Turbine wheels, turbine engines including the same, and methods of forming turbine wheels with improved seal plate sealing

Patent metadata

Field	Value
Publication number	US-11015472-B2
Application number	US-202017014547-A
Country	US
Kind code	B2
Filing date	Sep 8, 2020
Priority date	Dec 2, 2016
Publication date	May 25, 2021
Grant date	May 25, 2021

Abstract

A turbine engine includes a turbine wheel including a rotor disk and turbine blades connected to the rotor disk through blade mounts. The blade mounts and the rotor disk have fore and aft surfaces. The blade mount includes a blade attachment surface connecting the fore and aft surfaces with the turbine blade extending from the blade attachment surface. A gap is defined between and separating adjacent blade mounts and extends into the rotor disk. The gap includes a pocket having a fore opening and a rotor relief hole. The turbine wheel further includes a plug disposed in a rotor relief opening and a pocket seal disposed in the pocket. The turbine engine further includes a fore seal plate having an edge abutting the blade mounts about a circumference of the turbine wheel and a finger extending toward and contacting the plug to maintain the plug in the rotor relief opening.

First claim

What is claimed is:

1. A turbine engine comprising:
a turbine wheel including:
a rotor disk;
a plurality of turbine blades each operatively connected to the rotor disk through a blade mount with the blade mount bonded to the rotor disk and the blade mount and the rotor disk having a fore surface on a higher pressure side thereof and an aft surface on a lower pressure side thereof, wherein the blade mount comprises a blade attachment surface extending between and connecting the fore surface and the aft surface thereof with the turbine blade extending from the blade attachment surface;
a gap defined between adjacent blade mounts separating the blade mounts and extending into the rotor disk with the gap including a pocket having a fore opening in the fore surface, and the gap further including a rotor relief hole defined by and within the rotor disk and having a rotor relief opening in the fore surface;
a plug disposed in the rotor relief opening; and
a pocket seal disposed in the pocket; and

a fore seal plate having a fore plate edge abutting the blade mounts about a circumference of the turbine wheel and a finger extending toward and contacting the plug to maintain the plug in the rotor relief opening.

2. The turbine engine of claim 1 , wherein the finger is aligned with the rotor relief hole.

3. The turbine engine of claim 1 , wherein the rotor relief hole defines a longitudinal axis and the finger extends along the longitudinal axis.

4. The turbine engine of claim 1 , wherein the plug has a cap and a body extending from the cap with the body extending into the rotor relief hole, and the finger contacts the cap to maintain the plug in the rotor relief opening.

5. The turbine engine of claim 1 , wherein the pocket seal extends to the fore opening.

6. The turbine engine of claim 1 , wherein the rotor relief hole is connected to the pocket internally between the blade mount and the rotor disk.

7. The turbine engine of claim 6 , wherein the pocket seal extends to the rotor relief hole.

8. The turbine engine of claim 1 , wherein the pocket seal contacts the plug.

9. The turbine engine of claim 1 , wherein the pocket is free from an aft opening in the aft surface such that the pocket remains entirely closed at the aft surface of the adjacent blade mounts.

10. The turbine engine of claim 1 , wherein the pocket has only the fore opening to enable insertion of the pocket seal into the pocket.

11. The turbine engine of claim 1 , further comprising a radial seal seated between the fore seal plate and the blade mounts adjacent the fore plate edge and abutting the pocket seal to enhance sealing at the fore plate edge.

12. The turbine engine of claim 1 , wherein the blade mount is bonded to the rotor disk in the absence of a mechanical connection.

13. The turbine engine of claim 1 , wherein the pocket has a radially inward surface proximal the rotor disk and a radially outward surface distal to the rotor disk, and wherein the pocket seal is disposed along the radially outward surface.

14. The turbine engine of claim 1 , wherein the rotor relief hole is separate and spaced apart from the pocket in the blade mount.

15. The turbine engine of claim 1 , wherein the pocket is free from an opening in the blade attachment surface of the blade mount.

Assignees

• Honeywell Int Inc

Inventors

• Halfmann Steve
• Crites Daniel C
• Kahrs Michael
• Riahi Ardeshir
• Miller Jude

Classifications

• F05D2230/23

  by permanently joining parts together · CPC title

• F01D5/12

  Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title

• F01D5/3015

  with side plates · CPC title

• F01D11/006 Primary

  Sealing the gap between rotor blades or blades and rotor · CPC title

• F01D5/081

  Cooling fluid being directed on the side of the rotor disc or at the roots of the blades (F01D5/087 takes precedence) · CPC title