Carbon face seal

Patent metadata

Field	Value
Publication number	US-12276339-B2
Application number	US-202318578421-A
Country	US
Kind code	B2
Filing date	Jan 20, 2023
Priority date	Jan 21, 2022
Publication date	Apr 15, 2025
Grant date	Apr 15, 2025

Abstract

An apparatus has: a first member ( 120 ); a shaft ( 40; 50 ) rotatable relative to the first member about an axis; and a seal system ( 100 ). The seal system has a seal carrier ( 150 ) having: an axially-extending wall ( 156 ) having an inner diameter (ID) surface ( 160 ); and a radially-extending wall ( 154 ) having a first surface ( 158 ). A seal ( 102 ) is carried by the first member and has: an outer diameter (OD) surface ( 206 ); and a seal face ( 106 ). A seat ( 104 ) is carried by the shaft and has a seat face ( 108 ) in sliding sealing engagement with the seal face. One or more springs ( 132 ) bias the seal carrier relative to the first member so as to bias the seal face against the seat face. A key ( 240; 280; 300; 338 ) spans an interface between the seal carrier and the seal.

First claim

What is claimed is:

1. An apparatus comprising:
a first member;
a shaft rotatable relative to the first member about an axis; and
a seal system comprising:
a seal carrier having:
an axially-extending wall having an inner diameter surface; and
a radially-extending wall having a first surface;

a seal carried by the seal carrier in a radial interference fit with the seal carrier axially-extending wall inner diameter surface and having:
an outer diameter surface; and
a seal face;

a seat carried by the shaft and having a seat face in sliding sealing engagement with the seal face; and
one or more springs biasing the seal carrier relative to the first member so as to bias the seal face against the seat face,

wherein:
a key spans an interface between the seal carrier and the seal;
the key has:
a first portion in a through-hole in the seal carrier axially-extending wall;
a second portion in a hole in the seal carrier axially-extending wall; and
a third portion in a circumferentially-extending channel formed by respective grooves in the seal carrier and seal and joining the first portion to the second portion.

2. The apparatus of claim 1 wherein:
the key spans the seal carrier inner diameter surface and the seal outer diameter surface.

3. The apparatus of claim 2 wherein:
the radial interference fit provides a compressive stress in the seal of 10 MPa to 150 MPa.

4. The apparatus of claim 1 wherein:
the key comprises an epoxy.

5. The apparatus of claim 1 wherein:
the seal is a carbon seal.

6. The apparatus of claim 1 wherein:
the seal is a single piece.

7. The apparatus of claim 1 being a gas turbine engine.

8. A method for manufacturing the apparatus of claim 1 , the method comprising:
thermal interference fitting the seal to the seal carrier; and
forming the key in situ.

9. The method of claim 8 comprising said forming the key in situ wherein:
the forming the key in situ comprises curing epoxy.

10. The method of claim 9 wherein:
the forming the key in situ is after the thermal interference fitting; and
the forming the key in situ further comprises injecting the epoxy before the curing.

11. The method of claim 10 wherein:
the injecting the epoxy passes the epoxy through an inlet and an outlet, at least one of the inlet and the outlet being in the seal carrier.

12. The method of claim 11 wherein:
the injecting the epoxy passes the epoxy through an inlet leg from the inlet, an outlet leg to the outlet, and an intermediate leg circumferentially offsetting the outlet leg from the inlet leg.

13. The method of claim 11 wherein:
the injecting the epoxy passes the epoxy through a leg formed by mating grooves in the seal and seal carrier.

14. An apparatus comprising:
a first member;
a shaft rotatable relative to the first member about an axis; and
a seal system comprising:
a seal carrier having:
an axially-extending wall having an inner diameter surface; and
a radially-extending wall having a first surface;

a seal carried by the seal carrier in a radial interference fit with the seal carrier axially-extending wall surface and having:
an outer diameter surface; and
a seal face;

a seat carried by the shaft and having a seat face in sliding sealing engagement with the seal face; and
one or more springs biasing the seal carrier relative to the first member so as to bias the seal face against the seat face,

wherein:
a key spans an interface between the seal carrier and the seal; and
the key has:
a first portion in a through-hole in the seal carrier axially-extending wall;
a second portion in an axially-extending channel formed by respective grooves in the seal carrier axially-extending wall inner diameter surface and seal outer diameter surface; and
a third portion in a circumferentially-extending channel formed by respective grooves in the seal carrier and seal and joining the first portion to the second portion.

15. The apparatus of claim 14 wherein:
the key comprises an epoxy.

16. An apparatus comprising:
a first member;
a shaft rotatable relative to the first member about an axis; and
a seal system comprising:
a seal carrier having:
an axially-extending wall having an inner diameter surface; and
a radially-extending wall having a first surface;

a seal carried by the seal carrier in a radial interference fit with the seal carrier axially-extending wall inner diameter surface and having:
an outer diameter surface; and
a seal face;

a seat carried by the shaft and having a seat face in sliding sealing engagement with the seal face; and
one or more springs biasing the seal carrier relative to the first member so as to bias the seal face against the seat face,

wherein:
a key spans an interface between the seal carrier and the seal;
the key comprises a metallic pin;
the metallic pin has a shaft having:
an outboard portion in a through-hole in the seal carrier;
an inboard portion in a hole in the seal; and
a lateral protrusion backlocked against the seal carrier to resist outward displacement.

17. The apparatus of claim 16 wherein:
the seal is a carbon seal.

18. The apparatus of claim 16 wherein:
the seal is a single piece.

19. The apparatus of claim 16 being a gas turbine engine.

20. A method for manufacturing the apparatus of claim 16 , the method comprising:
thermal interference fitting the seal to the seal carrier; and
installing the key.

21. The method of claim 20 comprising said installing the key wherein:
the installing the key comprises driving the key through the seal carrier into the seal; and
the driving the key through the seal carrier compresses the lateral protrusion and then allows the lateral protrusion to expand to backlock against the seal carrier to resist outward displacement.

Assignees

• Rtx Corp

Inventors

• Mastro Jacob Peter
• Schwendenmann Andrew V

Classifications

• F16J15/3472 Primary

  Means for centering or aligning the contacting faces · CPC title

• F16J15/3452

  the pressing force resulting from the action of a spring · CPC title

• F05D2230/64

  using positioning or alignment devices for aligning or centring, e.g. pins · CPC title

• F05D2230/23

  by permanently joining parts together · CPC title

• F01D11/003

  by packing rings; Mechanical seals · CPC title