IP Library Granted Patent US 7,117,115
Granted Patent B2
US 7,117,115 · App. 11/124,085 · Granted Oct 3, 2006

Three-dimensional machine with simultaneous measurements

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Quick Facts
Patent No.
US 7,117,115
App. No.
11/124,085
Granted
Oct 3, 2006
Kind
B2
Abstract

A method for three-dimensional measurement of coordinates of a set of N predetermined points of the surface of a mechanical part to be measured, relatively to a predetermined reference system, and the direction cosines of the theoretical normals thereto at the theoretical points corresponding to the N predetermined points are known, and including a preparatory phase, in which the coordinate points, corresponding to the N predetermined points of a first mechanical part taken as a standard part, are measured; an initialization phase, in which displacement measurements (along the normals are read on the N points of the standard part; a measurement phase, in which N linear displacement measurements performed on the N points of the part to be measured corresponding to the N points of the standard part, are read; and a computation phase, in which the coordinates of the N points of the part to be measured are computed.

Claims (14)

1. A method for the three-dimensional measurement of coordinates (xli, yli, zli) of a set of N predetermined points (Plij) of the surface of a mechanical part to be measured relatively to a predetermined reference system (Ro) and in which the direction cosines (cxthij, cythij, czthij) of the theoretical normals (Nthij) thereto are known at the theoretical points (Pthij) corresponding to said N predetermined points (Plij), and including:

a preparatory phase, in which the coordinates (xoij, yoij, zoij) of N points (Poij), corresponding to said N predetermined points (Plij) of the surface of a first mechanical part taken as a standard part, are measured relatively to the reference system (Ro) and stored;

an initialization phase, wherein N linear displacement measurements (loij) along said normals (Nthij) are simultaneously and respectively read on said N points (Poij) of said standard part and stored;

a measurement phase, wherein N linear displacement measurements (llij), simultaneously and respectively performed on said N points (Plij) of the part to be measured, corresponding to the N points (Poij) of said standard part, are read and stored;

a computation phase, in which the three-dimensional coordinates (xlij, ylij, zlij) of the N points of the part to be measured are computed from the three-dimensional coordinates (xoij, yoij, zoij) of the N points of said standard part, from the linear measurements (loij, llij) and from the direction cosines (cxthij, cythij, czthij) of the N theoretical normals at these points, said computed three dimension coordinates being stored, displayed or printed.

2. The method according to claim 1 , wherein at each point, the measurement is linearly performed along the theoretical normal by an individual relative displacement sensor (Cij) at the point.

3. The method according to claim 2 , wherein each sensor (Cij) measurement is initialized beforehand, separately from that of the other sensors, but simultaneously with them.

4. The method according to claim 3 , wherein the sensors (Cij) are inductive sensors.

5. The method according to claim 1 , wherein the three-dimensional coordinates (xoij, yoij, zoij) of the N points of the standard part are measured by means of a 3D CMM.

6. A three-dimensional machine with simultaneous measurements for applying the method according to any of claims 1 to 5 , including a computing module, a control module and a measurement platen, wherein said machine includes at least one array of displacement sensors (Cij) arranged, in an open position, so as to allow a part to be mounted on the platen, and in a closed position, to put all the sensors (Cij) in operational contact for measuring the part.

7. The machine according to claim 6 , wherein said machine includes at least two arrays of arrays (Cij) positioned facing each other to surround the part.

8. The machine according to claim 6 , wherein the displacement sensors are inductive sensors.

9. The machine according to claim 6 , wherein the computing module is arranged so as to compute the overall geometrical characteristics of the surface of the part.

10. The machine according to claim 6 , wherein said machine is configured to reconstruct profiles of blades from turbine engines.

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 Aug 2, 2005
From: BEIGNON, DOMINIQUE; CHOQUET, PASCAL; GANDUBERT, JOEL; LEVY, JEAN-JACQUES
To: SNECMA MOTEURS
Reel/Frame 016830/0099 →