CN112372155A - Method for cutting I-steel and component - Google Patents
Method for cutting I-steel and component Download PDFInfo
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- CN112372155A CN112372155A CN202011215413.3A CN202011215413A CN112372155A CN 112372155 A CN112372155 A CN 112372155A CN 202011215413 A CN202011215413 A CN 202011215413A CN 112372155 A CN112372155 A CN 112372155A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/36—Removing material
- B23K26/38—Removing material by boring or cutting
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Abstract
The invention provides a method and a component for cutting I-steel, wherein the method for cutting the I-steel comprises the following steps: cutting off a protrusion part of a wing plate protruding from the surface of the web plate aiming at the first steel section; and cutting a target edge at the edge of the first steel section, and obtaining the target member, wherein the shape of the target edge is matched with the shape of a second I-shaped steel spliced by the target member.
Description
Technical Field
The invention relates to the field of cutting, in particular to a method and a component for cutting I-shaped steel.
Background
An i-beam, which is understood to be a steel material with an i-shaped cross section, may generally include a web and wing plates connected to both ends of the web, wherein the thickness of the wing plates is uniform in some i-beams, and the thickness of the wing plates is non-uniform in other i-beams, and the joint of the web and the wing plates may have a certain chamfer angle.
The I-steel can be cut into specific components, and the specific components can be spliced (or called spliced) with another I-steel in a T shape and welded together after being spliced (or called spliced). When the special component is formed by cutting, the chamfer at the connection part of the I-shaped steel web plate and the wing plate needs to be cut. In the prior art, a cutting head (e.g., a laser cutting head) is inserted between the wing plates, and then the i-beam is rotated, and the cutting head remains stationary during rotation, and then the cutting head can cut along the chamfer.
However, when the i-steel is rotated, the cutting head may touch the i-steel, thereby limiting the rotatable angle range of the i-steel, and correspondingly, for at least some types of i-steel (e.g. wide flange i-steel), the cutting head cannot effectively cut the chamfered portion, and thus cannot cut the above specific components.
Disclosure of Invention
The invention provides a method and a component for cutting I-steel, which aim to solve the problem that a cutting head cannot effectively cut a chamfer part.
According to a first aspect of the present invention, there is provided a method of cutting an i-steel for cutting a first i-steel into a target member having a tongue plate, the first i-steel including an i-shaped first steel segment for cutting to form the tongue plate;
the cutting method comprises the following steps:
cutting off a protrusion part of a wing plate protruding from the surface of the web plate aiming at the first steel section;
and cutting a target edge at the edge of the first steel section, and obtaining the target member, wherein the shape of the target edge is matched with the shape of a second I-shaped steel spliced by the target member.
Optionally, for the first steel segment, cutting off a protrusion part of the wing plate protruding from the surface of the web plate, including:
cutting a pair of L-shaped cutting paths in each wing of the first steel segment and cutting the projections based on the L-shaped cutting paths.
Optionally, cutting a pair of L-shaped cutting knife paths on each wing plate of the first steel segment, and cutting off the protrusion based on the L-shaped cutting knife paths, includes:
when a single L-shaped cutting knife path is cut, the outer side of the corresponding wing plate is controlled to face the cutting head; and controlling the cutting head to translate and cut the L-shaped cutting tool path from the outer side of the corresponding wing plate.
Optionally, the L-shaped cutting tool path includes a horizontal line tool path and a vertical line tool path that are vertically connected, and the vertical line tool path is parallel to the web of the first i-beam.
Optionally, the first i-beam further comprises an i-shaped second steel segment, and one end of the first steel segment, which is far away from the target edge, is connected with the second steel segment;
cutting a target edge in the edge of the first steel segment, comprising:
controlling one side of the web plate of the first I-shaped steel to face a cutting head;
controlling the cutting head to translate and cut the edge of the first steel segment from one side of the web to cut and demarcate a portion to be cut corresponding to the target edge, wherein the portion to be cut remains connected with only the second steel segment after the portion to be cut is cut and demarcated;
controlling the outer side of a wing plate of the first I-shaped steel to face the cutting head;
and controlling the cutting head to translate and cut the joint of the first steel section and the second steel section from the outer side of a wing plate so as to cut off the part to be cut and the second steel section.
Optionally, the first i-beam further comprises an i-shaped second steel segment, and one end of the first steel segment, which is far away from the target edge, is connected with the second steel segment;
a groove edge is provided in the target edge adjacent to the second steel segment.
