Pinned seal

Patent metadata

Field	Value
Publication number	US-10301957-B2
Application number	US-201514969604-A
Country	US
Kind code	B2
Filing date	Dec 15, 2015
Priority date	Dec 17, 2014
Publication date	May 28, 2019
Grant date	May 28, 2019

Abstract

An assembly includes a case structure, a seal interfacing with the case structure, a first pin, and a main pin hole on one of the seal and the case structure. The first pin extends through the main pin hole and is fixed relative to the other of the seal and the case structure. The assembly also includes a second pin and a secondary pin hole on one of the seal and the case structure. The second pin extends through the secondary pin hole. A cross-sectional gap area between the second pin and the secondary pin hole is greater than a cross-sectional gap area between the first pin and the main pin hole. Also included is a bolt hole on one of the seal and the case structure. The bolt hole is circumferentially located between the main pin hole and the secondary pin hole.

First claim

The invention claimed is:

1. An assembly for sealing at least one cavity in a gas turbine engine, the assembly comprising: a case structure; a seal interfacing with the case structure; a plurality of bolt holes configured to receive bolts or other securing elements, wherein the bolt holes are circumferentially spaced on one of the seal and the case structure; a main pin hole located circumferentially between a pair of bolt holes on one of the seal and the case structure; a first pin extending through the main pin hole, wherein the first pin is fixed relative to the other of the seal and the case structure; a secondary pin hole located circumferentially between an another pair of bolt holes on one of the seal and the case structure; and a second pin extending through the secondary pin hole, wherein the second pin is fixed relative to the other of the seal and the case structure, and wherein a cross-sectional gap area between the second pin and the secondary pin hole is greater than a cross-sectional gap area between the first pin and the main pin hole, wherein the plurality of bolt holes, the main pin hole, and the secondary pin hole are each positioned along a common circumference.

2. The assembly of claim 1 , wherein the main pin hole on one of the seal and the case structure has a cross-sectional shape that is the same as a cross-sectional shape of the first pin.

3. The assembly of claim 1 , wherein the secondary pin hole on one of the seal and the case structure has a cross-sectional shape that differs from a cross-sectional shape of the second pin.

4. The assembly of claim 3 , wherein the secondary pin hole on one of the seal and the case structure has a cross-sectional shape that is ovalized in a radial direction, and wherein the cross-sectional shape of the second pin is circular.

5. The assembly of claim 1 , wherein the case structure includes a flange defining a groove at a location on the case structure which interfaces with the seal.

6. The assembly of claim 5 , wherein a secondary seal is located within the groove.

7. The assembly of claim 1 , further comprising:
a first piston seal held by the seal on an outer end; and
a second piston seal held by the seal on an inner end.

8. The assembly of claim 1 , and further comprising:
another second pin; and
another secondary pin hole on one of the seal and the case structure, wherein the another second pin extends through the another secondary pin hole on one of the seal and the case structure, and wherein a cross-sectional area between the another second pin and the another secondary pin hole is greater than a cross-sectional area between the first pin and the main pin hole.

9. The assembly of claim 8 , wherein a number (n1) of bolt holes on one of the seal and the case structure circumferentially located between one of the secondary pin holes and the other of the secondary pin holes is different than a number (n2) of bolt holes on one of the seal and the case structure circumferentially located between the main pin hole and one of the secondary pin holes and between the main pin hole and the other of the secondary pin holes.

10. The assembly of claim 1 , wherein the case structure is an inner case and the seal is located between a mid-turbine frame cavity and a low pressure turbine rotor cavity.

11. A method of assembling a seal, the method comprising: inserting a first pin through a main pin hole on one of the seal and a case structure, wherein the first pin is fixed relative to the other of the seal and the case structure; inserting a second pin through a secondary pin hole on one of the seal and the case structure, wherein the second pin is fixed relative to the other of the seal and the case structure; and configuring the first pin within the main pin hole and the second pin within the secondary pin hole such that a cross-sectional gap area between the second pin and the secondary pin hole is greater than a cross-sectional gap area between the first pin and the main pin hole; wherein a plurality of bolt holes configured to receive bolts or other securing elements are circumferentially spaced on one of the seal and the case structure; and wherein each of the main pin hole and the secondary pin hole is located circumferentially between a pair of bolt holes on one of the seal and the case structure, wherein the plurality of bolt holes, the main pin hole, and the secondary pin hole are each positioned along a common circumference.

12. The method of claim 11 , further comprising:
inserting another second pin through another secondary pin hole on one of the seal and the case structure; and
configuring the another second pin within the another secondary pin hole such that a cross-sectional gap area between the another second pin and the another secondary pin hole is greater than a cross-sectional gap area between the first pin and the main pin hole.

13. The method of claim 12 , further comprising:
configuring a number of aligned bolt holes circumferentially between the second pins to differ from a number of aligned bolt holes circumferentially between both the first pin and one of the second pins and the first pin and the another of the second pins.

14. The method of claim 11 , further comprising:
inserting a secondary seal within a groove defined by a flange of the case structure at a location on the case structure which interfaces with the seal.

15. The method of claim 11 , wherein inserting the first pin and inserting the second pin comprises press-fitting the first pin and press-fitting the second pin into the case structure.

16. The method of claim 11 , wherein inserting the first pin, inserting the second pin, and configuring the first and second pins is performed as a blind assembly.

17. An assembly comprising: a seal comprising, a planar face; an outer portion extending generally radially from the planar face in a first direction at an angle; and an inner portion extending generally radially from the planar face in a second direction at an angle, wherein the first direction is generally opposite the second direction; a case structure including a planar face extending generally radially outward from the case structure, wherein the planar face of the case structure interfaces with the planar face of the seal; a plurality of bolt holes configured to receive bolts or other securing elements, wherein the bolt holes are circumferentially spaced on both the planar face of the seal and the planar face of the case structure, and wherein the bolt holes on the planar face of the seal and the bolt holes on the planar face of the case structure are aligned; a first pin, wherein the first pin is fixed relative to the other of the seal and the case structure; a main pin hole on both the planar face of the seal and the planar face of the case structure located circumferentially between a pair of bolt holes on both the planar face of the seal and the planar face of the case structure, wherein the main pin hole on the planar face of the seal and the main pin hole on the planar face of the case structure are aligned, and wherein the first pin extends through the main pin hole on both the planar face of the seal and the planar face of the case structure; a second pin, wherein the second pin is fixed relative to the other of the seal and the case structure; and a secondary pin hole on both the planar face of the seal and the planar face of the case structure located circumferentially between an another pair of bolt holes on both the planar face of the seal and the planar face of the case structure, wherein the secondary pin hole on the planar face

Assignees

• United Technologies Corp

Inventors

• Lemoine Jonathan
• Bauer Steven J

Classifications

• F01D11/005 Primary

  Sealing means between non relatively rotating elements · CPC title

• F05D2240/55

  Seals · CPC title

• F01D25/164

  Flexible supports; Vibration damping means associated with the bearing · CPC title

• F01D25/243

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title