Gas turbine engine with carbon/carbon composite piston seal

Patent metadata

Field	Value
Publication number	US-12352173-B2
Application number	US-202217994188-A
Country	US
Kind code	B2
Filing date	Nov 25, 2022
Priority date	Nov 25, 2022
Publication date	Jul 8, 2025
Grant date	Jul 8, 2025

Abstract

A gas turbine engine includes a rotor that that has a seal surface, a shaft that has an annular seal channel that opens to the seal surface, and a seal disposed in the annular seal channel for sealing against the seal surface. The seal is made of a composite having carbon fibers disposed in a carbon matrix.

First claim

What is claimed is:

1. A gas turbine engine comprising:
a rotor rotatable about an engine central axis and defining a bore having a seal surface;
a shaft received into the bore and rotatable about the engine central axis, the shaft defining an annular seal channel that opens to the seal surface; and
a seal disposed in the annular seal channel for sealing against the seal surface, the seal being diametrically oversized for the annular seal channel such that in a state of rest the seal is unseated with respect to a floor of the annular seal channel, the seal being made of a composite having carbon fibers disposed in a carbon matrix, the seal including an annular core extending along a central core axis that extends circumferentially around the engine central axis, and the carbon fibers are in a series of flat tows that are wound around the central core axis on the annular core such that each of the flat tows partially overlaps an immediately prior flat tow in the series of flat tows, the seal having split seam and the seal being flexible such that ends of the seal at the split seam can be moved apart in order to diametrically expand the seal to fit over the shaft, and the seal can be diametrically compressed into the annular seal channel in order to provide clearance for the shaft to be received into the bore.

2. The gas turbine engine as recited in claim 1 , wherein the carbon fibers are, by volume, 35% to 65% of the composite.

3. The gas turbine engine as recited in claim 1 , wherein edges of the flat tows lie in a plane of an outer surface of the seal.

4. The gas turbine engine as recited in claim 3 , wherein each of the flat tows are wound fully circumferentially around the central core.

Assignees

• Raytheon Tech Corp
• Rtx Corp

Inventors

• Winder Calvin Jay
• Maalouf Fadi S
• Bintz Matthew E
• Schutte Peter T
• Van Lieu Pieter
• Delarm Justin Roger
• Wright Anna Lauren
• Mohseni Hamidreza
• Lyders David R
• Fang Xiaomei

Classifications

• F05D2240/55

  Seals · CPC title

• F05D2230/10

  by removing material · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C7/28

  Arrangement of seals · CPC title

• C04B2235/5252

  having a specific pre-form · CPC title