IP Library › Granted Patent US 12,571,312
Granted Patent B2
US 12,571,312 · App. 18/771,029 · Granted Mar 10, 2026

Adaptive blending system and method for removing residual stress in turbine engine component

Inventors: Garrett Kernozicky (Mansfield, CT); Iuliana Cernatescu (Glastonbury, CT)
Assignee: RTX CORPORATION
F01D5/005B23P6/045G01N23/20008
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Quick Facts
Patent No.
US 12,571,312
App. No.
18/771,029
Granted
Mar 10, 2026
Kind
B2
Abstract

An adaptive blending system and method are disclosed. A blending operation is performed on defects of a turbine engine component based on an initial blending profile. The adaptive blending system ad method dynamically observes and detects strain data of the defects during the blending operation. The detected strain data of the defects are sent to a processor for analysis in a substantially real-time basis to obtain strain levels of the defects. The processor generates a strain level of a defect based on the detected strain data, and generates an adjusted blending profile for use in the blending operation.

Claims (17)

1 . A method for performing a blending operation on a damaged engine component, the method comprising:

operating the blending operation on a damaged region of the damaged engine component based on an initial blending profile;

detecting repaired conditions of the damaged region while the blending operation is performed, wherein the detecting captures strain data of the damaged region using a sensing device, and wherein the detecting is performed either periodically during the blending process or substantially real-time during the blending process;

processing the strain data to calculate a detected strain level;

adjusting the blending profile if the detected strain data fails to meet predetermined criteria, wherein the predetermined criteria includes an acceptable strain level; and

operating the blending process on the damaged region based on an adjusted blending profile, wherein the blending operation is completed when the detected strain level of the damaged region meets the acceptable strain level.

2 . The blending method of claim 1 , wherein the steps of detecting the repaired condition, adjusting the blending profile, and operating the blending process based on the adjusted blending profile are repeated until the predetermined criteria are met.

3 . The blending method of claim 1 , wherein the sensing device

emits an X-ray beam on the damaged region during the blending operation;

detecting diffracted X-rays received from the damaged region;

converts the diffracted X-rays to the strain data; and

sending the strain data to a processor for processing.

4 . The blending method of claim 3 , wherein the processor converts the strain data into digital data, compares the digital data with the predetermined criteria to calculate a detected strain level of the damaged region at the time when the repaired data is detected, wherein the predetermined criteria is stored in a database, and generates the adjustment data to adjust the blending profile if the strain level fails to meet an acceptable strain level.

5 . The blending method of claim 1 , further comprising outputting the image data to a user interface for review by an operator.

6 . The method of claim 1 , wherein the adjusting the blending profile if the detected strain data fails to meet predetermined criteria includes adjusting an operating angle, and operation time, an operating depth, and/or a force intensity of a blending tool.

7 . The method of claim 1 , wherein the adjusting the blending profile if the detected strain data fails to meet predetermined criteria occurs automatically.

8 . The method of claim 1 , wherein the predetermined criteria further include a threshold defect depth, a threshold defect length, a threshold aspect ratio, a threshold number of defects per blade, and/or a threshold number of defects per component.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 10, 2025
From: KERNOZICKY, GARRETT; CERNATESCU, IULIANA
To: RTX CORPORATION
Reel/Frame 069816/0643 →
Continuity (1)
Related Publication 20260015941A1 · Jan 15, 2026
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