Undulating stator for reducing the noise produced by interaction with a rotor

Patent metadata

Field	Value
Publication number	US-10358938-B2
Application number	US-201514790964-A
Country	US
Kind code	B2
Filing date	Jul 2, 2015
Priority date	Jul 3, 2014
Publication date	Jul 23, 2019
Grant date	Jul 23, 2019

Abstract

A stator designed to be placed radially in a flow which passes through one or more rotors which share the same axis of rotation, with a leading edge and a trailing edge. The leading edge and trailing edge are connected by a lower face and an upper face, wherein at least one of the faces of the stator has radial undulations which extend axially from the leading edge to the trailing edge. The radial undulations can have at least two bosses in the same azimuth direction, the amplitude of which is at least one centimeter on at least part of the axial length of the stator. A propulsion assembly formed by the rotor and the stator, and to a turbine engine comprising such assembly is also provided.

First claim

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:

1. An assembly comprising a rotor having an axis of rotation, and a stator which is placed radially in a flow which passes through said rotor, said stator being placed upstream or downstream of said rotor, said stator having an inner structure forming a core extending radially and a skin surrounding the inner structure, said skin having a leading edge and a trailing edge, said leading edge and trailing edge being connected by a lower face and an upper face, wherein said leading edge and trailing edge have radial undulations and at least one of the lower and upper faces of said skin has radial undulations which extend axially from the leading edge to the trailing edge to form an undulated surface, said radial undulations having at least two bosses in the same azimuth direction, an amplitude of said radial undulations being at least one centimeter on at least part of an axial length of the stator, said stator being configured to create pressure fluctuations on said undulated surface when the flow interacts with said undulated surface, said pressure fluctuations having temporal phase oscillations according to a radial position, said radial undulations of said undulated surface having azimuth maximums and/or minimums in a vicinity of zero mean dephasing regions for pressure on said undulating surface.

2. The assembly according to claim 1 , wherein the radial undulations have a wavelength which is substantially constant along a radial extension of the stator.

3. The assembly according to claim 1 , wherein the amplitude of the radial undulations is maintained as more than one centimeter from the leading edge to the trailing edge.

4. The assembly according to claim 1 , wherein the lower face and the upper face have the radial undulations.

5. The assembly according to claim 4 , wherein the radial undulations of the upper and lower faces are radially in phase.

6. The assembly according to claim 1 , wherein the core is designed to ensure a mechanical strength of said stator, and the skin forms the radial undulations on said at least one of the lower and upper faces.

7. The assembly according to claim 1 , wherein the radial undulations are propagated axially along mean current lines in said flow.

8. A turbine engine comprising an assembly according to claim 1 , wherein a ring of fixed guide vanes forms said stator.

9. A method for reducing the noise radiated by an assembly comprising a rotor having an axis of rotation, and a stator, the method comprising:
placing the stator radially in a flow which passes through said rotor and upstream or downstream of said rotor, said stator having a leading edge and a trailing edge, said leading edge and trailing edge being connected by a lower face and an upper face, said flow creating on at least one of said lower and upper faces pressure fluctuations with temporal phase oscillations according to a radial position, wherein radial undulations are provided on said trailing edge and leading edge, and on said at least one of the lower and upper faces which extend axially from the leading edge to the trailing edge, said radial undulations having at least two bosses in the same azimuth direction, an amplitude of said radial undulations being at least one centimeter on at least part of an axial length of the stator, with azimuth maximums and/or minimums in a vicinity of zero mean dephasing regions for pressure on said at least one of the lower and upper faces.

10. The assembly according to claim 1 , wherein the amplitude of said radial undulations is less than ten centimeters.

11. A method for reducing the noise radiated by an assembly comprising a rotor having an axis of rotation, and a stator, the method comprising:
placing the stator radially in a flow which passes through said rotor and upstream or downstream of said rotor, said stator having a leading edge and a trailing edge, said leading edge and trailing edge being connected by a lower face and an upper face;
providing radial undulations on at least one of the lower and upper faces of said stator, said radial undulations extending axially from the leading edge to the trailing edge to form an undulated surface and having at least two bosses and peaks in the same azimuth direction, an amplitude of said radial undulations being at least one centimeter on at least part of an axial length of the stator;
determining isophase curves on at least one of the lower and upper faces of said stator and from an inner radially edge and an outer radial edge of said undulated surface, each isophase curve delimiting a pressure fluctuation phase on said undulated surface; and
placing each boss and/or peak between two isophase curves which form zero mean dephasing regions for pressure on said undulated surface such that each pressure fluctuation phase has temporal phase oscillations according to a position of the boss and/or peak when the flow interacts with said undulated surface.

12. The method of according to claim 11 , wherein the trailing edge and the leading edge have radial undulations.

13. A turbine engine having an axis of rotation, the turbine engine comprising:
a fan and a stator, said stator being placed radially in a flow which passes through said fan, said stator being placed upstream or downstream of said fan, said stator having an inner structure forming a core extending radially and a skin surrounding the inner structure, said skin having a leading edge and a trailing edge, said leading edge and trailing edge being connected by a lower face and an upper face, wherein said leading edge and trailing edge have radial undulations and at least one of the lower and upper faces of said stator has radial undulations which extend axially from the leading edge to the trailing edge to form an undulated surface, said radial undulations having at least two bosses in the same azimuth direction, an amplitude of said radial undulations being at least one centimeter on at least part of an axial length of the stator, said stator being configured to create pressure fluctuations on said undulated surface when the flow interacts with said undulated surface, said pressure fluctuations having temporal phase oscillations according to a radial position, said radial undulations of said undulated surface having azimuth maximums and/or minimums in a vicinity of zero mean dephasing regions for pressure on said undulating surface.

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Romano Pascal Jérôme
• Jodet Norman Bruno André

Classifications

• F05D2240/122

  related to the trailing edge of a stator vane · CPC title

• F04D29/681

  especially adapted for elastic fluid pumps · CPC title

• F05D2240/123

  related to the pressure side of a stator vane · CPC title

• F05D2260/961

  by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape · CPC title

• F05D2240/121

  related to the leading edge of a stator vane · CPC title