Autonomous laser-powered vehicle

• US 9,850,711 B2
• Filed: 07/18/2014
• Issued: 12/26/2017
• Est. Priority Date: 11/23/2011
• Status: Active Grant

• Current Assignee: Stone Aerospace, Inc.
• Original Assignee: Stone Aerospace, Inc.
• Inventors: Stone, William C., Hogan, Bartholomew P.
• Primary Examiner(s): BLEVINS, JERRY M
• Application Number:
  US14/335,863
• Publication Number:
  US 20170211328A1
• Time in Patent Office: 1,257 Days
• Field of Search: 385134
• CPC Class Codes: B64G 1/00 Cosmonautic vehicles
• CPC Class Codes: B64G 99/00 Subject matter not provided for in other groups of this subclass
• CPC Class Codes: E21B 7/008 Drilling ice or a formation covered by ice
• CPC Class Codes: E21B 7/15 of electrically generated heat
• CPC Class Codes: G02B 19/0028 refractive and reflective surfaces, e.g. non-imaging catadioptric systems
• CPC Class Codes: G02B 19/0047 for use with a light source G02B19/009, G02B19/0095 take precedence; details of lighting devices in general F21V; non-semiconductor lasers having optical devices external to the laser cavity H01S3/005
• CPC Class Codes: G02B 23/2492 Arrangements for use in a hostile environment, e.g. a very hot, cold or radioactive environment
• CPC Class Codes: G02B 6/3624 Fibre head, e.g. fibre probe termination optical details of light guide terminations G02B6/241; reshaping of light guides G02B6/2552; optical details of coupling light into or out of fibre end G02B6/262
• CPC Class Codes: G02B 6/50 Underground or underwater installation; Installation through tubing, conduits or ducts
• CPC Class Codes: G02B 7/008 with means for compensating for changes in temperature or for controlling the temperature; thermal stabilisation

Abstract

An autonomous laser-powered vehicle designed to autonomously penetrate through ice caps of substantial (e.g., kilometers) thickness by melting a path ahead of the vehicle as it descends. A high powered laser beam is transmitted to the vehicle via an onboard bare fiber spooler. After the beam enters through the dispersion optics, the beam expands into a cavity. A radiation shield limits backscatter radiation from heating the optics. The expanded beam enters the heat exchanger and is reflected by a dispersion mirror. Forward-facing beveled circular grooves absorb the reflected radiant energy preventing the energy from being reflected back towards the optics. Microchannels along the inner circumference of the beam dump heat exchanger maximize heat transfer. Sufficient amount of fiber is wound on the fiber spooler to permit not only a descent but also to permit a sample return mission by inverting the vehicle and melting its way back to the surface.

Claims

1. An autonomous laser-powered vehicle for penetrating through ice, said vehicle comprising:

a laser power source;

a housing;

a fiber spooler mounted within said housing;

a fiber for transmitting a laser beam, said fiber having a first end and a second end, said first end of said fiber connected to said laser power source and said second end of said fiber wound about said fiber spooler;

a fiber connector having a first end and a second end, wherein said fiber is optically connected to said first end of said fiber connector;

a beam dispersion optics for receiving said laser beam, said beam dispersion optics optically connected to said second end of said fiber connector and wherein at least one beam dispersion lens expands said laser beam into a cone configuration;

a beam dump heat exchanger having a first end and a second end, said first end of said beam dump heat exchanger optically connected to said beam dispersion optics to receive said expanded laser beam;

a mirror connected to said second end of said beam dump heat exchanger, said mirror reflecting said expanded laser beam onto a side wall of said beam dump heat exchanger;

a nose heat exchanger having a first end and a second end, said first end of said nose heat exchanger connected to said mirror and said second end of said nose heat exchanger having a recessed portion containing a plurality of planar heat exchanger channels for cooling the temperature of said mirror;

an end plate connected to said recessed portion of said nose heat exchanger and having a forward melt jet for melting ice, said end plate having a plurality of melt water return channels drawing water back through said beam dump heat exchanger;

a synthetic aperture radar (SAR) antenna mounted on said beam dump heat exchanger for avoiding obstacles as said vehicle descends through ice;

a hot water jet pump assembly for pulling meltwater from said end plate as said vehicle descends through ice; and

an onboard power generation assembly electrically connected to electronics, sensors, pumps and other actuators onboard said vehicle.

2. The autonomous laser-powered vehicle as recited in claim 1, wherein said hot water jet pump assembly further comprise a plurality of hot water jet pumps in a parallel configuration.

3. The autonomous laser-powered vehicle as recited in claim 1, wherein said beam dump heat exchanger further comprises a plurality of circular beveled grooves within the inner circumference of said beam dump heat exchanger, said plurality of circular beveled grooves absorbing reflected light from said mirror to prevent reflection back towards said beam dispersion optics.

4. A beam dump assembly, said beam dump assembly comprising:

a laser power source;

a bare laser fiber through which a laser beam generated from said power source is transmitted;

a beam dispersion optics;

a fiber connector having a first and a second end, said first end connected to said bare laser fiber and said second end connected to said beam dispersion optics;

a beam expansion cavity; and

a beam dump heat exchanger having a cylindrical pressure vessel wall and a conical portion wherein said beam dump heat exchanger further comprises a plurality of beveled grooves within the circumference of a side wall within said beam dump heat exchanger.

5. The beam dump assembly, as recited in claim 4, wherein said plurality of beveled grooves are aligned to face the same direction as said laser beam entering said beam dump heat exchanger.

6. The beam dump assembly, as recited in claim 5, wherein said beam dump heat exchanger further comprises a dispersion mirror, said dispersion mirror reflecting said laser beam received to said side wall of said beam dump heat exchanger.

7. The beam dump assembly, as recited in claim 6, said beam dump heat exchanger further comprising a plurality of microchannel heat exchanger channels, said plurality of microchannel heat exchanger channels axially traversing said pressure vessel wall.

8. The beam dump assembly, as recited in claim 7, further comprising a radiation shield positioned between said beam dispersion optics and said beam expansion cavity for limiting backscatter radiation from heating said beam dispersion optics.