Instrumented flow passage of a turbine engine

Patent metadata

Field	Value
Publication number	US-9856743-B2
Application number	US-201514722877-A
Country	US
Kind code	B2
Filing date	May 27, 2015
Priority date	May 28, 2014
Publication date	Jan 2, 2018
Grant date	Jan 2, 2018

Abstract

An annular air flow passage for a turbine engine such as a turbojet or a turboprop, crossed by an instrumented rod that includes mechanism(s) for measuring characteristics of a flow potentially traveling along the passage, the rod extending between an outer annular wall and an inner annular wall of the passage. Outer connection(s) fasten(s) an outer end of the instrumented rod to the outer wall in a manner that is rigid in all directions, and inner connection(s) fasten(s) an inner end of the instrumented rod to the inner wall, in a manner that is rigid in the circumferential direction and that has at least one degree of freedom to move in a first direction extending between the inner and outer walls of the passage and having at least a radial component.

First claim

The invention claimed is:

1. An annular air flow passage for a turbine engine, the passage comprising:
an instrumented rod that crosses it and measures characteristics of a flow traveling along the passage, said rod extending between an outer annular wall and an inner annular wall of the passage, the passage being characterized in that outer connection means fasten an outer end of the instrumented rod to the outer wall rigidly in all directions, and inner connection means fasten an inner end of the instrumented rod to the inner wall rigidly in the circumferential direction of the passage and with at least one degree of freedom to move in a first given direction extending between the inner and outer walls of the passage,
wherein at least a radial component is present along the first given direction, and
wherein the inner connection means fasten the inner end of the instrumented rod to the inner wall with a degree of freedom to move in a second given direction substantially perpendicular to the first given direction.

2. A passage according to claim 1 , wherein a shoe and the inner end of the instrumented rod are engaged relative to each and configured to slide in at least said first given direction.

3. A passage according to claim 2 , wherein the shoe comprises a first shoe portion and a second shoe portion that are secured to each other and that define a housing in which the inner end of the rod is configured to move at least in said first given direction.

4. A passage according to claim 3 , wherein the housing is defined by a downstream lug extending outwards from the second shoe portion and by a U-shaped recess that is open in the downstream direction in the first shoe portion.

5. A passage according to claim 4 , wherein the second shoe portion is L-shaped with an axial wall carrying the downstream lug extending between the first shoe portion and the inner wall.

6. A passage according to claim 5 , wherein the axial wall of the second shoe portion is engaged axially in an axial groove in an inner face of the first shoe portion.

7. A passage according to claim 6 , wherein the thickness of said axial wall is greater than the depth of said axial groove.

8. A passage according to claim 3 , wherein the inner end of the rod is mounted with clearance relative to the second shoe portion.

9. A passage according to claim 2 , wherein at least one through orifice is formed in the inner end of the instrumented rod and is aligned in the circumferential direction with at least one through orifice in the shoe, a locking member being engaged through the at least one through orifice in the shoe and the at least one through orifice in the inner end of the instrumented rod.

10. A passage according to claim 9 , wherein the section of the at least one orifice in the shoe is contained within the section of the at least one orifice in the inner end of the rod.

11. A passage according to claim 10 , wherein said at least one orifice in the shoe or in the inner end of the rod is of oblong shape, being elongate in alignment with the instrumented rod.

12. A passage according to claim 9 , wherein the locking member engaged through the orifices in the shoe and the inner end of the rod is a self-locking bolt configured so as to avoid clamping the shoe against the instrumented rod.

13. A passage according to claim 1 , wherein a shoe is fastened rigidly to a first shroud forming the inner wall of the passage, said shroud being arranged downstream from an annular row of stationary vanes extending across the passage and upstream from a perforated second shroud for bleeding air, and wherein the outer end of the rod is fastened relative to the outer wall downstream from said row of stationary vanes.

14. A passage according to claim 13 , wherein the shoe has a downstream portion arranged axially facing the perforated second shroud and radially at a distance therefrom, the shoe being fastened to the inner end of the rod at said downstream portion.

15. A passage according to claim 1 , wherein the inner end of the instrumented rod is situated upstream relative to the outer end of the instrumented rod.

16. A passage according to claim 1 , wherein a spacer is mounted between the outer end of the instrumented rod and the outer wall of the passage.

17. A turbine engine comprising a passage according to claim 1 .

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Kockenpo Florian
• Acquaviva Jermone
• Corbin Claude Gaston
• Giordan Jeremy
• Seigneuret Nicolas
• Lamarche Nicolas

Classifications

• F01D17/08 Primary

  responsive to condition of working-fluid, e.g. pressure · CPC title

• F01D9/065

  Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids (see also F01D25/16, F01D25/24 and F01D25/26) · CPC title

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title

• F01D17/02

  Arrangement of sensing elements · CPC title

• F01D17/085

  to temperature · CPC title