IP Library › Granted Patent US 10,941,667
Granted Patent B2
US 10,941,667 · App. 16/174,553 · Granted Mar 9, 2021

Modulation of vane end serrations

Inventors: Claire Marie Figeureu (Moissy Cramayel, FR); Eric Pierre Georges Lemarechal (Moissy Cramayel, FR); Benjamin Bulot (Moissy Cramayel, FR); Mathieu Simon Paul Gruber (Moissy Cramayel, FR); Raphael Barrier (Paris, FR); Cyril Polacsek (Clamart, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
F01D9/041F01D5/141F04D29/544F04D29/667F04D29/681F01D5/148F01D5/282F01D25/162F05D2200/221F05D2200/24F05D2200/26F05D2220/36F05D2240/121F05D2250/182F05D2250/183F05D2250/184
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Quick Facts
Patent No.
US 10,941,667
App. No.
16/174,553
Granted
Mar 9, 2021
Kind
B2
Abstract

A stator vane including a vane root, a vane tip, a leading edge extending between the root and the tip, the leading edge having a serrated profile having a succession of teeth and of troughs each having an amplitude and a thickness, wherein a series of at least three teeth and three consecutive troughs starting from the vane root and/or from the vane tip have a growing amplitude and/or thickness.

Claims (30)

1. An outlet guide vane comprising:

a vane root configured to be attached to a hub;

a vane tip configured to be attached to a casing; and

a leading edge extending between the vane root and the vane tip, the leading edge having a serrated profile having a succession of teeth and of troughs each having an amplitude and a thickness,

wherein the serrated profile includes a series of at least three teeth and three consecutive troughs starting from at least one of the vane root or the vane tip, the series having at least one of an amplitude or a thickness of the teeth and of the troughs that follows a growing function, the growing function being a linear, parabolic, sinusoidal, or exponential function.

2. The outlet guide vane according to claim 1 , wherein the series comprises at least four teeth and four troughs or extends between 20 and 50% of a length of the outlet guide vane.

3. The outlet guide vane according to claim 1 , wherein the serrated profile follows a sinusoidal.

4. The outlet guide vane according to claim 1 , wherein the serrated profile follows the following function:

c ( r )= c 0 +h ·sin(2π r /λ)

wherein c 0 is a reference chord, h is an amplitude and λ is a wavelength of undulations and r is a radius

and wherein, within the series, at least one of the amplitude or the thickness of the teeth and of the troughs follows a linear function so that the serrated profile follows within said series the following function:

c ( r )= c 0 +h ·sin(2π r /λ)· K·r

where K is a constant,

or

wherein within the series, at least one of the amplitude or the thickness of the teeth and of the troughs follows a parabolic function so that the serrated profile follows within said series the following function:

c ( r )= c 0 +h ·sin(2π r /λ)· L·r 2

L is a constant,

or

wherein, within the series, at least one of the amplitude or the thickness of the teeth and of the troughs follows a sinusoidal function so that the serrated profile follows within said series the following function:

c ( r )= c 0 +h ·sin(2π r /λ)·sin( Mπ/ 2· r )

where M is a constant,

or

wherein, within the series, at least one of the amplitude or the thickness of the teeth and of the troughs follows an exponential function so that the serrated profile follows within said series the following function:

c ( r )= c 0 +h ·sin(2π r /λ)·exp( N·r )

where N is a constant.

5. The outlet guide vane according to claim 1 , wherein the outlet guide vane is made of composite material.

6. The outlet guide vane according to claim 1 , wherein the amplitude of the first trough or of the first tooth from the vane tip or from the vane root of the outlet guide vane is nonzero.

7. A straightener ring comprising a plurality of outlet guide vanes according to claim 1 , the outlet guide vanes being distributed circumferentially around a hub.

8. A turbomachine or test bed comprising an outlet guide vane according to claim 1 .

9. The outlet guide vane according to claim 1 , wherein an entire length of the leading edge includes the serrated profile.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 4, 2018
From: FIGEUREU, CLAIRE MARIE; LEMARECHAL, ERIC PIERRE GEORGES; BULOT, BENJAMIN; GRUBER, MATHIEU SIMON PAUL; BARRIER, RAPHAEL; POLACSEK, CYRIL
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 047670/0446 →
Priority Claims (1)
FR 1760212 · Oct 30, 2017 · national
Continuity (1)
Related Publication 20190170003A1 · Jun 6, 2019
Cited By (3)
US 12,497,934 US 12,612,883 US 12,698,747