Film riding seal assembly for turbomachinery

Patent metadata

Field	Value
Publication number	US-2016010480-A1
Application number	US-201414325452-A
Country	US
Kind code	A1
Filing date	Jul 8, 2014
Priority date	Jul 8, 2014
Publication date	Jan 14, 2016
Grant date	—

Abstract

An aerodynamic seal assembly for a rotary machine includes multiple sealing segments disposed circumferentially intermediate to a stationary housing and a rotor. Each of the segments includes a shoe plate with a forward load-bearing section and an aft load-bearing section configured to generate an aerodynamic force between the shoe plate and the rotor. The shoe plate includes at least one labyrinth teeth facing the rotor and positioned between the forward load-bearing section and the aft load-bearing section. The sealing segment also includes at least one spring connected to a pedestal located about midway of an axial length of the shoe plate and to a stator interface element. Further, the sealing segment includes a rigid segmented secondary seal attached to the stator interface element at one first end and in contact with the pedestal of the shoe plate at one second end.

First claim

1 . (canceled)

2 . An aerodynamic seal assembly for a rotary machine, the seal assembly comprising:
a plurality of sealing segments disposed circumferentially intermediate to a stationary housing and a rotor, wherein each of the segments comprises:
a shoe plate with a forward load-bearing section and an aft load-bearing section configured to generate an aerodynamic force between the shoe plate and the rotor, wherein the shoe plate comprises at least one labyrinth teeth facing the rotor and positioned between the forward load-bearing section and the aft load-bearing section, wherein the shoe plate is further configured to allow a flow of high pressure fluid into a front portion of the at least one labyrinth teeth and a low pressure fluid into a rear portion of the at least one labyrinth teeth;
at least one spring connected to a pedestal located about midway of an axial length of the shoe plate and to a stator interface element; and
a rigid segmented secondary seal attached to the stator interface element at one first end and in contact with the pedestal of the shoe plate at one second end, wherein the rigid segmented secondary seal is L-shaped and comprises of an L-shaped spline slot forming a radial spline slot and an axial spline slot located at sides of the L-shaped secondary seal for allowing splines to be inserted to prevent fluid leakages between adjacent sealing segments, and wherein the stator interface element comprises a spline slot that is aligned with the radial spline slot on the rigid segmented seal.

3 . The aerodynamic seal assembly of claim 2 , where the spring is a bellow spring or a flexure.

4 . The aerodynamic seal assembly of claim 2 , wherein each of the sealing segments comprises a line contact between a free end of the rigid segmented secondary seal and the pedestal of shoe plate separating a high pressure side and a low pressure side on either side of the line contact.

5 . The aerodynamic seal assembly of claim 4 , wherein the pedestal includes a nose protrusion forming the line contact with a flat radial surface at the free end of the rigid segmented secondary seal.

6 . The aerodynamic seal assembly of claim 4 , wherein the free end of the rigid segmented secondary seal comprises a nose protrusion forming the line contact with a flat radial surface of the pedestal of the shoe plate facing the low pressure side of the rotary machine.

7 . The aerodynamic seal assembly of claim 2 , wherein the at least one spring provided in each of the sealing segments comprises a circumferential width less than each of circumferential widths of the stator interface element and the shoe plate.

8 . The aerodynamic seal assembly of claim 2 , wherein the shoe plate comprises one or more forward ports located on a top portion for allowing the flow of high pressure fluid into the front portion of the at least on labyrinth teeth.

9 . The aerodynamic seal assembly of claim 8 , wherein the shoe plate comprises one or more aft ports located on the top portion of the shoe plate at a rear side of the pedestal for allowing the low pressure fluid into the rear portion of the at least one labyrinth teeth.

10 . The aerodynamic seal assembly of claim 8 , wherein the shoe plate comprises a forward shoe feeding groove formed due to different circumferential width of the top portion of the shoe plate and the forward load-bearing section towards a high pressure side of the rotary machine.

11 . The aerodynamic seal assembly of claim 8 , wherein the shoe plate comprises an aft shoe feeding groove formed due to different circumferential width of the top portion of the shoe plate and the aft load-bearing section towards a low pressure side of the rotary machine.

12 . The aerodynamic seal assembly of claim 8 , wherein the one or more forward ports are angled in a circumferential direction to impart swirl to the fluid as the fluid flows from the high pressure side to the front portion of the at least one labyrinth teeth.

13 . The aerodynamic seal assembly of claim 2 , wherein each of the forward load-bearing section and the aft load-bearing section comprises one or more Rayleigh steps for generating a thin film for an additional radial opening force on the sealing segment.

14 . The aerodynamic seal assembly of claim 2 , wherein one side of the shoe plate facing the rotor comprises a curvature larger than the curvature of the rotor.

15 . The aerodynamic seal assembly of claim 2 , wherein each of the forward load-bearing section and the aft load-bearing section is flexible due to small radial thickness.

16 . The aerodynamic seal assembly of claim 2 , further comprising the rotor with different radius along the axial direction about the at least one labyrinth teeth forming a radial step on the rotor for decelerating axial momentum of the fluids flowing axially from high pressure side to the low pressure side of the rotary machine.

17 . The aerodynamic seal assembly of claim 2 , further comprising the rotor having a plurality of grooves for generating aerodynamic force during operation of the rotary machine.

18 . The aerodynamic seal assembly of claim 2 , wherein the stator interface elements are joined together to form a non-segmented stator interface.

19 . The aerodynamic seal assembly of claim 2 , wherein the rigid segmented secondary seal segments are joined together to form a non-segmented rigid secondary seal.

20 .- 23 . (canceled)

24 . A rotary machine, comprising:
an aerodynamic seal assembly comprising a plurality of sealing segments disposed circumferentially intermediate to a stationary housing and a rotor, wherein each of the segments comprises:
a shoe plate with a forward load-hearing section and an aft load-bearing section configured to generate an aerodynamic force between the shoe plate and the rotor, wherein the shoe plate comprises at least one labyrinth teeth facing the rotor and positioned between the forward load-bearing section and the aft load-bearing section, wherein the shoe plate is further configured to allow a flow of high pressure fluid into a front portion of the at least one labyrinth teeth and a low pressure fluid into a rear portion of the at least one labyrinth teeth;
at least one spring connected to a pedestal located about midway of an axial length of the shoe plate and to a stator interface element; and
a rigid segmented secondary seal attached to the stator interface element at one first end and in contact with the pedestal of the shoe plate at one second end wherein the rigid segmented secondary seal is L-shaped and comprises of an L-shaped spline slot forming a radial spline slot and an axial spline slot located at sides of the L-shaped secondary seal for allowing splines to be inserted to prevent fluid leakages between adjacent sealing segments.

25 . The rotary machine of claim 24 , further comprising a plurality of splines seals inserted between adjacent sealing segments into the L-shaped spline slots.

26 . (canceled)

27 . An aerodynamic seal assembly for a rotary machine, the seal assembly comprising:
a plurality of sealing segments disposed circumferentially intermediate to a stationary housing and a rotor, wherein each of the segments comprises:
a shoe plate with a forward load-bearing section and an aft load-bearing section configured to generate an aerodynamic force between the shoe plate and the rotor, wherein the shoe plate comprises at least one labyrinth teeth facing the rotor and positi

Assignees

• Gen Electric

Inventors

• Bidkar Rahul Anil
• Giametta Andrew Paul
• Gibson Nathan Evan Mccurdy
• Cleveland Nicolas Joseph

Classifications

• 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

• F16J15/4478

  Pre-assembled packings · CPC title

• F01D11/025 Primary

  Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F16J15/442

  segmented · CPC title