Endwall plug cooling system

Patent metadata

Field	Value
Publication number	US-2023193781-A1
Application number	US-202117556524-A
Country	US
Kind code	A1
Filing date	Dec 20, 2021
Priority date	Dec 20, 2021
Publication date	Jun 22, 2023
Grant date	—

Abstract

A cooling system includes a nozzle guide vane endwall. The nozzle guide vane endwall includes a first wall and a second wall. The first wall includes a first opening that extends completely through the first wall into a primary flow path of a high-pressure turbine. The second wall includes a second opening that extends completely through the second wall into an inner passageway of the nozzle guide vane endwall. The inner passageway is configured to direct a cooling fluid to the first opening and/or the second opening. The first and second opening are configured to receive a plug or a probe.

First claim

What is claimed is:

1 . A cooling system, comprising:
a nozzle guide vane endwall, comprising:
a first wall comprising a first opening that extends completely through the first wall into a primary flow path of a high-pressure turbine, and
a second wall comprising a second opening that extends completely through the second wall into an inner passageway of the nozzle guide vane endwall, wherein
the inner passageway is configured to direct a cooling fluid to the first opening and/or the second opening, and
the first and second opening are configured to receive a plug or a probe.

2 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein
the plug or the probe substantially seals the second opening.

3 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein
the plug or the probe only partially seals the first opening.

4 . The cooling system of claim 1 , wherein
the first opening and the second opening together form a borescope port.

5 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein
the inner passageway is configured to direct the cooling fluid to strike the plug or the probe in a direction substantially perpendicular to a longitudinal axis of the plug or the probe to provide impingement cooling of the plug or the probe.

6 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein
the first opening is configured to direct the cooling fluid substantially parallel to a longitudinal axis of the plug or the probe to provide film cooling of the plug or the probe.

7 . The cooling system of claim 1 , wherein
the inner passageway is a first inner passageway; and the cooling system further comprises:
the plug or the probe disposed in the first opening and the second opening, and
a second inner passageway, wherein
with respect to the primary flow path, the second inner passageway is disposed downstream of the first inner passageway; and
the second inner passageway is configured to direct a second portion of the cooling fluid to strike the plug or the probe in a second direction substantially opposite to a first direction in which the first inner passageway directs a first portion of the cooling fluid.

8 . The cooling system of claim 1 , wherein the inner passageway comprises a pedestal and/or dam configured to divert and/or reflect the cooling fluid.

9 . The cooling system of claim 1 , wherein
the first and second walls form a portion of the inner passageway; and the first wall provides a barrier between the inner passageway and the primary flow path.

10 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein a gap is between the plug or the probe and the first wall within the first opening.

11 . The cooling system of claim 10 , wherein
the gap extends only partially around a circumference of the plug or the probe within the first opening and a remaining portion of the circumference of the plug or the probe within the first opening is substantially sealed to the first wall.

12 . The cooling system of claim 11 , wherein
the gap between the plug or the probe and the first wall within the first opening is configured to receive the cooling fluid from the inner passageway.

13 . The cooling system of claim 1 , further comprising:
the plug or the probe disposed in the first opening and the second opening, wherein
the first opening and the plug or the probe are configured to together direct the cooling fluid toward the primary flow path.

14 . The cooling system of claim 1 , wherein
the inner passageway is a first inner passageway; and the cooling system further comprises:
the plug or the probe disposed in the first opening and the second opening, and
a second inner passageway, wherein
with respect to the primary flow path, the second inner passageway is disposed downstream of the plug or the probe and the first inner passageway.

15 . A cooling system, comprising:
a nozzle guide vane endwall including:
a first wall comprising a first opening that extends completely through the first wall into a primary flow path of a turbine,
a second wall comprising a second opening that extends completely through the second wall into an inner passageway of the nozzle guide vane endwall, wherein
a center of the first opening is aligned with a center of the second opening,
the inner passageway is formed by the first wall and the second wall,
the inner passageway is configured to direct a cooling fluid to the first opening, and
the inner passageway comprises a pedestal and/or dam arranged to direct the cooling fluid toward the first opening; and

a plug or a probe disposed in the first opening and the second opening, wherein
the plug or the probe substantially fills the second opening of the second wall, and
a gap is between the first wall and the plug or the probe.

16 . The cooling system of claim 15 , wherein
the inner passageway is a first inner passageway; and the cooling system further comprises:
a second inner passageway, wherein
with respect to the primary flow path, the second inner passageway is disposed downstream of the plug or the probe and the first inner passageway.

17 . The cooling system of claim 16 , wherein
the second inner passageway is configured to direct a second portion of the cooling fluid to strike the plug or the probe in a second direction substantially opposite to a direction in which the first inner passageway directs a first portion of the cooling fluid.

18 . The cooling system of claim 15 , wherein
the first opening and the second opening form a borescope port.

19 . The cooling system of claim 15 , wherein
the inner passageway surrounds the plug or the probe.

20 . A cooling system, comprising:
a nozzle guide vane endwall, comprising:
a first wall comprising a first opening that extends completely through the first wall, wherein the first wall is configured to face a primary flow path of a high-pressure turbine, and
a second wall comprising a second opening that extends completely through the second wall, wherein:
the first wall and the second wall define an inner passageway of the nozzle guide vane endwall;
the first opening is located adjacent to the second opening;
the first and second opening are part of a borescope port configured to receive a plug or a probe through the first wall and the second wall; and
the inner passageway is configured to direct a cooling fluid to the borescope port.

Assignees

• Rolls Royce Nam Tech Inc
• Rolls Royce Corp

Inventors

• Moody Jack
• Holley Kevin P

Classifications

• F01D9/04

  forming ring or sector · CPC title

• F05D2240/128

  Nozzles · CPC title

• F05D2260/201

  by impingement of a fluid · CPC title

• F01D25/12 Primary

  Cooling · CPC title

• F05D2260/80

  Diagnostics · CPC title