Contacting dry face seal with tapered carbon nose

Patent metadata

Field	Value
Publication number	US-10619741-B2
Application number	US-201715701506-A
Country	US
Kind code	B2
Filing date	Sep 12, 2017
Priority date	Sep 12, 2017
Publication date	Apr 14, 2020
Grant date	Apr 14, 2020

Abstract

A face seal assembly for a gas turbine engine includes a seal body having a seal face defining a contact area disposed between tapered sides. The seal body defines an axial width between a back surface of the seal body and the seal face. A decrease in the axial width from wear increases the contact area. A bearing assembly and method are also disclosed.

First claim

What is claimed is:

1. A face seal assembly for a gas turbine engine comprising:
a seal body having a seal face defining a contact area disposed between tapered sides, the seal body defining an axial width between a back surface of the seal body and the seal face, wherein the seal face is centered between identical tapered sides, wherein one of the tapered sides begins at an inner diameter of the seal body and extends to the seal face and another of the tapered sides begins at an outer diameter and extends to the seal face; wherein a decrease in the axial width from wear increases the contact area.

2. The face seal assembly as recited in claim 1 , wherein tapered sides are disposed at an angle relative to the seal face between 30 and 60 degrees.

3. The face seal assembly as recited in claim 1 , wherein the seal body is one piece annular part that extends completely about an axis and the seal face comprises an annular contact surface engaging a rotating surface.

4. The face seal assembly as recited in claim 3 , wherein the face seal includes a radial width that is less than a radial width of the seal body.

5. The face seal assembly as recited in claim 4 , wherein a cross-sectional area of the face seal increases in a direction toward the back surface of the seal body.

6. The face seal assembly as recited in claim 3 , wherein the face seal is centered between an inner diameter and an outer diameter of the seal body.

7. The face seal assembly as recited in claim 1 , wherein the face seal is carbon.

8. A bearing assembly for a gas turbine engine comprising:
a bearing supporting a rotating part relative to fixed part;
a rotating face supported for rotation with the rotating part;
a seal body having a seal face defining a contact area disposed between tapered sides, the seal body defining an axial width between a back surface of the seal body and the seal face wherein the seal face is centered between identical tapered sides, wherein one of the tapered sides begins at an inner diameter of the seal body and extends to the seal face and another of the tapered sides begins at an outer diameter and extends to the seal face; and
a biasing member biasing the seal body against the rotating face generating a defined seal pressure between the rotating face and the seal body, wherein a decrease in the axial width from wear increases an area of the seal face and decreases the seal pressure.

9. The bearing assembly as recited in claim 8 , wherein the tapered sides are disposed at an angle relative to the seal face between 30 and 60 degrees.

10. The bearing assembly as recited in claim 9 , wherein the seal body is annular about an axis and the seal face comprises an annular contact surface engaging a rotating surface.

11. The bearing assembly as recited in claim 10 , wherein the face seal includes a radial width that is less than a radial width of the seal body.

12. The bearing assembly as recited in claim 8 , wherein a cross-sectional area of the face seal increases in a direction toward the back surface of the seal body.

13. The bearing assembly as recited in claim 8 , wherein the face seal is carbon.

14. A method of forming a seal between a static and rotating part of a gas turbine engine comprising:
supporting a rotating face on a rotating part;
supporting a seal body on a static structure, wherein the seal body has a seal face defining a contact area disposed between tapered sides, the seal body defining an axial width between a back surface of the seal body and the seal face, wherein the seal face is centered between identical tapered sides, wherein one of the tapered sides begins at an inner diameter of the seal body and extends to the seal face and another of the tapered sides begins at an outer diameter and extends to the seal face; and
generating a defined seal pressure between the rotating face and the seal body with a biasing member, wherein a decrease in the axial width from wear increases an area of the seal face and decreases the generated seal pressure.

15. The method as recited in claim 14 , wherein the tapered sides are disposed at an angle relative to the seal face between 30 and 60 degrees.

16. The method as recited in claim 15 , wherein a cross-sectional area of the face seal increases in a direction toward the back surface of the seal body and provides the decreased seal pressure.

17. The method as recited in claim 14 , wherein the face seal is carbon.

Assignees

• United Technologies Corp

Inventors

• Walker Brady
• Szolomayer Robert D

Classifications

• F05D2260/38

  by a spring, i.e. spring loaded or biased towards a certain position · CPC title

• F05D2250/292

  tapered · CPC title

• F16J15/30

  with sealing rings made of carbon · CPC title

• F01D25/183

  Sealing means · CPC title

• F05D2250/232

  conical · CPC title