referring now in detail to the accompanying drawings , exemplary embodiments of the aeration device of the present invention are provided , as well as examples of prior art devices . fig1 a and 1b provide top plan and front elevation views , respectively , of a prior art soil - aerating device 10 . the soil - aerating device 10 comprises a frame 18 from which support members 16 depend , the support members 16 having bearings 14 at their lower ends for communication with four tine gangs or rollers 12 . the tine gangs 12 are provided with a plurality of tine assemblies 13 . due to the bearings 14 and support members 16 at opposite ends of the tine gangs 12 taking up space outboard of the tine assemblies 13 and causing a gap between the aeration paths of adjacent tine gangs 12 , the prior art soil - aerating device 10 employed longitudinal alternate staggering of the tine gangs 12 in order to ensure evenly - spaced rows of aerated soil . such staggering of adjacent tine gangs 12 permitted the bearings 14 and support members 16 to be placed in front of ( or behind , as the case may be ) a portion of an adjacent tine gang 12 , thereby ensuring that the tine assemblies 13 are evenly spaced a distance “ a ”, such that there is no aeration path gap when such a device 10 is towed behind other powered machinery such as a tractor . however , although the staggered tine gang configuration addresses the gap problem , space restrictions may make uniform or symmetrical staggering difficult or impossible to achieve . also , using the device 10 can result in a phenomenon known in the art as “ dog - tracking ”. the result of dog - tracking is that one side of the device cultivates more aggressively than the other , leaving visible stripes in the land . dog - tracking usually occurs at larger swing angles , and the tractor steering can create a yaw moment in keeping the mounted device going straight where the tractor does not have a three - point hitch . where the tractor does not have a three - point hitch , this frequently resulting in patches or areas of soil being poorly aerated , thereby defeating the original purpose of the soil - aerating device 10 . in order to overcome problems of dog - tracking , prior art aeration devices would typically configure tine gangs laterally substantially along a common line , disposed substantially perpendicularly to the direction of travel of the device . fig2 a and 2b show top plan and front elevation views of such a prior art soil - aerating device 20 , having tine gangs 22 arranged substantially symmetrically . the soil - aerating device 20 comprises a frame 28 from which support members 26 depend , the support members 26 having bearings 24 at their lower ends for communication with four tine gangs 22 , the tine gangs 22 being provided with a plurality of tine assemblies 23 . disadvantageously , however , as may be seen from the front elevation view in fig2 b , while the dog tracking problem may have been addressed , a gap is created in the aeration path . due to lateral space taken up by the bearings 24 and support members 26 which support the tine gangs 22 at opposite ends thereof , such a configuration would typically result in distance “ b ” between mutually adjacent tine gangs 22 being greater than distance “ c ” separating each of the tine assemblies 23 on a tine gang 22 . such greater spacing “ b ” accordingly resulted in a wide strip of non - aerated soil ( or at least wider strip than is the case with the spacing “ c ”). in order to be able to produce uniformly - spaced strips of aerated soil without experiencing the problem of dog - tracking , the mayer patent taught a novel device design , as can be seen in fig3 a to 6 . fig3 a and 3b illustrate two embodiments of a soil - aerating device 30 having a frame 31 comprising a front member 32 , side members 34 , 35 , centre members 36 , 37 , and intermediate members 38 , 39 . the frame 31 is provided with a three - point hitch assembly 42 comprising lower couplings 43 , 44 and an upper coupling 45 . tine gangs 46 are provided containing tine assembles 47 . each tine gang 46 is suspended from the frame 31 by pairs of legs 48 . the lower end of legs 48 are connected to each tine gang 46 at a leg bearing 52 inboard of either the first ( in fig3 b ) or second ( in fig3 a ) tine assembly 47 from each end . each tine assembly 47 is spaced from an adjacent tine assembly 47 by an annular spacer 51 and from a leg bearing 52 by a shorter spacer 53 . all tine gangs 46 according to mayer consist of individual sets of tine assemblies 47 integral with a rotating hub 54 . fig4 a is a detailed view , partially in section , of the prior art dual cantilevered tine arrangement shown in fig3 a and described above . the cantilevered dual tine arrangement is mounted on the shaft 58 by means of a nut 60 threaded onto the shaft 58 with a washer 59 . this prior art dual tine arrangement comprises a pair of tine assemblies 47 each comprising a plurality of tines 55 formed from a casting , cast integral with a metallic hub 54 from which three tines 55 extend