IP Library Granted Patent US 8,973,428
Granted Patent B2
US 8,973,428 · App. 14/122,588 · Granted Mar 10, 2015

Method and device for measuring a part in a turbine engine

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Quick Facts
Patent No.
US 8,973,428
App. No.
14/122,588
Granted
Mar 10, 2015
Kind
B2
Abstract

A device for measuring a part in a turbine engine, including a rod including a portion with a profile that corresponds to a profile of a portion of a calibration part of a same type as a part under examination, the portion of the rod further including visible marks for remote measurement arranged along its length.

Claims (23)

1. A method of measuring deformation of a part in a turbine engine by a device including a rod including a portion with a profile that corresponds to a profile of a portion of a calibration part of same type as a part under examination, the portion of the rod further including visible marks for remote measurement arranged along its length, the method comprising:

a) inspecting the profile of the rod in three dimensions with help of a three-dimensional model of the profile of the portion of the calibration part;

b) engaging the rod in an endoscope orifice in a casing of the engine;

c) positioning and fastening the portion of the rod on the portion of the part for inspection that corresponds to the portion of the calibration part;

d) introducing an endoscope inside the casing of the engine;

e) measuring deformation of the portion of the part for inspection with help of the endoscope; and then

f) withdrawing the rod from the inside of the engine casing and performing the a) inspecting once more to verify that the rod has not been subjected to deformation during the b) engaging.

2. A method according to claim 1 , wherein the part is a blade of a rotor in an engine, and the method is performed on first and second portions of the blade in succession, the first portion is a leading edge of the blade and the second portion is a tip of the blade.

3. A method according to claim 1 , wherein, the part is a rotor blade in an engine and the rod is shaped to match the leading edge of the blade, and the rotor is turned until a rim of a free end of the portion of the rod comes into contact with a suction side face of the blade to align the portion of the rod with a leading edge of the blade.

4. A method according to claim 1 , wherein the visible marks for remote measurement comprise graduations that are regularly distributed along a length of the rod portion.

5. A method according to claim 4 , wherein each graduation is made in a form of a colored line with a color of each line differing from colors of adjacent colored lines.

6. A method according to claim 1 , wherein the device includes fastening and positioning means for fastening and positioning the rod portion in a stationary position in alignment with the portion of the part under examination that corresponds to the portion of the calibration part.

7. A method according to claim 6 , wherein, the part is a rotor blade arranged inside a casing of a turbine engine, and the fastening and positioning means comprises an endpiece engaged on the end of the rod remote from the shaped portion of the rod, the endpiece being fastened in an endoscope orifice in the casing of the engine and including an orifice for passing the endoscope.

8. A method according to claim 6 , wherein the positioning means includes a rim arranged at a free end of the portion of the rod and serving as an abutment for positioning the rod on the part under examination.

9. A method according to claim 1 , wherein the portion is connected to a second portion of the rod that is L-shaped.

10. A method according to claim 9 , wherein the portion of the rod follows the profile of a tip of a rotor blade and is inclined relative to a branch to which it is connected.

11. A method according to claim 9 , wherein the portion of the rod follows a profile of a leading edge of a rotor blade and it extends substantially perpendicularly to a branch of the L-shape to which it is connected and in a direction going away from an other branch of the L shape.

12. A device for performing the method according to claim 1 , comprising:

a rod including a portion with a profile that corresponds to a profile of a portion of a calibration part of same type as a part under examination,

the portion of the rod further comprising visible marks for remote measurement arranged along its length; and

fastening and positioning means for fastening and positioning the rod portion in a stationary position in alignment with the portion of the part under examination that corresponds to the portion of the calibration part.

13. A case for carrying the device according to claim 12 , comprising:

support means for supporting at least one rod, the support means comprising a plurality of studs, each supporting the rod at a predetermined height such that contact points where the support studs make contact with the rod define a three-dimensional model of a profile of a portion of the calibration part.

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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 26, 2013
From: BARTHELEMY, DENIS; ROSSIO, JEAN-DOMINIQUE; MONNIER, ERIC; PAGLIANO, FRANCOIS; MARTIN, PIERRE ALBERT, MARIE
To: SNECMA
Reel/Frame 031681/0553 →