Optionally, the target edge includes a web abutting edge, two chamfer abutting edges, and two flange abutting edges, the number of the groove edges is two, the shape of the chamfer abutting edge matches a chamfer at a joint of a flange and a web in the second i-steel, the shape of the flange abutting edge matches the shape of the inner surface of the flange in the second i-steel, and the shape of the web abutting edge matches the shape of the surface of the web in the second i-steel;
one groove edge, one wing plate butt joint edge, one chamfer butt joint edge, the web plate butt joint edge, the other chamfer butt joint edge, the other wing plate butt joint edge and the other groove edge are connected in sequence.
Optionally, the recessed depth of the edge of the groove is matched with the thickness of the wing plate in the first i-steel and the chamfer angle of the wing plate and the web plate, and the opening width of the edge of the groove is larger than the radius of the tail end of the cutting head.
Optionally, the first i-beam and/or the second i-beam are/is a wide-flange i-beam.
According to a second aspect of the present invention, there is provided a member cut by the method of cutting an i-beam according to the first aspect and its alternatives.
In the method and the component for cutting the I-beam, the problem that the target component cannot be directly cut from the chamfer angle of the wide-flange I-beam when the method for cutting the I-beam in the prior art is used for processing the wide-flange I-beam is particularly solved, wherein a scheme that the protruding part in the first steel section is cut off first and then the target edge is cut from the edge of the first steel section with the protruding part cut off is provided. In a further scheme, the edge of the target is additionally provided with the groove edge, so that the cut target edge is completely attached to the second I-steel, and the cutting head is prevented from colliding with an I-steel wing plate when cutting on the web plate plane.
Meanwhile, no matter how the angle of the second I-steel chamfer is changed (the angles of different types of I-steel chamfers may be different), the method disclosed by the invention is applicable to all kinds of I-steel chamfers and has better universality (for example, the method is applicable to splicing common light I-steel and wide-flange I-steel).
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
FIG. 1a is a first schematic diagram of splicing a member and an I-shaped steel;
FIG. 1b is a schematic diagram of splicing a member and an I-shaped steel;
FIG. 2 is a first schematic flow chart illustrating a method for cutting I-steel according to an embodiment of the present invention;
FIG. 3 is a schematic view of a target member cut to form in accordance with an embodiment of the present invention;
FIG. 4 is a schematic view of a cut-away tab in one embodiment of the present invention;
FIG. 5 is a structural schematic view of the first and second steel segments after the protrusions have been cut away in one embodiment of the invention;
FIG. 6 is a flowchart illustrating step S2 according to an embodiment of the present invention;
FIG. 7 is a first schematic view of an embodiment of the present invention for cutting and defining a portion to be cut;
FIG. 8 is a second schematic view of an embodiment of the present invention for cutting and defining a portion to be cut;
FIG. 9 is a third schematic view of an embodiment of the present invention cutting and demarcating a portion to be cut;
FIG. 10 is a schematic view of an embodiment of the present invention with portions to be cut away;
FIG. 11 is a schematic view of the configuration of the target edge in one embodiment of the present invention;
FIG. 12 is a first schematic view of a first embodiment of the present invention illustrating the cutting of an I-beam;
FIG. 13 is a second schematic view of a second embodiment of the present invention illustrating the cutting of an I-beam;
FIG. 14 is a flowchart illustrating step S3 according to an embodiment of the present invention;
FIG. 15 is a flowchart illustrating steps S32 and S33 according to an embodiment of the present invention;
FIG. 16 is a schematic diagram of the calculation of the offset in one embodiment of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The terms "first," "second," "third," "fourth," and the like in the description and in the claims, as well as in the drawings, if any, are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used is interchangeable under appropriate circumstances such that the embodiments of the invention described herein are capable of operation in sequences other than those illustrated or described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
The technical solution of the present invention will be described in detail below with specific examples. These particular embodiments may be combined with each other below, and details of the same or similar concepts or processes may not be repeated in some embodiments.
Referring to fig. 1a and 1b, the relationship between the target member 1 and the second i-beam 2 can be understood as follows: the tongue plate 11 of the target member 1 can be spliced (or called as inserted) between the two wing plates of the second i-beam 2, and after splicing, the tongue plate of the target member can be butted against the inner surfaces of the two wing plates of the second i-beam 2 and the surface of the web plate, and further can be butted against a chamfer angle between the wing plates and the web plate. Meanwhile, the non-tongue plate part of the target member 1 can be understood as a base body 12, the base body 12 can be in an i shape, and when the target member 1 is spliced with the second i-shaped steel 2, the base body 12 can abut against the end face, far away from the web, of the second i-shaped steel 2, and part of the base body can be arranged in a scheme, or can not abut against the end face.
