HOVER CMM

• US 20130215433A1
• Filed: 10/12/2010
• Published: 08/22/2013
• Est. Priority Date: 10/12/2010
• Status: Abandoned Application

• Current Assignee: Stephen James Crampton
• Original Assignee: Stephen James Crampton
• Inventors: Crampton, Stephen James
• Application Number:
  US13/878,888
• Publication Number:
  US 20130215433A1
• Time in Patent Office: Days
• US Class Current: 356/500
• CPC Class Codes: B64C 17/00 Aircraft stabilisation not otherwise provided for
• CPC Class Codes: B64U 10/14 with four distinct rotor axes, e.g. quadcopters
• CPC Class Codes: B64U 10/60 Tethered aircraft
• CPC Class Codes: B64U 10/80 UAVs characterised by their small size, e.g. micro air vehicles [MAV]
• CPC Class Codes: B64U 2101/26 for manufacturing, inspections or repairs
• CPC Class Codes: B64U 2101/35 for science, e.g. meteorology
• CPC Class Codes: B64U 30/26 Ducted or shrouded rotors
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 70/95 Means for guiding the landing UAV towards the platform, e.g. lighting means
• CPC Class Codes: G01B 21/04 by measuring coordinates of points
• CPC Class Codes: G01B 2210/58 Wireless transmission of information between a sensor or probe and a control or evaluation unit
• CPC Class Codes: G01B 9/02 Interferometers

Abstract

It is a purpose of this invention to provide a Hover CMM to accurately measure an object. The Hover CMM comprises: a probe, an air vehicle and a localiser. The probe is mounted on the air vehicle. The air vehicle transports the probe around the surface of the object. The localiser tracks the position and orientation of the probe. The air vehicle is capable of hovering, slow and rapid movement. The measurements made by the probe are synchronised with the measurements made by the localiser. In a further embodiment, multiple probes, multiple air vehicles and multiple localisers can be provided in a system. In a further embodiment, the air vehicle has additional propulsion means for reducing wander. In another embodiment, the air vehicle is tethered. In a further embodiment, a gantry is provided for tethering the air vehicle. In another embodiment, a tilting means is provided to incline the probe relative to the air vehicle. Methods are provided for measuring an object and for controlling the wander of the air vehicle.

Claims

1. A coordinate measuring machine comprising:

an air vehicle;

a probe mounted on said air vehicle;

a localiser for measuring the position and orientation of said probe;

operable such that accurate measures of an object are made.

2. A coordinate measuring machine in accordance with claim 1 wherein said air vehicle is a quad- rotor.

4. A coordinate measuring machine in accordance with claim 1 wherein said air vehicle is a helicopter.

5. A coordinate measuring machine in accordance with claim 1 wherein said probe is a non-contact probe for dimensional measurement.

6. A coordinate measuring machine in accordance with claim 5 wherein said non-contact dimensional measurement probe is optical.

8. A coordinate measuring machine in accordance with claim 1 wherein said probe is a contact probe for dimensional measurement.

9. A coordinate measuring machine in accordance with claim 1 wherein said probe is a quantity measuring probe.

10. A coordinate measuring machine in accordance with claim 1 wherein said probe is tiltable relative to said air vehicle.

11. A coordinate measuring machine in accordance with claim 1 that further comprises a probe mount and said probe mount comprises vibration absorption means.

12. A coordinate measuring machine in accordance with claim 1 wherein said localiser is an optical localiser.

13. A coordinate measuring machine in accordance with claim 12 wherein said optical localiser is a laser interferometer tracker.

15. A coordinate measuring machine in accordance with claim 1 wherein said localiser is a GPS localiser.

18. A coordinate measuring machine in accordance with claim 1 wherein there is a plurality of localisers.

19. A coordinate measuring machine in accordance with any of claim 1 that further comprises a tether to said air vehicle.

20. A coordinate measuring machine in accordance with claim 19 that further comprises a gantry for supporting said tether.

26. A coordinate measuring machine in accordance with claim 1 wherein said air vehicle further comprises additional propulsion means for reducing wander.

27. A coordinate measuring machine in accordance with claim 1 wherein said accurate measurements are accurate to better than 500 microns error.

28. A coordinate measuring machine in accordance with claim 1 wherein said probe is a tool for performing an operation on said object.

3. (canceled)

7. (canceled)

14. (canceled)

16. (canceled)

17. (canceled)

21-25. -25. (canceled)

29. (canceled)

30. A method for accurately measuring an object in a coordinate measuring machine comprising the following steps:

[Step 1] a first measurement is made of an object using a probe and a localiser at a first probe location and orientation;

[Step 2] an air vehicle moves the probe to a second location and orientation;

[Step 3] a second measurement is made of the object using the probe and the localiser at the second location and orientation;

where steps 2 and 3 are repeated until measurements of the object have been made from all required locations and orientations.

31. A method for controlling the wander in flight of an air vehicle with main propulsion means and additional propulsion means in a coordinate measuring machine comprising the following steps:

[Step 1] the 6-DOF position and orientation of said air vehicle is measured using a localiser;

[Step 2] a control loop compares at least said 6-DOF position and orientation with at least the demanded 6-DOF position and orientation;

[Step 3] said control loop generates control output signals to the main propulsion means and additional propulsion means on said air vehicle to reduce said wander;

where steps 1 to 3 are repeated until the flight terminates.