radially outwardly in an equally - angularly spaced relationship , i . e . at an angle of 120 degrees between adjacent tines 55 . the hub 54 has a central aperture 56 of hexagonal shape ( not shown ) and an annular projection 57 on each side . each tine gang 46 comprises a shaft 58 with a hexagonal section on which the tine assemblies 47 are mounted , with the tine assemblies 47 being keyed to the shaft 58 for rotation therewith . the intermediate tine assembles 47 are spaced from each other by annular spacers 51 which fit at opposite ends over the annular projections 57 of the adjacent tine assembles 47 . a bearing 52 carried by the lower end of the leg 48 is mounted on the shaft 58 . an adjacent tine assembly 47 is spaced from the bearing 52 by shorter - shaped spacers 53 which engage the annular projection 57 of the hub 54 at one end and the bearing 52 at the other end . these components are retained in an assembly on the shaft 58 by washers 59 and nuts 60 on threaded ends of the shaft 58 . fig4 b is a detailed view , partially in section , of the prior art single cantilevered tine assembly embodiment illustrated in fig3 b and discussed above , with a basic structure similar to that discussed above regarding fig4 a . referring now to fig5 and 6 , there is provided a detailed view of an integral tine assembly 47 . fig5 illustrates a detailed side elevation view of an integral tine assembly 47 , while fig6 illustrates a front elevation view . each tine assembly 47 is a metal casting with a hub 54 from which three tines 55 extend in equally - angularly spaced relationship , i . e . at an angle of 120 degrees between adjacent tines 55 . the hub 54 has a central aperture 56 and an annular projection 57 on each side . each tine 55 is in the form of a planar blade extending in a vertical plane from the hub 52 and having a pointed end 61 . a first ground engaging edge 62 extends , when the tine 55 is in a vertical downwardly extending position , in an upwardly and rearwardly inclined direction . a second edge 63 extends from the pointed end 61 to the hub 54 in a vertical direction , and a third edge 64 extends from the end of the first edge 62 . the first edge 62 is bevelled at 65 over the whole of its length , and the second edge 63 is bevelled at 66 over a major part of its length extending from the hub 54 , the bevelling of the first edge 62 being on the opposite side of tine 55 to the bevelling of second edge 63 . each tine 55 has a central longitudinal axis x midway between and parallel to the edges 63 , 64 which extend behind the rotational axis of the shaft 58 ( indicated at r in fig5 ), being spaced therefrom by a distance which in this embodiment is 0 . 625 inches . as shown especially in fig6 , each tine 55 is twisted about its central axis x by 8 degrees from the vertical plane parallel to the direction of travel , the axis x being perpendicular to the longitudinal axis of the shaft 58 . however , as stated above , the mayer device was of integral construction , which proved disadvantageous in some situations . should one of the tines in the integral tine assembly become damaged or irreparably worn , replacement of the whole integral assembly was necessary , an expensive and time - consuming situation , hence the need for the present invention . two embodiments of the present invention are illustrated by means of fig7 a , 7 b , 8 , 9 , 10 , and 11 . according to an aspect of the present invention as embodied in fig7 a and 7b , a soil - aerating device 100 is illustrated comprising a frame 106 for towing behind a vehicle ( not shown ), the frame 106 having legs 115 depending therefrom , the lower ends of the legs 115 being provided with bearing assemblies 116 . the bearing assemblies 116 communicate with a plurality of tine gangs or devices , two in this embodiment , each tine gang comprising outboard tine assemblies 118 having a plurality of tines 120 , four in this embodiment , the tines 120 similar in structure to those disclosed in mayer . referring now particularly to fig8 and 9 , each of the tine gangs or devices comprise a single outboard tine assembly 118 positioned outboard of the bearing assembly 116 , the single outboard tine assembly 118 comprising tines 120 . as can best be seen in fig9 , the gang comprises a hub 102 having an aperture 104 extending therethrough , a rotatable shaft 108 housed within the aperture 104 , and the hub 102 secured to the outboard end 114 of the shaft 108 by means of a bolt 110 engaged within a threaded hole 112 in the outboard end 114 of the shaft 108 , a disc 111 situated between the hub 102 and head of the bolt 110 . to communicate rotational motion of the shaft 108 to the hub 102 , the shaft 108 has a hexagonal cross section , and the aperture 104 is keyed to communicate with that cross section . although a hexagonal arrangement is set out , it will be clear to anyone skilled in the art that other means of communicating the rotation are possible , such as using other polygonal arrangements or a splined engagement . the bearing assembly 116 communicates with the