|Publication number||US3525405 A|
|Publication date||Aug 25, 1970|
|Filing date||Jun 17, 1968|
|Priority date||Jun 17, 1968|
|Publication number||US 3525405 A, US 3525405A, US-A-3525405, US3525405 A, US3525405A|
|Inventors||Coyne James C, Southworth Hamilton Jr|
|Original Assignee||Bell Telephone Labor Inc|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (3), Referenced by (40), Classifications (11)|
|External Links: USPTO, USPTO Assignment, Espacenet|
Aug. 25, 1970 J. c. COYNE E GUIDED EURROWING DEVICE 4 Sheets-Sheet 1 Filed June 17, 1968 J. c. cor/v5 INVENTOPS H. SOUTHWOR TH, JR.
ATTORNEK Aug. 25, 1970 c. CQYNE ETAL 3,525,405
GUIDED BURROWING DEVICE Filed June 17, 1968 4 Sheets-Sheet 2 FIG. 4
A IIIIIII FIG. .3
a. c. COYNE ETAL 3,525,405
GUIDED mmnowme 1mm 4 Sheets-Sheet :5
Aug. 25, 1970 Filed June 17, 1968 Aug. 25, 1970 J. C. COYNE ET AL GUIDED BURROWING DEVICE 4 Sheets-Sheet 4 Filed June 17, 1968 REMSGSQQ 30% MAR NNQ United States Patent O 3,525,405 GUIDED BURROWING DEVICE James C. Coyne, New Providence, N.J., and Hamilton Southworth, Jr., New York, N.Y., assignors to Bell Telephone Laboratories, Incorporated, Murray Hill, N.J., a corporation of New York Filed June 17, 1968, Ser.-No. 737,592 Int. Cl. E21b 7/04, 47/02 US. Cl. 175-19 8 Claims ABSTRACT OF THE DISCLOSURE A subterranean penetrator or mole for use in burrowing at relatively shallow grounddepths is steered by impingement of soil on the planar beveled face of its nose. As the mole advances, the soil impinges on flutes or the equivalent extending from the nose, causing the latter to rotate passively. In such case, the mole motion is a helix that approaches a straight line. Steering is accomplished by locking the nose in a selected position with respect to the nonrotating mole body, as With a clutch mechanism. The soil force component vertical to the nose face then causes the mole to arc in the plane normal to the beveled face and containing the moles longitudinal axis.
This invention relates generally tosubterranean penetrators of the type referred to as moles; and more particularly to an improved steering concept for such devices.
BACKGROUND OF THE INVENTION Subterranean penetrators are of considerable current interest to the electrical power and telephone industries in connection with the installation of underground cable and wire. These penetrators, and especially the guidable moles, offer an alternative to the trenching and plowing techniques now employed which usually severely disrupt normal ground surface activity and often require costly resurfacing .work.
The moles are a species of penetrator resembling in some respects a guided missile. Included in the mole proper is propulsion, steering and detection equipment, monitored and controlled from above ground. Examples of specific mole structures may be found in the patent applications of G. A. Reinold, Ser. No. 681,356, filed Nov. 8, 1967 and H. Southworth, Jr. Ser. No. 713,602, filed Mar. 18, 1968, now Pat. No. 3,465,834, both assigned to applicants assignee.
The present invention is concerned with an improved solution to the mechanical steering of moles in threedimensional soil.
By way of background, steering systems heretofore known are active in the sense that an external surface such as a vane or rudder must be moved against the soil by an actuator to establish a steering attitude. The steering vanes function much like the elevator or rudder of an aircraft. The physical force required to move any control surfaces into soil, however, is enormously large by comparison.
Other problems are also exhibited by present mole steering schemes. These include, for example, the difiiculty of steering in near-frozen or highly compacted soil where the required forces are often beyond the capacity of hydraulic actuators. They include as well the initial distance of mole penetration required before the rear-end mounted steering vanes contact the soil and thus become functional. This problem, inherent to rear steering moles, results in a much deeper than necessary vertical penetration of the ground by the mole before it levels out.
3,525,405 Patented Aug. 25, 1970 Accordingly, one object of the invention is to more effectively steer subterranean burrowing devices of the mole type.
A specific object of the invention is to substantially reduce the magnitude of forces needed to steer a mole.
An added object of the invention is to reduce the turning radius of a mole.
A further object of the invention is to simplify the mole planting process.
