IP Library Granted Patent US 7,290,769
Granted Patent B2
US 7,290,769 · App. 11/028,232 · Granted Nov 6, 2007

Sealing device with a brush gasket and flexible washer for a high-pressure turbine of a turbomachine

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Quick Facts
Patent No.
US 7,290,769
App. No.
11/028,232
Granted
Nov 6, 2007
Kind
B2
Abstract

A sealing device for sealing between two static portions of a turbomachine includes a brush gasket formed by a plurality of resilient bristles which are, at least in part, held in a housing. Each bristle has a main portion and a secondary portion interconnected by a bent portion. The secondary portion has a free end ensuring leaktight contact with a surface that is to be sealed of the other static portion. The sealing device further includes a flexible washer of bent section which has a free end bearing both against the free ends of the secondary portions of the bristles of the brush gasket, and against the surface that is to be sealed so that the free ends of the secondary portions of the bristles of the brush gasket are permanently in contact with the surface that is to be sealed.

Claims (42)

1. A sealing arrangement for a turbomachine comprising:

a static portion including a cavity defining a housing;

a sealing device including a brush gasket formed by a plurality of resilient sealing bristles, the brush gasket having a main portion and a secondary portion having a free end section, the brush gasket further including a bent portion interconnecting the main portion of the brush gasket to the secondary portion of the brush gasket, the main portion of the brush gasket being secured in said housing of said static portion, said free end section of the brush gasket extending outside said housing of said static portion in a free state configuration where said resilient sealing bristles are not axially deformed; and

a flexible washer having a curved section and an end portion, said curved section covering a portion of the main portion of the brush gasket and said end portion of said flexible washer bearing against the free end section of the brush gasket and, in said free state configuration where said resilient sealing bristles are not axially deformed, extending beyond said free end section of the brush gasket outside and away from said housing of said static portion.

2. A sealing arrangement for a turbomachine comprising:

a first static portion including a cavity defining a housing;

a second static portion, stationary with respect to the first static portion except subject to relative radial and axial movement with respect to a longitudinal axis of the turbomachine, spaced from said first static portion by a first space in a normal use position, said second static portion including a surface opposite to the cavity of said first static portion; and

a sealing device for sealing the first space between the first static portion and the second static portion in order to divide the first space into second and third spaces, the second space having a different pressure from a pressure in the third space;

said sealing device including:

a brush gasket formed by a plurality of resilient sealing bristles, the brush gasket having a main portion and a secondary portion, the secondary portion having a free end section, the brush gasket further including a bent portion interconnecting the main portion of the brush gasket to the secondary portion of the brush gasket, the main portion of the brush gasket being secured in said housing of said first static portion, said secondary portion of the brush gasket projects outside of said housing of said first static portion in a first direction so that the free end section of the brush gasket engages said surface of the second static portion; and

a flexible washer having a curved section and an end portion, said curved section covering a portion of the main portion of the brush gasket and said end portion of said flexible washer bearing against the free end section of the brush gasket and, the flexible washer further including a protruding portion connected to the end portion and bearing against said surface of the second static portion in said normal use position so that said free end section of the brush gasket is permanently in contact with said surface of the second static portion in said normal use position,

wherein, the free end section of the brush gasket is deflected in a second direction, opposite the first direction, by engagement with said surface of the second static portion by a first distance, and

the protruding portion of said flexible washer is deflected in the second direction by engagement with said surface of the second static portion by a second distance that is greater than the first distance.

3. A sealing arrangement according to claim 2 , wherein the flexible washer is substantially ω-shaped.

4. A sealing arrangement according to claim 2 , wherein said sealing device separates a higher pressure space from a lower pressure space and the higher pressure space is the second space, the lower pressure space is the third space, and the end portion of the flexible washer is exposed to the pressure in the lower pressure space.

5. A sealing arrangement according to claim 2 , further comprising a retaining ring for retaining the main portion of the brush gasket in the housing of the first static portion.

6. A sealing arrangement according to claim 5 , wherein the curved section of the flexible washer comprises a first lobe and a second lobe, said first lobe being inside said housing and said second lobe being at least partially outside said housing.

