method and apparatus for laminating composite tape on a substrate

专利摘要:
METHOD AND APPLIANCE FOR LAMINATION OF COMPOSITES. The present invention relates to composite tape which is laminated on a substrate (52, 56) using a gantry (57, 59) to move a tape laminating head (66, 78) along the length of the substrate. The laminating head is mounted for movement along a beam (60, 76) in the gantry that extends across the width of the substrate. The lamination direction can be changed by changing the angular orientation of the beam.
公开号:BR112014002296B1
申请号:R112014002296-8
申请日:2012-07-03
公开日:2021-02-09
发明作者:Thomas J. Hagman；Gregory L. Branch；James P. Dwyer；Brian E. Hood；Erik Lund；Wade M. Morris；Jonathan R. Schwedhelm；Thomas C. Stone
申请人:The Boeing Company；
IPC主号:

专利说明:

BACKGROUND INFORMATION 1. Field
[0001] The present invention relates to the manufacture of composite structures and is more particularly a method and apparatus for laying structures using automated layer lamination. 2. Background
[0002] Composite structures such as those used in the automotive, marine and aerospace industries can be manufactured using automated composite material application machines, commonly referred to as automated fiber laying machines (AFP) and composite tape laying machines (CTLMs) . These machines can be used in aerospace applications, for example, to manufacture large-scale structures by placing a plurality of strips of tape in continuous edge-to-edge contact, forming a wide, singular conformal bandwidth, which is compacted over a tool.
[0003] The machines described above employ fiber delivery heads that have a relatively high degree of operational flexibility, including the ability to add, loosen or cut any or all contiguous strips of tape independently of the others. However, these machines may not be well suited for laying relatively narrow and long structures, such as reinforcements and stringers, which require long strands of tape having a zero degree fiber orientation and many short strands of fiber orientation. not zero degree. For example, and without limitation, the aforementioned automated machines may have difficulty laying down long, zero-degree ribbon strokes that are not subject to wrinkling during formation and may not be efficient at laying down non-zero ribbon strokes that require very fast start-stop machine movements.
[0004] Consequently, there is a need for an automated composite tape laminating method and apparatus that are well suited for laying relatively narrow and long pieces that reduce or eliminate the formation of creases in the layer, reduce material wear and increase the laying rate of non-zero oriented tape strokes. summary
[0005] The described embodiments provide a method and apparatus for laminating narrow, relatively long laminated structures, such as stringers and reinforcements comprising multiple layers of different fiber orientations formed from unidirectional composite tape. The embodiments use narrow width strips capable of better combining the width dimensions of long narrow parts to reduce waste. The relatively long, zero-grade tape strokes can be laminated with improved creasing measures and the non-zero tape strokes can be efficiently laid and cut in a way that reduces material wear while increasing the laminating rate. The device is characterized by fast guillotine-type tape cutters that can be rotated to different cutter angles to make the cuts that eliminate the residue. Very short strips of tape can be quickly laminated. The guillotine cutters are characterized by a voice coil actuator specially indicated to perform the fast cutting movement. The cutter blade pivots along with the ribbon movement to reduce unwanted spikes in the ribbon tension. The laminating heads comprise multiple ribbon control modules that are laterally adjustable in order to adjust the clearances between the strips of joint tape. The tape control modules used to laminate the zero grade strokes allow cuts between the tape segments without significant gaps to form discontinuous tape strokes that can reduce the formation of creases in the layer. The laminating heads can be positioned accurately in relation to each other, so that the gap between the strips of tape can be varied, if desired.
[0006] According to a disclosed embodiment, the apparatus is provided for laminating composite tape to a substrate comprising a mobile laminator with respect to the substrate along a first axis. The laminator includes first and second spaced supports and a beam extending through the substrate along a second axis. The pivoting connections between the beam and each of the supports allow a change in the angular orientation relative to the beam with respect to the first axis. The apparatus further comprises at least one tape laminating head on the beams to laminate the composite tape to the substrate. The laminator can include a plurality of beams and a rolling head on each of the beams. The apparatus further comprises a plurality of pivoting connections between each of the beams and supports to allow a change in the angular orientation of each beam in relation to the first axis. The supports are movable independently of each other in a direction substantially parallel to the first axis. A sliding connection between the beam and one of the supports allows the beam to slide with respect to the support when the angular orientation of the beam has been changed. The tape laminating head includes a plurality of carts mounted for substantially parallel movement along the beam and a tape control module in each of the carts to seat a strip of the composite tape on the substrate.
[0007] According to another embodiment, a method is provided for laminating composite tape on the substrate. The method comprises moving a laminator and a substrate relatively along an axis and moving a ribbon control module along a beam in the gantry when the laminator and the substrate move relative to each other. The method further comprises using the ribbon control module to laminate at least one strip of composite ribbon onto the substrate and change the angular orientation of the beam relative to the axis. The angular orientation of the beam is changed by pivoting the beam.
[0008] According to another embodiment, a composite tape laminating head comprises a composite tape source and a compacting roller adapted to compact the tape on the substrate. The head also includes a ribbon feed assembly that feeds the ribbon from the ribbon source to the compacting roller and a cutter assembly including a reciprocating cutting blade to cut the ribbon fed to the compacting roller. The cutter assembly includes a rotor assembly for rotating the cutting blade to any of the plurality of cutting angles. The rotor assembly includes a housing and a cylinder rotatably mounted in the housing and the cutter assembly includes a piston coupled with the cutting blade and reciprocally mounted within the cylinder.
[0009] According to another embodiment, a method is provided for laminating composite tape on a substrate comprising the movement of a tape laminating head through the substrate at an angle oblique to an edge of the substrate. The method further comprises cutting pieces of the composite tape when the laminating head moves over the substrate, including cutting the tape substantially parallel to the edge of the substrate, and compacting the tape on the substrate.
[00010] According to another embodiment, a composite tape laminating head comprises a composite tape source, a compacting roller adapted to compact the tape against a substrate and a tape feed assembly to feed the tape from the source of tape to the compaction roller. The laminating head further comprises a tape cutter assembly for cutting the tape including a movable cutting blade along with the tape when the tape is being cut. The tape cutter assembly includes trunnions to pivot the blade on the head. The blade is pivotable along an arc during cutting and the ribbon cutting set includes an anvil against which the blade cuts the ribbon, where the anvil is pivotable along the arc with the blade.
[00011] According to yet another embodiment, a method is provided for laminating composite tape on the substrate comprising moving the tape laminating head through the substrate and feeding the composite tape to a compacting roller on the laminating head. The method further comprises using a cutting blade to cut pieces of the composite tape when the laminating head moves over the substrate, including the movement of the blade along with the tape when the blade is cutting the tape. The method also comprises compacting the tape on the substrate. The movement of the blade along with the tape includes the movement of the blade and the tape along an arc at substantially the same speed.
[00012] According to another embodiment, the composite tape laminating head comprises a source of composite tape and a compacting roller adapted to compact the tape against a substrate. The head also includes a ribbon feeding set to feed the ribbon from the ribbon source to a compacting roller and a cutting set to cut the ribbon, including the movable cutting blade and a movable anvil against which the blade cuts the ribbon. The laminating head also comprises a drive system to move the blade and the anvil in sync with each other. The blade and anvil are each rotatable and the drive system includes a pair of motors to rotate the blade and anvil at substantially the same rotational speed, respectively.
