Patent Grant
11401676
This application is a National Stage Application of International Application No. PCT/IB2019/054401, filed May 28, 2019, which claims benefit of Ser. No. 102018000005910, filed May 31, 2018 in Italy and which applications are incorporated herein by reference. To the extent appropriate, a claim of priority is made to each of the above-disclosed applications.
The present invention relates to an assembling and moving equipment and a method of using such equipment, for facilitating the assembling of components of a ground drilling machine.
When making foundation and ground-consolidation excavations, self-moving drilling machines are generally used, like the known one shown in
The simplest machines are equipped with a mast moving system that, through at least one hydraulic cylinder connected to both the mast and the base machine, effects a simple rotation of the mast relative to a connection fulcrum between the mast and the base machine, so that the mast can be switched from a horizontal transport configuration to a tilted or vertical working configuration. The distance between the excavation axis (or the axis of rotation of the tool in excavation conditions) and the axis of rotation of the turret is referred to in the industry as “working radius”. In the simplest machines, the variation of the working radius, when present, is effected by a slide that moves the whole mast supporting frame by a few tens of centimetres relative to the turret. More complex machines have a mast moving system that includes an additional hydraulic cylinder, which, by actuating a parallelogram-shaped kinematic mechanism, allows changing the working radius while keeping the mast angle constant. As an alternative, the second actuator may move a kinematic element directly in contact with the mast that is not of the parallelogram type and anyway for its simplicity and versatility allows changing the working radius while requiring a subsequent adjustment of the angle of inclination of the mast or antenna.
In order to prepare the machine for road transport out of the excavation site, it is necessary to lay down the mast into a substantially horizontal position, so that the total height of the machine in the transport configuration is as short as possible and allows complying with the height limits imposed by traffic regulations. In small-sized and medium-sized machines, the mast can be laid down either backwards onto the turret or forwards, in a cantilever fashion, in front of the cabin.
The demand for increasingly higher performance from excavating machines has led to a general increase in the dimensions and weights of big machines. This comes from the need for more powerful on-board components, higher mechanical strength of the structural parts, and increased excavation depths and diameters.
One consequence of such increased dimensions and weights consists of more complex machine transport phases. In fact, in order to be able to comply with the maximum weight limits allowed for road circulation of the vehicles to be used for transporting the excavating machine, it is often necessary to dismount some components from the machines during the transport phases. Likewise, in order to be able to comply with the maximum height limits allowed for road circulation of the vehicles to be used for transporting the excavating machine, it is often necessary to dismount those components which are highest when the machine is in the transport configuration. Excavation accessories and the rotary are often removed, but in the biggest machines it may become necessary to dismount the mast as well, separating it from the associated kinematic system or, more in general, from the base machine.
It follows that such components will then have to be reinstalled after reaching the working site, in order to bring the machine back into excavation operating conditions. Likewise, once on-site work is complete, such components will have to be dismounted again on site before the machine can be transported on the road again.
Mounting and dismounting bulky and heavy components of a machine, such as, for example, the mast, is a complex process that may turn out to be particularly difficult to carry out on site, where it is often the case that one cannot utilize the same equipment and structures that are available at a shop or at the manufacturing plant. As a consequence, assembly operations cannot be carried out on site with the same degree of safety.
In particular, it may turn out to be difficult to mount those components which are to be constrained to other structures of the machine through two distinct connection points providing two fulcrums. For example, the mast is an element that must be constrained to the base machine (or to the kinematic mechanism of the base machine) through a first connection fulcrum and also to the mast rotation actuator (generally a hydraulic cylinder) through a second connection fulcrum. Likewise, the mast rotation actuator must be constrained to the base machine (or to the kinematic mechanism of the base machine) through a first connection fulcrum and also to the mast through a second connection fulcrum. During the assembly process, the first connection fulcrum of the mast is connected to the base machine and, in the same manner, the first connection fulcrum of the mast rotation actuator is connected to the base machine; subsequently, the second connection fulcrum of the mast is connected to the second connection fulcrum of the mast rotation actuator. This second connection between the mast rotation actuator and the mast is particularly difficult because both the mast and the actuator are free to rotate about a fulcrum of their own and must therefore be mutually oriented until the second connection fulcrum of the mast becomes coaxial to the second connection fulcrum of the actuator. This step requires the availability of two distinct hoisting means, e.g. two support cranes, in order to be able to support and move both components independently until correct mutual orientation is achieved.
