Stator vane formed by a set of vane parts

Patent metadata

Field	Value
Publication number	US-10145253-B2
Application number	US-201314389433-A
Country	US
Kind code	B2
Filing date	Apr 4, 2013
Priority date	Apr 5, 2012
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

A stator vane for a turbine machine includes a set of vane parts arranged relative to each other to define air flow stream paths between vane parts, and a mechanism circulating a fluid to be cooled by the air flow.

First claim

The invention claimed is:

1. An outlet guide vane system comprising:
a stator vane for a turbine machine, the stator vane comprising
a set of at least two vane parts arranged relative to each other to define air flow stream paths between the at least two vane parts; and
means for circulating the fluid to be cooled by the air flow, the means for circulating being embedded in the at least two vane parts,

wherein the stator vane is an outlet guide vane of the outlet guide vane system,
wherein the at least two vane parts are arranged such that when observed in a plane orthogonal to the longitudinal direction of the stator vane, an aerodynamic profile of the stator vane is almost identical to an aerodynamic profile of a second, reference stator vane comprising a leading edge, a median section, and a trailing edge,
wherein the at least two vane parts comprises first, second, and third vane parts, the first and second vane parts combined defining the leading edge and the median section of the aerodynamic profile of the stator vane, the leading edge being formed by ends of the first and second vane parts, the third vane part defining the trailing edge of the aerodynamic profile of the stator vane, a downstream end of the first vane part being upstream of a downstream end of the second vane part, and the downstream end of the second vane part being upstream of a downstream end of the third vane part,
wherein the first vane part and the second vane part are superposed on each other to define a first separation therebetween forming a first air flow stream path, and the second vane part and the third vane part are superposed relative to each other to define a second separation therebetween forming a second air flow stream path,
wherein, for each of the first and second air flow stream paths, an inlet of the air flow stream path is further upstream than an outlet of the air flow stream path,
wherein the inlet of the first air flow stream path is at a furthest upstream portion of the stator vane, and
wherein the means for circulating the fluid to be cooled comprises fluid circulation pipes located on at least a portion of the at least two vane parts, a portion of the circulation pipes extending radially outside of the at least two vane parts.

2. The outlet guide vane system according to claim 1 , wherein at least one vane part has approximately a same aerodynamic profile as a lift surface.

3. The outlet guide vane system according to claim 1 , wherein the stator vane comprises one or plural support sections, distributed over a height of the vane, to mechanically retain the at least two vane parts to each other.

4. The outlet guide vane system according to claim 1 , wherein the means for circulating the fluid to be cooled comprises fluid flow channels formed on at least part of the stator vane covered by a cover plate defining an external surface of the at least two vane parts.

5. The outlet guide vane system according to claim 4 , wherein the fluid circulation pipes enable fluid distribution in the flow channels.

6. A turbine machine comprising an outlet guide vane system according to claim 1 .

7. The outlet guide vane system according to claim 1 , wherein the leading edge is formed by ends of the first and second vane parts.

8. The outlet guide vane system according to claim 1 , wherein the median section is thicker than the leading edge, and wherein the trailing edge is thinner than the leading edge.

Assignees

• Safran Aircraft Engines

Inventors

• Bordoni Nils

Classifications

• F05D2260/20

  Heat transfer, e.g. cooling · CPC title

• Y02T50/676

  Cross-Sectional Technologies · mapped topic

• F05D2260/213

  by the provision of a heat exchanger within the cooling circuit · CPC title

• F01D25/04

  Antivibration arrangements · CPC title

• F05D2260/22141

  using fins or ribs · CPC title