Efficient Flight Paths for Aerial Corridor Inspection

• US 20160229533A1
• Filed: 02/06/2015
• Published: 08/11/2016
• Est. Priority Date: 02/06/2015
• Status: Abandoned Application

• Current Assignee: Izak Jan Van Cruyningen
• Original Assignee: Izak Jan Van Cruyningen
• Inventors: van Cruyningen, Izak Jan
• Application Number:
  US14/616,107
• Publication Number:
  US 20160229533A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64C 13/18 using automatic pilot
• CPC Class Codes: B64C 31/024 with auxiliary power plant
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/10 autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: G05D 1/0005 with arrangements to save energy
• CPC Class Codes: G05D 1/0094 involving pointing a payload, e.g. camera, weapon, sensor, towards a fixed or moving target
• CPC Class Codes: G08G 5/0034 Assembly of a flight plan
• CPC Class Codes: G08G 5/0069 specially adapted for an unmanned aircraft

Abstract

FIG. 1 shows an efficient flight path for airframe 10 with camera 16 flying along a transmission line utility corridor containing towers 40, 42, and 44. Between the towers the airframe is in a fast linear glide 18 to check the right of way for encroachment. Abreast of tower 42, the airframe spirals down 20 with power plant 11 off to take more detailed pictures. When the tower inspection is complete, power plant 11 is turned on to start a power climb 22 back up to prepare for glide 24 to the next tower 44, where the airframe again spirals down 26 for a closer inspection. On the return flight, a close-in conductor inspection is flown in catenary arcs with glides 28, 32 on the downslope and power climb 30, 34 on the upslope.

Claims

1. An aerial inspection system for a corridor comprising:

an unmanned aerial vehicle,

a power plant that can be stopped and restarted in flight mounted on said vehicle to propel said vehicle,

an inspection sensor mounted on said vehicle to inspect said corridor,

glide means for movement of said vehicle with said power plant off,

power climb means for increasing altitude of said vehicle with said power plant on.

2. The aerial inspection system of claim 1, wherein glide means includes linear movement along said corridor.

3. The aerial inspection system of claim 1, wherein glide means includes spiral movement around objects of interest.

4. The aerial inspection system of claim 1, wherein said unmanned aerial vehicle uses a fixed wing airframe.

5. The aerial inspection system of claim 1, wherein said inspection sensor is a camera.

6. The aerial inspection system of claim 1, further comprising an autopilot mounted on said vehicle to direct said vehicle to fly said glide means and said power climb means.

7. The aerial inspection system of claim 6, wherein said autopilot calculates a glide start altitude prior to said power climb means.

8. The aerial inspection system of claim 6, further comprising flight planning means to create and communicate a flight plan for said autopilot.

9. The aerial inspection system of claim 1, wherein a plurality of unmanned aerial vehicles are flown at once to provide plural vantage points in said inspection.

10. A method for efficiently flying a segment of a flight plan during aerial inspection of a corridor comprising:

providing an unmanned aerial vehicle,

providing a power plant that can be turned on and off during flight mounted on said vehicle,

providing an inspection sensor mounted on said vehicle,

inspecting said corridor with said inspection sensor,

providing an autopilot mounted on said vehicle,

calculating glide start altitude on said autopilot,

climbing under direction of said autopilot to said altitude with said vehicle with said power plant on,

gliding said vehicle under direction of said autopilot with said power plant off.

11. The method of claim 10 further comprising spiral gliding said vehicle around a point of interest in said corridor with said power plant off.

12. The method of claim 10 wherein said unmanned aerial vehicle uses a fixed wing airframe.

13. The method of claim 10 wherein said inspection sensor is a camera.

14. The method of claim 10 wherein said inspecting, said calculating, said climbing, and said gliding are repeated for a plurality of flight segments in said flight plan.

15. The method of claim 14 further comprising

providing a flight planning computer that can communicate with said autopilot,

planning said plurality of flight segments to produce said flight plan,

communicating said flight plan to said autopilot.