Furthermore, the target member 1 and the second I-shaped steel 2 can be spliced in a T-shaped splicing mode. Meanwhile, the target member 1 may be cut for the first i-beam 3.
Referring to fig. 1b, there is illustrated a lightweight i-beam (also known as an H-beam) in which the inner surfaces of the flanges are generally not tapered, also known as the perpendicular relationship between the inner surfaces of the flanges (except for the chamfered portions) and the web surface. In contrast, referring to fig. 1a, a wide flange i-beam is illustrated, in which the inner surfaces of the flanges are generally tapered, which can also be understood as: the thickness of the wing plate varies, for example: along the direction of keeping away from the web, thickness diminishes from great.
The method for cutting an i-beam according to an embodiment of the present invention may be applied to cut the above-mentioned target member in an i-beam (i.e. a first i-beam), which may be, for example, the target member 1 shown in fig. 3, where, taking fig. 3 as an example, a portion on the left side of a dotted line is a specific example of the tongue plate 11, and a portion on the right side of the dotted line is a specific example of the i-shaped base 12. Meanwhile, the first I-beam and/or the second I-beam are wide-flange I-beams. For example, the non-WIDE I-beam can be cut into a target member for splicing the non-WIDE I-beam and can also be cut into a target member for splicing the WIDE I-beam; the wide-flange I-steel can be cut into target components for splicing non-wide-flange I-steel and can also be cut into target components for splicing wide-flange I-steel.
Corresponding to the tongue portion 11 and the base 12, the first i-beam 3 may include a first i-beam section 31 and a second i-beam section 32, the first section 31 is a section currently used for cutting the tongue portion 11, the second section 32 is a section currently used for forming the base, and the first section 31 is connected with the second section 32 (for example, an end of the first section away from the target edge is connected with the second section). In a specific example, the length of the first i-beam may be suitable for cutting out only one target member, or may be suitable for cutting out a plurality of target members.
At the same time, the tongue plate 11 shown in fig. 3, 4, 7, 10 can also be understood as a first steel section 31 of the first i-beam 3 during cutting, and the base body 12 shown in an i-shape can also be understood as a second steel section 32 of the first i-beam 3. Meanwhile, in fig. 4, 7, 10, 12 and 13, the cutting path during cutting is also represented by a thick line.
Referring to fig. 2, the method for cutting the i-beam includes:
s1: cutting off a protrusion part of a wing plate protruding from the surface of the web plate aiming at the first steel section;
s2: cutting a target edge on the edge of the first steel section, and obtaining the target component, wherein the shape of the target edge is matched with that of the second I-shaped steel, and the target component comprises the first steel section and the second steel section after cutting.
Referring to fig. 5, after step S1 is performed, the first section 31 of the first i-beam 3 is flat after the protrusions are cut, and the second section 32 is unchanged. Fig. 5 shows a first steel segment 31 and a second steel segment 32, and during the actual cutting process, the end of the first steel segment 31 far away from the second steel segment 32 and the end of the second steel segment 32 far away from the first steel segment 31 may be connected to other steel segments.
After step S1 is performed, the object to be cut is the first steel segment 31 (as shown in fig. 5) with the protruding portion cut off, and when the first steel segment is cut, the first i-section steel 3 is not required to be cut while rotating.
Therefore, the embodiment of the invention abandons the cutting method which needs to cut along the chamfer angle in the prior art, and the scheme of the embodiment of the invention is applied to the processing of the wide-flange I-steel, and particularly can solve the problem that the wide-flange I-steel cannot directly cut the target component from the chamfer angle.
Meanwhile, the method of the embodiment of the present invention is applicable regardless of the angle change at the chamfer of the second i-steel (the angle at the chamfer of different types of i-steel may be different), and has better universality, for example, it is applicable to common light i-steel (i.e. the second i-steel 2 shown in fig. 1 b) and also applicable to wide-flange i-steel (i.e. the second i-steel 2 shown in fig. 1 a).
In one embodiment, referring to fig. 4, step S1 may include: a pair of L-shaped cutting paths 41 is cut at each wing of the first steel segment and the projections are cut based on the L-shaped cutting paths.