[00013] According to another embodiment, a method is provided for laminating the composite tape to a substrate, comprising moving a laminating head over substrate and feeding the composite tape to a compacting roller in the laminating head. The method further comprises rotating a cutting blade and an anvil at substantially the same rotational speed, using the cutting blade and the anvil to cut the tape and compacting the tape on the substrate. Rotating the blade and anvil includes the use of separate motors to rotate the blade and anvil synchronizing the speed of the motors. Cutting the tape includes feeding the tape to a jaw between the rotating blade and the rotating anvil.
[00014] According to another embodiment, the apparatus is provided for laminating a composite tape on a substrate having an extension and width. The apparatus comprises at least one first movable laminator along the length of the substrate. The first laminator includes a pair of movable supports and a beam extending across the width of the substrate and coupled with each of the supports. The apparatus also comprises a first laminating head mounted on and movable along the beam to laminate the composite tape across the width of the substrate. The first laminating head includes a composite tape source, a compacting roller for compacting the tape on the substrate, a tape feeding set for feeding the tape from the tape source to the compacting roller and a tape cutter set for cut pieces of tape fed to the compaction roller. The tape cutter set includes a cutting blade mounted to move with the tape and rotatable to any plurality of angular cutting positions.
[00015] According to yet another embodiment, a method is provided for laminating composite tape on a substrate having an extension and a width, comprising movement relative to a first laminator and the substrate along the extension of the substrate and use of a head tape laminator on the first laminator to laminate the tape across the width of the substrate. The method further comprises relatively moving a second laminator and the substrate along the length of the substrate and using a second tape laminating head on the second laminator to laminate the tape along the length of the substrate.
[00016] In summary, according to one aspect of the invention, there is provided an apparatus for laminating composite tape on a substrate including a movable laminator with respect to the substrate along a first axis, the laminator including first and second spaced supports and a beam extending through the substrate along a second axis; pivoting connections between the beam and each of the supports to allow a change in the angular orientation of the beam in relation to the first axis; and at least one tape laminating head on the beam to laminate the composite tape to the substrate.
[00017] Advantageously, the apparatus in which the laminator includes a plurality of beams and a tape laminating head in each of the beams for laminating the composite tape on the substrate and the apparatus further comprises: a plurality of pivoting connections between each of the beams and the supports to allow a change in the angular orientation of each of the beams in relation to the first axis.
[00018] Advantageously, the apparatus in which the supports are movable independently of each other in a direction substantially parallel to the first axis.
[00019] Advantageously, the apparatus also includes a sliding connection between the beam and one of the supports to allow the beam to slide in relation to a support.
[00020] Advantageously, the apparatus in which the tape laminating head includes a plurality of carts mounted for substantially parallel movement along the beam; at least one tape control module on each of the carts to seat a strip of composite tape on the substrate; and means for aligning the ribbon control modules with respect to each other when the angular orientation of the beams is changed.
[00021] According to another aspect of the invention, a method of laminating composite tape on a substrate is provided, including relative movement of a tape laminator and the substrate along an axis; movement of a ribbon control module along a beam in the laminator; using the tape control module to laminate at least one strip of composite tape on the substrate; and changing the angular orientation of the beam in relation to the axis.
[00022] Advantageously, the apparatus in which the angular orientation of the beam is changed by pivoting the beam.
[00023] Advantageously the apparatus in which the angular orientation of the beam is changed by relative movement of the two supports, respectively, on the ends of the beam.
[00024] Advantageously, the apparatus in which the change in the angular orientation of the beam in relation to the axis includes the linear sliding of the beam in relation to one of the supports, and the method includes changing the departure of the position of the ribbon control module with based on the change in the angular orientation of the beam.
[00025] According to another aspect of the present invention, a composite tape laminating head is provided, including a composite tape source; a compacting roller adapted to compact the tape against a substrate; a tape feed assembly for feeding the tape from the tape source to the compaction roller; and a cutter assembly including a reciprocating cutting blade to cut the tape fed to the compacting roller, the cutter assembly further including a rotary assembly for rotating the cutting blade to any of a plurality of cutting angles.
[00026] Advantageously, the apparatus in which the rotor assembly includes a housing, a rotatable cylinder mounted in the housing and a piston coupled with the cutting and reciprocating blade inside the cylinder.
[00027] Advantageously, the apparatus in which the rotor assembly includes an actuator coupled with the cylinder to rotate the cylinder to any of the plurality of rotational positions.
[00028] Advantageously, the apparatus in which the cutter assembly still includes a valve adapted to be coupled with a pressurized air source and an electrical voice coil to operate the valve.
[00029] Advantageously, the apparatus in which the cutter set still includes an anvil against which the tape can be cut by the blade, the anvil being coupled and rotatable with the cylinder.
[00030] In accordance with yet another aspect of the present invention, a method of laminating composite tape on a substrate is provided, including the movement of a tape laminating head on a substrate at an angle oblique to an edge of the substrate; cutting pieces of composite tape when the laminating head moves through the substrate, including cutting the tape substantially parallel to the edge of the substrate; and compacting the tape on the substrate.
[00031] Advantageously, the apparatus also includes feeding composite tape to a compacting roller in the laminating head and in which the compacting of the tape is carried out by a compacting roller in the laminating head.
[00032] Advantageously, the apparatus further includes cutting pieces of tape including: reciprocating a cutting blade and blade orientation substantially parallel to the edge of the substrate.
[00033] Advantageously, the device still including blade orientation includes blade rotation.
[00034] Advantageously, the apparatus further including cutting pieces of tape includes the use of the blade to cut the tape against an anvil and orientation of the anvil to a position based on the orientation of the blade.
[00035] In accordance with yet another aspect of the present invention, a composite tape laminating head is provided, including a composite tape source; a compacting roller adapted to compact the tape against a substrate; a ribbon feed assembly for feeding the ribbon from the ribbon source to the compaction roller; and a tape cutter to cut the tape, including a movable cutting blade along with the tape when the tape is being cut.
[00036] Advantageously, the apparatus in which the tape cutter assembly includes trunnions for pivotally mounting the blade on the head.
[00037] Advantageously, the apparatus in which the blade is pivoted along an arc during a cut, and the tape cutter set includes an anvil against which the blade cuts the tape, in which the anvil is pivoted along the arc with the blade.
[00038] Advantageously, the apparatus still including a frame and in which the tape cutter assembly is pivotally mounted on the structure.
[00039] Advantageously, the apparatus in which the tape cutter assembly is rotatable to any of the plurality of cutting angles in the head.
[00040] According to another aspect of the present invention, there is provided a method of laminating the composite tape to a substrate, including the movement of a tape laminating head over the substrate; feeding of the composite tape to the compacting roller in the laminating head; use of a cutting blade to cut the pieces of the composite tape when the laminating head moves over the substrate, including the movement of the blade along with the tape when the blade is cutting the tape; and compacting the tape on the substrate.
[00041] Advantageously, the apparatus in which the movement of the blade together with the tape includes the movement of the blade and the tape along an arc.
[00042] Advantageously, the apparatus in which the blade is moved along the arc at substantially the same speed as the tape.
[00043] Advantageously the apparatus in which the use of a cutting blade to cut the tape into pieces includes cutting the tape against an anvil and moving the anvil together with the blade.
