Locking of rotor blades on a rotor disk

• US 4,389,161 A
• Filed: 12/19/1980
• Issued: 06/21/1983
• Est. Priority Date: 12/19/1980
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Brumen, Claudio
• Primary Examiner(s): Casaregola, Louis J.
• Assistant Examiner(s): Simenauer, Jeffrey A.
• Application Number:
  US06/218,241
• Time in Patent Office: 914 Days
• Field of Search: 416/221, 416/220 R, 416/218, 403/316, 403/317, 403/319, 403/355, 403/356, 403/358, 403/381, 403/359, 403/323, 403/324, 403/331
• US Class Current: 416/220.00R
• CPC Class Codes: F01D 5/326 Locking of axial insertion type blades by other means

Abstract

A rotor stage assembly 20 of the type adapted for use in an axial flow gas turbine engine is disclosed. The assembly includes a rotor disk 36, at least two rotor blades 42 and a scalloped lock pin 52. The scalloped lock pin has lugs 54. The disk is adapted by a groove 40 and each blade is adapted by a groove 48 to receive the scalloped lock pin. During assembly the scalloped lock pin is alignable with blade attachment slots 44 in the disk to enable insertion of the blades and is slidable in the grooves 40, 48 to bring each lug 54 on the scalloped pin into engagement with a corresponding groove in a rotor blade.

Claims

1. A method of installing rotor blades on a rotor disk comprising the steps of:

placing a scalloped lock pin having lugs in axial engagement with the periphery of the rotor disk by installing the pin in a groove which faces outwardly;

aligning the scalloped pin with slots in the disk to permit insertion of at least two rotor blades in a generally axial direction, each into a corresponding blade attachment slot in the disk;

inserting said rotor blades in the blade attachment slot such that a groove in each rotor blade is axially and radially aligned with and faces said groove in the disk;

sliding the scalloped lock pin along the groove in the disk to bring the lugs of the scalloped pin into engagement with the correspondingly aligned grooves in each of the rotor blades; and

securing the lock pin against circumferential movement.

2. In an axial flow rotary machine of the type having a rotor assembly which includes a disk having slots extending in a generally axial direction, each slot adapting the disk to receive a corresponding rotor blade, the improvement which comprises:

a rotor disk having a groove extending in a generally circumferential direction and facing in a generally outward direction;

at least two rotor blades each having a root, each root having a groove extending in a generally circumferential direction, facing and in axial and radial alignment with the groove in the disk;

at least one scalloped lock pin for engaging both the rotor disk and at least two rotor blades, each lock pin extending circumferentially in the disk groove to engage the disk and having radial lugs, each lug extending radially into the corresponding groove in the root of a corresponding blade to trap the rotor blade against fore and aft movement with respect to the disk, at least one pair of adjacent lugs being spaced one from the other a sufficient distance apart to permit passage of the blades therethrough.

3. The axial flow rotary machine of claim 2 wherein each slot has a width W and wherein each lug of said scalloped lock pin is spaced from the adjacent lug of said pin by a distance greater than the width W.