The two L-shaped cutting blade paths 41 of the same pair may be symmetrical with respect to the web of the first i-beam, each L-shaped cutting blade path 41 may be the same, and the distance between the two L-shaped cutting blade paths 41 of the same pair may be the same as the thickness of the web of the first i-beam, and further, the protruding portions protruding from the surface of the web may be all cut off.
The L-shaped cutting tool path can comprise a transverse line tool path and a vertical line tool path which are vertically connected, the vertical line tool path is perpendicular to the web plate of the first I-shaped steel, and the transverse line tool path can be perpendicular to (or not perpendicular to) the web plate of the first I-shaped steel and is positioned at the connecting part of the first steel section and the second steel section.
In some embodiments, if the end of the first steel segment away from the second steel segment is not connected to another steel segment, the protrusion may be cut off after the L-shaped cutting blade path 41 is cut, and in other embodiments, if the end of the first steel segment away from the second steel segment is connected to another steel segment (for example, the end of the wing plate of the first steel segment away from the second steel segment is connected to the wing plate of another steel segment), an Contraband-shaped blade path may be further cut on the basis of the L-shaped cutting blade path 41, and the protrusion may be cut off by using the Contraband-shaped blade path.
In a specific implementation process, when a single L-shaped cutting knife path is cut, the outer surface of the corresponding wing plate is controlled to face the cutting head 5, and the cutting can be realized by controlling the rotation of the first I-shaped steel 3; after rotation, the cutting head 5 can be controlled to translate and cut the L-shaped cutting path from the outer side of the corresponding wing plate.
In one embodiment, referring to fig. 6, step S2 may include:
s21: controlling one side of the web plate of the first I-shaped steel to face a cutting head;
s22: controlling the cutting head to translate and cut the edge of the first steel segment from one side of the web to cut and demarcate a portion to be cut corresponding to the target edge, wherein the portion to be cut remains connected with only the second steel segment after the portion to be cut is cut and demarcated;
s23: controlling the outer surface of a wing plate of the first I-steel to face the cutting head;
s24: and controlling the cutting head to translate and cut the joint of the first steel section and the second steel section from the outer side of a wing plate so as to cut off the part to be cut and the second steel section.
Referring to fig. 7, in step S21, the web of the first i-beam 3 may be turned towards the cutting head 5 by rotating the first i-beam 3, and then, in step S22, the edge of the first steel segment may be cut, and the corresponding cutting path may be, for example, the cutting path 42 shown in fig. 7, 8 and 9, and the shape of the cutting path 42 is the same as the shape of the target edge. In the actual cutting process, the portion outside the cutting blade path can be understood as the portion to be cut off by the cutting in step S22, and the portion to be cut does not directly fall off after step S22, but remains connected to the second steel segment 32.
Further, the portion to be cut off and the second steel segment 32 need to be cut off in step S24. To accomplish the cutting, referring to fig. 10, in step S23, the first i-beam is rotated to make one wing plate face the cutting head 5, and then the cutting blade path 43 is cut, and then the other wing plate face the cutting head 5, and then the cutting blade path 43 is cut.
Wherein, the portion to be cut off corresponding to the target edge can be understood as: after cutting the portion to be cut, a target edge may be formed.
A cutting head according to embodiments of the present invention may be referred to as a laser cutting head, although other cutting head arrangements are not excluded. Meanwhile, the "facing the cutting head 5" mentioned in the embodiment of the present invention may be the facing cutting head 5 (correspondingly, the cutting head 5 may cut vertically), or may be the non-facing.
In one embodiment, referring to fig. 11, a groove edge 111 is disposed in the target edge 110 and is adjacent to the second steel segment 32, and by disposing the groove edge 111, it is possible to: when the cutting in step S22 is performed, the cutting head 5 is less likely to touch the wings of the second steel segment 32.
In the embodiment of combining the edges of the grooves, the cut target edge is ensured to be completely attached to the second I-steel, and the cutting head is prevented from colliding with an I-steel wing plate when cutting on the web plane.