In the prior art, said assembling phase is usually carried out by following a procedure that will now be described with reference to a known machine 100 illustrated in
The drilling machine 1 further comprises a mast 5 and a kinematic mechanism 2 for moving the mast 5 relative to the turret 3. The kinematic mechanism 2 is connected to the turret 3 on one side and to the mast 5 on the other side. The kinematic mechanism 2, which is of the parallelogram type, moves the mast 5 while allowing adjusting the drilling height relative to the centre plate (also called working radius). The movement of the kinematic mechanism 2 is effected by at least one jack 6 acting upon the arm 7. The arm 7 has a first end hinged to the turret 3 and a second end hinged to a kinematic frame 8, usually referred to as “trapezium” or “trapezoid frame”. The trapezoid frame 8 is also connected to the turret 3 by means of at least one connecting rod 9 having the same length as the arm 7, thus forming an articulated parallelogram.
The trapezoid kinematic frame 8 has, in its front part, a mast connecting fulcrum 8a (shown in detail in
In a known variant, the jack 6 for moving the arm 7, instead of being directly associated with the kinematic frame 8, is associated with the arm 7. In those solutions using a parallelogram-type kinematic mechanism, by actuating the jack 6 acting upon the arm it is possible to cause the mast 5 to translate from a position in which the working radius is minimum to a position in which the working radius is maximum, while keeping the tilting angle thereof constant. At least one mast rotating cylinder 10, which connects the mast 5 to the kinematic frame 8, effects the lifting and lowering of the mast and adjusts the inclination thereof relative to the ground. This movement allows the mast 5 to switch from a substantially horizontal position, or transport position, to a substantially vertical position, or working position.
On the mast 5 there is a rotary 11, equipped with a per se known pull-push system 12. Through the rotary 11 a drilling assembly is arranged, such as a string of telescopic rods or kelly 13. The string of telescopic rods 13 is provided with an excavation tool 14, which may be, for example, a bucket or a helical drill; in particular, the excavation tool 14 is secured to the bottom end of the innermost rod of the string of telescopic rods 13, so as to be able to receive torque and thrust from said rod.
The procedure for mounting the mast on a machine of a known type can be described with reference to
In order to be able to install the mast on the machine in accordance with the prior art, the machine is first arranged with the kinematic mechanism in the lowered position and with the arm 7 only slightly tilted relative to the ground, so that the fulcrum 8a on the trapezium 8, to be connected to the mast, is slightly above the upper structure 3 and the cabin. In this condition, the mast tilting cylinder 10 has one end hinged to the trapezium 8 and is tilted backwards relative to the turret 3, so that the second end of the cylinder 10, to be connected to the mast 5, is above the turret. The cylinder 10, which would otherwise be free to rotate about the first fulcrum, is locked in position by interposing removable mechanical locators between the arm (or another part of the base machine) and the cylinder, or else by fastening it with a sling. Therefore, this step of locking the cylinder 10 requires the presence of personnel near the kinematic mechanism, in a poorly accessible, elevated area, for applying the cylinder locking means. This is therefore a dangerous task, especially when carried out on site.
The mast 5 is slung and hoisted by means of hoisting means, such as a bridge crane or a service crane, and is positioned over the machine. For simplicity,
The mast 5 is then brought close to the kinematic mechanism 2 by moving it through the hoisting means, while the kinematic mechanism is kept in a fixed position. The mast 5 is moved until the fulcrum 5a of the joint of the mast 5 matches the mast connecting fulcrum 8a on the trapezium 8. When the fulcrums 8a and 5a are coaxially aligned, a pin can be inserted in order to couple the two parts together. This step is difficult because the hoisting means, e.g. cranes or bridge cranes, allow for neither high precision nor fine adjustment of movements; therefore, achieving sufficient coaxiality to be able to insert the pin may require many manoeuvres and much time.
