Process for machining tubular parts and apparatus for carrying out the process

Claim 2

A process for machining a tubular part whose cross sections have circular internal and external circumferences, wherein the wall of said tubular part has an external circumference and an internal circumference which are not coaxial, resulting in varying wall thicknesses, comprising the steps of: (a) for a particular cross section, determining a reference diameter having one end at the tube surface at the point of maximum wall thickness and the other end at the tube surface at the point of minimum wall thickness, and determining the values of said maximum wall thickness and said minimum wall thickness; (b) determining the position of the center of the external circumference by locating the middle of the reference diameter; (c) determining the position of the center of the internal circumference on said reference diameter as spaced from the center of the external circumference in the direction of the minimum wall thickness by a distance equal to half of the difference between the maximum and minimum thicknesses; (d) fixing said tubular part, and displacing a tool carrier carrying a rotatable machining tool in a direction parallel to the longitudinal axis of said tubular part until aligned with said cross-section, and displacing said tool carrier transverse to said longitudinal axis so that said tool may rotate about an axis passing through the center of said internal circumference; (e) rotating said tool to describe a circle having as its center the center of said internal circumference at said cross-section, and radially displacing said tool in the direction of its axis of rotation to a desired depth of cut in the wall of said tubular part, and machining said wall until a desired substantially uniform wall thickness is obtained, said substantially uniform wall thickness being at most equal to said minimum wall thickness; and (f) removing said tool

Claim 3

A process according to claim 1 wherein after the tool is removed, steps (a) through (f) are repeated for another cross-section of said tubular part.

Claim 4

A process according to claim 1 or 2 wherein the dimensional characteristics of each section are supplied to the computing means of a numerically controlled machine tool which carries out the settings prior to each machining operation.

Claim 5

A process according to claim 1 or 2 wherein the tube is oriented about its longitudinal axis before the operation of machining in such a way that the reference axis of the section is parallel to the direction of transverse displacement of the carrier tool and carrier.

Claim 6

A process according to claim 4 wherein, after orientation of the tube, two sensors are brought into contact with the tube to determine the ends of the reference diameter.

Claim 7

A process according to claim 1 or 2 wherein the position and the thickness of the tube are continuously determined by means of an ultrasonic apparatus.

Claim 8

A process according to claim 6 wherein the maximum and minimum thicknesses and the position of the internal and external circumferences are determined by means of said ultrasonic apparatus.

Claim 9

A process for machining a tubular part according to claim 1 or 2, wherein said transverse displacement of said tool carrier and said radial displacement of said tool are maintained constant for a portion of the length of said part corresponding to several times the cutting width of said tool, comprising the steps of: (a) attributing to said portion a constant guide section which is very close to the several successive cross sections of the portion; (b) determining the characteristics of the guide section from the characteristics of said several successive sections; and (c) utilizing in machining an axis of rotation of the tool passing through the center of the internal circumference of the guide section, and the minimum wall thickness of said guide section as the maximum substantially uniform wall thickness after machining.

Claim 10

A process for machining a tubular part according to claim 8 comprising the following steps: (a1) determining for each of the successive cross sections of one said portion, the positon of the ends of the reference diameter going from the point at which the wall thickness is at a minimum to the point at which the wall thickness is at a maximum, and the values of said maximum and minimum wall thicknesses, (b1) taking as the angle of orientation of the reference diameter of the guide section of the portion, the arithmetic mean of the angles of orientation of the reference diameters of the successive cross sections, (c1) orienting the tubular part in such a way that said reference diameter of the guide section is parallel to the direction of said transverse diplacement of said tool carrier, (d1) bringing into contact with the tubular part two sensors whose points of contact define the ends of the reference diameter of the guide section and determining the position of the center of the external circumference of the guide section as the middle of said reference diameter, (e1) defining the maximum and minimum thicknesses of the guide section respectively as the arithmetic means of the maximum thicknesses and the minimum thicknesses of the successive sections of the portion, (f1) determining the position of the center of the internal circumference of the guide section as being located on the reference diameter of said guide section, at a distance from the center of the external circumference that is equal to half the difference between the maximum and minimum thicknesses of the guide section in the direction of the end of the reference diameter corresponding to the smallest thickness of tubular part, (g1) fixing said tubular part, and displacing said tool in a direction transverse to the longitudinal axis of said part so that said tool rotates about an axis passing through the center of the internal circumference of the guide section, (h1) radially displacing the tool in the direction of its axis of rotation to a cutting position where for the guide section, a constant wall thickness which is at most equal to its minimum thickness may be obtained, (i1) machining said tubular part, while maintaining said radial setting of the tool and displacing the tool carrier longitudinally along the portion for machining thereof, and (j1) removing the tool.

Claim 11

A process for machining a tubular part according to claim 8 comprising the following steps: (a2) determining for each of the successive cross sections of one said portion, the position of the ends of the reference diameter going from the point at which the wall thickness is at a minimum to the point at which the wall thickness is at a maximum, and the values of said maximum and minimum wall thicknesses, (b2) taking as the angle or orientation of the reference diameter of the guide section of the portion, the arithmetic mean of the angles of orientation of the reference diameters of the successive cross sections, (c2) orienting the tubular part in such a way that said reference diameter of the guide section is parallel to the direction of said transverse displacement of said tool carrier, (d2) bringing into contact with the tubular part two sensors whose points of contact define the ends of the reference diameter of the guide section and determining the position of the center of the external circumference of the guide section as the middle of said reference diameter, (e2) defining the maximum and minimum thicknesses of the guide section respectively as the arithmetic means of the maximum thicknesses and the minimum thicknesses of the successive sections of the portion, and (f2) computing the difference between said maximum and minimum thicknesses of the guide section, and comparing said difference with a predetermined eccentricity tolerance.

Claim 12

A process for machining a tubular part according to claim 10, wherein said difference is less than or equal to said eccentricity tolerance, and no subsequent machining is performed on said portion.

Claim 13

A process for machining a tubular part according to claim 10, wherein said difference is greater than said eccentricity tolerance, and the following steps are subsequently carried out: (g2) determining the position of the center of the internal circumference of the guide section as being located on the reference diameter of said guide section, at a distance from the center of the external circumference that is equal to half the difference between the maximum and minimum thicknesses of the guide section in the direction of the end of the reference diameter corresponding to the smallest thickness of tubular part, (h2) fixing said tubular part, and displacing said tool in a direction transverse to the longitudinal axis of said part so that said tool rotates about an axis passing through the center of the internal circumference of the guide section. (i2) radially displacing the tool in the direction of its axis of rotation to a cutting position where, for the guide section, a constant wall thickness which is at most equal to its minimum thickness may be obtained, (j2) machining said tubular part, while maintaining said radial setting of the tool and displacing the tool carrier longitudinally along the portion for machining thereof, and (k2) removing the tool.