Another specific object of the invention is to more effectively combat the tendency of moles to edge upward toward the soil surface in the course of their travel.
SUMMARY OF THE INVENTION The invention contemplates a front-steering mole in which the moles nose is given a beveled face and is mounted for free axial rotation with respect to the mole body. As the mole advances, the soil impinges on spiral flutes or the like connected with the noses outer surface, causing the nose to rotate. During nose rotation, the mole describes. a helical path which with rapid nose rotation approaches a straight line. Steering is accomplished by looking the nose in a selected rotational position with respect to the fixed three-dimensional soil ambient. The soil force component vertical to the now-stationary nose face causes the mole to arc in a plane normal to the beveled face and containing the moles longitudinal axis.
In an illustrative embodiment of this invention, rotational locking of the nose is achieved by a clutch controlled remotely.
Sensing of the bevel angle with respect to the soil ambient may be achieved as part of the overall guidance system of the mole. Several shapes of nose are specifically cited, with others readily envisionable, for imparting passive rotation to the nose as the mole advances in the soil. The essential elements in these cases are: a bevel or slant face of generally planar proportions, upon which a soil force component normal to the mole longitudinal axis can be developed; and a fixed surface reactive to the impingement of soil thereon to generate the passive rotation. The optimal bevel angle ranges between 30 and 35 as measured from the mole axis. One such reactive surface is a shaft with spiral flutes.
The invention and its further objects, features and advantages are further delineated in connection with the detailed description to follow of an illustration embodiment.
THE DRAWING DETAILED DESCRIPTION OF AN ILLUSTRATIVE EMBODIMENT FIG.'1 shows a subterranean penetrator suitable for carrying out the invention. The penetrator or mole, designated '1, consists of a generally cylindrical propulsion section 2 with several longitudinal stabilizing fins 3 afiixed to its exterior, and a forward section 4. The propulsion system may be of the linear impact type described in the showing the aforementioned patent application Ser. No. 713,602. The fins 3 serve to preclude undue rotation of propulsion section 2.
STRUCTURE Forward section 4 is substantially coaxial with section 2 and is mounted for axial rotation with respect to section 2. In the FIG. 1 embodiment, forward section 4 comprises a shaft 5 with auger flutes 6. Typically, shaft 5 is eight to twelve inches in length; and propulsion section 2 is five feet in length.
Pursuant to a prime facet of the invention, shaft 5 terminates in a beveled nose 7. The nose 7 is a planar solid surface intersecting the mole axis at an angle optimally of from 30 to 35. Forward section 4 is mounted in propulsion section 2 through thrust and journal bearings 8 shown in FIG. 2 in which a shaft extension 9 is normally free to rotate. However, the rotational freedom is arrested by some suitable mechanism such as a clutch which, for example, may include clutch plate 10 mounted on shaft 9 and a second clutch plate 11 mounted upon a nonrotatable piston 12. Clutch plates 10 and 11 may be of the locking pin type for example.
Piston 12 travels in a hydraulic cylinder 13 which is governed by a control system 14 that includes a solenoid 15 and a. directional hydraulic valve 16. The hydraulic connections between valve 16 and cylinder 13 are conventional and accordingly not shown. Solenoid 15 is powered and remotely controlled through conductors contained in the main control line 23.
Clutch plate 11 includes a plurality of pins 17; and clutch plate 10 includes a corresponding number of engagement slots 18 for the pins 17. When it is desired to allow free rotation of forward section 4, including its slanted nose, the solenoid 15 is actuated so that the piston 12 is thrust to its rearward position as depicted in FIG. 2. When a locking of section 4 and section 2 is in order, solenoid 15 is operated to cause piston 12 to thrust forward to engage pins 17 into slots 18. Other clutching and locking arrangements are, of course, readily envisionable by those practiced in the art.
The underlying inventive principle is that the slantnosed forward section 4 when prevented from rotating with respect to the relatively fixed propulsion section 2, will steer the mole in an arc. The radius of the arc, depending upon soil, nose bevel angle and mole length and diameter, varies between about 30 and 50 feet. The are generally lies in a plane that contains the normal to the nose bevel surface and the mole axis. When the forward section 4 is allowed to passively rotate, then the movement of the mole is a helical path which approaches a straight line if the nose is rotating fast enough, i.e., 2 radian per foot of linear advance.
