Wear resistant frame liner joint assembly for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10323847-B2
Application number	US-201514984733-A
Country	US
Kind code	B2
Filing date	Dec 30, 2015
Priority date	Dec 30, 2015
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

A tripod joint assembly for connecting first and second overlapping panel segments of a flowpath liner in a gas turbine engine includes a threaded fastener extending through an opening in the first overlapping panel segment and adjacent to an outer segment edge of the second overlapping panel segment disposed on the first overlapping segment. The assembly further includes a tripod plate having first and second plate edges and an access hole therebetween. The first plate edge contacts the first overlapping panel segment, the second plate edge contacts the outer segment edge of the second overlapping panel segment. The access hole is disposed around the threaded fastener. First and second washers are disposed around the threaded fastener, the first washer on the tripod plate opposite to the overlapping panel segments, and the second washer on the first washer opposite to the tripod plate. A threaded locknut secures the assembly.

First claim

What is claimed is:

1. A tripod joint assembly for connecting a first overlapping panel segment and a second overlapping panel segment of a flowpath liner in a gas turbine engine, the tripod joint assembly comprising:
a threaded fastener extending through an opening in the first overlapping panel segment and adjacent an outer segment edge of the second overlapping panel segment disposed on the first overlapping panel segment;
a tripod plate having a first plate edge and a second plate edge and an access hole therebetween, the first plate edge contacting the first overlapping panel segment, the second plate edge contacting the outer segment edge of the second overlapping panel segment, and the access hole disposed around the threaded fastener;
a first washer disposed around the threaded fastener on the tripod plate opposite the first overlapping panel segment and the second overlapping panel segment;
a second washer disposed around the threaded fastener on the first washer opposite the tripod plate; and a threaded locknut secured to the threaded fastener and contacting the second washer opposite the first washer;
wherein the second washer is a spring washer having an angle that angles radially inwardly towards the threaded fastener and upwardly away from the first washer and the threaded locknut is configured to apply a spring bias by compressing the second washer against the first washer; and
wherein a central surface of the first washer further includes a substantially flat surface including an annular lip, wherein the annular lip is disposed near the threaded fastener facing the second washer, such that the annular lip comes in contact with the second washer to prevent the second washer from reversing the angle downwardly towards the first washer when the threaded locknut is tightened.

2. The tripod joint assembly according to claim 1 , wherein the tripod plate includes a flat surface opposite the first overlapping panel segment and the second overlapping panel segment, and wherein the tripod plate flat surface includes a concave seat around the access hole.

3. The tripod joint assembly according to claim 2 , wherein the first washer includes a convex surface configured to mate with the concave seat of the tripod plate.

4. The tripod joint assembly according to claim 1 , wherein the first overlapping panel segment is a fairing platform.

5. The tripod joint assembly according to claim 4 , wherein the fairing platform includes a protruding mounting base configured to contact the first plate edge of the tripod plate.

6. The tripod joint assembly according to claim 1 , wherein the first plate edge of the tripod plate includes a protrusion, and the first overlapping panel segment includes a locating indentation configured to receive a portion of the protrusion.

7. The tripod joint assembly according to claim 1 , wherein the second overlapping panel segment includes a contact surface opposite the first overlapping panel segment, and wherein the second plate edge of the tripod plate includes a plate engagement surface having two buttons configured to engage the contact surface of the second overlapping panel segment.

8. The tripod joint assembly according to claim 7 , wherein the two buttons are convex with respect to the plate engagement surface.

9. The tripod joint assembly according to claim 1 , wherein the first overlapping panel segment includes an expansion surface configured to slidably engage a first surface of the outer segment edge of the second overlapping panel segment adjacent the expansion surface, and wherein the expansion surface and adjacent the first surface each include a wear-resistant coating disposed between the first overlapping panel segment and the second overlapping panel segment.

10. The tripod joint assembly according to claim 9 , wherein the tripod plate includes an engagement surface facing the second overlapping panel segment and having a wear-resistant coating disposed thereon, and wherein the outer segment edge of the second overlapping panel segment includes a second surface opposite the first surface, and having a wear-resistant coating disposed thereon between the tripod plate and the outer segment edge.

11. The tripod joint assembly according to claim 9 , wherein the tripod plate is unitary and comprises a wear-resistant material.

12. A flowpath liner assembly for a gas turbine engine, the flowpath liner assembly comprising:
an annular forward hanger;
an annular aft hanger;
a plurality of overlapping panel segments disposed radially between the annular forward hanger and the annular aft hanger, each of the plurality of overlapping panel segments having first and second opposing engagement edges extending in the radial direction;
a plurality of fairing platforms disposed radially between the annular forward hanger and the annular aft hanger, each of the plurality of fairing platforms including first and second opposing extension edges extending in the radial direction, the plurality of fairing platforms configured to be disposed in an alternating arrangement with the plurality of overlapping panel segments, and each of the first and second opposing extension edges configured to overlap with a respective adjacent engagement edge of the first and second opposing engagement edges; and
a plurality of tripod joint assemblies configured to respectively couple each of the first and second opposing extension edges with a respective adjacent engagement edge of the first and second opposing engagement edges, each of the plurality of tripod joint assemblies comprising:
a threaded fastener extending through an opening in a first overlapping panel segment of the plurality of overlapping panel segments and adjacent an outer segment edge of a second overlapping panel segment of the plurality of overlapping panel segments disposed on the first overlapping panel segment;
a tripod plate having a first plate edge and a second plate edge and an access hole therebetween, the first plate edge contacting the first overlapping panel segment, the second plate edge contacting the outer segment edge of the second overlapping panel segment, and the access hole disposed around the threaded fastener;
a first washer disposed around the threaded fastener on the tripod plate opposite the first overlapping panel segment and the second overlapping panel segment;
a second washer disposed around the threaded fastener on the first washer opposite the tripod plate; and
a threaded locknut secured to the threaded fastener and contacting the second washer opposite the first washer;
wherein the second washer is a spring washer having an angle that angles radially inwardly towards the threaded fastener and upwardly away from the first washer and the threaded locknut is configured to apply a spring bias by compressing the second washer against the first washer; and
wherein a central surface of the first washer further includes a substantially flat surface including an annular lip, wherein the annular lip is disposed near the threaded fastener and facing the second washer, such that the annular lip comes in contact with the second washer to prevent the second washer from reversing the angle downwardly towards the first washer when the threaded locknut is tightened.

13. The flowpath liner assembly according to claim 12 , wherein each of the plurality of fairing platforms includes at least one hollow airfoil configured to allow air communication therethrough.

14. The flowpath liner assembly according to claim 12 , wherein the spring washer comprises the first washer configured to couple with the tripod plate about the threaded fastener and the sec

Assignees

• Gen Electric

Inventors

• Oswald Eric Robert
• Ryczek Scott Patrick
• Bosel Tod Kenneth
• Czachor Robert

Classifications

• F23R3/50

  Combustion chambers comprising an annular flame tube within an annular casing (toroidal combustion chambers F23R3/52) · CPC title

• F05D2230/642

  using maintaining alignment while permitting differential dilatation · CPC title

• F23R3/60 Primary

  Support structures; Attaching or mounting means · CPC title

• F05D2230/90

  Coating; Surface treatment · CPC title

• F16B39/28

  by special members on, or shape of, the nut or bolt (F16B39/26 takes precedence; locknuts F16B39/12) · CPC title