This invention relates to excavators. More specifically, the invention is an excavator that generates zero horizontal reaction force when excavating a surface region.
Lunar soil/regolith excavation is considered a vital requirement for future space missions to the Moon and other extra-terrestrial bodies such as Mars, asteroids, or even comets. The regolith is necessary for purposes of In-Situ Resource Utilization (ISRU) in order to create needed commodities such as propellants, breathable air, buffer gases, water for plant growth, portable drinking water for life support, manufacturing, and science as well as to pursue civil engineering construction such as landing pads, berms, roads, surface stabilization for dust control and thermal heat sinks, foundations, structures, habitats, and micro-meteorite/radiation shielding. The excavation of regolith is extremely difficult because deeper regolith (i.e., at depths of 30 cm and more) has bulk densities as high as 1.8 grams/cm3. Specifically, the very small regolith grain particles (e.g., 0-100 microns) exhibit strong cohesion due to electrostatic forces, van der Waals forces, and interlocking morphology.
In addition to the problems associated with regolith density, the low weight in space surface environments (e.g., the Moon's gravity is ⅙th that of the Earth) means that the mass of the excavator vehicle is of little or no value in terms of generating a reaction force for the excavator blade and scoop. That is, the excavator's blade and scoop cannot penetrate the regolith using conventional excavation techniques. In comparison, Earth-based excavators can utilize a brute force solution simply by making the excavator heavy to thereby create the desired reaction force. Due to the current high costs of lifting goods into space (i.e., approximately $4,000/kilogram), as well as packaging and launch vehicle shroud volume constraints, regolith excavation machines designed for use on extra-terrestrial bodies must necessarily be both small and lightweight. Accordingly, conventionally-designed excavation machines are not suitable options for in-space applications.
Accordingly, it is an object of the present invention to provide an excavator for use in low-gravity environments.
Another object of the present invention is to provide an excavator that is small and lightweight.
Still another object of the present invention is to provide an excavator for regolith excavation on extra-terrestrial bodies.
Other objects and advantages of the present invention will become more obvious hereinafter in the specification and drawings.
In accordance with the present invention, an excavator includes a mobile chassis, a first bucket drum, and a second bucket drum. The first bucket drum has a first axis of rotation and is coupled to the chassis. The first bucket drum has at least one first scoop formed thereon that is adapted to dig into a surface when the first bucket drum is placed on the surface and is rotated about its first axis of rotation in a first direction. The second bucket drum has a second axis of rotation and is coupled to the chassis. The second bucket drum has at least one second scoop formed thereon that is adapted to dig into the surface when the second bucket drum is placed on the surface and is rotated about its second axis of rotation in a second direction that is opposite to the first direction. The first bucket drum and second bucket drum are coupled to the chassis for positioning thereof on the surface at opposing ends of the chassis. Each first scoop on the first bucket drum is a mirror image of one second scoop on the second bucket drum when (i) the first bucket drum and second bucket drum are on the surface adjacent opposing ends of the chassis, and (ii) the first bucket drum is rotated in the first direction and the second bucket drum is simultaneously rotated in the second direction.
Other objects, features, and advantages of the present invention will become apparent upon reference to the following description of the preferred embodiments and to the drawings, wherein corresponding reference characters indicate corresponding parts throughout the several views of the drawings and wherein:
Referring now to the drawings, simultaneous reference will be made to
Excavator 10 includes a mobile chassis or vehicle 12 that could be manned or unmanned without departing from the scope of the present invention. Since excavator 10 produces zero reaction forces during excavation operations, it is well suited for space applications that will generally make use of an unmanned form of vehicle 12. For such unmanned applications, a controller 14 will generally be mounted on vehicle 12. Controller 14 could include stored programs for pre-planned operations of excavator 10, could be responsive to control signals received from a remote source for “on the fly” operations of excavator 10, or could control excavator 10 using a combination of stored programs and remotely-received instructions. The choice of controller 14 and how it achieves its control functions are not limitations of the present invention.
Vehicle 12 can be any suitable structure that can navigate over a surface 100 to include a variety of surface types (e.g., smooth, rocky, hilly, hard, soft, etc.). By way of example vehicle 12 could be outfitted with one or more endless treads or tracks 12A capable of moving and navigating vehicle 12 over a surface as track 12A is driven by a motor 16 (e.g., an electric motor) controlled by controller 14. Such single or multi-track type vehicles and their navigation are well understood in the art. It is further to be understood that wheels could be used in combination with track 12A or in place thereof without departing from the scope of the present invention.
Disposed on opposing ends of vehicle 12, at mirror image locations on vehicle 12 relative to its center 12C, are bucket drum assemblies 20 and 30. Since assemblies 20 and 30 are identical in construction, a description of just assembly 20 (using reference numerals in the 20's) will be provided herein with the corresponding elements of assembly 30 being referenced by numerals in the 30's.