Once the connecting pin between the mast 5 and the kinematic support 8 has been inserted, the machine 100 will be in the condition shown in
By using a second hoisting means, distinct from the one(s) used for hoisting the mast 5, the cylinder 10 is moved by changing its angle of inclination and turning it about its first fulcrum, through which it is hinged to the trapezium 8, until the second fulcrum of the cylinder 10 becomes coaxial to the fulcrum 5b of the mast. In addition to changing the angle of inclination of the cylinder 10, it may also be necessary to change the length thereof by hydraulically actuating it in order to move its rod.
Once coaxiality has been obtained between the fulcrum of the cylinder 10 and the fulcrum 5a of the mast, it is possible to insert the pin and connect the two components cinematically to each other. Once connected, the mast can be tilted by actuating the cylinder 10.
It is clear that, during the assembling phase of the machine 100 shown in
Similar problems arise during the phase of dismounting the mast 5, which follows a procedure that is substantially inverse to the above-described installation procedure. The mast 5 is tilted backwards and the kinematic mechanism 2 is lowered to bring the fulcrum 8a just above the turret 3. After slinging the mast 5, this is supported by means of a first hoisting means, such as a crane or a bridge crane, whereto the slings are hooked. At this point, it is necessary to first remove the pin that connects the cylinder 10 to the fulcrum 5b of the mast. In order to carry out this step, it is also necessary to support the cylinder 10 with a second hoisting means, so as to prevent said cylinder, following the extraction of the connecting pin, from falling under its own weight, turning about the remaining fulcrum connecting it to the trapezium. This rotation might be particularly dangerous because of the weight of the cylinder, which might hit other components of the machine, thus damaging them, and also because during the pin removal operations some personnel may be present in the vicinity. Subsequently, while still supporting the mast 5 with a hoisting means, the connecting pin between the fulcrum 8a of the kinematic support 8 and the fulcrum 5b of the mast 5 must be extracted. The extraction of this pin may turn out to be problematical as well in that, once the cylinder 10 has been released from the mast 5, part of the mast's weight will be borne by the connection between the fulcrum 8a of the trapezium 8 and the fulcrum 5a of the mast. This weight portion, although much less than the entire mast's weight, since the mast 5 is supported by the hoisting means, is however sufficient to considerably increase the friction of the connecting pin at the fulcrums 8a and 5a. This results in greater difficulty in extracting the pin and consequent longer disassembly times.
The simultaneous use of two distinct hoisting means for moving the mast 5 and the cylinder 10 while assembling the excavating machine 100, wherein each one of the two hoisting means is connected to the mast or to the cylinder through flexible connecting means, such as chains or slings, turns out to be very complex and problematical. In fact, the slings of one of the two hoisting means may interfere with the slings of the other means or with one of the two components to be assembled together.
It is one object of the present invention to overcome the above-mentioned drawbacks, and particularly to provide an equipment and a method for assembling components of a drilling machine, which can reduce the risks deriving from movements of hinged or constrained components, e.g. hydraulic cylinders, and assembly times, in a simple and easy way for the operator.
This and other objects of the present invention are achieved through a drilling machine, a method of assembling the drilling machine, and an assembling and moving equipment as set out in the independent claims.
Further optional features of the assembling and moving equipment, machine and method are set out in dependent claims. The annexed claims are an integral part of the technical teachings of the present description.
The features and advantages of the present invention will become more apparent from the following non-limiting description provided by way of example with reference to the annexed schematic drawings, wherein:
Those parts or elements which are similar to, or perform the same function as, those of the known drilling machine designated as 100 and previously described with reference to
The following will briefly describe the drilling machine 1 shown in the drawings by way of non-limiting example. The drilling machine 1, which is conveniently equal to the prior-art one shown in
The kinematic mechanism 2 is connected on one side to the main body (e.g. to the turret 3) and on the other side to the mast 5. The kinematic mechanism 2 comprises an arm 7 having a first end hinged to the main body and a second end hinged to a kinematic frame 8. The kinematic frame 8 is further connected to the main body (e.g. to the turret 3) through at least one connecting rod 9, thus forming an articulated parallelogram. A linear actuator 6, e.g. a jack, is mounted to the main body and to the kinematic frame 8 for moving the kinematic frame 8.