[00044] Advantageously, the apparatus in which the movement of the blade together with the tape includes the pivoting of the blade when the tape is being fed to the compaction roller.
[00045] In accordance with yet another aspect of the present invention, a composite tape laminating head is provided, including a composite tape source; a compacting roller adapted to compact the tape against a substrate; a ribbon feed assembly for feeding the ribbon from the source to the compaction roller; a cutter assembly for cutting the tape including a movable cutting blade and a movable anvil against which the blade cuts the tape; and a drive system for moving the blade and the anvil in sync with each other.
[00046] Advantageously, the device in which the blade and the anvil are each rotatable.
[00047] Advantageously, the device in which the drive system includes a pair of motors to rotate the blade and the anvil, respectively.
[00048] Advantageously, the apparatus in which the motors are synchronized to, respectively, rotate the blade and the anvil at substantially the same rotational speeds.
[00049] Advantageously, the apparatus in which the tape cutter assembly includes: a housing; and first and second articulated rotors for rotation in the housing and, respectively, having the blade and anvil attached to them for rotation with them.
[00050] In accordance with yet another aspect of the present invention, a method of laminating composite tape on a substrate is provided, including moving a tape laminating head over the substrate; feeding the composite tape to a compacting roller on the head laminator; rotation of a cutting blade and an anvil at substantially the same rotational speed; use of the blade and anvil to cut the tape; and compacting the tape on the substrate.
[00051] Advantageously, the apparatus in which the rotation of the blade and the anvil includes the use of separate motors to rotate the blade and the anvil; and engine speed synchronization.
[00052] Advantageously, the apparatus in which the cut of the tape includes feeding the tape to a jaw between the rotating blade and the rotating anvil.
[00053] Advantageously, the apparatus in which the cutting and compacting of the tape includes the formation of a discontinuous tape course on the substrate by cutting and compacting a series of tapping tape segments substantially without gaps between the tape segments.
[00054] In accordance with another aspect of the present invention, another apparatus is provided for laminating composite tape on a substrate having an extension and a width, including at least one first movable laminator along the length of the substrate, the first laminator including a pair of movable supports and a beam extending across the width of the substrate and coupled with each of the supports; a first laminating head mounted on and movable along the beam to laminate the composite tape on the substrate, the first laminating head including a composite tape source, a compacting roller for compacting the tape on the substrate, a tape feed assembly for feed the tape from the tape source to the compacting roller and a tape cutter set to cut pieces of tape fed to the compacting roller, the tape cutter set including a cutting blade mounted for movement along with the tape and rotatable to any of a plurality of angular cutting positions.
[00055] Advantageously, the device also includes pivoting connections between the beam and the supports allowing changes in the angular orientation of the beam.
[00056] Advantageously, the apparatus in which the first laminating head laminates the composite tape across the width of the substrate; and the supports are movable relative to each other along the length of the substrate.
[00057] Advantageously, the apparatus in which the tape cutter assembly includes a movable anvil through an arc together with the tape and the blade during a tape cut.
[00058] Advantageously, the apparatus further including a second movable laminator along the length of the substrate, the second laminator including a beam extending across the width of the substrate; and a second laminating head mounted on the beam of the second laminator for laminating the composite tape on the substrate along the length of the substrate, the second laminating head including a composite tape source, a compacting roller for compacting the tape on the substrate, a set tape feed that feeds the tape from the tape source to the compacting roller, and a tape cutter assembly for cutting pieces of ribbon fed to the compacting roller.
[00059] Advantageously, the apparatus in which the tape cutter assembly on the second laminating head includes a rotating cutting blade, a rotating anvil and a pair of motors synchronized with each other to rotate, respectively, the blade and the anvil at substantially the same speed rotational.
[00060] In accordance with another aspect of the present invention, another method of laminating a composite part seated on a substrate having an extension and a width is provided, including, relatively movably, a first laminator and the substrate along the extension the substrate; the use of a first laminating head on the first laminator to laminate the tape across the width of the substrate; relatively secondly a second laminator and the substrate along the extension of the substrate; and using a second tape laminator head on the second laminator to laminate the tape along the length of the substrate.
[00061] Advantageously, the apparatus in which the use of the first tape laminating head in the first laminator to laminate the tape includes cutting edges of the tape substantially parallel to an edge of the substrate.
[00062] Advantageously, the apparatus in which the cutting ends of the tape substantially parallel to an edge of the substrate includes rotation of a cutting blade for an orientation of the blade substantially parallel to the substrate edge.
[00063] Advantageously, the apparatus in which the use of a first tape laminating head in the first laminator to laminate the tape across the width of the substrate includes the use of a cutting blade to cut pieces of tape against an anvil and the movement of the blade and the anvil along with the tape when the tape is being cut.
[00064] Advantageously, the apparatus in which the use of the second laminating head in the second laminator to laminate the tape along the length of the substrate includes passage of the tape to the jaw between a rotating cutting blade and a rotating anvil; and rotating the blade and the anvil at substantially the same rotational speed as the tape is being cut.
[00065] Advantageously, the apparatus in which the use of the first tape laminating head to laminate the tape across the width of the substrate includes the movement of the first laminating head along a beam and the method further includes changing the direction that the tape it is laminated on the substrate by the first rolling head by changing the angular orientation of the beam.