In order to ensure that the cutting head does not touch the wing of the second steel section 32, in a specific example, the recess depth of the groove edge 111 matches the thickness of the wing in the first i-steel, and the chamfer of the wing and the web, for example: if the chamfered portion to which the wing plate is connected is regarded as a part of the wing plate: the recessed depth of the groove edge 111 may be equal to the maximum thickness of the wing, and if the wing and the chamfered portion to which it is connected are considered as different portions, the recessed depth of the groove edge 111 may be equal to the sum of the maximum thickness of the wing and the chamfered width. In other examples, compared to the example in fig. 11, the recessed depth may be deeper again, which can ensure that the cutting head 5 is not easy to touch the wing plate of the second steel segment 32, and meanwhile, the recessed depth may also be shallower than that in fig. 11, no matter which way is adopted, as long as the groove edge 111 is adopted, because it has a certain recessed depth, the cutting head 5 can be prevented from touching the wing plate of the second steel segment 32 to a certain extent, and further, both can fall within the range of the above embodiments.
In order to substantially avoid the collision of the cutting head 5 with the wing (especially for wide flange i-beams), the opening width of the groove edge 111 may be larger than the radius of the distal portion of the cutting head 5. The end part position can be understood as a part position of the tail end of the cutting head possibly having collision risk, and the position and the range of the part position can be correspondingly changed with different cutting heads and different I-shaped steel chamfers.
Referring to fig. 11, the target edge 110 may include a web abutting edge 114, two chamfered abutting edges 113, and two flange abutting edges 112, the number of the groove edges 111 is two, the shape of the chamfered abutting edges 113 matches the chamfer angle of the connection between the flange and the web in the second i-beam, the shape of the flange abutting edges 112 matches the inner surface shape of the flange in the second i-beam, and the shape of the web abutting edge 114 matches the surface shape of the web in the second i-beam;
one groove edge 111, one wing butt edge 112, one chamfer butt edge 113, the web butt edge 114, the other chamfer butt edge 113, the other wing butt edge 112 and the other groove edge 111 are connected in sequence, and meanwhile, the groove edge 111 is also connected with the second steel section 32 (i.e. connected with the base 12).
In the actual cutting process, if one end of the first steel segment 31, which is far away from the second steel segment 32, is connected with another steel segment, the web abutting edge 114 may be formed by cutting the first steel segment 31 and another steel segment when the corresponding cutting tool path 42 and cutting tool path 43 are cut; if the end of the first steel segment 31 remote from the second steel segment 32 is not connected to another steel segment (or can be understood to have been previously cut), then no cutting path for the abutting edges of the webs may be required in steps S22, S24, namely: the cutting blade path 42 may not include a blade path of the web butt edge.
In the specific implementation process, if the end of the second steel segment 32 far away from the first steel segment 31 is also connected with other steel segments, then: the second steel segment 32 may be cut off from the other steel segments by cutting the cutter path 44 shown in fig. 12 and the cutter path 45 shown in fig. 13, thereby obtaining the target member. It can be seen that the target member obtained in step S2 may be obtained naturally after the target edge is cut, or the second steel segment 32 and other steel segments may be cut before, during or after the target edge is cut, so that the target member including the cut first steel segment and the cut second steel segment can be obtained finally.
The aforementioned controlling of the translation of the cutting head may be controlling of the translation of the cutting head along an XY plane (i.e. a plane formed by an X axis and a Y axis), and accordingly, an axis (also understood as a length direction) of the first i-beam to be cut is parallel to the Y axis, and a rotation axis of the first i-beam is also parallel to the Y axis.
For the first I-steel, the first I-steel can be arranged on the chuck through the clamping jaw, then the first I-steel is driven to rotate by controlling the rotation of the chuck, at the moment, the rotation axis of the clamping jaw and the central axis of the first I-steel are mutually overlapped or parallel, when the rotation axis and the central axis of the first I-steel are not overlapped (namely are parallel), deviation exists, at the moment, as the position of the rotation axis is the position under a mechanical coordinate system, the cutting head is controlled on the basis of the mechanical coordinate system, and if the deviation is not predetermined during control and the position of the cutting tool path is adjusted on the basis of the deviation, the cutting position is easy to cause. For example: when the aforementioned L-shaped cutting path is cut, if the deviation is not considered sufficiently, the web of the first i-steel of the cutting knife is cut.
The above references to the central axis of the i-beam are to be understood as: an axis passing through the center of the web of the I-steel. The axis is understood to be along the length of the i-beam.
In some schemes, if the first i-beam adopts a wide flange i-beam, then: the above-mentioned deviations can occur in particular when the universal jaws are replaced by jaws which are dedicated to the machining of wide-flange i-beams, as is often required when fixing the first i-beam to the chuck.