The kinematic frame 8 has, in its front part, a connecting joint 8a configured to be coupled to a corresponding joint 5a on the mast through a pin-type connection. This connection allows the mast 5 to rotate forwards about the fulcrum 8a of the kinematic frame 8, and possibly also to make small lateral rotations, when the joint 5a is a cardan joint.
In one possible variant, instead of being directly hinged to the kinematic frame 8, the linear actuator 6 is hinged to the arm 7. The actuation of the linear actuator 6 allows the mast 5 to be translated from a position having the minimum working radius to a position having the maximum working radius, while keeping the angle of inclination thereof constant.
There is at least one first linear actuator (in particular having a cylinder 10), which connects the mast 5 to the kinematic frame 8, for adjusting the inclination of the mast 5 relative to the kinematic frame 8, and hence relative to the ground. This movement allows the mast 5 to switch from a substantially horizontal position, or transport position, to a substantially vertical position, or working position. The mast 5 is therefore hinged at two points, or fulcrums: one connecting it to the kinematic frame 8 and one connecting it to one end of the first linear actuator. The first linear actuator will hereafter also be referred to as “cylinder 10”, without however limiting the scope of the invention. Unlike the machine 100 previously described, the machine 1 is fitted with an assembling and moving equipment 20a, 20b, wherein such equipment is implemented in accordance with one exemplary embodiment of the present invention.
The drilling machine 1 of the present invention comprises:
a main body,
a mast 5, whereon a drilling tool 14 is to be mounted,
a kinematic mechanism 2 configured for movably constraining the mast 5 to the main body while allowing mutual rotation thereof, wherein the kinematic mechanism 2 includes at least one elongated component configured for being hinged at its two ends,
an assembling and moving equipment 20a, 20b, comprising:
The assembling and moving equipment 20a, 20b is configured in a manner such that, when the drilling machine 1 is in an assembling configuration, in which one end of the elongated component is released and the moving element is acting upon the elongated component, the movement of the moving element relative to the portion of the drilling machine 1 to which it is mounted will cause a rotation of the elongated component.
In particular, the elongated component is a first linear actuator with a rod and a cylinder 10. The first linear actuator has, in the variant shown herein, one end hinged to the mast 5.
The elongated component is meant to be an element that, when the drilling machine 1 is in an operating condition (i.e. when the kinematic mechanism 2 has been installed and is supporting the mast 5), is hinged at both of its own ends. The elongated component may also be a connecting rod, e.g. like those designated as 7, 9. The elongated element is configured for transmitting an axial force passing through its two hinging points.
Conveniently, the moving element includes a freely rotatable support roller 24 adapted to rest on the elongated component, in particular on the first linear actuator (preferably on the cylinder 10) in order to allow the elongated component to slide on the support roller 24.
In the preferred example shown herein, the machine comprises a support base 21 adapted to be removably fixed to a portion of the drilling machine 1. The moving element is mounted movably relative to the support base 21, and the moving actuator 22 is adapted to control the relative position between the moving element and the support base 21. In particular, the support base 21 is mounted to the kinematic mechanism 2, conveniently to the arm 7.
Preferably, the moving element comprises a moving arm 23a, 23b hinged to the portion of the drilling machine 1, and the moving actuator 22 is adapted to control the relative angular position between the moving arm 23a, 23b and the portion of the drilling machine 1 to which the moving arm 23a, 23b is hinged.
In particular, the moving element is a moving arm 23a, 23b hinged to the support base 21. The rotation of the moving arm 23a, 23b relative to the support base 21 can cause a rotation of the elongated component. The moving actuator 22 is adapted to control the relative angular position between the support base 21 and the moving arm 23a, 23b.
Preferably, the moving actuator 22 is a linear actuator hinged to the support base 21 and to the moving arm 23a, 23b, and conveniently comprises a cylinder and a rod; for example, the moving actuator 22 is a hydraulic or pneumatic cylinder. In the example, the main body includes the turret 3, which is preferably rotatable. The moving arm 23a, 23b has the merit of being compact, especially when it is in the lowered or idle position, in which position it does not act upon the cylinder 10.