In implementing the inventive steering mechanism, it is of course desirable to detect and monitor the moles position, heading and roll as well as the relative angular position of the forward rotating section 4 with respect to the nonrotating rear section 2. The disclosure of Scott et al. Pat. 3,375,885 illustrates one method for steering a mole.
An alternate scheme is to locate the detectors in propulsion section 2 of the mole 1 and to measure the relative angular position of the nose by some independent method. One such method is shown in FIG. 3 and consists of a simple spiral cam 19 rigidly attached to the rotating nose section through shaft extension 9, a linear variable diflerential transformer 20 rigidly attached to the mole body, and a spring-loaded cam follower 21 which forms part of the core piece 22 of transformer 20. The primary winding 20a and secondary wind-ing 20b of transformer 20 are connected through wires 42 to a voltage reading device (not shown) at a monitoring station. Rotation of the cam 19 displaces the core piece 22 and produces a voltage output proportional to core displacement. Other methods of measurement can readily be envisioned.
4 OPERATION In contrast to earlier penetrators which require that a trench be dug for their introduction into ground the mole 1 of the present invention advantageously is inserted from ground level into a soil bulk 24 below a roadway, for example, as depicted in FIG. 5. A shallow vertical pilot hole sometimes may be desirable to prime the mole I initially. Mole 1 is directed along a path 25 substantially as shown. The benefit of trenchless planting stems from the forward steering feature of the invention which enables the mole to commence steering as soon as fins 3 take hold.
The clutch plates 10, 11 are disengaged to allow free rotation of the forward slanted nose 7. As the mole 1 is propelled into the-ground, the soil engages the flutes 6,
causing nose 7 to rotate. A generally helical path is described by the forward motion of nose 7. Turns are initiated by engaging clutch plates 10, 11 at a selected attitude of the slant nose 7 with respect to the soil ambient. Linear movement is acheived by disengaging clutch plates 10, 11. As the mole progresses, it can tow the telephone or electrical cable to be installed in the ground.
Piston 12, in addition to its translational movement, can be designed to rotate shaft 9 in either direction through clutch plates 10, 11. This expedient can be implemented in numerous conventional ways, and provides a control over the rotational position of nose 7 with respect to section 2 which is not dependent upon the forward movement of the mole 1. Such a positive control would, for example, substantially reduce or eliminate the overtravel which the mole occasionally undergoes in the process of orienting the slant nose 7. With positive control, turns can be initiated or terminated at any point in the moles travel. Moreover, a powered forward section with flutes or flights can be useful as a secondary propulsion system.
Numerous expedients to impart rotation to the forward section 4 can be envisioned. FIGS. 6 through 10 depict five alternative structures to develop the necessary rotation of a slanted nose such as 7. In FIGS. 6 through 10, the soil path with respect to the slant face and the rotation-producing mechanism, and the direction of shaft rotation, are designated respectively by the numerals 26 and 27. Similarly, in each of FIGS. 6 through 10, the numeral 7 denotes the slanted portion of the nose, corresponding to element 7 of the mole in FIG. 1.
In FIG. 6', rotation is imparted to a shaft 4 by a scoop 28 that is built up upon one side of slant nose 7. A rib 29 in the shape of a semiellipse surrounds this scooped portion 28. The soil moves in a curved path up and around scoop 28, imparting an opposite rotation to shaft The embodiment of FIG. 7 makes use of a warped or funnel section 30 built up to one side of the slant nose 7. The soil follows an elongated course through the funnel, causing the desired rotation.
The expedient in the FIG. 8 embodiment involves a scoop 31 below the plane of slant nose 7. Here the scoop takes the form of a flared snow plow with the soil flow pushing up on the plow. Additionally the net soil force normal to slant nose 7 produces a downward movement applied on the opposite side of the nose. The two movements are additive, and rotation is in the same direction as exhibited in the FIGS. 6 and 7 structures.
In FIG. 9, reliance for rotation is placed upon a pair of ribs 32, 33 between which a scoop 34 is defined. The structure is similar to that of FIG. 6.
Finally, the embodiment in FIG. 10 incorporates ramp consisting of raised side sections of the slant nose 7, with the soil being directed up this ramp. At the top, the soil impinges upon an anger flight 36 which causes an opposite rotation to the shaft 4.
It is apparent that all of the embodiments described for generating the necessary free rotation can be constructed, as it were, in left-hand versions if so desired. In each such case, the rotation is in a direction opposite to the right-hand versions.
