IP Library Granted Patent US 8,627,695
Granted Patent B2
US 8,627,695 · App. 12/988,436 · Granted Jan 14, 2014

Method for ultrasound shot-blasting of turbomachine parts

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,627,695
App. No.
12/988,436
Granted
Jan 14, 2014
Kind
B2
Abstract

A method for ultrasound shot-blasting by a cloud of balls set in motion through contact with a sonotrode having one metallic surface including an area of difficult access, characterized in that the surface is that of a hook axially restrained on a turbomachine blade including a groove provided between the hook and the base of the blade, and the cloud of balls is contained in a chamber encompassing the groove and the surface portion outside the groove.

Claims (25)

1. A method for ultrasound shot-blasting a metal surface of a turbomachine blade including a foot which is slidably mountable in a dovetailed axial slot of a disk, and a hook which axially retains the turbomachine blade in the dovetailed axial slot of the disk, comprising:

placing a plurality of balls in a chamber to shot-blast a hook of the turbomachine blade; and

subjecting a vibrating surface of the chamber to ultrasound oscillations by a sonotrode to create a cloud of balls striking the metal surface including the hook of the turbomachine blade which axially retains the turbomachine blade, the metal surface including a groove provided between the hook and the foot of the blade, and a surface portion outside said groove,

wherein the cloud of balls is contained in the chamber encompassing said groove and said surface portion outside said groove, and the chamber is defined by first and second walls on two opposite sides, the vibrating surface on one side, and the surface supporting the hook on another side between the first and second walls, and

wherein the cloud of balls in the groove shot-blasts an interior of the groove between the hook and the foot of the blade and shot-blasts the surface portion outside said groove.

2. The shot-blasting method as claimed in claim 1 , wherein said groove has a width of between 1.5 mm and 10 mm and a depth of between 1.5 mm and 20 mm.

3. The shot-blasting method as claimed in claim 1 or 2 , wherein balls have:

a diameter less than or equal to 2.5 mm, and

a weight greater than or equal to 0.5 g.

4. The shot-blasting method as claimed in claim 3 , wherein amplitude of ball movements is greater than or equal to 20 μm.

5. The shot-blasting method as claimed in claim 1 , wherein shot-blasting treatment time is between 5 and 200 seconds.

6. The shot-blasting method as claimed in claim 1 , wherein the balls have a diameter of between 300 μm and 2.5 mm.

7. The shot-blasting method as claimed in claim 1 , wherein the balls are steel bearing balls, tungsten carbine balls, or aluminum balls.

8. The shot-blasting method as claimed in claim 1 , wherein the hook is made with a material from the group comprising steel, titanium alloys, nickel-based superalloys or aluminums.

9. The shot-blasting method as claimed in claim 1 , wherein the groove provided between the hook and the foot of the blade has a width between 1.5 mm and 10 mm, and a depth between 1.5 mm and 20 mm.

10. A method for ultrasound shot-blasting a metal surface of a turbomachine blade including a hook which axially retains the turbomachine blade, comprising:

placing a plurality of balls in a chamber; and

subjecting a vibrating surface of the chamber to ultrasound oscillations by a sonotrode to create a cloud of balls striking the metal surface including the hook of the turbomachine blade which axially retains the turbomachine blade, the metal surface including a groove provided between the hook and a foot of the blade, and a surface portion outside said groove,

wherein the cloud of balls is contained in the chamber encompassing said groove and said surface portion outside said groove, and the chamber is defined by first and second walls on two opposite sides, the vibrating surface on one side, and the surface supporting the hook on another side between the first and second walls, and

wherein the surface supporting the hook on another side between the first and second walls comprises a portion of the foot of the blade in contact with the first chamber wall, and a portion of a platform of the blade in contact with the second chamber wall.

11. A method for ultrasound shot-blasting a metal surface of a turbomachine blade including a hook which axially retains the turbomachine blade, comprising:

placing a plurality of balls in a chamber; and

subjecting a vibrating surface of the chamber to ultrasound oscillations by a sonotrode to create a cloud of balls striking the metal surface including the hook of the turbomachine blade which axially retains the turbomachine blade, the metal surface including a groove provided between the hook and a foot of the blade, and a surface portion outside said groove,

wherein the cloud of balls is contained in the chamber encompassing said groove and said surface portion outside said groove, and the chamber is defined by first and second walls on two opposite sides, the vibrating surface on one side, and the surface supporting the hook on another side between the first and second walls, and

wherein the hook which axially retains the turbomachine blade comprises an axial portion parallel to the blade platform, a radial portion perpendicular to the axial portion, and a rounded transition area between the axial portion and the radial portion, with the blade foot and the radial portion creating the groove between the hook and the foot of the blade.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →