IP Library Granted Patent US 7,305,898
Granted Patent B2
US 7,305,898 · App. 11/143,484 · Granted Dec 11, 2007

Installation for non-destructive inspection of a part

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Quick Facts
Patent No.
US 7,305,898
App. No.
11/143,484
Granted
Dec 11, 2007
Kind
B2
Abstract

An installation for non-destructive inspection makes use simultaneously of sensors responsive to different physical characteristics. In an example, a sensor support, e.g. a kind of carriage having running wheels via which it comes into contact with the surface to be inspected, is fitted with two types of sensor, namely an eddy current sensor and at least one ultrasound sensor.

Claims (18)

1. An installation for non-destructive inspection of a rotor-forming part having an axis of revolution and including annular cavities axially adjacent to one another, the installation comprising a sensor support suitable for moving over a surface of said rotor-forming part to be inspected, and means for combining circular displacement and radial displacement of said support and/or of said rotor-forming part, and said support being fitted with a plurality of sensors for sensing different physical characteristics in order to pick up data groups specific to said sensors, and corresponding to respective defined zones of said surface, in a single scan thereof,

wherein said rotor-forming part includes a common space extending axially between said annular cavities, the installation including a horizontal turntable on which said rotor-forming part can be placed for inspection, a vertical column movable above said turntable and arranged to engage in said common space of said rotor-forming part for inspection, a chain of locking links mounted to slide along said column, and a deflector carried by said column and comprising an angled guide duct for said chain, presenting a lateral outlet through which the chain leaves substantially horizontally in the form of a rigid segment having links blocked mutually one against another, the end of said rigid segment being connected to said sensor support to move said sensor support while facing a surface for inspection of said rotor-forming part.

2. An installation according to claim 1 , wherein said sensors make use of different physical phenomena.

3. An installation according to claim 1 , wherein said sensors include an eddy current sensor and at least one ultrasound sensor, and said support is fitted with said eddy current sensor and with said at least one ultrasound sensor.

4. An installation according to claim 1 , wherein said sensor support includes running wheels via which said sensor support comes into contact with said surface to be inspected during said scan.

5. An installation according to claim 1 , further comprising a vessel containing a coupling liquid, wherein said sensor support is constrained to move in said coupling liquid.

6. An installation according to claim 5 , wherein said coupling liquid is water.

7. An installation according to claim 1 , including a horizontal turntable on which said part is placed so that said axis of revolution coincides with the axis of rotation of said turntable.

8. An installation according to claim 7 , wherein said turntable is installed in a vessel filled with a coupling liquid.

9. An installation according to claim 7 , wherein said support is attached in hinged manner to the end of displacement means arranged to move said support radially relative to the axis of rotation of said turntable.

10. An installation according to claim 3 , wherein said at least one ultrasonic sensor includes two ultrasound sensors and said support is fitted with said two ultrasound sensors disposed on either side of said eddy current sensor.

11. An installation according to claim 10 , wherein said eddy current sensor is arranged to be placed facing an individual zone under inspection, and wherein the two ultrasound sensors are oriented so that action axes of said two ultrasound sensors converge substantially towards said individual zone.

12. An installation according to claim 11 , wherein said action axes lie substantially in the same plane.

13. An installation according to claim 12 , wherein said two ultrasound sensors are operated in alternation.

14. An installation according to claim 1 , wherein said turntable is located in the bottom of a vessel shaped and dimensioned to receive said part, and wherein said vessel is filled with a coupling liquid necessary for proper operation of at least one of the said sensors.

15. An installation according to claim 1 , wherein said deflector houses a sprocket wheel meshing with said chain and driven by a controlled electric motor.

16. An installation according to claim 1 , wherein said deflector is connected to the bottom end of said column, and wherein said column is vertically movable to enable said deflector to be positioned at a height suitable for enabling said sensor support to scan a given annular area of said part.

17. An installation according to claim 1 , wherein said turntable has a vertical axis of rotation.

Assignments (4)
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 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 3, 2005
From: CABANIS, PATRICK; COULETTE, RICHARD; MARCEAU, CHRISTIAN
To: SNECMA MOTEURS
Reel/Frame 016656/0643 →