Turbomachine blade, in particular a fan blade, and its method of manufacture

• US 20050084377A1
• Filed: 10/18/2004
• Published: 04/21/2005
• Est. Priority Date: 10/20/2003
• Status: Active Grant

• Current Assignee: Safran Aircraft Engine Company
• Original Assignee: Snecma Moteurs
• Inventors: Dambrine, Bruno, Coupe, Dominique, Molinari, Olivier
• Granted Patent: US 7,101,154 B2
• Time in Patent Office: Days
• US Class Current: 416/223.R
• CPC Class Codes: B29B 11/16 comprising fillers or reinforcement non-woven fabrics per se D04H1/00, D04H3/00
• CPC Class Codes: B29C 70/24 oriented in at least three directions forming a three dimensional structure
• CPC Class Codes: B29C 70/48 and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] , e.g. by vacuum
• CPC Class Codes: D03D 25/005 Three-dimensional woven fabrics
• CPC Class Codes: F01D 5/282 Selecting composite materials, e.g. blades with reinforcing filaments
• CPC Class Codes: F04D 29/023 especially adapted for elastic fluid pumps
• CPC Class Codes: F04D 29/324 Blades
• CPC Class Codes: F05D 2300/6012 Woven fabrics
• CPC Class Codes: F05D 2300/603 Composites; e.g. fibre-reinforced
• CPC Class Codes: F05D 2300/614 Fibres or filaments
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 29/49336 Blade making
• CPC Class Codes: Y10T 29/49337 Composite blade
• CPC Class Codes: Y10T 442/3195 Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]

Abstract

The composite turbomachine blade of the present invention comprises a preform made of yarns or fibers woven in three dimensions and a binder maintaining the relative disposition between the yarns of the preform. Said preform is made up of warp yarns and of weft yarns, the direction of the warp yarns forming the longitudinal direction of the preform. In characteristic manner, said preform comprises at least a first portion made using a first weave forming the airfoil of the blade, and a second portion made using a second weave forming the root of the blade, and the first and second portions are united by a transition zone in which the first weave is progressively modified to end up with the second weave, thereby obtaining a reduction at least in the thickness of the blade between the second portion and the first portion. The invention is applicable to making a fan blade for a turbojet.

Claims

1. A composite turbomachine blade comprising a preform of yarns or fibers woven in three dimensions and a binder maintaining the relative disposition between the yarns of the preform, said preform being made up of warp yarns and of weft yarns, the direction of the warp yarns forming the longitudinal direction of the preform, wherein said preform comprises at least a first portion made with a first weave and forming the airfoil of the blade, and a second portion made using a second weave and forming the root of the blade, and wherein the first portion and the second portion are united by a transition zone in which the first weave is progressively modified to end up with the second weave, thereby obtaining a reduction at least in the thickness of the blade between the second portion and the first portion.

2. A blade according to claim 1, wherein said first portion and said second portion do not present the same number of warp yarns.

3. A blade according to claim 1, wherein said yarns or fibers belong to the group constituted by carbon fibers, glass fibers, silica fibers, silicon carbide fibers, aluminum fibers, aramid fibers, and aromatic polyamide fibers.

4. A blade according to claim 1, wherein the shrinkage angle of the warp yarns lies in the range 2°

to 10°

.

5. A blade according to claim 1, wherein said first portion and said second portion present different warp/weft volume ratios.

6. A blade according to claim 5, wherein said first portion presents a warp/weft volume ratio lying in the range 80/20% to 50/50%, and wherein said second portion presents a warp/weft volume ratio lying in the range 30/70% to 50/50%.

7. A blade according to claim 1, wherein the count of the warp yarns varies between the edge and the remainder of the blade, the warp yarns at the edge being finer.

8. A blade according to claim 7, wherein the count of the warp yarns at the edge of the blade is about 900 tex and wherein the count of the warp yarns in the remainder of the blade is about 1800 tex.

9. A blade according to claim 1, wherein the first weave presents a base pattern comprising firstly at least thirty-six weft yarns disposed in a staggered configuration of columns having at least four weft yarns superposed in a vertical direction and spaced apart in a longitudinal direction by a step size, alternating with columns of at least five superposed weft yarns, the columns being separated by the same step size, the weft yarns being distributed in at least eight columns extending in a vertical direction, the weft yarns thus being disposed on at least nine levels, and secondly at least twenty-four warp yarns disposed in at least eight vertical planes that are parallel to one another in a transverse direction alternating between planes of a first type containing at least four superposed parallel warp yarns, and planes of a second type containing at least three superposed parallel warp yarns, said planes of a first type having:

