Methods and apparatuses for blade locking

Patent metadata

Field	Value
Publication number	US-12221899-B2
Application number	US-202318210347-A
Country	US
Kind code	B2
Filing date	Jun 15, 2023
Priority date	Jun 15, 2023
Publication date	Feb 11, 2025
Grant date	Feb 11, 2025

Abstract

A lock lug for inhibiting movement of a plurality of rotor blades includes a body and an engagement mechanism. The body is sized and configured to be received within the rim slot of the rotor disk and defines a dovetail receiving aperture. The engagement mechanism extends from the body and has a retracted configuration configured to allow entry and exit of a dovetail of at least one or more of the plurality of rotor blades into and out of the dovetail receiving aperture and an extended configuration configured to block the dovetail from entering the dovetail receiving aperture.

First claim

What is claimed is:

1. A lock lug for inhibiting movement of a plurality of rotor blades within a rim slot along a circumference of a rotor disk, comprising:
a body sized and configured to be received within the rim slot of the rotor disk, the body comprising:
a first sidewall;
a second sidewall opposite the first sidewall;
a bottom that extends from the first sidewall to the second sidewall connecting the first and second sidewalls forming a dovetail receiving aperture configured to receive a dovetail of a rotor blade; and

an engagement mechanism comprising a spring connected to one or more of the first sidewall, second sidewall and bottom, the engagement mechanism is configured to extend from the body and having (i) a retracted configuration configured to allow entry and exit of a dovetail of at least one or more of the plurality of rotor blades into and out of the dovetail receiving aperture and (ii) an extended configuration configured to block the dovetail from entering the dovetail receiving aperture.

2. The lock lug of claim 1 , wherein the spring biases the engagement mechanism toward the extended configuration.

3. The lock lug of claim 1 , wherein the engagement mechanism extends from the bottom of the body and biases the body radially outward.

4. The lock lug of claim 1 , wherein the engagement mechanism comprises a spring, wherein the spring extends outward from the body when the engagement mechanism is in the extended configuration.

5. The lock lug of claim 1 , further comprising a standoff extending radially upward from the body, wherein the standoff is operable to move the engagement mechanism from the extended configuration to the retracted configuration when depressed.

6. The lock lug of claim 1 , wherein the engagement mechanism extends from the first sidewall of the body.

7. The lock lug of claim 1 , wherein the engagement mechanism extends into the dovetail receiving aperture.

8. The lock lug of claim 1 , wherein the engagement mechanism comprises a spacer, wherein the spacer extends into the dovetail receiving aperture when the engagement mechanism is in the extended configuration, thereby inhibiting rotation of the plurality of rotor blades within the rim slot.

9. The lock lug of claim 8 , further comprising the spring operable to extend the spacer into the dovetail receiving aperture.

10. A rotor disk assembly comprising:
a rotor disk comprising a rim slot extending along a circumference of the rotor disk and a load slot intersecting the rim slot;
a plurality of rotor blades disposed within the rim slot of the rotor disk; and
a lock lug disposed within the rim slot of the rotor disk, the lock lug comprising:
a body sized and configured to be received within the rim slot of the rotor disk, the body moveable between an assembly position and an engaged position, the body comprising:
a first sidewall;
a second sidewall opposite the first sidewall;
a bottom that extends from the first sidewall to the second sidewall connecting the first and second sidewalls forming a dovetail receiving aperture configured to receive a dovetail of a rotor blade, wherein the dovetail receiving aperture receives a dovetail of the plurality of rotor blades when the body is in the assembly position and is offset from the dovetail when the body is in the engaged position; and
an engagement mechanism comprising a spring connected to one or more of the first sidewall, second sidewall and bottom, the engagement mechanism is configured to extend from the body and operable to retain the body in the engaged position, wherein the engagement mechanism has (i) a retracted configuration that places the body in the assembly position within the rim slot to allow entry and exit of the dovetail of the plurality of rotor blades into and out of the dovetail receiving aperture and (ii) an extended configuration that places the body in the engaged position within the rim slot thereby offsetting the dovetail receiving aperture from the dovetail such that the dovetail is blocked from entering the dovetail receiving aperture.

11. The rotor disk assembly of claim 10 , wherein the engagement mechanism extends from the bottom of the body and biases the body radially outward toward the engaged position.

12. The rotor disk assembly of claim 10 , wherein the bottom inhibits rotation of the dovetail when the body is in the engaged position.

13. The rotor disk assembly of claim 10 , wherein the engagement mechanism extends from the first sidewall and the second sidewall of the body.

14. The rotor disk assembly of claim 10 , wherein the engagement mechanism comprises a first spring disposed within the first sidewall and a first spacer adjacent to the first spring, wherein the first spring is operable to extend the first spacer into the dovetail receiving aperture.

15. The rotor disk assembly of claim 14 , wherein the engagement mechanism further comprises a second spring disposed within the second sidewall and a second spacer adjacent to the second spring, wherein the second spring is operable to extend the second spacer into the dovetail receiving aperture.

16. The rotor disk assembly of claim 10 , wherein the first sidewall extends into the load slot.

17. The rotor disk assembly of claim 10 , wherein at least one of the plurality of rotor blades defines a platform notch disposed above the lock lug.

Assignees

• Gen Electric

Inventors

• Ganiger Ravindra Shankar
• Pachaiappan Dharmaraj
• Ganji Nageswar Rao
• Namadevan Arvind
• Carnes Jeffrey D
• Lavender Charles Eric
• Ballman Steven Mark

Classifications

• F01D5/303

  in a circumferential slot · CPC title

• F01D5/3023

  of radial insertion type, e.g. in individual recesses · CPC title

• F01D5/32 Primary

  Locking, e.g. by final locking blades or keys · CPC title

• F01D5/3007

  of axial insertion type · CPC title

• F01D5/326 Primary

  Locking of axial insertion type blades by other means · CPC title