7. A sealing arrangement according to claim 6 , wherein said second lobe bears against the retaining ring.

8. A sealing arrangement according to claim 5 , wherein the flexible washer is between said main portion of the brush gasket and said surface of the second static portion, and also between said secondary portion of the brush gasket and said retaining ring.

9. A sealing arrangement according to claim 2 , wherein the bent portion of the brush gasket is right angled so that the secondary portion of the brush gasket extends substantially perpendicularly to the main portion of the brush gasket.

10. A sealing arrangement according to claim 2 , wherein the brush gasket is disposed so that the main portion of the brush gasket extends substantially perpendicularly to a longitudinal axis of the turbomachine, and so that the secondary portion of the brush gasket extends substantially parallel to said longitudinal axis of the turbomachine.

11. A sealing arrangement according to claim 2 , wherein the curved section of the flexible washer comprises a first lobe and a second lobe, said first lobe being inside said housing and said second lobe being at least partially outside said housing.

12. A sealing arrangement according to claim 11 , wherein said first lobe includes a first arm inside said housing, said first arm having a first portion in contact with said main portion of the brush gasket.

13. A sealing arrangement according to claim 12 , wherein said first arm of said first lobe has a second portion not in contact with said main portion of the brush gasket.

14. A sealing arrangement according to claim 13 , wherein said second portion of said first arm of said first lobe contacts a wall of said housing of the first static portion.

15. A sealing arrangement according to claim 14 , wherein said first lobe includes a second arm having a first portion in contact with said main portion of the brush gasket.

16. A sealing arrangement according to claim 15 , wherein said second arm of said first lobe has a second portion not in contact with said main portion of the brush gasket.

17. A sealing arrangement according to claim 12 , wherein said first lobe includes a second arm having a first portion in contact with said main portion of the brush gasket.

18. A sealing arrangement according to claim 17 , wherein said second arm of said first lobe has a second portion not in contact with said main portion of the brush gasket.

19. A sealing arrangement according to claim 17 , wherein said second lobe includes a third arm connected to said second arm of the first lobe.

20. A sealing arrangement according to claim 19 , wherein said second lobe includes a fourth arm connected to the end portion of the flexible washer.

21. A sealing arrangement according to claim 20 , wherein said end portion of the flexible washer and said third arm are separated by a clearance.

22. A sealing arrangement according to claim 2 , wherein part of the flexible washer is positioned within an area partially bounded by said main portion of the brush gasket, said surface of the second static portion and said secondary portion of the brush gasket.

23. A sealing arrangement comprising:

a first static portion including a cavity defining a housing;

a second static portion, stationary with respect to the first static portion except subject to relative radial and axial movement with respect to a longitudinal axis of the turbomachine, spaced from said first static portion by a first space in a normal use position, said second static portion including a surface opposite to the cavity of said first static portion; and

a sealing device for sealing the first space between the first static portion and the second static portion in order to divide the first space into second and third spaces, the second space having a different pressure from a pressure in the third space;

said sealing device including:

a brush gasket formed by a plurality of resilient sealing bristles, the brush gasket having a main portion and a secondary portion, the secondary portion having a free end section, the brush gasket further including a bent portion interconnecting the main portion of the brush gasket to the secondary portion of the brush gasket, the main portion of the brush gasket being secured in said housing of said first static portion, said secondary portion of the brush gasket projects outside of said housing of said first static portion in a first direction so that the free end section of the brush gasket engages said surface of the second static portion; and

a flexible washer having a curved section and an end portion, said curved section covering a portion of the main portion of the brush gasket and said end portion of said flexible washer bearing against the free end section of the brush gasket and, the flexible washer further including a protruding portion connected to the end portion and bearing against said surface of the second static portion in said normal use position so that said free end section of the brush gasket is permanently in contact with said surface of the second static portion in said normal use position,

wherein, the free end section of the brush gasket is deflected in a second direction, opposite the first direction, by engagement with said surface of the second static portion by a first distance, and

the protruding portion of said flexible washer is deflected in the second direction by engagement with said surface of the second static portion by a second distance that is greater than the first distance.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →