Flow guiding device and method for forming a flow guiding device

Patent metadata

Field	Value
Publication number	US-10954885-B2
Application number	US-201815970034-A
Country	US
Kind code	B2
Filing date	May 3, 2018
Priority date	May 5, 2017
Publication date	Mar 23, 2021
Grant date	Mar 23, 2021

Abstract

A flow guiding appliance of a turbomachine, in particular of an aircraft engine, for a partial exit flow of an outlet guide vane of a compressor, wherein, a flow guiding element delimits an annular channel about a shaft of the turbomachine. A frictional engagement connecting surface at the circumference of the flow guiding element connects the flow guiding element to another structural component of the turbomachine. The frictional engagement connecting surface with a closed enveloping surface can be inserted in a deformed state into the structural component with a circular cylindrical sealing surface with at least two opposite points. The at least two points of the closed enveloping surface are arranged in at least two opposite frictionally engaged contact areas of the circular cylindrical sealing surface following deformation. The invention also relates to a method for creating a flow guiding element.

First claim

The invention claimed is:

1. A flow guiding appliance of a turbomachine for a partial flow of an exit flow of an outlet guide wheel of a compressor of the turbomachine, comprising:
a flow guiding element delimiting an annular channel about a shaft of the turbomachine,
a frictional engagement connecting surface at the circumference of the flow guiding element for connecting the flow guiding element to a separate structural component of the turbomachine, where the structural component includes a circular cylindrical sealing surface,
wherein the frictional engagement connecting surface includes a closed enveloping surface including an elliptical cross section with two contact points positioned respectively at opposite ends of a major axis of the closed enveloping surface, the closed enveloping surface being deformable to be positioned within the circular cylindrical sealing surface such that in an assembled state, the two contact Diets frictionally engage two opposite contact areas of the circular cylindrical sealing surface.

2. The flow guiding appliance according to claim 1 , wherein the elliptical cross section has an eccentricity of between 0.95 and 0.999.

3. The flow guiding appliance according to claim 1 , wherein the frictional engagement connecting surface has a diameter tolerance of +/−0.3 mm.

4. The flow guiding appliance according to claim 1 , wherein the circular cylindrical sealing surface has a diameter tolerance of +/−0.1 mm.

5. The flow guiding appliance according to claim 1 , wherein the annular channel at least partially has at least one chosen from a constant radial height, a convergent part, and a divergent part.

6. The flow guiding appliance according to claim 1 , wherein, in the assembled state, there are two gaps between the closed enveloping surface and the circular cylindrical sealing surface.

7. The flow guiding appliance according to claim 6 , wherein a greatest radial width of the two gaps is less than 0.5 mm.

8. The flow guiding appliance according to claim 6 , wherein a greatest radial width of the two gaps is less than 0.3 mm.

9. The flow guiding appliance according to claim 6 , wherein a greatest radial width of the two gaps is less than 0.2 mm.

10. The flow guiding appliance according to claim 1 , wherein the flow guiding element is made of a nickel alloy.

11. A turbomachine, comprising the flow guiding appliance and the structural component according to claim 1 .

12. The turbomachine according to claim 11 , wherein the turbomachine includes a high pressure compressor, an outlet guide vane of the high-pressure compressor and a combustion chamber, and the flow guiding appliance extends axially from the outlet guide vane up to a central area of the combustion chamber.

13. The flow guiding appliance according to claim 1 , wherein the elliptical cross section has an eccentricity of between 0.99 and 0.996.

14. A method for attaching a flow guiding appliance to a turbomachine, comprising:
providing:
a turbomachine, comprising:
a compressor including an outlet guide wheel;
a structural component including a circular cylindrical sealing surface,

a flow guide applicaince for a partial flow of an exit flow of the outlet guide wheel, the flow guiding appliance comprising:
a flow guiding element for delimiting an annular channel about a shaft of the turbomachine,
a frictional engagement connecting surface at a circumference of the flow guiding element for positioning within the circular cylindrical sealing surface,
wherein the flow guiding appliance initially includes a circular cylindrical molded body at the frictional engagement connecting surface,

using a forming tool with a non-circular cross section to give the frictional engagement connecting surface an elliptical cross section with two contact points positioned respectively at opposite ends of a major axis of the frictional engagement connecting surface,
deforming the frictional engagement connecting surface to fit within the cylindrical sealing surface,
inserting the flow guiding element in the deformed state into the circular cylindrical sealing surface such that the two contact points frictionally engage two opposite contact areas of the circular cylindrical sealing surface.

15. A turbomachine, comprising:
a compressor including an outlet guide wheel;
a structural component including a circular cylindrical sealing surface,
a flow guiding appliance for a partial flow of an exit flow of the outlet guide wheel, the flow guiding appliance comprising:
a flow guiding element delimiting an annular channel about a shaft of the turbomachine,
a frictional engagement connecting surface at a circumference of the flow guiding element positioned within the circular cylindrical sealing surface,

wherein the frictional engagement connecting surface includes a closed enveloping surface that is non-circular to form two opposite contact points frictionally engaging two opposite contact areas of the circular cylindrical sealing surface, and two gaps between the closed enveloping surface and the circular cylindrical sealing surface, the two gaps respectively positioned circumferentially between the two opposite contact areas.

16. The turbomachine according to claim 15 , wherein:
the turbomachine further comprises a combustion chamber;
the compressor is a high pressure compressor, and
the flow guiding appliance extends axially from the outlet guide vane up to a central area of the combustion chamber.

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Sikorski Igor
• Phillips Jason

Classifications

• F01D25/243

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• F01D5/084 Primary

  the fluid circulating at the periphery of a multistage rotor, e.g. of drum type · CPC title

• F02C7/18

  the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

• F02F7/0085

  Materials for constructing engines or their parts · CPC title

• F02C3/00

  Gas-turbine plants characterised by the use of combustion products as the working fluid (generated by intermittent combustion F02C5/00) · CPC title