[00066] Advantageously, the apparatus also includes the rectification of the part tray in a mesh format, using the second laminator to move a rectifier over the part tray. Brief Description of Drawings
[00067] The new aspects believed to be characteristics of the advantageous embodiments are described in the attached claims. Advantageous embodiments, however, as well as a preferred mode of use, other objectives and their advantages, will be better understood with reference to the following detailed description of an advantageous embodiment of the present invention, when read in conjunction with the accompanying drawings, in which: Figure 1 is an illustration of a functional block diagram of the apparatus for laminating composite materials; Figure 2 is an illustration of a flow chart of a method for laminating composite materials; Figure 3 is an illustration of a plan view of an embodiment of the apparatus shown in Figure 1; Figure 4 is an illustration of a plan view of the area indicated as "Figure 4" in Figure 3; Figure 5 is an illustration of an isometric view of the nonzero grade laminator used to seat nonzero belts forming part of the apparatus shown in Figures 3 and 4. Figure 6 is an illustration of an end view taken in the direction indicated as "Figure 6 "in Figure 4; Figure 7 is an illustration similar to Figure 5, but showing the non-zero grade laminator reoriented to seat the strokes at 45 degrees; Figure 8 is an illustration of a plan view of the laminator shown in Figure 7; Figure 9 is an illustration of a side view of one of the group beams forming part of the non-zero grade laminator shown in Figures 5-8. Figure 10 is an illustration of a perspective view of the group beams shown in Figure 9; Figure 11 is an illustration of a perspective view of one of the ribbon control modules and guide rail of the associated cart forming part of the group beam shown in Figures 9 and 10; Figure 12 is an illustration of a perspective view of the ribbon control module and associated cart shown in Figure 11; Figure 13 is an illustration showing the strokes of tape laid by successive passes of the nonzero laminator to form a 45 degree layer; Figure 14 is an illustration of a flow chart of a method of laminating composites using the non-zero grade laminator shown in Figures 5-8; Figure 15 is an illustration of an isometric view of the zero grade laminator shown in Figures 1 and 2 for laying substantially zero grade layers; Figure 16 is an illustration of another isometric view of the zero grade laminator shown in Figure 15, taken from the bottom; Figure 17 is an illustration of a single ribbon course seated by the zero grade laminator shown in Figures 15 and 16; Figure 18 is an illustration of one side of a tape control module employed in the zero grade laminator shown in Figures 15 and 16; Figure 19 is an illustration on the other side of the tape control module shown in Figure 18; Figure 20 is an illustration similar to Figure 19, but detailed to show the subsets of the tape control module; Figure 21 is an end view of the cutter rotor and anvil rotor forming part of the ribbon control module shown in Figures 18-20; Figure 22 is an illustration of a plan view of a layer having discontinuous strips of tape seated by the zero grade laminator shown in Figures 15 and 16. Figure 23 is an illustration of the area indicated as "Figure 23" in Figure 22; Figure 24 is an illustration of a flowchart of a method of laminating composites using the zero grade laminator shown in Figures 15 and 16; Figure 25 is an illustration of an isometric view of a portion of one of the tape control modules used in the nonzero laminator in Figures 5-8; Figure 26 is an illustration of a perspective view showing additional details of the cutter assembly forming part of the ribbon control module shown in Figure 25; Figure 27 is an illustration of a diagrammatic view showing the movement of the cutting blade of the cutter assembly shown in Figures 25 and 26, together with the tape and the anvil during a cut; Figure 28 is an illustration of a flowchart of a method of laminating tape using the tape control module shown in Figure 25; Figure 29 is an illustration of a singular 45 degree ribbon course, cut at angles parallel to the substrate and showing areas of wear outlined by the angular cuts; Figure 30 is an illustration of a flowchart of a method of laminating composite materials using tape cuts parallel to a substrate edge as shown in Figure 29; Figure 31 is an illustration of a perspective view of a tape cutter assembly forming part of the tape control module shown in Figure 25; Figure 32 is an illustration of a sectional view taken along line 32 - 32 in Figure 31; Figure 33 is an illustration of a cross-sectional view similar to Figure 32, but showing additional details of the cutter assembly; Figure 34 is an illustration of a top view of the ribbon control module shown in Figure 26, showing the rotary blade actuator in a first position; Figure 35 is an illustration similar to Figure 34, but showing the blade rotator actuator having been actuated for a second position; Figure 36 -38, respectively, illustrating the cutter assembly shown in Figures 31-33 in three different rotational positions; Figure 39 is an illustration of a block diagram of the basic electrical and pneumatic components of an apparatus shown in Figures 1 and 3; Figure 40 is an illustration of an aircraft production flowchart and service methodology. Figure 41 is an illustration of a block diagram of an aircraft. Detailed Description
[00068] With reference first to Figure 1, the laminating apparatus 50 for laying a composite part 52 on a substrate that can comprise a table 54 or tool largely comprises first and second laminators 56, 58, each of which are automatically operated by a controller 86 which it can comprise a PC, PLC (programmable logic controller) or other electronic controller. The table or substrate 54 and the laminators 56, 58 are relatively mobile, in the illustrated embodiment, the laminators 56, 58 are independently mobile relative to the table 54, however, in other embodiments, this relative movement can be carried out by the movement of the relative table 54 to laminators 56, 58. Table 54 may include a table lift control 53 to control the elevation of table 54 and thus the vertical distance between seat 52 and laminators 56, 58. Seat 52 can comprise multiple layers (not shown) laminated composite tape, where each layer is formed by laminating multiple strips of the unidirectional tape on table 54 or a pre-seated layer of part tray 52. The layers of part tray 52 may have fiber orientations with based on a predetermined layered scale. As will be discussed in more detail below, the laminating apparatus 50 is particularly well suited for laying relatively long and narrow parts such as stringers and reinforcers (not shown) used in the aerospace industry.
[00069] The second laminator 58, sometimes referred to below as the zero-grade laminator 58, is adapted to simultaneously laminate multiple strokes (not shown in Figure 1) of the unidirectional composite tape generally in the zero-degree orientation. In the case of relatively long, narrow part 52 trays, the zero degree orientation extends along the length of the part tray 52. The laminator 58 includes a gantry 57 comprising a cross beam 60 extending across the table 54 and supported at their opposite ends by the supports 62, 64. One or more ribbon laminating heads 66 are mounted for movement along the beam 60. Each of the laminating heads 66 can include one or more ribbon control modules 68 that work to cut , add and compress the pieces of the composite tape (not shown in the Figure) on the part tray 52.
[00070] The first laminator 56, sometimes referred to below, referred to as a non-zero laminator 56, slides unidirectional composite tape along orientations other than zero degree orientations. For example, and without limitation, the first laminator 56 to laminate the unidirectional composite tape oriented at 45, 90 or 135 degrees with respect to a reference direction, such as the longitudinal axis (the X axis in Figure 3) of the part tray 52 Other angular orientations of the rolling direction are also possible. The non-zero laminator 56 includes a gantry 59 comprising a group of substantially parallel beams 76 supported by a pair of support frames 72, 74. Support frames 72, 74 are mounted on rails 107 (Figures 3 and 6) on table 54 for movement along the length of the table 54. Each of the beams 76 includes one or more laminating heads 78. Each of the laminating heads 78 includes one or more ribbon control modules 80 that work to cut, add and compact the composite ribbon unidirectional against the part tray 82, when the laminating head 78 travels along the beams 76. A first set of actuators 82 can be provided to adjust the spacing between the beams 76 and a second set of actuators 84 can be provided to adjust the spacing between those adjacent the ribbon control modules 80 in each of the rolling heads 78.
[00071] Figure 2 illustrates a method of laminating composite parts using laminator apparatus 50 shown in Figure 1. Beginning at 88, the first non-zero grade laminator 56 and substrate 54 are moved relative to each other. As previously mentioned, the substrate may comprise a table 54, and a previously laid tool or layer forming part of the layer tray 52. In step 90, one or more laminating heads 78 in the non-zero grade laminator 56 is used to laminate tape composite across the width (Y axis 98 in Figure 3) of the substrate 54, at the desired non-zero angles relative to the extension (X axis 98) of the substrate 54. In step 92, the zero grade laminator 58 and the substrate 54 are moved relative axially along the extension (X-axis 98) of the substrate 52, 54. In step 94, one or more of the rolling heads 66 in the zero grade laminator 58 is used to laminate the unidirectional composite tape along the length of the substrate 54 Steps 88 - 94 can be repeated to apply a plurality of strokes of the composite tape forming multiple layers of piece tray 52. In the illustrated example, substrate 54 is fixed and laminators 56, 58 are movable relative to substrate 54 however, in other embodiments, it may be possible to move substrate 54 relative to laminators 56, 58.
[00072] Figures 3 and 4 illustrate a typical embodiment of the laminating apparatus 50. The laminating apparatus 50 operates in a three-dimensional coordinate system X, Y, Z 98 in which the X axis corresponds to the extension of the part tray 52, the Y-axis 98 corresponds to the "W" width of part tray 52, and the Z-axis 98 extends substantially normal to the X - Y plane. Rollers 56, 58, respectively, are aligned with each other and move independently on the rails 107 on the table 54 along the extension of the table 54 (X-axis 98) to seat the layers of the piece tray 52 on the surface of the table 54a. As previously mentioned, the part tray 52 can be relatively long in relation to its "W" width and can comprise a composite part such as reinforcement or a stringer used in aerospace or other applications. In the illustrated example, the surface of the table 54a is substantially flat, however in other embodiments, the surface 54a can be a tool (not shown) having some degree of curvature or contour.
