IP Library Granted Patent US 7,800,364
Granted Patent B2
US 7,800,364 · App. 12/436,829 · Granted Sep 21, 2010

Device for inspecting tangential recesses in a rotor disk

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Quick Facts
Patent No.
US 7,800,364
App. No.
12/436,829
Granted
Sep 21, 2010
Kind
B2
Abstract

An inspection device for inspecting tangential recesses in a rotor disk by means of eddy currents is disclosed. The device includes a probe containing a plurality of sensors arranged to acquire a plurality of data series during a scan stroke, and the probe is mounted on moving equipment that is slidable in a support that is provided with two positioning members for co-operating with recesses neighboring the recess for inspection.

Claims (11)

1. An inspection device for inspecting tangential recesses in a rotor disk by means of eddy currents, the device comprising:

a probe of cross-section with an outline that matches the outline of the section of such a recess,

wherein said probe includes

a plurality of sensors arranged for acquiring a plurality of data series during a scan stroke in the longitudinal direction of the recess,

a support with two positioning members, each of said positioning members includes a rod extending from the support which is inserted and cooperates respectively with two recesses neighboring the recess for inspection, and

sliding moving equipment carrying said probe and arranged to guide said probe along said recess during inspection.

2. An inspection device according to claim 1 , wherein the two positioning members include two expandable elements spaced apart by a distance corresponding to the distance between said neighboring recesses, said elements being arranged to be engaged and locked therein to position said support in such a manner that said probe can be engaged in said tangential recess for inspection.

3. A device according to claim 1 , including indexing means for monitoring at least one of the position the progress of the probe in said recess for inspection.

4. A device according to claim 1 , wherein said sensors are distributed in blocks of the probe, the blocks being hinge-mounted with outwardly-directed resilient bias so as to guarantee that said blocks make contact against the corresponding zones of said recess for inspection.

5. A device according to claim 1 , including a multi-channel generator-receiver for activating all of the sensors substantially simultaneously at different positions along the probe in said recess for inspection.

6. A device according to claim 1 , wherein the sensors are disposed at the leading end of the probe.

Assignments (3)
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 →
MERGER Recorded May 17, 2018
From: SNECMA SERVICES SA (A/K/A SNECMA SERVICES)
To: SNECMA
Reel/Frame 045829/0954 →