical profiles for outlet guide vane preforms do not exceed 10° between the various geometrical profiles.

5. A method according to claim 1 , wherein the manufacturing includes densifying the common outlet guide vane preform with a matrix.

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 Sep 24, 2015
From: GIMAT, MATTHIEU; COUPE, DOMINIQUE MARIE CHRISTIAN; MAHIEU, JEAN-NOËL; MARCHAL, YANN DIDIER SIMON
To: SNECMA; SAFRAN
Reel/Frame 036647/0729 →