Mining machine with moveable cutting assembly and method of using the same

Information

  • Patent Grant
  • 6270163
  • Patent Number
    6,270,163
  • Date Filed
    Monday, September 14, 1998
    25 years ago
  • Date Issued
    Tuesday, August 7, 2001
    22 years ago
Abstract
A mining machine (20) for combined entry and retreat cutting of material located in underground seams including, a movable mainframe (21), a wing (50, 51) extending ahead of the movable mainframe, a cutter assembly (100) positionable proximate the end of the wing for entry cutting a hole in the material when the wing is aligned with the direction of movement of the mainframe, a pivotal connection (130) between the mainframe and the wing for orienting the wing at an angle to the direction of the movement of the mainframe, and a carriage mechanism (80) for moving the cutter assembly along the wing for cutting of the material in proximity to the wing during retreat cutting of the material.
Description




TECHNICAL FIELD




The present invention relates generally to a method and apparatus for mining minerals, such as coal, from underground seams. More particularly, the present invention relates to a method and apparatus for carrying out high wall and underground mining operations of mineral seams in a highly efficient, safe, and inexpensive manner. More specifically, the present invention relates to a method and apparatus for carrying out high wall and underground mining operations wherein substantially the entirety of a mineral seam can be recovered, selective collapse of the ground into the mined seam can be effected, and the apparatus and method of operation are relatively simple while permitting high production rates.




BACKGROUND ART




Mining equipment has long been a key to economically successful mining operations. Originally, underground mining of thicker seams was the primary focus for coal-mining enterprises. With significant depletion of thick seams and additional focus on the safety and health implications of such mining, more attention has been concentrated in recent years on mining thinner seams of coal in both surface and underground mining operations. To accomplish better economics, surface miners uncovered as much overburden as was economically feasible for a given thickness of coal and then augured underground into the exposed high wall, recovering additional tons without the expense of removing the overburden. Until recently, these were round augers limited to short underground penetration distances. The advent of the high wall miner using a continuous underground mining machine in front of a conveyor system has allowed significant improvement in penetration depths. The major drawbacks in all auger and high wall mining operations have been localized roof falls and leaving enough space between holes to prevent collapse of the complete hill structure. Leaving enough coal to prevent collapse is extremely inefficient in that substantial pockets of coal remain after the mining operation, and there are possibilities of later subsidence into the bore holes in an uncontrolled and unscheduled manner. The aforesaid inefficiency of conventional high wall mining is particularly significant in instances where the surface of the seam follows a curvilinear path, such that only an extremely small fraction of the seam can be retrieved when employing spaced surface holes.




Efforts have been made over the years to improve recovery rates achievable by high wall mining apparatus. In that respect, different cutter head designs have been developed to achieve improved cutting action. There have also been developments in improving power systems and equipment reliability to reduce down time of high wall mining equipment.




Also, efforts have been made to expand the application of high wall miners beyond traditional applications by effecting higher and wider cuts. In this respect, cutter heads with larger diameters have been developed, together with larger motors, increased conveyor speeds, and the requisite interface equipment. Another more sophisticated approach has been the development of equipment that initially cuts a conventional bore and then proceeds to ream the bore to slightly larger dimensions. In this latter respect, a bore is made horizontally, normally with conventional cutting apparatus. In most instances, these high wall miners cut substantially greater quantities of minerals during the entry phase, with the hole size being only slightly augmented by reaming cutters. In this respect, various types of cutters have been developed for the reaming action, which are normally contracted during the conventional cutting and subsequently expanded during the return cutting operation. In other instances, the main cutter may be pivoted or otherwise minimally offset from the hole produced during the entry phase to produce the retreat reaming cut.




These combined cutting and reaming machines achieve only minor productivity advancements in relation to the complexities and disadvantages that are involved. In most instances, the cutters for the reaming operation are normally located rearwardly on the machine from the entry phase cutters. This, of course, presents the possibilities of a roof collapse, which can trap the mining equipment underground. As a result, limitations are frequently applied to the extent of the cut made by the reaming cutters, such as to minimize the possibility of roof collapse. These systems also have the disadvantage that even though round holes are cut, frequently there remain potential subsidence problems years after mining operations are completed. Thus, developments in high wall mining equipment over recent years have, for the most part, involved refinements to existing equipment and methods.




DISCLOSURE OF THE INVENTION




Therefore, an object of the present invention is to provide a mining machine and process that is particularly useful in regard to high wall and underground mining operations in constituting a total subsidence remote mining system. Another object of the present invention is to provide such a mining machine and process wherein a coal seam is entered by cutting a relatively small and narrow rectangular hole, which is, therefore, not prone to accidental collapse during the entry phase of a mining operation. Another object of the present invention is to provide such a mining machine and process wherein wings of substantial length are expanded to carry out cutting during a retreat mining operation, such that a great preponderance of the mining operation is effected during the retreat mining operation. Another object of the present invention is to provide a mining machine that employs a pair of adjacent, vertically-mounted cutter heads that cut a relatively narrow square or rectangular hole during entry into a mineral seam. A further object of the present invention is to provide a mining machine wherein the cutters employed in the entry phase are movably mounted on a pair of wings for positioning at the leading extremity of the wings during the entry cutting operating phase. Still another object of the invention is to provide such a mining machine wherein the cutting heads move along the length of the wings during the spreading of the wings to the retreat cutting position and, thereafter, during the retreat cutting operation. Yet a further object of the invention is to provide such a mining machine wherein each wing contains an auger that transports cut minerals from a seam to an auger conveyor in the mainframe of the machine that, in conjunction with suitable extensible conveying apparatus, transports cut minerals to the surface of the ground.




A still further object of the present invention is to provide a mining machine wherein the cutting width during the retreat cutting phase approaches the length of the two wings. A further object of the present invention is to provide such a mining machine wherein during the retreat cutting phase, each cutting cycle along the leading edge of the wings is followed by movement of the wings in the direction of the retreat cut, which is approximately the diameter of the cutting heads. Yet another object of the present invention is to provide such a mining machine wherein the same two cutters are variously positioned and operated to effect the cutting operations during both the entry and retreat operations of the machine. Yet a further object of the present invention is to provide such a mining machine that allows for essentially complete recovery of a coal seam, irrespective of the terrain conditions, which is not possible with conventional high wall machinery.