shaft 108 immediately inboard of the hub 102 . the gang further comprises a flange 122 at the extreme outboard end of the gang , the flange 122 mechanically fastened to the tines 120 of the outboard tine assembly 118 and a second flange 124 on the hub 102 by means of a plurality of bolts 126 extending therethrough . the outboard tine assembly 118 , hub 102 , and flange 122 are therefore positioned outboard of the bearing assembly 116 resulting in the outboard tine assembly 118 being cantilevered from the shaft 108 . referring now particularly to fig1 and 11 , a dual outboard tine device is illustrated , although a single outboard tine device is provided on the right - hand side of the gang for ease of comparison . the dual outboard tine device comprises inner and outer hubs 128 , 130 , the inner hub 128 having an aperture 132 extending therethrough , the shaft 108 within the aperture 104 , communication of the shaft 108 rotation to the hub 102 by the same means described above . the inner hub 128 is secured to an outboard end 114 of the shaft 108 in the same fashion as was the case with the single outboard tine device , by means of a bolt 110 threadably engaged in a hole 112 in the shaft 108 , a disc 111 situated between the inner hub 128 and head of the bolt 110 . the bearing assembly 116 communicates with the shaft 108 immediately inboard of the inner hub 128 . in the embodiment of this aspect of the invention , there are two outboard tine assemblies , an inner assembly 134 and an outer assembly 136 , each comprising a plurality of tines 120 . the inner hub 128 is provided with a first flange 138 and the outer hub with a second flange 140 , the two flanges 138 , 140 mechanically fastened together with the tines 120 of the inner outboard tine assembly 134 therebetween , by means of a plurality of bolts 126 . an outer flange 142 , roughly analogous to the flange of the single outboard tine device , is mechanically fastened to an inner flange 144 on the outer hub 130 , the tines 120 of the outer outboard tine assembly 136 therebetween . when fully assembled and secured , the elements shown in fig1 would have the appearance illustrated in fig1 . in the single outboard tine arrangement , there is only one tine assembly 118 cantilevered outboard of the bearing assembly 116 , while in the dual outboard tine arrangement there are two tine assemblies 134 , 136 cantilevered outboard of the bearing assembly 116 . the utility of the present invention becomes clear in the following situation . if an operator ( not shown ) is using the soil - aerating device 100 to aerate a patch of soil , the problem of dog - tracking is addressed by the outboard cantilever feature of the design . also , if one of the tines 120 becomes damaged by striking a rock or other submerged danger , or if a flange 122 cracks due to the stresses placed on the tines 120 , the operator can disassemble the device simply by loosening the various bolts 126 , 110 , replace the damaged tine 120 or flange 122 , and reassemble the device . as can therefore be seen , the present invention provides a gang arrangement on a soil - aerating device that addresses the problem of aeration row gaps , but it also provides an easily disassembled tine assembly structure to enable quick , simple , and inexpensive repairs or replacements when a tine becomes worn or damaged , without requiring the costly replacement of entire integrated assemblies . while particular embodiments of the present invention have been described in the foregoing , it is to be understood that other embodiments are possible within the scope of the invention and are intended to be included herein . it will be clear to any person skilled in the art that modifications of and adjustments to this invention , not shown , are possible without departing from the spirit of the invention as demonstrated through the exemplary embodiments . for example , while there is currently a flange on the hub , one possible modification would be to eliminate the flange altogether by providing a hub of wider diameter and having the bolts fasten directly to the hub . the invention is therefore to be considered limited solely by the scope of the appended claims .
an outboard tine device for soil - aerating equipment is disclosed comprising a hub having an aperture , a rotatable shaft within the aperture and mounted on the soil - aerating equipment , an outboard tine assembly comprising a plurality of outwardly protruding tines , and a securing member adjacent an outboard side of the outboard tine assembly removably securing the outboard tine assembly to the hub , wherein the securing member and hub are respectively positioned on opposing sides of and adjacent to the outboard tine assembly , wherein the outboard tine assembly , hub and securing member are positioned outboard of the mounting assembly resulting in the outboard tine assembly being cantilevered from the shaft . a dual outboard tine device is also disclosed . the outboard tine device is directed to uniform aerating and enabling easier replacement of damaged tines .