Claims
- 1. A core break-off mechanism comprising: an inner, core break-off tube extending along a tube axis which is sleeved within and angularly rotatable relative to an outer drill tube, wherein the core break-off tube has a tubular wall of varying thickness such that its inside diameter (C-ID) is offset with respect to its outside diameter (C-OD) by a pre-determined amount in a radial direction transverse to the tube axis, and the drill tube has a tubular wall of varying thickness such that its inside diameter (D-ID) is offset with respect to its outside diameter (D-OD) by the same pre-determined amount in a radial direction, and wherein the drill tube has a drill end and a stepped indented shoulder on one lateral side of the tube axis proximate said drill end by which an end of the core break-off tube is retained within the drill tube, whereby when the break-off tube and the drill tube are held in one relative rotational alignment, the two offsets cancel each other such that the D-OD of the drill tube and the C-ID of the break-off tube are centered together on the tube axis and are in positional alignment for drilling a core from base rock to a desired depth, and when the break-off tube is rotated 180 degrees with respect to the drill tube, the offsets add together, causing the rock core within the inner tube to become radially displaced by a distance equal to the sum of the two offsets so as to generate sufficient force to break off the rock core from the base rock.
- 2. A core break-off mechanism according to claim 1, further including a pushrod arranged to be axially movable within the core break-off tube for ejecting the core sample.
- 3. A core break-off mechanism according to claim 2, wherein the pushrod is provided with a drill bit on its end such that the pushrod can be advanced to the end of the core break-off tube and function as an extension of a drill bit provided at a drill tube of the drill tube.
- 4. A core break-off mechanism according to claim 1, further comprising a core drill assembly that provides a drill bit change-out capability for readily changing the drill tube.
- 5. A core break-off mechanism according to claim 4, wherein the drill bit change-out capability is provided by small bit locking balls set into the drill tube that protrude outward but are contained from falling out yet allowed to move inward by engaging with grooves cut into the inside of the drill tube, thus holding the drill tube in place.
- 6. A method of drilling into rock and taking a core sample without generating load stresses on the local terrain comprising:
providing an inner, core break-off tube extending along a tube axis which is sleeved within and angularly rotatable relative to an outer drill tube, wherein the core break-off tube has a tubular wall of varying thickness such that its inside diameter is offset with respect to its outside diameter by a pre-determined amount in a radial direction transverse to the tube axis, and the drill tube has a tubular wall of varying thickness such that its inside diameter is offset with respect to its outside diameter by the same pre-determined amount in a radial direction; drilling into the rock with a drill end of the drill tube and with the break-off tube and the drill tube held in one relative rotational alignment such that the two offsets cancel each other and the drill tube and break-off tube are centered together on the tube axis; and rotating the break-off tube relative to the drill tube by about 180 degrees with respect to the drill tube, so that the offsets add together and cause the rock core within the inner tube to become radially displaced by a distance equal to the sum of the two offsets to generate sufficient force to break off the rock core from the base rock.
Parent Case Info
[0001] This U.S. patent application claims the priority filing date of U.S. Provisional Application Ser. No. 60/228,155 of filed on Aug. 25, 2001, by the same inventor, having the same title.
Government Interests
[0002] The subject matter of this U.S. patent application was developed under contract with the National Aeronautics and Space Administration (NASA), Contract No.______. The U.S. Government has certain rights in the invention.
Provisional Applications (1)
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Number |
Date |
Country |
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60228155 |
Aug 2000 |
US |