[00073] The surface of the table 54a can incorporate resistance heating elements (not shown) in order to heat the piece tray 52 and thereby increase lamination rates. The table 54 can be removable and / or portable to allow the transport of completed piece trays 52 off the line in order to increase the use of the machine. The table 54 can be moved vertically along the Z axis 98 by the motors (not shown) operated by controller 86. The adjustable position of the table along the Z axis 98 using the table elevation control 53 (Figure 1) allows changes to be made at the distance between the surface of table 54a (Figure 1) / tray of part 52 and rolling heads 66, 78. This allows compensation to be made to increase the thickness of the laminated part when additional layers are placed, while maintaining the course relatively short compaction and allowing quick change of the top surface of the same 54a.
[00074] The gantry 57 forming the part of the zero grade laminator 58 comprises a transversely extending beam 60 which is pivotally connected by its opposite ends to a pair of supports 62, 64, which are independently films substantially parallel to the X-axis 98. The supports 62, 64 can be mounted on rails 107 on the table 54 for movement along the X axis 98. One or more rolling heads 66 are mounted for movement along the beam 60, transversely across the width of the table 54.
The portico 59 forming part of the non-zero grade laminator 56 comprises a plurality of substantially parallel beams 76, each being supported on and pivotally coupled by its opposite ends with a pair of laterally spaced frame supports 72, 74. The frame supports 72.74 are driven along the rails 107 (see Figures 3 and 6) by motors of the gantry driver103 which moves the gantry 59 along the extension of the table 54. Alternatively, the gantry 59 can be supported on the wheels ( not shown) or other structures to guide the movement of gantry 59 along the extension of the table 54. A pair of cantilever arms 100 supports the flexible control cables 102 that couple the controller 86 (Figure 1) with actuators 82, 84, ribbon control modules 80 and other controlled elements forming part of laminator 58.
[00076] Figures 5 and 6 illustrate additional details of the non-zero grade laminator 56. Each of the frame supports 72, 74 of gantry 59 is generally rectangular and includes open sides 72a, 74a through which one end 104 of each of beams 76 can pass. Each of the beams 76 is suspended from a horizontal frame member 72b, 74b forming part of the frame supports 72, 74. The actuators 82 are coupled between the beams 76 and frame members 74b and work to adjust the pitch or spacing " D "between the beams 76. In the illustrated embodiment, each of the beams 76 includes a laminating head 78 comprising a group of three ribbon control modules 80. However, more or less than three ribbon control modules 80 can be employed. Also, although four beams 76 have been illustrated, more or less than four beams can be employed. In the exemplary embodiment, laminator 56 can simultaneously laminate up to 12 strokes of tape with each pass of four laminating heads grouped 78 on substrate 54.
[00077] Each of the rolling heads 78 includes an actuator 84 that controls the pitch or distance "D2" between the ribbon control modules 80 in beam 76. In Figures 3-6, gantry 59 is illustrated in its 90-degree orientation degrees at which the beams 76 are aligned substantially parallel to the Y axis and the ribbon control modules 80 traverse along the beams 76 to seat the unidirectional tape which has a substantially 90 degree fiber orientation. In this configuration, the frame supports 72, 74 are substantially aligned with each other in the direction of travel along the X 98 axis.
[00078] The frame supports 72, 74 are independently movable with respect to each other, parallel to the X axis 98, in order to change the angular orientation of each of the beams 76 that are pivotally mounted on the frame supports 72, 74. The common angular orientations of beams 76 are 45, 90 and 135 degrees, however, other angular orientations are possible. Figures 7 and 8 show the frame supports 72, 74 having been moved along the X 98 axis relative to each other in order to orient the beams 76 at an angle of 45 degrees in relation to the X 98 axis. The change in the angular orientation of the beams 76 and thus, in the direction of the displacement of the rolling heads 78 along the beams 76, they can be altered by sending the control signals to the drive motors 103 that take at least one of the support frames 72, 73 to be displaced parallel to the X-axis 98 relative to another support frame 72, 74. When the support frames 72, 74 are displaced in relation to each other, the beams 76 articulate about the axis parallel to the Z axis 98 for the desired angular orientation. When the beams 76 are pivoted to the desired rolling angle, the alignment of the tape control module 80 with respect to each other along the axis 98 can be adjusted in such a way that the modules 80 can simultaneously start laying the tape on an edge of the substrate 54. In the illustrated example, with the beams 76 having been pivoted to an orientation of 45 degrees in relation to the X axis 98, the rolling heads 78 simultaneously seat multiple strokes of tape having angled orientation of 45 degrees. After a set of ribbon strokes is seated, gantry 59 is advanced incrementally along the X axis 98 to the following index position where the following set of non-zero ribbon strokes is laid by the rolling heads 78. Once that the beams 76 can be pivoted to a desired angle and the tape control modules 80 can be realigned with respect to each other to simultaneously start laminating a non-zero grade layer, a wide streak of tape strokes can be laid without excessive advance of modules 80, resulting in a high lamination rate. As previously mentioned, the table 54 can be incrementally moved along the Z axis 98 by the motors (not shown) operated by the controller 86 to compensate for the thickness of each just laid layer, thus keeping the compaction stroke relatively short.
[00079] Figures 9 and 10 illustrate additional details of one of the beams 76 and the associated rolling heads 78. Each of the beams 76 includes a pivot bearing 118 at one end and a pivoting and sliding bearing 120 spaced from the pivot bearing. 118. The pivot bearing 118 pivotably joins beam 76 in one of the frame supports 72 and the pivoting and sliding bearing 120 engages beam 76 in the other frame support 74 for both, pivoting movement and linear sliding movement, when beam 76 changes its angular orientation. As previously described, the laminating head 78 comprises a group of three ribbon control modules 80, however more or less than three ribbon control modules 80 are possible. In the illustrated example, each of the laminating heads 78 laminates three substantially parallel strips of the unidirectional composite tape on the substrate 54. Referring also to Figures 11 and 12 below, each of the tape control modules 80 is attached to a cart 108 having running blocks 110,112 on the linear rail that slide along the linear rails 116 of a support 106. The trolleys 108 are driven along the rails 116 by linear servo motors 115 mounted on the trolleys 108. Each of the supports 106 is mounted by the severe lock actuators 114 on one of the beams 76.
[00080] Figure 13 illustrates the lamination of a relatively narrow layer 147 having a 45 degree fiber orientation on a substrate 52 using the non-zero grade laminator 58. The layer 147 is formed by multiple passes of four laminating heads 78 in the beams 76 on the substrate 52. During a first step 124 of the rolling heads 78, twelve strips of 45 degree tape 132 are seated by twelve tape control modules 80 on the four beams 76, in a spaced relation to each other as shown by arrows 145 After the first step 124, the gantry 59 is moved an incremental distance along the X axis 98 and the laminating heads 78 seat a second set of 45 degree tape strips in a second step 126. This laying process is repeated during the third step 128 and a fourth step 130 until the strips of tape 132 form a substantially continuous layer 147. After each layer 147 is formed, table 54 (Figure 4) can be moved incrementally , descendingly, along the Z axis 98 by the table elevation control 53 to compensate for the additional laminated thickness added by layer 147.