Therefore, referring to fig. 14, before step S1, the method may further include:
s3: and determining the deviation between the central axis of the first I-beam and the rotating axis of the first I-beam.
The rotating shaft center of the first I-shaped steel can be understood as the rotating shaft center of the chuck.
Further, before performing steps S1 and S2, the position of each cutter path may be adjusted according to the deviation, for example, the position of the L-shaped cutter path may be adjusted according to the deviation.
In the specific implementation process, the two wing plates of the first I-shaped steel can be respectively characterized as a first wing plate and a second wing plate, and then: referring to fig. 14, step S3 may specifically include:
s31: controlling the first I-beam to rotate to a first direction around the rotating shaft center, and measuring and calculating the position of a central axis of the surface of a first wing plate of the first I-beam at the moment to obtain first position information;
s32: controlling the first I-beam to rotate around the rotating axis to a second direction, and measuring and calculating the central axis position of the surface of a second wing plate of the first I-beam at the moment to obtain second position information;
s33: and determining the deviation of the central axis of the first I-shaped steel relative to the rotating axis according to the first position information and the second position information.
Wherein the surface of the wing panel refers to the outer surface of the corresponding wing panel.
Further, referring to fig. 15, step S32 may include:
s321: controlling a cutting head to move above the first strake surface;
s322: controlling the cutting head to move along a first direction, and acquiring the position of the cutting head when the cutting head moves to a first boundary of the first wing plate to obtain first boundary information; the first direction is parallel to the first wing plate surface and perpendicular to the rotation axis;
s323: controlling the cutting head to move along a second direction, and acquiring the position of the cutting head when the cutting head moves to a second boundary of the first wing plate to obtain second boundary information; the first direction is opposite to the second direction;
s324: and calculating the first position information according to the first boundary information and the second boundary information.
Referring to fig. 15, step S33 may include:
s331: controlling a cutting head to move above the second wing plate surface;
s332: controlling the cutting head to move along a third direction, and acquiring the position of the cutting head when the cutting head moves to the first boundary of the second wing plate to obtain third boundary information; the third direction is parallel to the first wing plate surface and perpendicular to the rotation axis;
s333: controlling the cutting head to move along a fourth direction, and acquiring the position of the cutting head when the cutting head moves to a second boundary of the second wing plate to obtain fourth boundary information; the third direction is opposite to the fourth direction;
s334: and calculating the second position information according to the third boundary information and the fourth boundary information.
In steps S322, S323, S332, and S333, the process of acquiring the position and obtaining the boundary information may be, for example: in the moving process of the cutting head, distance information detected by a distance measuring sensor (such as a capacitance sensor) of the cutting head is monitored in real time, the distance information can represent the distance between the cutting head and the surface of the wing plate, if the distance information is detected to be suddenly increased (for example, the variation and the variation amplitude exceed a threshold value), the cutting head is determined to reach a boundary, coordinates of the cutting head at the moment are recorded to be used as corresponding boundary information, and the coordinates can be converted into coordinates of a boundary position to be used as corresponding boundary information by combining the distance between the cutting head and the surface of the wing plate.
In a specific example, the first orientation and the second orientation differ by a rotation angle of 180 degrees. The rotating axis is perpendicular to the X axis and the Z axis of the mechanical coordinate system;
when the first I-steel is in the first orientation, the first wing plate surface is perpendicular to the Z axis;
in fig. 16, for ease of understanding, an i-beam is drawn in an i-shape, in which:
point a characterizes: the position of the central axis of the first wing surface in the XZ plane in a first orientation (e.g., the surface of the first wing faces the Z axis forward);
point b characterizes: a position of the central axis of the second wing surface in the XZ plane in a first orientation (e.g., the surface of the first wing facing negative in the Z-axis);
point a' characterizes: the position of the central axis of the first wing surface in the XZ plane when in the second orientation (e.g., the surface of the first wing faces the Z axis forward);
point b' characterizes: a position of the central axis of the second wing surface in the XZ plane in a second orientation (e.g., the surface of the first wing facing negatively in the Z-axis);
point M characterizes: the position of the rotating shaft center on the XZ plane;
point S characterizes: the central axis of the I-shaped steel is in the position of the XZ plane.
