Distributor device for cooling air within an engine

Patent metadata

Field	Value
Publication number	US-9920643-B2
Application number	US-201514696806-A
Country	US
Kind code	B2
Filing date	Apr 27, 2015
Priority date	May 14, 2014
Publication date	Mar 20, 2018
Grant date	Mar 20, 2018

Abstract

A distributor device for distributing cooling air within a gas turbine engine, the device including a base mountable adjacent an inlet for air to be distributed; and a deflector supported by the base and in fluid communication with the air inlet, the deflector being configured to direct air from the air inlet in a plurality of directions within the engine; wherein the deflector includes one or more deflecting surfaces curvilinearly configured to direct the air differentially in a plurality of desired directions within the engine. In embodiments the deflecting surface(s) is/are curved and are so configured such that air from the air inlet is directable either: (i) in directions of travel in each of a plurality of desired different, non-parallel directions within the engine; or (ii) in each of a plurality of desired different directions within the engine with different flow rates.

First claim

The invention claimed is:

1. A distributor device for distributing cooling air within a gas turbine engine, the device comprising:
a base mountable adjacent an inlet for air to be distributed; and
a deflector supported by the base via a spine which is located within the air inlet and in fluid communication with the air inlet, the deflector being configured to direct air from the air inlet in a plurality of directions within the engine;
wherein the deflector comprises one or more deflecting surfaces curvilinearly configured to direct the said air differentially in a plurality of desired directions within the engine,
wherein the base comprises a tubular support which is mounted within a mouth of the or the respective air inlet, and the spine is supported within the tubular support by virtue of being mounted thereon via one or more support elements which extend between an inner surface of the tubular support and spine to provide a passage for a flow of cooling air from the inlet between the spine and tubular support and on to the curvilinearly configured deflecting surfaces of the deflector.

2. The distributor device according to claim 1 , wherein the deflector comprises one or more deflecting surfaces curvilinearly configured to direct air in each of a plurality of desired different, non-parallel directions of travel.

3. The distributor device according to claim 2 , wherein the one or more curvilinearly configured deflecting surfaces of the deflector is/are curved in at least two planes which are non-parallel to one another, said planes being defined as (i) each being generally parallel to the direction of air flow from the or the respective air inlet and incident on the deflecting surface(s), and (ii) being angled with respect to one another at an angle of between 0° and 180° .

4. The distributor device according to claim 1 , wherein a said deflecting surface has a uniform curvature or curve function substantially completely through 360° therearound, whereby air is directable substantially uniformly or equally in all directions therearound.

5. The distributor device according to claim 1 , wherein the one or more support elements include one or more brackets, webs, ribs, vanes, struts, or arms.

6. The distributor device according to claim 5 , wherein the deflector comprises a central or axial spine constituting an anchoring portion onto which the plurality of support elements are mounted or attached, and from which the deflecting surface(s) of the deflector extend(s) with a gap between the said deflecting surface(s) and the tubular support for allowing passage therethrough of air undergoing distribution or directing having impinged on the or the deflecting surface(s).

7. The distributor device according to claim 5 , wherein:
(i) a plurality of said brackets, webs, ribs, vanes, struts, arms or other support elements are substantially uniformly aligned with each other and all generally substantially parallel to the direction of flow of air from the air inlet towards and onto the deflecting surface(s) of the deflector; or
(ii) a plurality of said brackets, webs, ribs, vanes, struts, arms or other discrete support elements each have a helical configuration.

8. The gas turbine engine comprising:
a space for distribution therewithin of cooling air;
at least one air inlet for delivering cooling air into the space; and a distributor device for distributing cooling air within a gas turbine engine, the device comprising:
a base mountable adjacent an inlet for air to be distributed; and
a deflector supported by the base via a spine which is located within the air inlet and in fluid communication with the air inlet, the deflector being configured to direct air from the air inlet in a plurality of directions within the engine;
wherein the deflector comprises one or more deflecting surfaces curvilinearly configured to direct the said air differentially in a plurality of desired directions within the engine,
wherein the base comprises a tubular support which is mounted within a mouth of the or the respective air inlet, and the spine is supported within the tubular support by virtue of being mounted thereon via one or more support elements which extend between an inner surface of the tubular support and spine to provide a passage for a flow of cooling air from the inlet between the spine and tubular support and on to the curvilinearly configured deflecting surfaces of the deflector.

9. The distributor device for distributing cooling air within a gas turbine engine, the device comprising:
a base mountable adjacent an inlet for air to be distributed; and
a deflector supported adjacent the inlet via a spine which is at least partially located within the air inlet and in fluid communication with the air inlet, the deflector being configured to direct air from the air inlet in a plurality of directions within the engine;
wherein the deflector comprises one or more deflecting surfaces curvilinearly configured to direct the said air differentially in a plurality of desired directions within the engine,
wherein the base comprises a tubular support which is mounted within a mouth of the or the respective air inlet, and the spine is supported within the tubular support by virtue of being mounted thereon via one or more support elements which extend between an inner surface of the tubular support and spine to provide a passage for a flow of cooling air from the inlet between the spine and tubular support and on to the curvilinearly configured deflecting surfaces of the deflector.

10. The distributor device as claimed in claim 9 , wherein the spine extends from a central portion of the deflector into the inlet.

11. The distributor device as claimed in claim 9 , wherein the spine includes an anchoring portion onto which the one or more support elements are mounted or attached, and from which the deflecting surface(s) of the deflector extend(s) with a gap between the said deflecting surface(s) and the inlet for allowing passage therethrough of air undergoing distribution or directing having impinged on the or the deflecting surface(s).

12. The distributor device as claimed in claim 11 , wherein the support elements include one or more of brackets, webs, ribs, vanes, struts, arms or other discrete support elements.

13. The distributor device as claimed in claim 12 , wherein the support elements are substantially aligned with each other and are generally parallel to the direction of flow of air from the air inlet towards and onto the deflecting surface(s) of the deflector.

Assignees

• Rolls Royce Plc

Inventors

• Manzoori Reza
• Balsdon Julian Glyn

Classifications

• F01D11/24

  by selectively cooling-heating stator or rotor components · CPC title

• F02C7/18

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

• F01D9/06 Primary

  Fluid supply conduits to nozzles or the like · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F01D9/065 Primary

  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