[00081] Figure 14 illustrates the total steps of a method of laminating composite tape to a substrate 52 or 54 using laminator 56 shown in Figures 5 - 8. Starting at 134, laminator 56 and substrate 52/54 are moved relative to each other along an axis 98 which, in the example shown, is the X axis 98. In 136, one or more ribbon control modules 80 are moved along a beam 76 in laminator 56 and in 138, the tape control module 80 is used to laminate at least one strip of tape on the substrate 52/54. In 140, the lamination direction is changed by changing the angular orientation of beam 76 relative to the X 98 axis, articulating beam 76 around a Z axis 98. After each layer has been laminated on the substrate 52/54 in steps 134 - 140, the height of the substrate 52/54 relative to the ribbon control modules 80 and thus the distance between them can be adjusted along the Z axis 98 to compensate for the thickness of the just laid layer. This adjustment can be performed by adjusting the elevation of the table 54 shown in Figures 3 and 4.
[00082] Attention is now directed to Figures 15 and 16 which illustrate additional details of the zero grade laminator 58 shown in Figures 1, 3 and 4. The laminator 56 includes a gantry 57 comprising a pair of supports 62, 64 , respectively, on opposite sides of the table 54 and a beam 60 that extends through the table 54 and is retained by the support 62, 64. The beam 60 is connected to the supports 62, 64 by the spaced pivoting bearings 150, 152 similar to the pivoting bearings 118, 120 previously discussed in connection with Figures 9 and 10. Although not shown in the drawings, the pivot bearing 152 may include a slide assembly similar to that used in the pivot and slide bearing 120 shown in Figure 10 that allows the pivot bearing 152 to slide linearly. Pivoting bearings 150, 152 allow beam 60 to change its angular orientation in relation to the X axis 98. This change in angular orientation can be effected by moving one of the supports 62, 64 relative to another support 62, 64 along the X axis 98 A pair of rolling heads 66 is mounted on rails 148 for movement along the length of beam 66. Each rolling head 66 includes a plurality of ribbon control modules 68 which will be described in more detail below. In other embodiments, laminator 58 may include more than three rolling heads 66 or just a single rolling head 66.
[00083] The tape control modules 68 can seat the strips of composite tape in the edge-to-edge relationship continuously or discontinuously along the length of the part tray 52, in the direction of the X-98 axis. shown in Figure 17, since the angular orientation of beam 60 can be changed, it is possible to vary the alpha angular orientation of tape strips 155 in relation to the X axis 98. In some embodiments, the angular orientation of beam 60 can be changed in a relatively small amount such that the alpha angle of the tape strokes 155 is between approximately 0 and 5 degrees. However, in other embodiments, depending on the layer scale specified for a particular piece tray 52, beam 60 can be rotated to angular orientations such that the alpha angle of the ribbon strips 155 is greater than 5 degrees and up to approximately 45 degrees. The strokes of tapes laminated by laminator 58 along the length of the part tray 52 having alpha orientation angles between approximately 5 and 45 degrees can provide the part with additional cross-layer stiffness which can reduce the number of cross-layers required that are laminated by the non-zero grade laminator 56 and / or can improve part performance. The laminator 56 may further include ultrasonic grinding heads 142 for grinding the trays into networked parts, and a process inspection apparatus in process 144 for measuring the gaps between adjacent courses of the laminated tape. Grinding the part tray to a mesh format using the rectifier heads 142 is advantageous since it can eliminate the need for machining the part tray after it is cured and can allow the part to be co-cured rather than co-linked with other parts. Although not shown in the drawings, the alpha angular orientation of tape strips 155 can be changed by mounting laminating heads 66 on beam 60 for rotation about the Z axis 98.
[00084] Attention is now directed to Figures 18, 19 and 20 which illustrate the additional details of one of the ribbon control modules 68 employed in laminator 56 shown in Figures 15 and 16. A ribbon source set comprises a unidirectional ribbon coil 172 and may include appropriate active tension and braking mechanisms (not shown) for ribbon feeding. A ribbon feed assembly 162 stretches the ribbon from the source assembly 160 and feeds it to a cutter assembly 166. The cutter assembly 166 includes a synchronized cutter drive system comprising a pair of synchronized servo motors 182, 184 mounted in housing 188. Servo motors 182, 184, respectively, drive a cutter rotor 190 and an anvil rotor 192 are pivoted for rotation in housing 188. Cutter rotor 190 and anvil rotor 190 together form a jaw 197 (Figures 18 and 21) for which the tape is fed and cut between a cutting blade 200 and anvil surface 195 on anvil rotor 192.
[00085] An add / compact set 179 includes gripping rollers (Figure 18) 176 and rails 186 that guide the reel tape 172 to a compaction roller 178 that compresses the cut piece of tape 156 against a substrate 54 (Figure 18) . A pickup assembly 168 captures a paper liner (not shown) removed from tape 156 before tape 156 is fed to compaction roller 178 and rolls the paper liner against take-up reel 180. A lifter assembly 164 raises and lowers sets 160 , 162, 179 and 186 and controls the compaction force applied to the tape 156 by the compaction roller.
[00086] Figure 21 illustrates an embodiment of the cutter rotor 190 and the anvil rotor 192 employed in the ribbon control module 160 shown in Figures 18 - 20. The cutter rotor 190 includes an elongated cutting blade 200 mounted on the body of the rotor 194. A pair of bearings 196 at opposite ends of rotor body 194 mount roller 190 for rotation in housing 188 in Figure 20. An axle 198 coupled to rotor body 194 is connected to servomotor 182. The cutter rotor 190 and the anvil rotor 192 are positioned to form a jaw 197 to which the tape 156 is fed. The anvil rotor 192 includes an anvil body 192 provided with mounting bearings 192 and an external anvil surface 195 against which the blade 200 cuts the tape 156. The servo motors 182, 184 shown in Figures 19 and 20 are synchronized to drive the cutter and anvil rotors 190, 192, each at substantially the same speed.
[00087] Figures 22 and 23 illustrate a typical composite layer 206 formed of multiple substantially parallel zero degree strokes 208. The synchronization of the cutter and anvil speed described above allows the tape 156 to enter the cutter assembly 166 (Figure 20) to be successively cut into short segments of strip 208a seated in end-to-end contact without substantial gaps between them, to form discontinuous strips 208. The number 210 indicates an area 210 of layer 206 where each of the strokes 208 is discontinuous and comprises multiple segments 208a separated by cuts 212. As best seen in Figure 23, the stripping tap segments 208a in each stroke 208 is substantially continuous with each other with little or no gap between them. The use of multiple cuts in ribbon strokes 208 with little or no play can assist in reducing or eliminating groove in layer 208 during forming. Although only one section 210 of layer 208 is shown to have multiple cuts 212, tape strokes 208 having multiple cuts 212 can be formed in any area of layer 206 or be extended end to end one or more or all strokes 208 of the layer 206.