In accordance with one possible variant, the moving element can slide linearly relative to the support base 21, being for example a fork conveniently including the support roller 24. In accordance with a further variant, the moving element is a kinematic mechanism, e.g. a compound lever, or a parallelogram-type jack (e.g. similar to a car jack), or a pantograph actuator.
In accordance with one possible variant of the invention, the support base 21 is absent and the moving element is constrained movably, e.g. by means of a hinge, to a portion of the drilling machine 1, such as an element of the kinematic mechanism 2, e.g. the arm 7. For example, two hinge-type connections 21a, 21b are integral with (e.g. welded to) a portion of the machine (e.g. the arm 7), to which the moving actuator 2 and the moving arm 23a, 23b are pivoted.
In the present embodiment, the moving element (e.g. the moving arm 23a) acts upon only one respective elongated element (e.g. cylinder 10). In accordance with one possible variant of the invention, the moving element acts upon a plurality of elongated elements; for example, a single moving arm 23a acts upon two cylinders 10. In accordance with a further possible variant of the invention, a plurality of moving arms act upon only one respective elongated element; for example, two moving arms 23a act upon one cylinder 10. The drilling machine shown herein by way of example has a plurality of, in particular two, assembling and moving equipment 20a, 20b; it is however possible to employ a single assembling and moving equipment.
Preferably, the moving element is adapted to take an idle condition in which it does not act upon the elongated component, and an operating condition in which it acts upon the elongated component. In the idle condition, the moving element is spaced apart from the elongated component; in the operating condition, the moving element rests on the elongated component. When the elongated component (e.g. the actuator with the cylinder 10) is hinged at its two ends, the moving element will be in the idle condition, thus not interfering with the hinged element; when the elongated component is not constrained at one end, the moving element will be in the operating condition for moving or supporting said elongated component.
The assembly comprising the support base 21, the actuator 22 and the moving arm 23a, once such components have been constrained to each other, forms a simple kinematic mechanism. The actuation of the moving actuator 22 causes a rotary movement of the moving arm 23a and support roller 24 relative to the hinge of the hinging joint 21b. This movement results in the roller 24 moving away from or closer to the support base 21, in particular in a direction that is substantially perpendicular to the base plate, and therefore substantially perpendicular to the fixing surface. Advantageously, the moving actuator 22 allows for slow and accurate movements of the moving arm 23a, e.g. through the use of a limited oil flow, in case of a hydraulic actuator, or through an accurate voltage or current adjustment, in case of an electric actuator. The assembling and moving equipment 20a, 20b can thus be used, when assembling and fitting the drilling machine 1, for moving parts of the machine itself, particularly structures equipped with two hinges, which are first constrained to the machine 1 through a first hinge and then need to be oriented with high precision to make it possible to constrain also the second hinge to the machine 1. In particular, the equipment must be secured to the machine in a position between a fixed component of the machine 1 and that part of the machine which needs to be moved for the assembling operation (in the example, the cylinder 10 of the first linear actuator).
The part of the machine 1 that needs to be moved, after having been constrained at a first fulcrum, is made to rest on the support roller 24 and the moving actuator 22 is operated in order to move the moving arm 23a until the correct orientation of the part to be moved is obtained, which allows constraining also the second hinge of said moved part. The support roller 24 preferably has a self-centring shape adapted for housing the component to be moved and suitable for preventing or limiting any undesired lateral movements of such component. For example, in a first embodiment shown in
The use of the assembling and moving equipment 20a, 20b turns out to be particularly advantageous, for example, during the steps of assembling a drilling machine 1 in order to simplify and speed up the steps of connecting the cylinders 10 for rotating the mast 5 to the mast 5 itself. Since the kinematic mechanism of the drilling machine 1 very often includes a pair of cylinders 10 arranged side by side and protruding outwards from the opposed sides of the arm 7, it is conceivable to mount on the arm 7 a pair of assembling and moving equipments 20a, 20b as shown in
An advantageous installation position for the equipments 20a, 20b on the drilling machine 1 and a way of using them can be better described with reference to
In the configuration of
In
For increased safety during the road transport phase, a retaining tool (30) may optionally also be installed on the machine 1, to be preferably constrained to the assembling and moving equipments 20a and 20b, configured for holding the elongated component, in particular the first linear actuator, in particular the cylinder 10, in the lowered or transport position. The retaining tool 30 shown in the drawing is removably fixed to the moving arm 23a or 23b of each equipment 20a or 20b. If there are two or more cylinders 10, it is advantageous to employ a single retaining tool 30 to be constrained to both equipments 20a and 20b, as shown in
The mast 5 is transported in proximity to the machine 1 and slung by means of straps or chains connected to removable hoisting fittings provided on both sides of the mast 5. The mast 5 is hoisted by using a hoisting means such as a crane or a bridge crane. For simplicity and clarity, only the hook of such hoisting means is shown.