Another object of the present invention is to provide a high wall mining machine that allows for total subsidence, which is not possible with existing high wall miners. Another object of the present invention is to provide an underground mining machine that, in not requiring the presence of workers in the subsidence area, allows for recovery of much thinner seams than existing total-recovery systems. Another object of the present invention is to provide such a mining machine wherein the cutters and wings operate in close proximity to uncut minerals in the seam and constitute the trailing portion of the machine during the retreat phase, thereby minimizing possibilities of collapse or roof falls due to what is, in effect, a shielded area of in-place minerals preceding the total subsidence that is effected by the subject machine.




Yet a further object of the present invention is to provide a mining machine that cuts a minimum of minerals during the entry phase while employing sensors to gather information in regard to the topography of the seam. This information can then be used to adjust the location of the retreat mode to maximize positioning within a seam for full recovery by taking into account changes in topography that take place during the retreat mode when the great majority of the material recovery takes place. A further object of the present invention is to provide such a mining machine wherein controlled retraction and expansion of the wings is possible during retreat in order to vary the cutting width to accommodate a crooked high wall as it follows the contour of hills, which is not possible with a fixed-width machine. This expansion and retraction is also desirable in order to leave the high wall intact as the machine withdraws from the hole. Still another object of the present invention is to provide such a mining machine that may be constructed to optimize performance in various seam heights and various cutting widths appropriate for particular geological conditions.




Yet a further object of the present invention is to provide such a mining machine that uses sidewall grippers for movement of the miner and conveying equipment into and out of the seam, therefore requiring only a fraction of the size of supporting equipment outside of the hole as compared to conventional high wall mining machines whose weight must be sufficient to propel the equipment into and out of the hole. Sidewall grippers are possible in this application because the minerals proximate to the previously mined hole will not be mined until the retreat phase, which is after the grippers have passed, whereas conventional methods must leave a pillar between holes large enough to support the roof. Yet a further object of the present invention is to provide such a milling machine that requires a minimum of operators, and is relatively inexpensive in comparison with conventional high wall machines having comparable mining characteristics.




In general, the present invention contemplates a mining machine for combined entry and retreat cutting of material located in underground seams including, a movable mainframe, a wing extending ahead of the movable mainframe, a cutter assembly positionable proximate the end of the wing for entry cutting a hole in the material when the wing is aligned with the direction of movement of the mainframe, a pivotal connection between the mainframe and the wing for orienting the wing at an angle to the direction of movement of the mainframe, and a carriage mechanism for moving the cutter assembly along the wing for cutting of the material in proximity to the wing during retreat cutting of the material.




The present invention also contemplates a method of mining minerals located in an underground seam, including the steps of cutting an entry hole in the underground seam, locating a mining machine having a wing-mounted cutter assembly in the entry hole, moving the cutter assembly lengthwise of the wing to effect a widening cut of the entry hole in the area adjacent to the wing, spreading the wing angularly into the widening cut effected by the cutter assembly, sequentially repeating the moving of the cutter assembly lengthwise of the wing to effect a further widening cut to the entry hole and the spreading of the wing angularly into widening cuts until the wing is displaced through a desired angle, instituting retreat motion increments of the mining machine and the wing subsequent to advance cuts by the cutter assembly lengthwise of the wings, whereby a retreat cut of a width exceeding the width of the entry hole is accomplished.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a partially-schematic top plan view of exemplary mining apparatus according to the concepts of the present invention, shown in relation to a bore into an underground mineral seam and depicting the overall layout.





FIG. 2

is a partially-schematic side-elevational view of the mining apparatus of

FIG. 1

showing additional features of the overall layout.





FIG. 3

is an enlarged fragmentary-elevational view of the apparatus of

FIG. 1

taken substantially along the line


3





3


of FIG.


1


and showing a wing, a carriage, a support arm, and a cutting head.





FIG. 4

is an enlarged elevational view of the mining apparatus of

FIG. 1

taken substantially along the line


4





4


of FIG.


1


and showing details of the interrelation between the wings and the carriages.





FIG. 5

is an enlarged fragmentary-elevational view of the mining apparatus of

FIG. 1

taken substantially along the line


5





5


of FIG.


1


and showing details of the interconnection between the movable mainframe and the wings.





FIG. 6

is a vertical sectional view of the mining apparatus of

FIG. 1

taken substantially along the line


6





6


of

FIG. 5

with portions broken away and showing details of the interconnection between the mainframe and the wings.





FIG. 7

is a vertical elevational view of the mining apparatus of

FIG. 1

taken substantially along the line


7





7


of FIG.


1


and showing details of the wing spread control mechanism.





FIGS. 8A-8D

schematically depict the sequence of operations of the wing-spread control mechanism in moving a wing from the closed to the open position.





FIG. 9

is a rear-elevational view of the mining apparatus of

FIG. 1

taken substantially along the line


9





9


of FIG.


2


and showing details of the mainframe and augers.





FIG. 10

is a side-elevational view of an alternate form of wing construction designed to steer the mining apparatus vertically to follow an undulating mineral seam.





FIG. 11

is an elevational view similar to

FIG. 4

showing the alternate form of wing construction of FIG.


10


and particularly the movable bottom plate for steering the mining apparatus.





FIG. 12

is an elevational view similar to

FIG. 7

showing the alternate form of wing construction of FIG.


10


and particularly the control elements for the movable bottom plate for steering the mining apparatus.





FIGS. 13A-13L

schematically depict the sequence of operations of the mining apparatus of

FIG. 1

during an operating cycle of entry and retreat in mining a seam of minerals.











PREFERRED EMBODIMENT FOR CARRYING OUT THE INVENTION




The mining machine according to the concepts of the present invention is generally indicated by the numeral


20


in

FIGS. 1 and 2

. As shown, the mining machine


20


is depicted in operative relation to a cut hole H in the entry phase of a typical high wall mining operation. For purposes of orientation, the mining machine


20


is depicted as proceeding in the cut hole H from right to left, as depicted in

FIGS. 1 and 2

.




The mining machine


20


has as a primary component a mainframe assembly, generally indicated by the numeral


21


, that interfaces with conveyors extending to the surface of the ground. The mainframe assembly


21


has, as a primary structural member, a platform


22


, which may be a down-turned U-shaped member, as best seen in FIG.


9


. The platform


22


carries on its upper surface an attached housing


23


, which may also be of a down-turned U-shaped configuration. Still referring to

FIGS. 1

,


2


, and


9


, the housing


23


encloses a mainframe drive assembly, generally indicated by the numeral


25


. As shown, the mainframe drive assembly


25


has a pair of advance and retract cylinders


26


and


27


that are conveniently positioned in parallel, side-by-side relationship. The advance and retract cylinders


26


,


27


each have a blind end


28


attached to the platform


22


and a rod end


29


, which is operative as hereinafter described.