The deviation is determined according to the following formula:
wherein:
Zaz-axis coordinates characterizing the mid-axis of the surface of the first wing in a first orientation (e.g., the surface of the first wing faces forward in the Z-axis), i.e., Z-axis coordinates in the first position information;
Zb’z-axis coordinates characterizing a central axis of the surface of the second wing in a second orientation (e.g., the surface of the first wing faces forward in the Z-axis), i.e., Z-axis coordinates in the second position information;
Xaan X-axis coordinate characterizing a central axis of the first wing surface when in a first orientation (e.g., the surface of the first wing faces forward in the Z-axis); i.e. the X-axis coordinate in the first position information;
Xb’an X-axis coordinate characterizing a central axis of the surface of the second wing when in a second orientation (e.g., the surface of the first wing faces forward in the Z-axis); i.e., the X-axis coordinate in the second position information;
Δ X represents a deviation component in the X-axis direction in the deviation;
Δ Z represents a deviation component in the Z-axis direction in the deviation;
wherein Za、Zb、Xa、Xb’It can be obtained by finding the coordinates of the midpoint of the boundary information of the same wing panel.
The embodiment of the invention also provides a component which is obtained by cutting by using the method for cutting the I-shaped steel related to the above alternative.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (10)
1. A method of cutting an I-beam to cut a target member having a tongue plate from a first I-beam comprising an I-shaped first steel segment for cutting to form the tongue plate;
the cutting method is characterized by comprising the following steps:
cutting off a protrusion part of a wing plate protruding from the surface of the web plate aiming at the first steel section;
and cutting a target edge at the edge of the first steel section, and obtaining the target member, wherein the shape of the target edge is matched with the shape of a second I-shaped steel spliced by the target member.
2. The method of cutting an i-steel according to claim 1, wherein cutting off a protrusion of a wing plate protruding from a web surface for the first steel segment comprises:
cutting a pair of L-shaped cutting knife paths on each wing plate of the first steel section, and cutting off the protruding part based on the L-shaped cutting knife paths.
3. The method of cutting an i-section according to claim 2, wherein cutting a pair of L-shaped cutting paths at each wing of the first steel segment and cutting off the protrusion based on the L-shaped cutting paths comprises:
when a single L-shaped cutting knife path is cut, the outer surface of the corresponding wing plate is controlled to face the cutting head; and then controlling the cutting head to translate and cut the L-shaped cutting tool path from the outer side of the corresponding wing plate.
4. The method of claim 2, wherein the L-shaped cutting path comprises a transverse line cutting path and a vertical line cutting path which are vertically connected, and the vertical line cutting path is parallel to the web of the first I-beam.
5. A method according to any one of claims 1 to 4, wherein the first I-section further comprises an I-shaped second section, the end of the first section remote from the target edge being joined to the second section;
cutting a target edge in the edge of the first steel segment, comprising:
controlling one side of the web plate of the first I-shaped steel to face a cutting head;
controlling the cutting head to translate and cut the edge of the first steel segment from one side of the web to cut and demarcate the portion to be cut corresponding to the target edge, wherein the portion to be cut remains connected with the second steel segment only after the portion to be cut is cut and demarcated;
controlling the outer surface of a wing plate of the first I-steel to face the cutting head;
and controlling the cutting head to translate and cut the joint of the first steel section and the second steel section from the outer side of a wing plate so as to cut off the part to be cut and the second steel section.
6. A method according to any one of claims 1 to 4, wherein the first I-section further comprises an I-shaped second section, the end of the first section remote from the target edge being joined to the second section, the target edge having a grooved edge therein immediately adjacent the second section.
7. The method according to claim 6, wherein the target edges comprise a web abutting edge, two chamfer abutting edges and two wing abutting edges, the number of the groove edges is two, the shape of the chamfer abutting edges is matched with the chamfer of the joint of the wing and the web in the second I-steel, the shape of the wing abutting edges is matched with the shape of the inner surface of the wing in the second I-steel, and the shape of the web abutting edges is matched with the shape of the surface of the web in the second I-steel;
one groove edge, one wing plate butt joint edge, one chamfer butt joint edge, the web plate butt joint edge, the other chamfer butt joint edge, the other wing plate butt joint edge and the other groove edge are connected in sequence.
8. The method of claim 6, wherein the recess has a depth corresponding to the thickness of the wing plate in the first i-beam and the chamfer of the wing plate and the web, and the recess has an opening width greater than the radius of the cutting head at the distal end.
9. A method according to any one of claims 1 to 4, wherein the first and/or second I-section is a wide flange I-section.
10. A member obtained by cutting the i-section steel according to any one of claims 1 to 9.
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