A further variation of the basic invention is depicted in FIG. 11. This structure differs from that of FIG. 1 in that the nose rotation is generated not by the forward section but by the mole as a whole. In FIG. 11, a forward section designated 37 includes a slant nose 38 which is similar to the slant nose 7 of FIG. 1. As in the previous versions, the forward section 7 is rotatably mounted in a rear section 40, and is engaged and disengaged therefrom through a clutch mechanism designated 39. Clutch 39 can be of the type already described with respect to the FIG. 2 embodiment. The rear section 40 includes auger flights 41 along its outer edge. As the mole advances through the ground, its flights 41 cause the rear section 40 to rotate. If clutch 39 is engaged, the slant nose 38 will also rotate and thus describe a helical path through the ground. Relative rotation-sensing mechanisms of the type earlier referred to are employed to gauge the attitude of slant nose 38. When it is desired to steer the mole, the clutch 39 is disengaged, allowing the slant nose 38 to stop rotating in unison with the rear section 40. When a turn is completed, the clutch 39 is reengaged causing the slant nose 38 to commence rotating again. It is, of course, necessary to provide rotatable couplings (not shown) between the rear section 40 and line 23. This method permits a reduction in length of the front section due to the absence of flutes and the mole becomes steerable immediately upon insertion into the ground.
In addition to the advantages already noted, each embodiment of the invention exhibits a reduced turning radius and a substantially reduced steering power requirement. These benefits arise because the nose bevel which effects the steering is built-in and therefore always available for use without the delays and power expeditures involved with forcing a steering element against the soil. Moreover, the tendency of moles to edge upwardly into the weaker soil regimes is readily countered in the present invention by instituting a delay in the nose rotation in favor of downside bias. Finally, the soil penetration rates during turns of moles equipped in accordance with the invention is greater than earlier moles because the tunnel area of soil being displaced to effect the tunnel is smaller.
It is to be understood that the embodiments described herein are merely illustrative of the principles of the invention. Various modifications may be made thereto by persons skilled in the art without departing from the spirit and scope of the invention.
What is claimed is:
1. Steering apparatus for a subterranean penetrator comprising: a slant-face nose rotatably mounted at the forward end of said penetrator;
means for continuously rotating said nose during said penetrators advance;
means for sensing the rotational position of said slant face with respect to the penetrator proper; and
means for locking said nose and said penetrator in any selected rotational juxtaposition.
2. A method of steering a mole in a soil ambient comprising the steps of:
causing a slant-face nose at the moles forward tip to rotate as the mole advances in the soil; and
terminating the nose rotation at a selected attitude of the nose with respect to said ambient.
3. A subterranean penetrator comprising:
a propulsion section;
a forward section comprising a cylindrical shaft having a common longitudinal axis with said propulsion section, said shaft terminating in a slant-face nose;
means for mounting said forward section with respect to said propulsion section for rotation about said common axis;
means for imparting rotation to said forward section;
soil engaging fins for rotationally stabilizing said propulsion section; and
means for engaging and disengaging said forward and said propulsion sections in selected rotational juxtapositions.
4. A subterranean penetrator in accordance with claim 3, wherein said rotation-imparting means comprises helical flutes in the surface of said shaft for rotationally reacting to incident soil forces.
5. A subterranean penetrator in accordance with claim 3, wherein said slant-face nose comprises a surface each element of which is disposed to said longitudinal axis by an angle of between 25 and 35.
6. A subterranean penetrator in accordance with claim 3, wherein said surface is substantially planar and intersects said longitudinal axis at an angle of between 25 and 30.
7. A subterranean penetrator in accordance with claim 3, wherein said rotation-imparting means comprises soil contacting surfaces which are an integral part of said slant-face nose.
8. A subterranean penetrator in accordance with claim 3, wherein said rotation-imparting means comprises direct drive disposed in said propulsion section and coupled to said forward section.
References Cited UNITED STATES PATENTS 3,298,449 1/ 1967 Bachman et a1. 175-94 X 3,326,008 6/1967 Baran et al 175-19 X 3,375,885 5/1968 Scott et al. 17526 ERNEST R. PURSER, Primary Examiner R. E. FAVREAU, Assistant Examiner U.S. Cl. X.R. l45, 61, 94
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|U.S. Classification||175/19, 175/94, 175/61, 175/45|
|International Classification||E21B7/26, E21B7/04, E21B7/00|
|Cooperative Classification||E21B7/04, E21B7/26|
|European Classification||E21B7/04, E21B7/26|