[00088] Figure 24 illustrates a method of laminating composite tape using tape control module 160 shown in Figures 18-20. Starting at 214, the ribbon laminating head 66 is moved over substrate 54 and at 216, the ribbon is fed to the compaction roller 178 of one or ribbon control modules 160 forming part of the laminating head 66. In 218, a blade 200 and anvil 192 are rotated at substantially the same speed and at 220, the cutting blade 200 and anvil 192 are used to cut the tape in batches or segments 208a. In 222, the discontinuous strips of tape or segments 208a are compacted on the substrate 54. Finally, after a layer has been laminated on the substrate 54 in steps 214-222, the height of the substrate 54 relative to the rolling head 66, and so on. distance between them, can be adjusted along the Z 98 axis to compensate for the thickness of the tray. This adjustment can be accomplished by adjusting the elevation of the table 54 shown in Figures 3 and 4.
[00089] Attention is then directed to Figures 25 and 26 which illustrate portions of one of the ribbon control modules 80 used in the rolling heads 78 (Figures 1, 5-12). A tape / cutter add-on assembly 226 is mounted by sleeves 232 on a subframe 230 for pivoting movement around an axis 234 that extends normal to the direction of travel (not shown) of the rolling head 78. The subframe 230 is mounted for linear up and down movement on a main frame 224 by means of a sliding assembly 228. The pivoting assembly 226 includes a reciprocating guillotine-type cutting blade 238 located substantially in the center of the assembly 226 that cuts the ribbon (no shown) passing over an anvil 250. The rollers 242 hold the blade 238 in position against the anvil 250 during a ribbon cut. The tape / addition / cutter assembly 226 positions the end of the tape consistently and accurately. As will be discussed in more detail later, the cutting blade 238 can be rotated by an actuator 240 to any of a plurality of cutting positions to obtain cutting of angled strips, such as those previously described in connection with Figure 13.
[00090] With particular reference to Figure 26, the composite tape from a tape source (not shown) on the tape control module 80 is fed through a guide 244 and through a roller 246 to the tape add / cutter 226 in which it is cut by blade 238 and then compacted against a substrate (not shown) by a compaction roller 236 in subframe 230. During a ribbon cut, pivot assembly 226 pivots about axis 234 when the blade 238 passes through the tape and separates it against the anvil 250.
[00091] Figure 28 diagrammatically illustrates a cut of tape manufactured "in motion" by the pivoting assembly 226. During the cut, blade 238 and anvil 250 move with each other through an arc 252, from the position shown in 256 to the position shown in 258. At 256, blade 238 moves downwardly 254 and initially engages tape 156. As blade 238 and anvil 250 continue to move along arc 252, blade 238 moves across the tape 156 and pass the anvil 250 until the tape is separated into 258. Thus, the blade 238 moves along with the anvil 250 well with the tape 156 during a cut until the cut is complete. As a result of this simultaneous movement of the blade 238 and the tape 156 during a "moving" cut, the voltage spikes in the tape 156 can be reduced, which can assist in smoothly feeding the tape to the compaction roller 236 and reducing the possibility of the tape rising from the substrate following the compaction.
[00092] Figure 28 illustrates the steps of a method of laminating composite tape against a substrate 54 using laminating head 78 of the type employing the pivoting cutter assembly 226 shown in Figures 25 and 26. Starting in 270, the tape laminating head 78 is moved over the substrate and in 272, the tape is fed to a compaction roller 236. In 274, a blade 238 is used to cut pieces of tape when the head 78 continues to move. Blade 238 is moved along with the tape during a cut. In 276, the cut piece of the tape is compacted on the substrate 54.
[00093] With reference, after Figure 29, as previously discussed in connection with Figure 13, a laminating head 78 employing ribbon control modules 80 of the type shown in Figures 26 and 27 can be used to laminate the ribbon strokes non-zero 132 on a substrate 54 in which the ends 85 of the ribbon course 132 are angled cut, substantially parallel to the edges 52a of the substrate 52. By cutting the ends 85 of the ribbon 132 substantially parallel to the edges of the substrate 52a, more than normal at the longitudinal edges 135 of tape 132, a worn tape area indicated by the cross hatched area 132a is removed. These angular tape cuts are made by rotating the cutting blade 238 in such a way that it is substantially parallel to the edges of the substrate 52a.
[00094] Figure 30 illustrates a method of laminating non-zero ribbon strokes on a substrate 54 using angled ribbon cuts shown in Figure 29. Starting at 280, a laminator head 78 is moved over a substrate 54 at an angle 137 (Figure 29) oblique to an edge 52a of the substrate 54. At 282, the pieces of tape 132 are cut when the head 78 moves over the substrate 54; the tape 132 is cut substantially parallel to the substrate edge 32a. At 284, the cut tape 132 is compacted on the substrate 54.
[00095] Figures 31, 32 and 33 illustrate additional details of pivot addition / cutter assembly 226 previously discussed in connection with Figures 25 and 26 and particularly aspects that allow angular tape cuts to be made as described above. The cutter assembly 226 includes a rotor assembly 245 comprising a cylinder 248 having a bearing 314 rotatable within a housing 288. The cylinder 248 includes a top of the cylinder 290 that rotates with the cylinder 248. A reciprocating piston 300 within the cylinder 248 is attached to the upper end of blade 238. Blade 238 may have an appropriate non-stick coating (not shown) such as titanium nitride or a PVD (physical vapor deposition) to prevent the blade from sticking to the tape resin during cuts . The anvil 250, together with a tape holder 286, are connected by an anvil arm 304 to cylinder 248 and thus can be rotated together with cylinder 248 into housing 288. A blade lock 308 secures blade 238 to piston 300 and can be released to allow removal and replacement of the blade from the bottom of assembly 226. A foam pad 298 can be provided between piston 300 and the top of cylinder 290 to cushion the movement of piston 300 when it reaches its upper end of movement.
[00096] The piston 300 and thus the reciprocating movement of the blade 238 are triggered by the pressurized air that enters the cutter assembly 226 through the air inlet orifice 296. As best seen in Figure 33, the air that enters the inlet orifice 296 it passes through a coil valve 308 controlled by an electrical voice coil 294. The pressurized air allowed to pass through valves 308 during a cutting cycle enters valve holes 310 and the top of cylinder 290 to cylinder 248. Multiple pairs of valve orifices 310 are provided, which respectively connect valve 308 with cylinder 248, depending on the rotational position of cylinder 248 and blade 238. Pressurized air entering cylinder 248 forces piston 300 and thus blade 238 down to cut a piece of thread against the anvil 250. The voice coil 294 is exceptionally fast acting and causes the coil valve 308 to be actuated and retracted at high speeds that facilitate quick cutting strokes by blade 238.
[00097] Figures 34 and 35 illustrate the mechanical connection between the three position linear actuator 240 shown in Figures 25 and 26 and the top of the cylinder 290. In the illustrated example, the linear actuator is a pneumatically operated three position cylinder, however , other forms of actuators are possible. The three-position actuator 240 linearly moves an output shaft 240a to any of the three linear positions. The output shaft 240a is pivotally connected to the top of cylinder 290 and rotates the top of cylinder 290 together with cylinder 248, blade 238 and anvil 250 to any desired number of rotational positions which, in the illustrated embodiment, comprise positions of 45, 90 and 135 degrees relative to the direction of travel of the ribbon control module 80. Figures 36, 37 and 38, respectively, illustrate blade rotation 238 to cut positions of 45, 135 and 90 degrees.
