Gas turbine seal

Patent metadata

Field	Value
Publication number	US-10408077-B2
Application number	US-201715416541-A
Country	US
Kind code	B2
Filing date	Jan 26, 2017
Priority date	Jan 26, 2017
Publication date	Sep 10, 2019
Grant date	Sep 10, 2019

Abstract

A labyrinth seal includes a first annular member positioned on a center axis and a second annular member disposed circumferentially around the first annular member. A seal land is disposed on one of the first annular member and the second annular member. The seal land is positioned radially between the first annular member and the second annular member relative the center axis. A seal plate is disposed on the other of the first annular member and the second annular member. The seal plate extends radially toward the seal land and includes a plate body extending between a base and a tip of the seal plate. The plate body extends along a majority of a radial span of the seal plate on a first plane. The tip of the seal plate extends axially and radially away from the plate body on a second plane.

First claim

The invention claimed is:

1. A labyrinth seal comprising:
a first annular member positioned on a center axis;
a second annular member disposed circumferentially around the first annular member, wherein the first annular member and the second annular member form a flowpath therebetween with an upstream end and a downstream end;
a seal land disposed on one of the first annular member and the second annular member, and positioned radially between the first annular member and the second annular member relative the center axis; and
a seal plate disposed on the other of the first annular member and the second annular member, wherein the seal plate extends radially toward the seal land, wherein the seal plate comprises:
a plate body extending between a base and a tip of the seal plate, wherein the plate body extends along a majority of a radial span of the seal plate on a first plane,
wherein the tip of the seal plate extends axially and radially away from the plate body on a second plane, and
a flange extending radially away from the plate body toward the seal land, and wherein the flange is spaced axially downstream from the tip.

2. The labyrinth seal of claim 1 , wherein the seal plate is disposed on the first annular member, and wherein the first annular member is a rotor configured to rotate about the center axis.

3. The labyrinth seal of claim 2 , wherein the seal land is disposed on the second annular member, and wherein the second annular member is a stator.

4. The labyrinth seal of claim 3 , wherein the tip of the seal plate extends axially upstream and radially outward from the plate body.

5. The labyrinth seal of claim 4 , wherein the seal land comprises an annular trench, and wherein the tip of the seal plate and the flange are both disposed inside the annular trench.

Assignees

• United Technologies Corp
• United Tehnologies Corp

Inventors

• Port Daniel F

Classifications

• F05D2250/71

  curved · CPC title

• F04D29/102

  especially adapted for elastic fluid pumps · CPC title

• F01D11/02 Primary

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title

• F04D29/164

  of an axial flow wheel · CPC title

• F16J15/4472

  with axial path · CPC title