Bucket drum assembly 20 includes a rotatable bucket drum 22 coupled to vehicle 12 by a cantilevered assembly 24 that is pivotally coupled to vehicle 12 at pivot coupling 26. There could be another cantilevered assembly on the other side of vehicle 12 for support of bucket drum 22 without departing from the scope of the present invention. Briefly, cantilevered assembly 24 is controlled by controller 14 to pivot about coupling 26 (as indicated by two-headed direction arrow 28A) to thereby position bucket drum 22 on surface 100 (
Cantilevered assembly 24 includes a rigid support arm 24A and mechanisms to rotate bucket drum 22 clockwise about a longitudinal axis 22A thereof as indicated by direction arrow 28B or counterclockwise as indicated by direction arrow 28C. Briefly, the mechanisms to rotate bucket drum 22 can include a motor 24B provided (or incorporated) in cantilevered assembly 24 coupled to a gear assembly (“G”) 24C provided on bucket drum 22. Motor 24B could be controlled via instructions received from controller 14. Cantilevered assemblies 24 and 34 keep the respective bucket drums' longitudinal axes 22A and 32A parallel to one another throughout operation of excavator 10.
As is generally known in the art, the term “bucket drum” refers to a drum-like device/assembly having open-ended scoops formed thereon that communicate with interior region(s) within the drum. When the drum is rotated at a surface region such that each scoop scrapes/digs into the surface, scraped/dug material is deposited into the interior region(s). Accordingly, in the present invention, each bucket drum 22 includes/defines an interior volume (or volumes) accessible only via one or more open scoops 22B (two are illustrated) formed on bucket drum 22. In the illustrated embodiment, the interior region of bucket drum 22 is indicated in a general fashion by the region between dashed lines 22D. The number of scoops 22B is not a limitation of the present invention. For clarity of illustration in
Each of scoops 22B is open at one end 22C with open end 22C designed to cut into a surface during excavation. As will be explained further below, open end 22C can be sharp, serrated, etc., to more readily dig into a surface during excavation. A sacrificial edge (not shown in
When bucket drum 22 is rotated in clockwise direction 28B about its longitudinal axis 22A, each open end 22C of a scoop 22B forms the leading edge thereof. Conversely, when bucket drum 32 is rotated in counterclockwise direction 38C about its longitudinal axis 32A, each open end 32C of a scoop 32B forms the leading edge thereof. The significance of this will be explained in an operational description of excavator 10.
With continued reference to
The above-described configuration, positioning, scoop synchronization, and counter-rotation of bucket drums 22 and 32 result in a zero horizontal reaction force (i.e., parallel to surface 100) on excavator 10. More specifically, symmetric and “equal-but-opposing” digging forces are generated as each mirror-image scoop pair 22B/32B is in engagement with surface 100. The opposing horizontal forces cancel one another out thereby resulting in a net horizontal reaction force of zero. In addition, rotation of bucket drums 22 and 32 in this fashion places respective cantilevered assembles 24 and 34 in compression (i.e., a condition that support arms 24A and 34A can better tolerate) as compared to being placed in tension.
Surface material cut/dug and scooped by each scoop 22B/32B falls into the interior volume region 22D (or regions) within the respective bucket drum 22/32. To retain material in each bucket drum during its excavation rotation, baffles (See
As mentioned above, a number of scoops can be provided on each bucket drum. For example, the number of scoops and distribution thereof about the rotating periphery of a bucket drum can be designed such that there is always at least one scoop in engagement with a surface during excavation rotation of the bucket drum. By doing this on both bucket drums, the zero horizontal reaction force will be continuous during excavation. An embodiment for achieving this is illustrated in
Referring now to
Referring now to
The advantages of the present invention are numerous. The present invention is directed to a completely new type of excavator capable of overcoming all of the problems associated in space environments on planetary bodies with conventional excavation apparatus. In particular, the present invention is a compact, lightweight, scalable regolith excavator that uses counter-rotating bucket drums mounted on each end of the excavator. During excavation, the excavator generates a zero horizontal reaction force due to the effective self-cancellation of the symmetrical and equal-but-opposing digging forces created by the counter-rotating bucket drums. In addition, the bucket drum design can incorporate multiple small scoops that reduce the digging forces at any given moment in the excavation operation, while being capable of hauling and dumping the regolith load without a separate storage container or dump bin. An improved baffle design reduces clogging and improves material retention.
In addition to the above-described excavation features and advantages, the opposing-end bucket drum placement can be used to manipulate the excavator in a variety of ways. For example, bucket drum positioning and selective rotation thereof can be used to help the excavator perform maneuvers such as climbing stepped surfaces, extracting itself from soft terrain, righting itself if tipped over, raising up the chassis for maintenance purposes, and achieve a wide variety of robotic poses.
Although the invention has been described relative to a specific embodiment thereof, there are numerous variations and modifications that will be readily apparent to those skilled in the art in light of the above teachings. It is therefore to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described.
This application claims the benefit under 35 U.S.C. §119(e) of U.S. Provisional Patent Application Ser. No. 61/649,008 filed May 18, 2012, the contents of which are incorporated herein by reference.
The invention described herein was made in the performance of work under a NASA contract and by an employee of the United States Government and is subject to the provisions of Public Law 96-517 (35 U.S.C. §202) and may be manufactured and used by or for the Government for governmental purposes without the payment of any royalties thereon or therefore. In accordance with 35 U.S.C. §202, the contractor elected not to retain title.
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Entry |
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D. Larry Clark et al., “A Novel Approach to Planetary Regolith Collection: the Bucket Drum Soil Excavator,” American Institute of Aeronautics and Astronautics SPACE 2009 Conference and Exposition, AIAA 2009-6430, Sep. 14, 2009. |
Number | Date | Country | |
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61649008 | May 2012 | US |