Orbital drilling system and associated methods and apparatuses

Patent metadata

Field	Value
Publication number	US-9770769-B2
Application number	US-201615004769-A
Country	US
Kind code	B2
Filing date	Jan 22, 2016
Priority date	Jan 22, 2016
Publication date	Sep 26, 2017
Grant date	Sep 26, 2017

Abstract

Described herein is an orbital drilling system that includes an orbital drilling machine and a cutter. The orbital drilling machine includes a spindle and an eccentric rotation mechanism. The spindle is rotatable about a cutter axis. The eccentric rotation mechanism is coupled to the spindle and configured to orbit the spindle about an orbital axis, offset from the cutter axis. The cutter is co-rotatably coupled to the spindle and comprises a plurality of cutting edges, collectively defining a cutting diameter of the cutter. The cutting diameter of the cutter is adjustable.

First claim

What is claimed is:

1. An orbital drilling system, comprising:
an orbital drilling machine, comprising:
a spindle, rotatable about a cutter axis; and
an eccentric rotation mechanism, coupled to the spindle and configured to orbit the spindle about an orbital axis, offset from the cutter axis; and

a cutter, co-rotatably coupled to the spindle and comprising a plurality of cutting edges, collectively defining a cutting diameter of the cutter, wherein the cutting diameter of the cutter is adjustable.

2. The orbital drilling system according to claim 1 , wherein the cutter further comprises a body and a plurality of inserts adjustably fixed to the body, each of the plurality of inserts defining one of the cutting edges and being radially adjustable relative to the body to adjust the cutting diameter of the cutter.

3. The orbital drilling system according to claim 2 , wherein the cutter further comprises a manual adjustment mechanism, configured to manually radially adjust the plurality of inserts relative to the body.

4. The orbital drilling system according to claim 3 , wherein the manual adjustment mechanism comprises a cam, comprising a non-round engagement surface configured to:
engage the plurality of inserts;
upon rotation of the cam in a first rotational direction, urge the plurality of inserts radially outwardly relative to the body of the cutter; and
upon rotation of the cam in a second rotational direction, opposite the first rotational direction, allow the plurality of inserts to be moved radially inwardly relative to the body of the cutter.

5. The orbital drilling system according to claim 3 , wherein the manual adjustment mechanism comprises a wedge, comprising a tapered surface configured to:
engage the plurality of inserts;
upon translational movement of the wedge relative to the body in a first translational direction, parallel to the cutter axis, urge the plurality of inserts radially outwardly relative to the body of the cutter; and
upon translational movement of the wedge relative to the body in a second translational direction, opposite the first translational direction, allow the plurality of inserts to be moved radially inwardly relative to the body of the cutter.

6. The orbital drilling system according to claim 3 , wherein the manual adjustment mechanism comprises a plurality of shims, each positionable between a respective one of the plurality of inserts and the body to support the insert following a manual radial adjustment of the insert.

7. The orbital drilling system according to claim 6 , wherein the plurality of shims each has a dimension equal to a desired radial adjustment of the plurality of inserts.

8. The orbital drilling system according to claim 3 , wherein the cutter further comprises a plurality of fasteners, each configured to adjustably fix a respective one of the plurality of inserts to the body of the cutter.

9. The orbital drilling system according to claim 8 , wherein:
each of the plurality of inserts comprises a slot, through which a respective one of the plurality of fasteners extends to adjustably fix the insert to the body of the cutter; and
each fastener moves translationally along the slot of a respective insert as the insert is radially adjusted relative to the body.

10. The orbital drilling system according to claim 2 , wherein the cutter further comprises an automated adjustment mechanism, configured to automatically radially adjust the plurality of inserts relative to the body of the cutter.

11. The orbital drilling system according to claim 10 , wherein the automated adjustment mechanism comprises an electronically-controlled actuator, coupled with the plurality of inserts and selectively operable to radially move the plurality of inserts relative to the body of the cutter.

12. The orbital drilling system according to claim 11 , wherein:
the automated adjustment mechanism further comprises a wedge, comprising a tapered surface configured to:
engage the plurality of inserts;
upon translational movement of the wedge relative to the body in a first translational direction, parallel to the cutter axis, urge the plurality of inserts radially outwardly relative to the body of the cutter; and
upon translational movement of the wedge relative to the body in a second translational direction, opposite the first translational direction, urge the plurality of inserts to be moved radially inwardly relative to the body of the cutter; and

the wedge is coupled to the electronically-controlled actuator and translationally movable relative to the body via selective operation of the electronically-controlled actuator.

13. The orbital drilling system according to claim 11 , wherein:
the automated adjustment mechanism further comprises a control module, operatively coupled with the electronically-controlled actuator; and
the control module is configured to direct the electronically-controlled actuator to radially move the plurality of inserts relative to the body of the cutter.

14. The orbital drilling system according to claim 13 , wherein:
the control module is operatively coupled with the orbital drilling machine to control rotation of the spindle and cutter about the cutter axis and orbital rotation of the spindle about the orbital axis;
the control module is configured to:
direct the electronically-controlled actuator to radially move the plurality of inserts relative to the body of the cutter such that the cutter has a first cutting diameter;
control rotation of the spindle and cutter with the first cutting diameter about the cutter axis and orbital rotation of the spindle about the orbital axis to form a hole in a workpiece having a first hole diameter greater than the first cutting diameter;
direct the electronically-controlled actuator to radially move the plurality of inserts relative to the body of the cutter such that the cutter has a second cutting diameter larger than the first cutting diameter; and
control rotation of the spindle and cutter with the second cutting diameter about the cutter axis and orbital rotation of the spindle about the orbital axis to enlarge the hole in the workpiece from the first hole diameter to a second hole diameter larger than the first hole diameter.

15. The orbital drilling system according to claim 1 , wherein the offset between the cutter axis and the orbital axis is non-adjustably fixed.

16. A method of forming a hole in a workpiece, comprising:
providing an offset between an orbital axis, about which a cutter orbits, and a cutter axis, about which the cutter rotates;
adjusting a cutting diameter of the cutter;
rotating the cutter about the cutter axis to cut material in the workpiece; and
while rotating the cutter about the cutter axis to cut material in the workpiece, orbiting the cutter about the orbital axis to form a hole in the workpiece having a first hole diameter greater than the cutting diameter.

17. The method according to claim 16 , wherein:
the cutter comprises a plurality of cutting edges, collectively defining the cutting diameter of the cutter; and
adjusting the cutting diameter of the cutter comprises manually moving the plurality of cutting edges radially away from or radially towards the cutter axis.

18. The method according to claim 16 , wherein:
the cutter comprises a plurality of cutting edges, collectively defining the cutting diameter of the cutter; and
adjusting the cutting diameter of the cutter comprises automatically moving the plurality of cutting edges radially away from or radially towards the cutter a

Assignees

• Boeing Co

Inventors

• Holleman Wesley E
• Farrell Nicholas R

Classifications

• B23C5/2462 Primary

  the adjusting means being oblique surfaces · CPC title

• B23C5/2208

  for plate-like cutting inserts  (B23C5/2226, B23C5/2234 take precedence) · CPC title

• B23C3/005

  Rails · CPC title

• B23B31/2073 Primary

  Axially fixed cam, moving jaws (B23B31/20125 takes precedence) · CPC title

• Y10T409/307616

  with means to move cutter eccentrically · CPC title