As seen in

FIGS. 1

,


2


, and


9


, the mainframe assembly


21


also includes a pair of mainframe clamping mechanisms, generally indicated by the numerals


35


and


36


. As shown, the mainframe clamping mechanisms


35


,


36


include enlarged clamping plates


37


that extend laterally to either side of the mainframe assembly


21


. The mainframe clamping plates


37


are attached to one or more clamping cylinders


38


, which are affixed to the housing


23


as by cap screws


39


. As best seen in

FIG. 9

, the clamping cylinders


38


are selectively actuated to move the clamping plates


37


into and out of engagement with the rectangular cut hole H produced by mining machine


20


in a known manner for moving the mainframe assembly


21


in incremental steps into and out of a cut hole H.




Referring now to

FIGS. 1

,


2


,


5


, and


9


, the mainframe assembly


21


includes a mainframe conveyor system, generally indicated by the numeral


40


. The mainframe conveyor system


40


has an elongate chute


41


that may be generally rectangular in cross-section. As shown, the chute


41


fits within the U-shaped platform


22


for relative motion with respect to platform


22


and housing


23


longitudinally of mainframe assembly


21


.




Mounted internally of chute


41


of mainframe conveyor system


40


are a pair of mainframe augers


42


,


43


that extend substantially the length of the chute


41


. The augers


42


,


43


preferably have auger shafts


44


and


45


that are in substantially parallel alignment and extend substantially the longitudinal length of the chute


41


. The auger shafts


44


,


45


are supported on brackets


46


carrying bearings


47


(

FIG. 5

) preferably proximate the ends of and, as might be necessary, interspersed along the length of shafts


44


,


45


. The auger shafts


44


,


45


carry spiral blades


48


, which may be any of various designs known in the industry. The auger shafts


44


,


45


are driven by one or more suitable auger motors


49


to transport coal or other minerals along and to the rear of mainframe assembly


21


, which is from left-to-right, as depicted in

FIGS. 1 and 2

of the drawings. It will be appreciated that additional conveyor units (not shown), which may be the same as or similar to mainframe conveyor system


40


, may be attached to the chute


41


proximate auger motors


49


to transport mined minerals to the surface where cut hole H commences as the mining machine


20


proceeds underground following a seam of minerals.




Disposed ahead of the mainframe assembly


21


of mining machine


20


in exemplary cut hole H are a pair of cutter wing assemblies, generally indicated by the numerals


50


and


50


′. As viewed from the top and facing into the cut hole H in

FIG. 1

, the left cutter wing assembly is designated by the numeral


50


, and the right cutter wing assembly is designated by the numeral


50


′. The cutter wing assemblies


50


and


50


′ may be of identical configuration except that each is constructed essentially as a mirror image of the other. Therefore, the following discussion covers the structure of both of the cutter wing assemblies


50


and


50


′, although directed specifically to the left cutter wing assembly


50


. Referring now to

FIGS. 1-6

of the drawings, cutter wing assembly


50


has an outwardly open L-shaped frame


51


. As shown, the frame


51


has a vertical member


52


and a lower horizontal member


53


.




Positioned within the lower reaches of L-shaped frame


51


proximate the joinder of vertical member


52


and horizontal member


53


is a wing conveyor system, generally indicated by the numeral


55


. The wing conveyor system


55


has a wing auger


56


that extends essentially the full length of the L-shaped frame


51


. The wing auger


56


has a wing auger shaft


57


extending beyond both longitudinal extremities of wing auger


56


and rotatably mounted in relation to a front support post


59


and a rear support post


60


affixed to the frame


51


.




It will thus be appreciated that rotation of wing auger


56


ofwing conveyor system


55


in the direction indicated in

FIGS. 3-5

of the drawings would serve to transport loose material in cut hole H from front to rear of cutter wing cutter assembly


50


as restrained by the L-shaped frame


51


. It is further to be appreciated that cut material introduced at any position longitudinally of wing conveyor system


55


from outwardly of wing conveyor system


55


will be transported rearwardly within the L-shaped frame


51


to the rear of cutter wing assembly


50


.




The wing conveyor system


55


interrelates with and is powered by a conveyor interconnect mechanism, generally indicated by the numeral


65


. The conveyor interconnect mechanism


65


consists of a short extent of auger


66


, which is joined at its ends to wing auger shaft


57


and mainframe auger shaft


44


as by universal joints


67


and


68


, respectively.




It will thus be appreciated that auger motor


49


may power both the mainframe conveyor system


40


and the wing conveyor system


55


due to the conveyor interconnect mechanism


65


. It will also be understood that with appropriate placement of the universal joints


67


,


68


of conveyor interconnect mechanism


65


, cutter wing assembly


50


may be displaced angularly with respect to the mainframe assembly


21


while still providing for rotation of the augers


42


and


66


. Further, the section of auger


66


on conveyor interconnect mechanism


65


effects transfer of cut material from the wing conveyor system


55


to the mainframe conveyor system


40


and subsequently within the chute


41


, such as to move cut material rearwardly of the mining machine


20


.




Cutter wing assembly


50


is movable a distance longitudinally of, and angularly with respect to, mainframe assembly


21


by a pivot assembly, generally indicated by the numeral


70


, as best seen in

FIGS. 2

,


5


, and


6


. The pivot assembly


70


has a drive plate


71


that is attached to the rod end


29


of advance and retract cylinder


26


of mainframe drive assembly


25


and to the chute


41


of mainframe conveyor system


40


. The drive plate


71


has an attached forward projecting offset arm


72


that mounts a spherical bearing socket


73


. The cutter wing assembly


50


has a laterally projecting auxiliary frame


74


with spaced parallel arms


75


and


76


that carry a rod


77


mounting a spherical ball that engages the spherical bearing socket


73


in offset arm


72


of drive plate


71


. It will be appreciated that the interconnection between spherical ball


78


and spherical bearing socket


73


permits a substantial extent of lateral angular motion of cutter wing assembly


50


relative to mainframe assembly


21


. In addition, the spherical ball


78


and spherical bearing socket


73


permit a minor extent of vertical angular motion of cutter wing assembly


50


relative to mainframe assembly


21


.




The cutter wing assembly


50


has a cutter carriage assembly, generally indicated by the numeral


80


, located generally within the L-shaped frame


51


and above the wing conveyor system


55


. Referring to

FIGS. 1-6

, inclusive, the cutter carriage assembly


80


has a carriage frame


81


having a horizontal leg


82


and an upright leg


83


that generally parallels the horizontal member


53


and vertical member


52


of L-shaped frame


51


, respectively (FIG.


4


). The carriage frame


81


is movable along essentially the fill longitudinal length of L-shaped frame


51


of cutter wing assembly


50


on a pair of spaced, horizontally-disposed rails, namely, upper rail


84


and lower rail


85


. As shown, the rails


84


,


85


are of a V-shaped, in-turned configuration that matingly engage correspondingly grooved upper wheels


86


and lower wheels


87


of carriage frame


81


. As best seen in

FIGS. 3 and 4

, the carriage frame


81


has a pair of horizontally-spaced upper wheels


86


and a pair of lower wheels


87


, all of which are freely rotatably mounted on carriage frame


81


by bolts


88


. Thus, the carriage frame


81


is mounted for horizontal travel for positioning along the L-shaped frame


51


of cutter wing assembly


50


.




The carriage frame


81


is selectively positioned along the rails


84


,


85


by a carriage drive assembly, generally indicated by the numeral


90


. The carriage drive assembly


90


consists of a discontinuous drive chain


91


having one end affixed to a first chain end attachment bracket


92


and the other end affixed to a second chain end attachment bracket


93


, both rigidly attached to upright leg


83


of the carriage frame


81


. The drive chain


91


is reeved about an idler sprocket


94


mounted proximate the forward end of the L-shaped frame


51


of cutter wing assembly


50


. The drive chain


91


is also reeved about a drive sprocket


95


that is affixed to L-shaped frame


51


proximate the rear or trailing end of cutter wing assembly


50


. The drive sprocket


95


is mounted on the shaft


96


(see

FIG. 6

) of a carriage drive motor


97


. The drive motor


97


is a reversible motor that may be energized to move carriage frame


81


at a selected speed and a selected direction along the rails


84


,


85


attached to the L-shaped frame


51


of the cutter wing assembly


50


.




The cutter carriage assembly


80


operatively mounts a cutter assembly, generally indicated by the numeral


100


, which is best seen in

FIGS. 1-4

of the drawings. The cutter assembly


100


has a cutter head


101


that, as shown, consists of a pair of axially-aligned, vertical-oriented drums


102


. The exterior surface of the drums


102


carries aplurality of axially- and circumferentially-spaced cutters


103


that are designed to effect a cut in a mineral seam, dirt, and the like encountered in mining operations. The drums


102


are rotated by hydraulic motors


104


positioned within the confines of the drums


102


. The drums


102


have axially-outward end caps


105


that are non-rotatably affixed on splined shafts


106


of the hydraulic motors


104


. Thus, it will be appreciated that the drums


102


may be selectively rotated by hydraulic motors


104


at a desired speed to optimize cutting operations effected by the cutters


103


on drums


102


. The hydraulic motors


104


may advantageously be reversible, such as to permit rotation of drums


102


in either direction, depending on cutting techniques being employed, and to permit brief reversals in the rotational direction of drums


102


of cutter head


101


in the event drums


102


become temporarily jammed due to the quantity or content of the material being cut at a given time.




Interposed between and mounting drums


102


on each cutter head


101


is an elongate cutting arm


110


. The cutting arm


110


mounts opposed extending collars


111


to which the hydraulic motors


104


are attached as by bolts


112


. The collars


111


also seat bearings


113


outwardly thereof upon which drums


102


rotate when actuated by hydraulic motors


104


. It will be appreciated that the cutter assembly


100


and its interrelation with cutting arm


110


is merely exemplary of various types of cylindrical cutting heads that are known in the industry. Any of various cylindrical cutter head designs could be employed as long as appropriately sized and powered.




The extremity of cutting arm


110


opposite the cutter head


101


is pivotally affixed to the carriage frame


81


. As shown, the cutting arm


110


is non-rotatably affixed to a pivot pin


114


(FIG.


3


). The pivot pin


114


extends through a portion of carriage frame


81


and has a gear


115


non-rotatably affixed thereon. Thus, it will be appreciated that rotation of the gear


115


provides equiangular rotation of cutting arm


110


about the pivot pin


114


. The gear


115


is in engagement with a pinion


116


. The pinion


116


is mounted on a shaft


117


of a rotary actuator


118


attached to the carriage frame


81


. Thus, it will be seen that energizing rotary actuator


118


effects angular movement of cutter head


101


about pivot pin


114


through action of the shaft


117


and the pinion


116


. In that respect, the cutter head


101


may be rotated from a position substantially in alignment with L-shaped frame


51


of cutter wing assembly


50


, as seen in

FIGS. 1 and 2

, to a position substantially perpendicular thereto, as depicted, for example, in

FIG. 13D

of the drawings.




Referring now to

FIGS. 4 and 7

, each of the wing assemblies


50


and


50


′ have a wing clamping assembly, generally indicated by the numeral


120


. The left cutter wing assembly


50


has a wing clamping assembly


120


, and the cutter wing assembly


50


′ has a wing clamping assembly


120


′, both of which are located on the interior or inboard side of cutter wing assemblies


50


,


50


′ and, like the other components of the cutter wing assemblies


50


,


50


′, are substantially identical except that each is the mirror image of the other and that certain elements are offset to obviate interference. The wing clamping assembly


120


is provided to retain cutter wing assembly


50


in a preselected position while cutter carniage assembly


80


is moving along rails


84


,


85


to expand a cut hole H in a manner hereinafter detailed. The wing clamping assembly


120


consists of a rear clamping cylinder


121


that activates a rear upper clamp plate


122


and a rear lower clamp plate


123


. It will thus be appreciated that actuation of rear clamping cylinder


121


moves rear upper clamp plate


122


into engagement with the top of a cut hole H and rear lower clamp plate


123


into the bottom of a cut hole H.




The wing clamping assembly


120


also includes a front upper clamping cylinder


124


that powers a front upper clamp plate


125


from the retracted, solid-line position to the engagement position


125


′ with the top of a cut hole H. A front lower clamping cylinder


126


carries a front lower clamp plate


127


from the retracted, solid-line position of

FIG. 7

to the extended position


127


′ contacting the lower surface of the cut hole H. The front upper clamping cylinder


124


and the front lower clamping cylinder


126


are attached to the vertical member


52


of the L-shaped frame


51


of cutter wing assembly


50


. The rear clamping cylinder


121


is mounted in a manner hereinafter described.




Referring now particularly to

FIGS. 4

,


7


, and


8


A, the angular positioning of each of wing cutter assemblies


50


and


50


′ relative to mainframe assembly


21


is effected by a wing spreader assembly, generally indicated by the numeral


130


, operating in conjunction with the wing clamping assembly


120


. The wing spreader assembly


130


includes a rotating shaft


131


that moves in a plurality of spaced bearings


132


attached to vertical member


52


of L-shaped frame


51


. As seen, the shaft


131


is substantially vertically mounted on the frame


51


and is selectively directionally rotated by a rotary actuator


133


shown mounted intermediate the length of the shaft


131


. Operatively interrelated with the shaft


131


of wing spreader assembly


130


are an upper spreader cylinder


134


and a lower spreader cylinder


135


that, as seen in

FIG. 7

, are oriented substantially perpendicular to shaft


131


and substantially horizontal. The rod end of each of the spreader cylinders


134


,


135


is attached by a clamping collet


136


to the shaft


131


, such as to rotate with shaft


131


, which is rotated by the rotary actuator


133


. The blind ends of the cylinders


134


,


135


have a projecting eye


137


that receives through shafts


138


which freely rotatably mounts rollers


139


to either side of the eye


137


. The blind ends of cylinders


134


,


135


are releasably retained in L-shaped brackets


140


that are mounted on the inner surface of vertical member


52


of L-shaped frame


51


of the cutter wing assembly


50


′ (see FIGS.


7


and


8


A). Thus, the spreader cylinders


134


,


135


are interconnected between the two cutter wing assemblies


50


,


50


′ during a portion of their operational sequence, as hereinafter detailed. The upper spreader cylinder


134


and lower spreader cylinder


135


remain in a vertical plane during lateral horizontal motion because rear clamping cylinder


121


is affixed to both upper spreader cylinder


134


and lower spreader cylinder


135


as by welds


141


. Synchronization of the cylinders


134


,


135


assured by the parallelogram linkage created with the shaft


131


and rear clamping cylinder


121


.




An exemplary operational capability of the manipulation of cutter wing assemblies


50


,


50


′, with respect particularly to the cutter wing assembly


50


, is depicted in the form of the sequential schematic top plan views of

FIGS. 8A-8D

. In

FIG. 8A

, the cutter wing assemblies


50


and


50


′ are shown in side-by-side, parallel alignment and in alignment with the mainframe assembly


21


. Preparatory to an initial spreading of the cutter wing assembly


50


, the front upper clamping cylinder


124


and the front lower clamping cylinder


126


of cutter wing assembly


50


′ are actuated to the clamping position. In the ensuing discussion regarding

FIGS. 8A-8D

, it will be assumed in all cases that the front lower clamping cylinder


126


is actuated to the clamping position or to the retracted position at any time the front upper clamping cylinder


124


is actuated to the clamping position or the retracted position with respect to both of the cutter wing assemblies and


50


and


50


′. The front upper clamping cylinder


124


and the rear clamping cylinder


121


of cutter wing assembly


50


are activated to the rod retracted position.




At that time, the spreader cylinders


134


,


135


are actuated to rotate cutter wing assembly


50


about pivot assembly


70


. As depicted in

FIG. 8B

, this actuation of the spreader cylinders


134


,


135


produces an extent of clearance between cutter wing assemblies


50


and


50


′, such as to provide sufficient space for subsequent operating steps. Once the rods of spreader cylinders


134


,


135


are fully extended, as essentially depicted in

FIG. 8B

with rollers


139


engaging L-shaped bracket


140


of cutter wing assembly


50


′, and the front cylinder


124


is clamped, the rotary actuator


133


is energized to effect counterclockwise rotation of spreader cylinders


134


,


135


relative to shaft


131


. This results in the rollers


139


at the blind end of spreader cylinders


134


,


135


departing from their contacting relationship with the L-shaped bracket


140


and following an arcuate path, as depicted in FIG.


8


C. The spreader cylinders


134


,


135


are actuated to retract the rod contemporaneously with the activation of rotary actuator


133


in order to prevent interfering engagement of frame


51


of cutter wing assembly


50


′ with the rollers


139


.




The operation of cutter cylinders


134


and


135


to retract the piston rods while the spreader cylinders


134


,


135


are rotated about shaft


131


by actuation of rotary actuator


133


continues until a position of cutter wing assembly


50


components, as depicted in

FIG. 8D

, is achieved. At that point, the cylinder rod of spreader cylinders


134


,


135


is substantially retracted, and the spreader cylinders


134


,


135


are oriented substantially perpendicular to frame


51


of cutter wing assembly


50


. While the orientation of

FIG. 8D

is desirable under certain circumstances, it may be appropriate to otherwise orient the spreader cylinders


134


,


135


as by placing them more in parallel alignment with the mainframe assembly


21


. Thereafter, the rear clamping cylinder


121


is actuated to the clamping position, with the front upper clamping cylinder


124


actuated to the clamping position to effect cutting operations by cutter assembly


100


along cutter wing assembly


50


. After the conclusion of the cutting operation, the front upper clamping cylinder


124


is activated to the retracted position, such that the spreader cylinders


134


,


135


may be actuated to extend the piston rods thereof to move the cutter wing assembly


50


into a further angularly-spread position from whence material can be cut by cutter assembly


100


. Subsequent repetitions of the cutting and moving sequence from

FIG. 8D

permit any desired extent of angular pivoting of the cutter wing assembly


50


relative to mainframe assembly


21


.




In order to effect vertical adjustments of the mining machine


20


during the entry phase to better follow a mineral seam and maintain the cut hole H centered therein, modified cutter wing assemblies


150


and


150


′, depicted in

FIGS. 10-12

of the drawings, may advantageously be employed. Upward and downward steering of the cutter wing assemblies


150


and


150


′ is effected by a modified L-shaped frame


151


. As in the instance of cutter wing assemblies


50


and


50


′, the structures are identical, except that each is the mirror image of the other, such that only the cutter wing assembly


150


is hereinafter described.




In essence, L-shaped frame


151


is a two-piece structure having a vertical member


152


with a downward extremity that is bifurcated by an attached retainer plate


153


to form a vertically-extending groove


154


. The groove


154


receives an L-shaped bottom plate


155


having a horizontal leg


156


similar to horizontal member


53


of cutter wing assembly


50


. A vertical leg


157


interfits within the groove


154


formed between vertical member


152


and retainer plate


153


. The bottom plate


155


is fixed within groove


154


proximate the rear end of cutter wing assembly


150


by a pivot pin


160


, such that bottom plate


155


is rotatable thereabout to raise and lower the front end of bottom plate


155


. The extent of vertical movement of the front end of bottom plate


155


may be controlled by one or more throughbolts


162


that extend through vertical member


152


of L-shaped frame


151


, through groove


154


, and through retainer plate


153


. The throughbolts


162


also extend through a vertical slot


163


in the vertical leg


157


of bottom plate


155


, such that bottom plate


155


may move vertically the length of slots


163


about pivot pin


160


. The vertical position of the front end of bottom plate


155


may be selectively controlled by a steer-down cylinder


165


having its blind end attached to a top pin


166


, which is affixed to vertical member


152


of L-shaped frame


151


and its rod end attached to a bottom pin


167


, which is affixed to vertical leg


157


of bottom plate


155


.




The cutter wing assembly


150


is shown in solid lines in its normal operating position in

FIGS. 10-12

of the drawings. As shown, the steer-down cylinder


165


has its rod extended with the bottom plate


155


extended downwardly, such that the throughbolts


162


engage the top of the slots


163


. In this position, the horizontal leg


156


of bottom plate


155


is essentially perpendicular to the ends of the vertical member


152


of the frame


151


. Actuation of the steer-down cylinder


165


to retract its rod raises bottom plate


155


at the front end thereof to raise the horizontal leg


156


to the chain-line position


156


′, as best seen in FIG.


11


. This causes cutter wing assembly


150


′ to steer downwardly to maintain cutter assembly


100


selectively positioned within a mineral seam that is downwardly inclined.




In order to achieve upward steering of cutter wing assembly


150


, the front lower clamping cylinder


126


may be actuated to extend the front lower clamp plate


127


from the retracted, solid-line position of

FIG. 12

to the extended position


127


′, which is below the horizontal leg


156


of bottom plate


155


. In this instance, the front upper clamp plate


125


operated by front upper clamping cylinder


124


is not actuated to permit upward steering or deflection of cutter wing assembly


150


while front lower clamp plate


127


is in the extended position


127


′ (see FIG.


12


). Since the front lower clamp plate


127


is maintained extended during upward steering of cutter wing assembly


150


, clamp plate


127


may have an upturned leading edge


128


and an upturned trailing edge


129


to prevent front lower clamp plate


127


from digging into or catching on the lower surface of the cut hole H. Thus, the cutter wing assemblies


150


,


150


′ may be steered downwardly or upwardly to optimize following a mineral seam based upon information developed from prior cut holes H, from the cut hole H being made at the time, or during retreat mining based upon information developed during the entry phase of the mining operation.




An exemplary operating sequence for a method of mining minerals employing a mining machine


20


is schematically depicted in

FIGS. 13A-13L

. The mining machine


20


is depicted creating the cut hole H in a high wall W defined by the surface of the earth.




As viewed throughout as a plan view, the mining machine


20


is depicted in

FIG. 13A

at initial entry into the high wall W. The cutter assemblies


100


on each cutter wing assembly


50


,


50


′ are rotated counterclockwise and clockwise, respectively, as seen in a top plan presentation. The wing conveyor systems


55


of the cutter wing assemblies


50


and


50


′, being initially unconfined, deposit minerals outwardly of the high wall W, as seen in FIG.


13


A.




The mining machine


20


is advanced to produce a cut hole H following a mineral seam by advancing the cutter wing assemblies


50


,


50


′ with the clamping mechanisms


35


,


36


engaging the sides of the cut hole H, as depicted in FIG.


13


B. When extension of the advance and retract cylinders


26


,


27


of mainframe drive assembly


25


is completed, the clamping mechanisms


35


,


36


are retracted out of engagement with the cut hole H, and the mainframe assembly


21


of mining machine


20


is advanced by retracting the advance and retract cylinders


26


,


27


to pull the mainframe assembly


21


into close proximity to the cutter wing assemblies


50


,


50


′, as seen in FIG.


13


C. The clamping mechanisms


35


,


36


are then expanded into engagement with the walls W of cut hole H preparatory to a further advance of cutter wing assemblies


50


,


50


′, such that the cutter assemblies


100


effect further cutting advance into a mineral seam. As seen in

FIG. 13B

, with the mainframe assembly


21


within the cut hole H, cut minerals are discharged rearwardly of mining machine


20


by the wing conveyor system


55


and mainframe conveyor system


40


for discharge outside the high wall W. As the mining machine


20


proceeds further into a mineral seam from the high wall W, as seen in

FIG. 13C

, additional lengths of conveyor may be supplied in a manner well known in the art to continue the discharge of cut material outwardly of the high wall W.




Once the cut hole H has reached a desired depth in a mineral seam, the clamping mechanisms


35


,


36


are extended to engage the cut hole H to temporarily hold mining machine


20


in position, as depicted in FIG.


13


D. At that time, with the cutter assemblies


100


continuing their cutting action, the rotary actuators


118


of cutting arms


110


are actuated to pivot the cutter assemblies


100


from a position in alignment with cutter wing assemblies


50


,


50


′, as seen in

FIG. 13C

, to a position perpendicular to the cutter wing assemblies


50


,


50


′, as seen in FIG.


13


D.




Thereafter, the carriage drive assemblies


90


of cutter carriage assemblies


80


are activated to move the cutter assemblies


100


lengthwise of, or from the front to the rear of, the cutter wing assemblies


50


and


50


′ to reach the position depicted in

FIG. 13E

of the drawings. During this widening cut of the original entry cut hole H, the cutter assemblies


100


,


100


continue to deposit cut minerals for transport via the wing conveyor systems


55


and mainframe conveyor system


40


for deposit outwardly of the high wall W, as previously described.




Once this widening cut is effected, the cutter assemblies


100


are returned to their position in alignment with cutter wing assemblies


50


,


50


′ by actuation of cutter carriage assembly


80


and the pivoting of cutting arms


110


,


110


. At this time, the spreading of cutter wing assemblies


50


and


50


′ is commenced to effect angular displacement of the cutter wing assemblies


50


and


50


′ relative to mainframe assembly


21


by virtue of the pivot assemblies


70


. The initial angular separation between cutter wing assembly


50


and cutter wing assembly


50


′ is effected by actuation of spreader cylinders


134


,


135


of wing spreader assembly


130


associated with each of the cutter wing assemblies


50


,


50


′, with the components of wing clamping assembly


120


being positioned as discussed hereinabove in conjunction with the description of

FIGS. 8A-8D

. With cutter assembly


100


continuing to cut as depicted in

FIG. 13F

, cutter wing assembly


50


is displaced angularly with respect to cutter wing assembly


50


′.




As seen in

FIG. 13G

, the wing spreader assembly


130


of cutter wing assembly


50


is disengaged from the cutter wing assembly


50


′, while the cutter assembly


100


is moved from alignment with cutter wing assembly


50


to a position perpendicular thereto and then along the length of cutter wing assembly


50


, as depicted in

FIG. 13G

, to effect a further widening cut to the entry cut hole H. Suitable repetitions of this motion may be effected until the wing spreader assembly


130


associated with cutter wing assembly


50


can be repositioned perpendicular thereto by actuation of rotary actuator


133


to achieve the positioning depicted in FIG.


13


H. Details of the positioning steps and actuation of wing clamping assembly


120


are discussed hereinabove in conjunction with the description of

FIGS. 8C and 8D

. Repeat sequencing of the wing clamping assembly


120


and wing spreader assembly


130


, with intermittent movement of cutter assembly


100


along cutter wing assembly


50


, may be employed to achieve any desired degree of angular positioning of cutter wing assembly


50


relative to cutter wing assembly


50


′.




Thereafter, stepped angular movement of cutter wing assembly


50


′ may be effected in the manner just described for cutter wing assembly


50


, with sequential cutting steps by cutter assembly


100


preceding each angular actuation of cutter wing assembly


50


′ until such time as cutter wing assemblies


50


and


50


′ are equiangularly disposed relative to the longitudinal axis of the mainframe assembly


21


of mining machine


20


. Once the position depicted in

FIG. 13I

is achieved, the retreat mining operation commences in its most productive form, wherein the full widened area bounded by cutter wing assemblies


50


,


50


′ is mined as the mining machine


20


retreats in step fashion from the entry cut hole H. In the retreat mining operation, the clamping mechanisms


35


,


36


of mainframe assembly


21


are engaged, as are the rear upper clamp plates


122


of wing clamping assembly


120


. At such time, the cutter wing assemblies


50


and


50


′ are moved toward the high wall W by actuation of the advance and retreat cylinders


26


,


27


of mainframe drive assembly


25


to retract the piston rods and by synchronized extension of the piston rods of upper and lower spreader cylinders


134


,


135


of the cutter wing assemblies


50


,


50


′ into an area previously cleared by cutter assemblies


100


of the cutter wing assemblies


50


,


50


′. Release and movement of the clamping mechanisms


35


,


36


of mainframe assembly


21


and wing clamping assemblies


120


to the retract piston rods of rear clamping cylinders


121


and extend the piston rods of advance and retract cylinders


26


,


27


of mainframe drive assembly


25


is effected. Thereafter, wing clamping assemblies


120


and clamping mechanisms


35


,


36


are actuated to the clamping position preparatory to a repetition of the motion of cutter assemblies


100


along the length of cutter wing assemblies


50


and


50


′ and are returned to the position depicted in FIG.


13


I. This cut and advance sequence with cutter wing assemblies


50


,


50


′ angularly displaced, as depicted in

FIG. 13I

is repeated through the entire retreat cutting operation or for a substantial portion of the retreat of mining machine


20


to the high wall W.




In instances where it is desirable to retain a high wall W substantially intact, an incremental closing or reduction in angularity of the cutter wing assemblies


50


,


50


′ relative to the mainframe assembly


21


may be effected. In such instance, the procedure depicted in

FIGS. 13J-13L

may be employed. The cutter assemblies


100


are returned only a portion of the length of the cutter wing assemblies


50


,


50


′ and subsequently effect a cut of only a portion of the length of the cutter wing assemblies


50


,


50


′, as seen in

FIG. 13J

of the drawings.




Thereafter, the mainframe assembly


21


may be step-wise further withdrawn from the cut hole H, such that an even narrower cut is effected. In this respect, it will be appreciated that retaining the rear clamp plates


122


,


123


in engagement with the top and bottom of the cut hole H while the mainframe drive assembly


25


retracts the pistons of advance and retract cylinders


26


,


27


to thereby retract cutter wing assemblies


50


and


50


′ tends to angularly inwardly displace the cutter wing assemblies


50


,


50


′, as can be seen in comparing

FIGS. 13J and 13K

of the drawings. Subsequent to achieving the position of

FIG. 13K

, rotation of the cutter assemblies


100


may be discontinued, and carriage drive assembly


90


may be disconnected, such that cutter assemblies


100


may be displaced along cutter wing assemblies


50


and


50


′. The rear upper clamp plates


122


are retracted out of contact with cut hole H, and the engagement of cutter assemblies


100


with the coal causes further angular closing of the cutter wing assemblies


50


,


50


′. The rotary actuators


133


of wing spreader assemblies


130


are actuated to return the wing spreader assemblies


130


to their original position as collapse of the cutter wing assemblies


50


,


50


′ to their original parallel position is effected, as depicted in process in FIG.


13


L.




While an exemplary operating sequence for entry and retreat mining has been described hereinabove, it will be appreciated by persons skilled in the art that a great number of variations or alterations in the operating sequence may be employed with the flexibility of the mining machine


20


herein disclosed without departing from the scope of the present invention. For instance, the direction of rotation of the cutter assemblies


100


may be altered during some or all of the cutting operations from that depicted in

FIGS. 12A-12L

. Further, differing sequential operations of the various elements of the cutter wing assemblies


50


and


50


′ might be employed, depending upon the constitution of the mineral seam and the constitution of adjacent underground seams, and other operational factors. Also, the entry hole may be cut by a different machine, with the mining machine


20


providing the spreading and retreat cutting operations.



