Apparatus for automated rastering of an end effector over an airfoil-shaped body

Patent metadata

Field	Value
Publication number	US-9334066-B2
Application number	US-201313861934-A
Country	US
Kind code	B2
Filing date	Apr 12, 2013
Priority date	Apr 12, 2013
Publication date	May 10, 2016
Grant date	May 10, 2016

Abstract

A mechanism for adjusting the orientation of an end effector (e.g., a non-destructive inspection sensor) during movement over a contoured surface, comprising: (1) a pneumatic or spring-loaded plunger shaft that facilitates positioning of an end effector onto a highly contoured surface by allowing a wide range of vertical motion; (2) a rocker pivotably coupled to a distal end of the plunger shaft, the rocker being pivotable about a horizontal axis to allow a pair of follower wheels coupled to distal ends of the rocker arms to follow the contoured surface and keep the end effector oriented correctly relative to the surface without tipping over; and (3) a hozzle (i.e., an end effector holder) attached to the rocker for rotation therewith, the end effector being coupled to the hozzle by an elastomeric gasket or a plurality of springs which allow the orientation of the end effector relative to the hozzle to change in response to contact forces.

First claim

The invention claimed is:

1. A mechanism comprising:
a plunger housing;
a plunger shaft that is supported by and has a range of vertical motion relative to said plunger housing;
a rocker pivotably coupled to a distal end of said plunger shaft by a revolute joint, said rocker comprising first and second arms, and first and second follower wheels pivotably coupled to respective distal ends of said first and second arms;
an end effector holder attached to or integrally formed with said rocker for rotation therewith;
an end effector; and
means for coupling said end effector to said end effector holder in a manner that allows said end effector to tilt relative to said end effector holder in any direction in response to forces exerted on said end effector and then urges said end effector toward an untilted position when said forces are removed.

2. The mechanism as recited in claim 1 , wherein said end effector comprises a non-destructive inspection sensor or sensor array.

3. The mechanism as recited in claim 2 , wherein said non-destructive inspection sensor comprises a pitch-catch sensor, said pitch-catch sensor comprising a pair of contact feet.

4. The mechanism as recited in claim 1 , further comprising means for urging said plunger shaft to move downward relative to said plunger housing.

5. The mechanism as recited in claim 1 , further comprising means for urging said rocker toward a neutral position in response to said rocker adopting a non-neutral position.

6. An automated apparatus for moving said mechanism as recited in claim 1 over a surface of an airfoil-shaped body, comprising:
a chassis adapted to travel along an airfoil-shaped body in a spanwise direction, said plunger housing being attached to and carried by said chassis;
a first actuator for moving said chassis in said spanwise direction;
a guide element mounted to said chassis, said guide element being disposed in a chordwise direction;
a slider element slidably coupled to and movable along said guide element, said slider element being attached to or integrally formed with said plunger housing of said mechanism;
a second actuator for moving said slider element in said chordwise direction; and
a computer system which is programmed to activate said first and second actuators at different times to produce rastering of said end effector.

7. The apparatus as recited in claim 6 , further comprising a position tracking system which tracks the position of said end effector during rastering motion.

8. A mechanism comprising:
a plunger housing;
a plunger shaft that is supported by and has a range of vertical motion relative to said plunger housing;
a rocker pivotably coupled to a distal end of said plunger shaft by a revolute joint, said rocker comprising first and second arms, and first and second follower wheels pivotably coupled to respective distal ends of said first and second arms;
an end effector holder attached to or integrally formed with said rocker for rotation therewith, said end effector holder comprising a ring-shaped portion;
an end effector surrounded by said ring-shaped portion of said end effector holder; and
an elastomeric gasket having an inner perimeter attached to said end effector and an outer perimeter attached to said ring-shaped portion of said end effector holder,
wherein said end effector is suspended within said ring-shaped portion of said end effector holder by said elastomeric gasket.

9. The mechanism as recited in claim 8 , wherein said elastomeric gasket has sufficient elasticity to allow said end effector to tilt relative to said end effector holder in any direction in response to forces exerted on said end effector and then urge said end effector toward an untilted position when said forces are removed.

10. The mechanism as recited in claim 8 , wherein said end effector comprises a non-destructive inspection sensor or sensor array.

11. The mechanism as recited in claim 10 , wherein said non-destructive inspection sensor comprises a pitch-catch sensor, said pitch-catch sensor comprising a pair of contact feet.

12. The mechanism as recited in claim 8 , further comprising means for urging said plunger shaft to move downward relative to said plunger housing.

13. An automated apparatus for moving said mechanism as recited in claim 9 over a surface of an airfoil-shaped body, comprising:
a chassis adapted to travel along an airfoil-shaped body in a spanwise direction, said plunger housing being attached to and carried by said chassis;
a first actuator for moving said chassis in said spanwise direction;
a guide element mounted to said chassis, said guide element being disposed in a chordwise direction;
a slider element slidably coupled to and movable along said guide element, said slider element being attached to or integrally formed with said plunger housing of said mechanism;
a second actuator for moving said slider element in said chordwise direction; and
a computer system which is programmed to activate said first and second actuators at different times to produce rastering of said end effector.

14. The apparatus as recited in claim 13 , further comprising a position tracking system which tracks the position of said end effector during rastering motion.

15. A mechanism comprising:
a plunger housing;
a plunger shaft that is supported by and has a range of vertical motion relative to said plunger housing;
first elastomeric or mechanical spring means coupled to a distal end of said plunger shaft;
a rocker coupled to a distal end of said plunger shaft by said first elastomeric or spring means, said rocker comprising first and second arms, and first and second follower wheels pivotably coupled to respective distal ends of said first and second arms;
an end effector holder attached to or integrally formed with said rocker for movement therewith;
an end effector; and
second elastomeric or mechanical spring means for coupling said end effector to said end effector holder,
wherein said first elastomeric or mechanical spring means enable said rocker to tilt relative to said plunger shaft and said second elastomeric or mechanical spring means enable said end effector to tilt relative to said end effector holder.

16. The mechanism as recited in claim 15 , wherein said end effector comprises a non-destructive inspection sensor or sensor array.

17. The mechanism as recited in claim 15 , further comprising means for urging said plunger shaft to move downward relative to said plunger housing.

18. An automated apparatus for moving an end effector over a surface of an airfoil-shaped body, comprising:
a chassis adapted to travel along an airfoil-shaped body in a spanwise direction;
a first actuator for moving said chassis in said spanwise direction;
a guide element mounted to said chassis, said guide element being disposed in a chordwise direction;
a slider element slidably coupled to and movable along said guide element;
a second actuator for moving said slider element in said chordwise direction;
a plunger housing attached to or integrally formed with said slider element;
a plunger shaft that is supported by and has a range of vertical motion relative to said plunger housing;
a rocker pivotably coupled to a distal end of said plunger shaft by a revolute joint, said rocker comprising first and second arms, and first and second follower wheels pivotably coupled to respective distal ends of said first and second arms;
an end effector holder attached to or integrally formed with said rocker for rotation therewith;
an end effector that is

Assignees

• Boeing Co

Inventors

• Tapia William Joseph
• Fogarty Michael D
• Hafenrichter Joseph L
• Georgeson Gary E

Classifications

• G01N2291/044

  Internal reflections (echoes), e.g. on walls or defects · CPC title

• G01N2291/2694

  Wings or other aircraft parts · CPC title

• B64F5/0045 Primary

  Operations & Transport · mapped topic

• G01N2291/0289

  Internal structure, e.g. defects, grain size, texture · CPC title

• G01N2291/102

  one emitter, one receiver · CPC title