Auxiliary power units and other turbomachines having ported impeller shroud recirculation systems

Patent metadata

Field	Value
Publication number	US-9377030-B2
Application number	US-201313853951-A
Country	US
Kind code	B2
Filing date	Mar 29, 2013
Priority date	Mar 29, 2013
Publication date	Jun 28, 2016
Grant date	Jun 28, 2016

Abstract

Embodiments of a turbomachine, such as a gas turbine engine, are provided. In one embodiment, the turbomachine includes an impeller, a main intake plenum in fluid communication with the inlet of the impeller, and an impeller shroud recirculation system. The impeller shroud recirculation system includes an impeller shroud extending around at least a portion of the impeller and having a shroud port therein. A shroud port cover circumscribes at least a portion of the shroud port and cooperates therewith to at least partially define an impeller recirculation flow path. The impeller recirculation flow path has an outlet positioned to discharge airflow into the main intake plenum at a location radially outboard of the shroud port when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine.

First claim

What is claimed is:

1. A turbomachine, comprising:
an impeller having an inlet and a rotational axis;
a main intake plenum in fluid communication with the inlet of the impeller;
an impeller shroud recirculation system, comprising:
an impeller shroud extending around at least a portion of the impeller and having a shroud port therein;
a shroud port cover circumscribing at least a portion of the shroud port; and
an impeller recirculation flow path defined, at least in part, by the shroud port cover and the impeller shroud, the impeller recirculation flow path having an outlet positioned to discharge airflow into the main intake plenum at a location radially outboard of the shroud port when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine;

wherein the impeller recirculation flow path further comprises a radially-extending diffuser section fluidly coupled between the shroud port and the main intake plenum, the radially-extending diffuser section extending in essentially a radial direction away from the rotational axis from a point radially inboard of the impeller to a point radially outboard thereof.

2. The turbomachine of claim 1 wherein the distance between the outlet of the impeller recirculation flow path and the rotational axis of the impeller is substantially equivalent to or greater than one half the maximum outer diameter of the impeller.

3. The turbomachine of claim 1 wherein the radially-extending diffuser section is at least partially defined by the shroud port cover.

4. The turbomachine of claim 1 wherein the radially-extending diffuser section has a flow passage width W 1 , and wherein the outlet of the impeller recirculation flow path includes a bellmouth having a radius R 1 less than width W 1 .

5. The turbomachine of claim 1 wherein the impeller shroud recirculation system further comprises a plurality of de-swirl vanes positioned within the radially-extending diffuser section and angularly spaced about the rotational axis of the impeller.

6. The turbomachine of claim 1 further comprising an intake housing assembly defining the main intake plenum, the outlet of the impeller recirculation flow path recessed within the intake housing assembly.

7. The turbomachine of claim 1 wherein the impeller recirculation flow path has an angled outlet region configured to discharge airflow into the main intake plenum in an aftward direction when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine.

8. The turbomachine of claim 1 further comprising a bellmouth structure upstream of the impeller, the bellmouth structure extending between impeller shroud and the shroud port cover.

9. The turbomachine of claim 1 wherein the shroud port cover comprises a trailing flange, and wherein the turbomachine further comprise a wall axially spaced from the trailing flange to define at least a portion of the radially-extending diffuser section.

10. The turbomachine of claim 1 wherein the impeller recirculation flow path further comprises an annular recirculation plenum fluidly at least partially defined by the shroud port cover and coupled between the radially-extending diffuser section and the main intake plenum.

11. The turbomachine of claim 10 wherein the annular recirculation plenum circumscribes at least a portion of the impeller port shroud.

12. The turbomachine of claim 10 wherein the shroud port cover comprises:
an outer plenum wall; and
a trailing flange extending radially from the outer plenum wall.

13. The turbomachine of claim 12 wherein the outer plenum wall bounds the outer circumference of the shroud port cover, and wherein the trailing flange bounds a leading face of the radially-extending diffuser section.

14. The turbomachine of claim 1 further comprising a tubular perforated plate fluidly coupled between the main intake plenum and the inlet of the impeller.

15. The turbomachine of claim 14 wherein the outlet of the impeller recirculation flow path is positioned radially inboard of and radially adjacent to the tubular perforated plate.

16. The turbomachine of claim 14 wherein the outlet of the impeller recirculation flow path is positioned radially outboard of the tubular perforated plate.

17. The turbomachine of claim 16 wherein an aft end portion of the tubular perforated plate is disposed axially adjacent an aft end portion of the shroud port cover.

18. A turbomachine, comprising:
an impeller;
an impeller shroud extending around at least a portion of the impeller and having a shroud port therein;
a shroud port cover disposed around the impeller shroud and separated therefrom by a radial gap;
an impeller recirculation flow path at least partially defined by the impeller shroud and the shroud port cover, the impeller recirculation flow path discharging airflow upstream of the impeller when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine;
wherein the impeller recirculation flow path comprises a radially-elongated diffuser section extending away from the rotational axis of the impeller in a radial direction to reduce the circumferential velocity component of airflow bled from the impeller prior to discharge of the airflow upstream of the impeller;
wherein the radially-elongated diffuser section is located between the shroud port and the trailing end of the impeller, as taken along the rotational axis of the impeller; and
wherein the radially-elongated diffuser section comprises an outlet located radially outboard of the impeller.

19. A turbomachine, comprising:
an intake housing assembly containing a main intake plenum and having a sidewall partially bounding the main intake plenum;
an impeller having an inlet in fluid communication with the main intake plenum;
an impeller shroud extending around at least a portion of the impeller and having a shroud port therein; and
an impeller recirculation flow path having an inlet fluidly coupled to the shroud port and having an outlet recessed within the sidewall of the intake housing assembly, the impeller recirculation flow path configured to discharge airflow into the main intake plenum at a location radially outboard of the shroud port when pressurized air flows from the impeller, through the shroud port, and into the impeller recirculation flow path during operation of the turbomachine;
wherein the impeller recirculation flow path further comprises a radially-extending diffuser section fluidly coupled between the shroud port and the main intake plenum, the radially-extending diffuser section extending in essentially a radial direction away from a rotational axis of the impeller from a point radially inboard of the impeller to a point radially outboard thereof.

20. The turbomachine of claim 19 wherein the impeller recirculation flow path comprises a diffuser section that is elongated in a radial direction and that is also recessed within the sidewall of the intake housing assembly.

Assignees

• Honeywell Int Inc

Inventors

• Matwey Mark
• Mansour Mahmoud
• Sheoran Yogendra Y

Classifications

• F04D29/444

  Bladed diffusers · CPC title

• F04D27/0207

  by bleeding, bypassing or recycling fluids (influencing the boundary layer by an uncontrolled bleeding of the working fluid F04D29/681) · CPC title

• F04D29/441

  especially adapted for elastic fluid pumps · CPC title

• F04D29/682

  by fluid extraction · CPC title

• F05D2250/51

  Inlet · CPC title