The mast 5 is moved over the turret 3, so that the joint 5a of the mast 5 is close to the fulcrum 8a of the kinematic support 8 and the joint 5b of the mast is close to the free hinge of the rod of the cylinder 10.
The mast 5 is then moved by using an auxiliary hoisting means, such as crane, until the joint 5a of the mast 5 and the joint 8a of the kinematic frame 8 are coaxial, thus reaching the condition shown in
Subsequently, the equipments 20a and 20b are moved in order to change the angle of inclination of the cylinders 10 until the free end of the cylinder 10, in particular of the rod of the cylinder 10, becomes coaxial to the joint 5b of the mast 5, as shown in
Advantageously, when moving the cylinders 10 in order to switch from the condition of
In a preferred construction variant, the machine 1 may comprise a centring support or device 40, e.g. installed on the mast 5 in proximity to the joint 5a connecting it to the trapezium 8, as visible in
By screwing or unscrewing the screws 43 it is possible to adjust the length of the screw 43 section that protrudes underneath the adjustment body 42. When the joint 5a of the mast 5 is brought closer to the joint 8a of the trapezium 8, the adjustment screws 43 can be made to abut on the body of the trapezium 8 that surrounds the respective joint 8a. This may facilitate centring the joint 5a with the joint 8a by adjusting the length of the screws 43. Once the adjustment screws 43 have come in abutment with the body that surrounds the joint 8a, by screwing in the screw 43 a thrust will be generated between the mast 8 and the trapezium 8, which will cause a small displacement of the mast 5, since it 5 has not been constrained yet. Due to the fact that the adjustment screws 43 are oriented in different directions, by screwing or unscrewing them it is possible to obtain very precise movements of the mast 5 in two directions in a plane perpendicular to the axis of the joint 5a, 8a. Through such adjustments one can achieve an accurate coaxial alignment between the joint 5a and the joint 8a, thereby facilitating the insertion of the connecting pin through the mast 5 and the trapezium 8. When the screws 43 are in the correct position to ensure a perfect alignment, they can be locked by means of a locknut. In this manner, during the next assembly operations it will no longer be necessary to repeat the adjustment, since it will suffice to rest the adjustment screws 43 on the semi-circular body of the trapezium 8 in proximity to the joint 8a to immediately obtain the coaxial alignment between the joint 5a of the mast 5 and the joint 8a of the trapezium 8.
The use of the centring support 40 turns out to be advantageous also during the phase of dismounting the mast 5, when switching from the condition of
It is to be understood that the use of the assembling and moving equipments 20a, 20b has been explained in detail herein with reference to the process of mounting and connecting the cylinders 10 for rotating the mast 5, but this does not prevent using such equipments for precisely moving any other component of the machine that needs to be constrained through two hinges located at its ends. It is therefore possible to constrain a first hinge and then use the assembling and moving equipment 20a, 20b to facilitate the assembling of a second hinge. For example, instead of the cylinder 10, the elongated component acted upon by the assembling and moving equipment 20a, 20b may be a connecting rod of the kinematic mechanism 2 or a further linear actuator hinged at its ends.
