IP Library Granted Patent US 7,359,829
Granted Patent B2
US 7,359,829 · App. 11/426,121 · Granted Apr 15, 2008

Method of inspecting the profile of the connection zone between the cylindrical portion and the taper of a roller for a turbomachine roller bearing

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Quick Facts
Patent No.
US 7,359,829
App. No.
11/426,121
Granted
Apr 15, 2008
Kind
B2
Abstract

A method of inspecting the profile of the connection zone between the cylindrical portion and the taper of a roller for a turbomachine roller bearing. The method includes taking a measurement of the surface profile of the roller; on the basis of a calculation of the first derivative of the measured profile, calculating straight line segments for each of the geometrical zones of the roller, where the straight line segments model the first derivative of the measured profile; calculating the radii of curvature of the surface profile of the roller by taking the first derivative of the straight line segments; and comparing the calculated radii of curvature with predefined threshold values in order to verify continuity thereof.

Claims (33)

1. A method of inspecting a surface profile of the connection zone between the cylindrical portion and the taper of a roller for a turbomachine roller bearing, the surface profile of said roller being geometrically defined by geometrical zones including at least one first zone corresponding to the taper of the roller, by at least one second zone corresponding to the connection zone between the cylindrical portion and the taper of said roller, and by a third zone corresponding to the cylindrical portion of said roller, the method comprising the steps of:

in a real space, taking a measurement of the surface profile of the roller;

in a theoretical space, determining theoretical straight line segments;

on the basis of a calculation of the first derivative of the measured surface profile and the theoretical straight line segments, calculating straight line segments for each of said geometrical zones of the roller, where said straight line segments model the first derivative of the measured surface profile in order to filter out disturbances that are superposed on the measured surface profile;

calculating radii of curvature of the surface profile of the roller by taking the first derivative of the straight line segments; and

comparing the calculated radii of curvature with predefined threshold values in order to verify continuity thereof.

2. A method according to claim 1 , wherein the step of calculating straight line segments comprises:

selecting a theoretical surface profile for the roller;

calculating the first derivative of the theoretical surface profile in order to obtain the theoretical straight line segments for each of said geometrical zones of the roller;

calculating the distance between the first derivative of the measured surface profile and the theoretical straight line segments; and

calculating the gradient and the intercept on the ordinate of each straight line segment by minimizing the distance between the first derivative of the measured surface profile and the theoretical straight line segments.

3. A method according to claim 2 , in which the step of minimizing the distance between the first derivative of the measured profile and the theoretical straight line segments is performed by the least squares method.

4. A method according to claim 2 , in which the theoretical surface profile of the first geometrical zone of the roller is a circular arc, the theoretical surface profile of the second geometrical zone of the roller is another circular arc, and the theoretical surface profile of the third geometrical zone of the roller is rectilinear.

5. A method of inspecting a surface profile of the connection zone between the cylindrical portion and the taper of a roller for a turbomachine roller bearing, the surface profile of said roller being geometrically defined by geometrical zones including at least one first zone corresponding to the taper of the roller, by at least one second zone corresponding to the connection zone between the cylindrical portion and the taper of said roller, and by a third zone corresponding to the cylindrical portion of said roller, the method comprising the steps of:

in a real space, taking a measurement of the surface profile of the roller;

on the basis of a calculation of the first derivative of the measured surface profile, calculating straight line segments for each of said geometrical zones of the roller, where said straight line segments model the first derivative of the measured surface profile;

calculating radii of curvature of the surface profile of the roller by taking the first derivative of the straight line segments; and

comparing the calculated radii of curvature with predefined threshold values,

wherein the step of calculating straight line segments comprises:

selecting a theoretical surface profile for the roller;

in a theoretical space, calculating the first derivative of the theoretical surface profile in order to obtain theoretical straight line segments for each of said geometrical zones of the roller;

calculating the distance between the first derivative of the measured surface profile and the theoretical straight line segments; and

calculating the gradient and the intercept on the ordinate of each straight line segment by minimizing the distance between the first derivative of the measured surface profile and the theoretical straight line segments.

6. The method of claim 1 , wherein said step of taking said measurement of the surface profile of the roller is performed by a sensor configured to follow said surface profile of the roller and to transmit a signal to a computer, said signal corresponding to a position of the sensor as the sensor travels along said surface, and

wherein said calculating steps are performed by said computer.

7. The method of claim 1 , wherein said predefined threshold values correspond to minimum radii of curvature for connections zones between the cylindrical portion and tapers of the roller.

8. The method of claim 5 , wherein said calculating steps are performed by a computer.

9. A method of inspecting a surface profile of the connection zone between the cylindrical portion and the taper of a roller for a turbomachine roller bearing, the surface profile of said roller being geometrically defined by geometrical zones including at least one first zone corresponding to the taper of the roller, by at least one second zone corresponding to the connection zone between the cylindrical portion and the taper of said roller, and by a third zone corresponding to the cylindrical portion of said roller, the method comprising the steps of:

selecting a theoretical surface profile of the roller such that the theoretical surface profile of the first geometrical zone of the roller is a circular arc, the theoretical surface profile of the second geometrical zone of the roller is another circular arc, and the theoretical surface profile of the third geometrical zone of the roller is rectilinear;

taking a measurement of the surface profile of the roller;

on the basis of a calculation of the first derivative of the measured surface profile and first derivatives of the selected theoretical surface, calculating straight line segments for each of said geometrical zones of the roller, where said straight line segments model the first derivative of the measured surface profile in order to filter out disturbances that are superposed on the measured surface profile;

calculating radii of curvature of the surface profile of the roller by taking the first derivative of the straight line segments; and

comparing the calculated radii of curvature with predefined threshold values in order to verify continuity thereof.

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 Aug 7, 2006
From: DUSSERRE-TELMON, GUY FRANK PAUL; LEEDER, LAURENT
To: SNECMA
Reel/Frame 018158/0566 →