Apparatus for and method of processing an edge of a tube

Patent metadata

Field	Value
Publication number	US-9682456-B1
Application number	US-201314044340-A
Country	US
Kind code	B1
Filing date	Oct 2, 2013
Priority date	Oct 2, 2013
Publication date	Jun 20, 2017
Grant date	Jun 20, 2017

Abstract

An abrading apparatus for processing an edge of a tube is disclosed. The abrading apparatus includes a rotational symmetry axis and a chassis comprising an input side, an output side opposite the input side, and an input coupler on the input side of the chassis. The input coupler is coaxial with the rotational symmetry axis. The abrading apparatus also includes a centering member, coupled to the output side of the chassis and coaxial with the rotational symmetry axis, and abrasive members, coupled to the output side of the chassis. The abrasive members define an abrasive face radially spaced outwardly from and generally symmetric about the rotational symmetry axis and facing in a direction generally parallel to the rotational symmetry axis.

First claim

The invention claimed is:

1. An abrading apparatus for processing an edge of a tube, the abrading apparatus comprising:
a rotational symmetry axis;
a chassis comprising an input side, an output side opposite the input side, and an input coupler on the input side, wherein the input coupler is coaxial with the rotational symmetry axis;
a centering member, coupled to the chassis on the output side and coaxial with the rotational symmetry axis, wherein:
the centering member is a non-abrasive disc having a non-metallic circumferential surface, and
the centering member is rotatable relative to the tube; and

abrasive members, coupled to the chassis on the output side, wherein:
each of the abrasive members comprises an abrasive face region perpendicular to the rotational symmetry axis,
the rotational symmetry axis is non-coincident with the abrasive face region of any one of the abrasive members,
at least one of the abrasive members comprises a stem and abrasive elements extending along the rotational symmetry axis, and
the chassis comprises at least one socket adapted to receive the stem.

2. The abrading apparatus of claim 1 , wherein abrasive face regions of the abrasive members collectively define an abrasive face.

3. The abrading apparatus of claim 2 , wherein the centering member extends farther from the chassis along the rotational symmetry axis than the abrasive face.

4. The abrading apparatus of claim 1 , wherein the chassis further comprises a partially enclosed housing around the abrasive members.

5. The abrading apparatus of claim 1 , wherein the chassis further comprises at least one through opening in communication with the input side of the chassis and the output side of the chassis.

6. The abrading apparatus of claim 1 , wherein the centering member is rotatable relative to the chassis.

7. The abrading apparatus of claim 6 , wherein the centering member is configured to be removable from the chassis without tools.

8. The abrading apparatus of claim 1 , further comprising an output shaft extending from the output side of the chassis, wherein the centering member is coupled to the output shaft.

9. The abrading apparatus of claim 8 , wherein the output shaft is fixed relative to the chassis, and wherein the centering member is rotatably coupled to the output shaft.

10. The abrading apparatus of claim 1 , wherein the input coupler comprises a shank.

11. The abrading apparatus of claim 10 , further comprising an output shaft on the output side of the chassis, wherein the input coupler and the output shaft are integral with each other.

12. The abrading apparatus of claim 10 , wherein the input coupler comprises a receiver.

13. The abrading apparatus of claim 1 , wherein the abrasive elements are filamentary.

14. The abrading apparatus of claim 1 , wherein the abrasive members are rotatably coupled to the chassis.

15. The abrading apparatus of claim 1 , wherein the abrasive members are removably coupled to the chassis.

16. An abrading apparatus for processing edges of tubes, the abrading apparatus comprising:
a rotational symmetry axis;
a chassis comprising an input side, an output side opposite the input side, and an input coupler on the input side, wherein the input coupler is coaxial with the rotational symmetry axis;
centering members configured to be selectively and alternatively coupled to the chassis on the output side and to be coaxial with the rotational symmetry axis, wherein:
at least one of the centering members and at least another one of the centering members have different transverse dimensions,
each of the centering members comprises a non-abrasive, non-metallic disc; and abrasive members, coupled to the output side of the chassis, wherein:
each of the abrasive members comprises an abrasive face region perpendicular to the rotational symmetry axis,
the rotational symmetry axis is non-coincident with the abrasive face region of any one of the abrasive members,
at least one of the abrasive members comprises a stem and abrasive elements extending along the rotational symmetry axis, and
the chassis comprises at least one socket adapted to receive the stem.

17. An abrading apparatus for processing an edge of a tube, the abrading apparatus comprising:
a rotational symmetry axis;
a chassis comprising an input side, an output side opposite the input side, and an input coupler on the input side, wherein the input coupler is coaxial with the rotational symmetry axis;
a centering member, coupled to the chassis on the output side and coaxial with the rotational symmetry axis, wherein the centering member is a non-abrasive, non-metallic disc;
abrasive members, coupled to the chassis on the output side, wherein:
each of the abrasive members comprises an abrasive face region perpendicular to the rotational symmetry axis,
the rotational symmetry axis is non-coincident with the abrasive face region of any one of the abrasive members; and

a housing that partially encloses the abrasive members and extends substantially parallel to the rotational symmetry axis beyond the abrasive face region of each of the abrasive members, the housing being adapted to contain debris traveling perpendicular to the rotational symmetry axis during processing of the edge of the tube.

18. The abrading apparatus of claim 17 , wherein the chassis includes at least one through opening in communication with the input side of the chassis and the output side of the chassis.

Assignees

• Boeing Co

Inventors

• Mcgeary Mark E

Classifications

• B24B9/007 Primary

  for end faces of tubes · CPC title

• B24D13/145

  having a brush-like working surface · CPC title

• B24D13/20

  Mountings for the wheels · CPC title

• B24B23/028

  Angle tools · CPC title

• B24B27/0076

  grinding machines comprising two or more grinding tools · CPC title