Claims
  • 1. A mining machine for combined entry and retreat cutting of material located in underground seams comprising, a moveable mainframe, a wing extending ahead of said movable mainframe and having a first end and a second end, a cutter assembly positionable proximate said first end of said wing for entry cutting a hole in the material when said wing is aligned with the direction of movement of said mainframe, a pivotal connection between said mainframe and said second end of said wing for orienting said wing at an angle to the direction of movement of said mainframe, and a carriage mechanism for moving said cutter assembly along said wing for cutting of the material in proximity to said wing during retreat cutting of the material.
  • 2. A mining machine according to claim 1, wherein said cutter assembly includes a drum cutter.
  • 3. A mining machine according to claim 2, wherein said drum cutter has a vertical axis of rotation.
  • 4. A mining machine according to claim 2, wherein said drum cutter produces a square entry hole.
  • 5. A mining machine according to claim 1, wherein said cutter assembly is mounted on said carriage mechanism for moving said cutter assembly along said wing.
  • 6. A mining machine according to claim 5, including a cutting arm carrying said cutter assembly and mounted for travel on rails affixed to and extending longitudinally on said wing.
  • 7. A mining machine according to claim 6, wherein said carriage mechanism is selectively driven by a drive motor mounted on said wing.
  • 8. A mining machine according to claim 1, wherein said wing has a wing conveyor for transfer of the material cut by said cutter assembly to said mainframe.
  • 9. A mining machine according to claim 8, wherein said mainframe has a mainframe conveyor for receiving and transferring the material received from said wing conveyor.
  • 10. A mining machine according to claim 9, including a conveyor interconnect mechanism joined to said wing conveyor and said mainframe conveyor by universal joints, thereby permitting angular spreading of said wing relative to said mainframe.
  • 11. A mining machine according to claim 1, wherein said wing has a wing clamping assembly for selectively anchoring and releasing said wing relative to the material.
  • 12. A mining machine according to claim 11, wherein said wing clamping assembly includes front and rear clamping cylinders each moving upper and lower clamping plates.
  • 13. A mining machine according to claim 1, wherein said wing has a wing spreader assembly for orienting said wing at selected angles with respect to said mainframe.
  • 14. A mining machine according to claim 13, wherein said wing spreader assembly includes at least one spreader cylinder pivotable about said wing to selected positions to angularly move said wing.
  • 15. A mining machine according to claim 14, wherein one end of said at least one spreader cylinder is affixed to a pivot shaft mounted on said wing and a clamping cylinder selectively anchors said at least one spreader cylinder.
  • 16. A mining machine according to claim 1, further comprising an additional wing paralleling said wing when both are aligned with said mainframe.
  • 17. A mining machine according to claim 16, wherein said additional wing is pivotally connected to said mainframe for orienting said additional wing at an angle to the direction of movement of said mainframe in a direction opposite the orienting of said wing.
  • 18. A mining machine according to claim 16, including means for maintaining said wing and said additional wing equiangularly displaced during retreat cutting.
  • 19. A mining machine according to claim 16, wherein said wing and said additional wing are separately individually positioned and controlled.
  • 20. A mining machine according to claim 1, wherein said cutter assembly includes a drum cutter having a motor mounted therein for rotating said drum cutter.
  • 21. A method of mining minerals located in underground seams comprising the steps of:cutting an entry hole with a cutter assembly mounted on a wing preceding a mainframe assembly, moving said cutter assembly lengthwise of said wing to effect a widening cut of the entry hole in the area adjacent to said wing, spreading said wing angularly into the widening cut effected by said cutter assembly, sequentially repeating the moving of said cutter assembly lengthwise of said wing to effect a further widening cut to the, entry hole and the spreading of said wing angularly into widening cuts until said wing is displaced through a desired angle, instituting retreat motion increments of said mainframe assembly and said wing subsequent to advance cuts by said cutter assembly lengthwise of said wings, whereby a retreat cut of a width exceeding the width of the entry hole is accomplished.
  • 22. A method according to claim 21 further comprising the step of, orienting said cutter assembly in longitudinal alignment with said wing during the effecting of the entry cut hole.
  • 23. A method according to claim 21 further comprising the step of, forming a rectangular entry cut hole by employing a cylindrical cutter rotating on a vertical axis.
  • 24. A method according to claim 21 further comprising the step of, retracting said wing angularly toward alignment with said mainframe assembly prior to completing a retreat cut, whereby the entry area is maintained substantially intact.
  • 25. A method according to claim 21 further comprising the step of, pivoting said cutter assembly out of alignment with said wing preparatory to moving of said cutter assembly lengthwise of said wing.
  • 26. A method according to claim 21, further comprising the step of, employing a pair of wings, each mounting a cutter assembly.
  • 27. A method according to claim 26 further comprising the step of, orienting each of said cutter assemblies in longitudinal alignment with its respective wing during the cutting of the entry hole.
  • 28. A method according to claim 26 further comprising the step of, spreading said wings in opposite angular directions prior to instituting said retreat motion increments.
  • 29. A method according to claim 28 further comprising the step of, leveraging a spreading mechanism of one of said wings against the other of said wings to initiate angular separation between said wings.
  • 30. A method according to claim 26 further comprising the step of, fully spreading said pair of wings prior to instituting said retreat motion increments.
  • 31. A method of mining minerals located in an underground seam comprising the steps of:cutting an entry hole in the underground seam, locating a mining machine having a wing-mounted cutter assembly in the entry hole, moving said cutter assembly lengthwise of said wing to effect a widening cut of the entry hole in the area adjacent to said wing, spreading said wing angularly into the widening cut effected by said cutter assembly, sequentially repeating the moving of said cutter assembly lengthwise of said wing to effect a further widening cut to the entry hole and the spreading of said wing angularly into widening cuts until said wing is displaced through a desired angle, instituting retreat motion increments of said mining machine and said wing subsequent to advance cuts by said cutter assembly lengthwise of said wings, whereby a retreat cut of a width exceeding the width of the entry hole is accomplished.
  • 32. A method of mining minerals from a seam comprising the steps of:advance cutting an entry hole in the seam, positioning a mining machine having a wing mounting a cutter assembly in the entry hole, effecting a widening cut of the entry hole in the area adjacent to the wing by moving the cutter assembly along the wing, angularly displacing the wing into the widening cut of the entry hole, sequentially repeating the effecting of a widening cut and the angularly displacing of the wing into the widening cut until the wing is displaced through a desired angle, incrementally withdrawing the wing into retreat cuts by the cutter assembly along the wing while maintaining the wing at the desired angle, whereby a retreat cut of a width exceeding the width of the entry hole is accomplished.
  • 33. A mining machine for retreat cutting of material located in seams comprising, a movable mainframe, first and second wings carried by said mainframe, cutter assemblies mounted on each of said first and second wings, carriages on each of said first and second wings for selectively moving said cutter assemblies along said first and second wings for cutting of the material in proximity to said first and second wings, and pivotal connectors between said mainframe and said first and second wings for orienting said first and second wings in opposite angular directions relative to the direction of movement of said mainframe.
  • 34. A mining machine for retreat cutting of material located in seams comprising, a movable mainframe, a wing carried by said mainframe, a cutter assembly mounted on said wing for selective movement along said wing for cutting of the material in proximity to the wing, a pivotal connector between said mainframe and said wing permitting the orienting of said wing at an angle to the direction of movement of said mainframe, and a spreader assembly to angularly move said wing relative to said mainframe.
  • 35. A mining machine according to claim 34 further comprising, a clamping mechanism interconnected with said spreader assembly to selectively release and anchor said spreader assembly in the material to incrementally move said wing.
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Entry
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