Flow guiding system, turbo engine with a flow guiding system and method for manufacturing a flow guiding system

Patent metadata

Field	Value
Publication number	US-9719424-B2
Application number	US-201414584242-A
Country	US
Kind code	B2
Filing date	Dec 29, 2014
Priority date	Dec 31, 2013
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

The invention relates to a flow guiding system for a turbo engine, in particular an aircraft engine, characterized by an air intake device taking a thermal management air stream from a free flowing air stream during the operation of the turbo engine and at least one flow guiding means for guiding the thermal management air stream to at least one target region to be thermally managed in the turbo engine. The invention also relates to a turbo engine with a flow guiding system and a method for manufacturing a flow guiding system.

First claim

The invention claimed is:

1. A flow guiding system for an aircraft turbo engine, comprising:
an air intake device including an inlet, an outlet and an enclosed passage between the inlet and the outlet, the inlet being connected to a free flowing air stream during operation of the turbo engine to direct a thermal management air stream from the free flowing air stream, the outlet being positioned in a chamber of the turbo engine,
a flow guiding device positioned in the chamber spaced apart from the outlet,
wherein the flow guiding device comprises a guide surface,
the outlet being oriented toward the flow guiding device so that an axis of flow of the thermal management air stream at the outlet is directed toward the guide surface, and the guide surface is oriented such that the axis of flow is deflected by the guide surface toward a target device in the chamber, such that the thermal management air stream impacts the guide surface and is deflected toward the target device,
wherein the guide surface is at least one chosen from flat, at least partially flat and at least partially curved.

2. The flow guiding system according to claim 1 , wherein the thermal management air stream is a cooling air stream or a heating air stream.

3. The flow guiding system according to claim 1 , wherein the free flowing air stream comprises at least one chosen from a bypass stream in a turbofan engine, an air stream taken from a core of the turbo engine and an ambient air stream outside the turbo engine.

4. The flow guiding system according to claim 1 , wherein the guide surface includes a triangular base plate and lateral guide plates.

5. The flow guiding system according to claim 4 , wherein the axis of flow is directed onto an apex of the triangular base plate so that the thermal management air stream is diffused towards the target device.

6. The flow guiding system according to claim 1 , wherein the flow guiding device is integrated into at least one chosen from a part of a surface of a core part of a turbofan engine and a casing radially outside a bypass duct of a turbofan engine.

7. The flow guiding system according to claim 1 , wherein the target device includes at least one chosen from an electronic device, a coated section of the turbo engine, a bearing, a core casing, a connector, a plastic part, an actuator for vanes in the turbo engine, a movable part in the turbo engine, a fuel line, an oil line, and a seal of the turbo engine.

8. The flow guiding system according to claim 1 , wherein at least one chosen from the air intake device and the guide surface is movable to adjust deflection of the axis of flow and the thermal management air stream.

9. The flow guiding system according to claim 8 , and further comprising a control system configured to measure an operating parameter from at least one chosen from shaft speed, an outside temperature, a temperature in a bypass duct, a temperature within a core engine, a temperature in a casing of the turbo engine, a strain measurement from the target device or outside the turbo engine, and the control system is configured to control, based on the operating parameter, at least one chosen from movement of the air intake device, movement of the guide surface and a shape of the guide surface for adjusting the thermal management air flow to achieve a predetermined thermal management target.

10. The flow guiding system according to claim 1 , wherein at least one chosen from the air intake device and the flow guiding device is formed from one piece of metal sheet.

11. The flow guiding system according to claim 1 , wherein the air intake device protrudes into the free flowing air stream or is recessed from the free flowing air stream.

12. A aircraft turbo engine, including the flow guiding system according to claim 1 .

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Teia Dos Santos Mendes Gomes Luis Daniel

Classifications

• F01D25/12

  Cooling · CPC title

• F02C7/04

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

• F02C7/042

  having variable geometry · CPC title

• F02C7/14

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title

• F05D2260/209

  using vortex tubes · CPC title