a first warp yarn connecting a top end weft yarn of a column of at least five weft yarns to the upper intermediate weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two steps, and returning onto a top end weft yarn) of a column of at least five weft yarns, spaced apart from the first column by at least four steps,

a second warp yarn connecting an upper intermediate weft yarn of a column of at least five weft yarns to the middle weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two steps, and returning onto an upper intermediate weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least four steps,

a third warp yarn connecting a middle weft yarn of a column of at least five weft yarns to the lower intermediate weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two steps, and returning onto a middle weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least four steps,

a fourth warp yarn connecting a lower intermediate weft yarn of a column of at least five weft yarns to the bottom end weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two steps, and returning onto a lower intermediate weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least four steps,

said planes of a second type having;

a first warp yarn connecting a top end weft yarn of a column of at least four weft yarns to the upper intermediate weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two steps, and returning onto a top end weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least four steps,

a second warp yarn connecting an upper intermediate weft yarn of a column of at least four weft yarns to the lower intermediate weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two steps, and returning onto an upper intermediate weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least four steps,

a third warp yarn connecting a lower intermediate weft yarn of a column of at least four weft yarns to the bottom end weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two steps, and returning onto a lower intermediate weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least four steps.

10. A blade according to claim 1, wherein the second weave presents a base pattern comprising firstly at least forty-five weft yarns disposed in a staggered configuration of columns of at least four weft yarns superposed in a vertical direction, the columns being separated in a longitudinal direction by a step size, and being in a staggered configuration relative to columns of at least five superposed weft yarns, the columns being separated by the same step size, the weft yarns being distributed in at least ten columns extending in a vertical direction, the weft yarns thus being disposed on at least nine levels, and secondly at least forty warp yarns disposed in at least ten vertical planes that are parallel to one another in a transverse direction, each plane containing at least four superposed parallel warp yarns with alternating planes of a first type and planes of a second type, said planes of a first type having:

a first warp yarn connecting a top end weft yarn of a column of at least five weft yarns to the top end weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a top end weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least five steps,

a second warp yarn connecting an upper intermediate weft yarn of a column of at least five weft yarns to the upper intermediate weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto an upper intermediate weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least five steps,

a third warp yarn connecting a middle weft yarn of a column of at least five weft yarns to the lower intermediate weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a middle weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least five steps,

a fourth warp yarn connecting a lower intermediate weft yarn of a column of at least five weft yarns to the bottom end weft yarn of a column of at least four weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a lower intermediate weft yarn of a column of at least five weft yarns, spaced apart from the first column by at least five steps,

said planes of a second type having;

a first warp yarn connecting a top end weft yarn of a column of at least four weft yarns to the upper intermediate weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a top end weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least five steps,

a second warp yarn connecting an upper intermediate weft yarn of a column of at least four weft yarns to the middle weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto an upper intermediate weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least five steps,

a third warp yarn connecting a lower intermediate weft yarn of a column of at least four weft yarns to the lower intermediate weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a lower intermediate weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least five steps,

a fourth warp yarn connecting a bottom end weft yarn of a column of at least four weft yarns to the bottom end weft yarn of a column of at least five weft yarns spaced apart from the preceding column by at least two and a half steps, and returning onto a bottom end weft yarn of a column of at least four weft yarns, spaced apart from the first column by at least five steps, the parallel groups of four warp yarns being offset longitudinally by a step of the same size as the step from one plane to the adjacent plane.

11. A blade according to claim 1, wherein the second portion of the blade presents a core zone with weft yarns that are larger, having a count that is different from that of the weft yarns surrounding said core zone.

12. A blade according to claim 11, wherein the count of the weft yarns in the core zone of the second portion of the blade is about 3600 tex and wherein the count of the weft yarns surrounding said core zone is about 1800 tex.

13. A blade according to claim 1, wherein said binder belongs to the group formed by organic resins, refractory substances, and metals.

14. A blade according to claim 1, constituting a fan blade for a turbojet.

15. A method of manufacturing a fan blade for a turbojet, the method comprising the following steps:

weaving warp yarns and weft yarns so as to form a preform of yarns or fibers that is woven in three dimensions, being made up of warp yarns and weft yarns, the direction of the warp yarns forming the longitudinal direction of the preform, said preform including at least a first portion made with a first weave and a second portion made with a second weave, said first portion and said second portion being united by a transition zone in which the first weave is progressively modified to end up with the second weave, thereby obtaining a reduction at least in the thickness of the blade between the second portion and the first portion;

cutting said preform to the shape and dimensions of the component portions of the blade;

providing a mold in which said preform is placed;

injecting a binder into said mold in order to impregnate the entire preform, the binder comprising a thermosetting resin;

heating said mold; and

extracting a molded part from the mold.