The invention also concerns a method for assembling a drilling machine 1. Starting from a condition wherein a structural element of the drilling machine 1 is released from the rest of the drilling machine 1, and wherein one end of the elongated component is released (
bringing the structural element in proximity to an area of the drilling machine 1 where it has to be mounted,
hinging the structural element to a part of the kinematic mechanism 2 at a first fulcrum,
operating the assembling and moving equipment 20a, 20b so as to rotate the elongated component,
hinging the free end of the elongated component to the structural element at a second fulcrum.
Conveniently, the structural element to be mounted is the mast 5. For example, the first fulcrum is defined by the connection of the joints 5a, 8a, and the second fulcrum is defined by the connection of the joint 5b with the end joint (in the example, a hole) of the cylinder actuator 10. In fact, the mast 5 is hinged to the kinematic mechanism 2 at two points or fulcrums.
With reference to the example, the elongated component is the first linear actuator with a rod and a cylinder 10, and there is a step of operating the first linear actuator in order to move the free end thereof (e.g. the left end of the cylinder actuator 10 in
Further optional steps of the assembling procedure may include, for example:
removing the retaining tool 30, if present, or
hinging the structural element to be mounted, e.g. the mast 5, through the use of the centring support 40.
For completeness' sake, and without any limitation, a particular procedure for assembling the mast 5 and the cylinders 10 through the use of the assembling and moving equipments 20a, 20b, starting from the transport condition of
The invention also comprises a method for disassembling the drilling machine 1, wherein the same steps as previously described are substantially carried out in reverse order. Merely by way of example, the particular procedure for dismounting the mast 5 and disconnecting the mast rotation cylinders 10 through the use of the assembling and moving equipments 20, starting from the working condition and arriving at the transport condition of
The invention also relates to a kit comprising the assembling and moving equipment 20a and 20b, and optionally also the centring support 40. Such kit can be easily mounted to and dismounted from a drilling machine 1 and ensures quick and safe installation of the components thereof, such as the mast 5. The use of the kit is advantageous for assembling or disassembling the drilling machine 1.
The present invention offers numerous advantages. Thanks to their elongated and slim shape, the assembling and moving equipments 20a and 20b can be left installed on the machine also when the machine is in operation. In fact, if the equipments 20a and 20b are kept in the fully lowered position, with the actuator 22 completely extended, they will never interfere with any other movable parts of the kinematic mechanism 2 or of the machine 1. This provides additional time savings when mounting or dismounting the mast because it will not be necessary to install and remove the equipments 20a, 20b each time. The equipments can nevertheless be dismounted at any time by simply removing the connection between the support base 21 and the arm.
The assembling and moving equipments 20a, 20b allow for precise and easily adjustable movements of the cylinders 10 both during the phase of mounting the mast 5 on the kinematic mechanism 2 and during the phase of dismounting and separating the mast from the kinematic mechanism. In particular, they avoid the need for simultaneously using several hoisting means for moving the mast and the cylinders at the same time. According to the present invention, the cylinders 10 are raised and oriented by means of said equipments.
The assembling and moving equipments 20a, 20b can advantageously be left installed on the machine even during the working phases, since they will not interfere with the movements of the parts of the kinematic mechanism or of the machine 1.
Of course, without prejudice to the principle of the invention, the forms of embodiment and the implementation details may be extensively varied from those described and illustrated herein by way of non-limiting example, without however departing from the scope of the invention as set out in the appended claims.
| Number | Date | Country | Kind |
|---|---|---|---|
| 102018000005910 | May 2018 | IT | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/IB2019/054401 | 5/28/2019 | WO | 00 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2019/229645 | 12/5/2019 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 3645343 | Mays | Feb 1972 | A |
| 3664436 | Beagan, Jr. | May 1972 | A |
| 20100319222 | Lanzl | Dec 2010 | A1 |
| Number | Date | Country |
|---|---|---|
| 1983147 | Oct 2008 | EP |
| 2459837 | Jan 2014 | EP |
| Entry |
|---|
| International Search Report and Written Opinion for PCT/IB2019/054401, dated Sep. 20, 2019. |
| Number | Date | Country | |
|---|---|---|---|
| 20210214910 A1 | Jul 2021 | US |