[00098] Figure 39 is a functional block diagram showing the control components of the device 50. As previously indicated, the controller 86 can comprise a PC, PLC or other electronic controller device and works to control a series of pneumatic and electrical controls on each of the laminators 56, 58 and table elevation control 53. Elements of the first laminator 56 controlled by controller 86 include the cutter driver 322, ribbon control module functions 324, ribbon control module linear motors 115, beam spacing and ribbon control module spacing actuators 82, 84, respectively, and gantry driver motors 102. Controller 86 operates gantry frame driver 102 to incrementally advance gantry 59 and thus the grouped beams 76, to the following rolling position, as described in connection with Figure 13. When the gantry frame driver changes the rolling annulus of the beams 76 by displacement of the frame supports 72, 74 in relation to each other, the controller 86 sends the control signals to the linear drive motors of the ribbon control module 115 which realigns the modules 80 in relation to each other along of the beams 76, in such a way that the modules 80 can simultaneously begin to settle the tape along a starting edge of the substrate 54 (for example, edge 52a in Figure 13).
[00099] In the case of laminator 58, controller 86 controls the gantry motion trigger 318, blade rotor motor 182, anvil rotor motor 184 and ribbon module control functions 320 which include, for example, without limitation, addition and cutting functions as well as compaction pressure. Controller 86 can also control the operation of one or more grinding heads 53 in laminator 58 which can be used to cut part tray 52 to a network shape. The speeds of the servo motors 182, 184 are synchronized by the controller 86, as previously discussed. The gantry driver 318 may include, for example and without limitation, wheel motors (not shown) that drive the gantry 57 (Figures 15 and 16) along the extension of the table 54, as well as motors (not shown) that drive the rolling heads 66 through gantry beam 60.
[000100] Embodiments of the invention can find use in a variety of potential applications, particularly in the transportation industry, including for example, aerospace, marine, automotive and other applications where automated seating equipment can be used. Thus, with reference below to Figures 40 and 41, embodiments of the invention can be used in the context of an aircraft manufacture and service method 326 as shown in FIG. 40 and an aircraft 328 as shown in Figure 41. Aircraft applications of the reported embodiments may include, for example, without limitation, seating of reinforcing members such as, without limitation, reinforcements and stringers. During pre-production, exemplary method 326 may include specification and design 330 for aircraft 328 and procurement of material 332. During production, component and subassembly manufacturing 334 and system integration 336 for aircraft 328 takes place. Next, aircraft 328 can proceed through certification and shipping 338 in order to be put into service 340. Although in service by a customer, aircraft 328 is scheduled for routine maintenance and service 342, which may also include modification, reconfiguration , repolling, etc.
[000101] Each of the method 326 processes can be performed or performed by a systems integrator, a third party, and / or an operator (for example, a customer). For the purposes of this description, a system integrator may include, without limitation, any number of aircraft manufacturers and subcontractors to the main system; a third party may include, without limitation, any number of vendors, subcontractors, and suppliers; and an operator can be an airline, leasing company, military entity, service organization, etc.
[000102] As shown in Figure 41, aircraft 328 produced by exemplary method 326 can include an aviation structure 344 with a plurality of systems 346 and an interior 348. Examples of high-level systems 346 include one or more of a flight system propulsion 350, an electrical system 352, a hydraulic system 354 and an environmental system 356. Any number of other systems can be included. Although an aerospace example is shown, the principles of the invention can be applied to other industries such as marine and automotive industries.
[000103] The Systems and methods realized here can be employed during any one or more of the production stages and service method 326. For example, component or subsets corresponding to the 334 production process can be manufactured or manufactured in a manner similar to the components or subsets produced while the 328 aircraft is in service. Also, one or more embodiments of the apparatus, embodiments of the method or a combination thereof can be used during production stages 334 and 336, for example, by substantially expediting assembly or reducing the cost of a 328 aircraft. Similarly, one or more embodiments of the apparatus, embodiments of the method or a combination thereof may be used while aircraft 138 is in service, for example and without limitation for maintenance and service 342.
[000104] The description of the different advantageous embodiments has been presented for purposes of illustration and description and is not intended to be exhaustive or limited to the embodiments in the disclosed form. Many modifications and variations will be made evident to those skilled in the art. In addition, different advantageous embodiments can provide different advantages when comparing the other advantageous embodiments. The embodiment or embodiments are selected and described in order to better explain the principles of the embodiments, the practical application and to enable others skilled in the art to understand the invention for various embodiments with various modifications that are appropriate to the particular intended use.

权利要求:
Claims (7)
[0001]
1. Apparatus (50) for laminating composite tape on a substrate (54), characterized by comprising: a laminator (56) movable in relation to the substrate (54) along a first axis, the laminator (56) including first and second spaced supports (62, 64) and a beam (60) extending through the substrate (54) along a second axis; pivoting connections between the beam (60) and each of the supports (62, 64) to allow a change in angular orientation of the beam (60) with respect to the first axis; and at least one tape laminating head (66) on the beam (60) for laminating the composite tape to the substrate (54).
[0002]
Apparatus (50) according to claim 1, characterized in that the laminator (56) includes a plurality of beams (60) and a tape laminating head (66) in each of the beams (60) to laminate the composite tape on the substrate (54), and the apparatus (50) further comprises: a plurality of pivoting connections between each of the beams (60) and the supports (62, 64) to allow a change in the angular orientation of each of the beams (60) in relation to the first axis.
[0003]
Apparatus (50) according to claim 1 or 2, characterized in that the supports (62, 64) are movable independently of each other in a direction substantially parallel to the first axis.
[0004]
Apparatus (50) according to any one of the preceding claims, characterized in that it also comprises a sliding connection between the beam (60) and one of the supports (62, 64) to allow the beam (60) to slide in relation to a support.
[0005]
Apparatus (50) according to any one of the preceding claims, characterized in that the tape laminating head (66) includes: a plurality of carts (108) mounted for substantially parallel movement along the beam (60); at least one tape control module (80) on each of the carts (108) to seat a strip (132) of composite tape on the substrate (54); and means for aligning the at least one ribbon control module (80) on one of the carts (108) with respect to at least one ribbon control module (80) on the other one of the carts (108) when the angular orientation of the beam (60) is changed.
[0006]
6. Method of laminating composite tape to a substrate (54) used by the apparatus as defined in any one of claims 1 to 5, characterized in that it comprises: relatively moving a tape laminator (56) and the substrate (54) over a axle; moving a ribbon control module (80) along a beam (60) in the laminator (56); using the tape control module (80) to laminate at least one strip (132) of composite tape onto the substrate (54); and changing the angular orientation of the beam (60) with respect to the axis by moving relatively two supports (62, 64), respectively, at the ends (104) of the beam (60), so that the beam is pivoted.
[0007]
7. Method according to claim 6, characterized in that the change in the angular orientation of the beam (60) in relation to the axis includes linear sliding of the beam (60) in relation to one of the supports (62, 64) and the The method further comprises: changing the starting position of the ribbon control module (80) based on the change in the angular orientation of the beam (60).

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法律状态:
2018-04-03| B06F| Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]|

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2019-10-15| B06U| Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]|

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2020-05-26| B06A| Patent application procedure suspended [chapter 6.1 patent gazette]|

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2020-12-01| B09A| Decision: intention to grant [chapter 9.1 patent gazette]|

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2021-02-09| B16A| Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]|Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 03/07/2012, OBSERVADAS AS CONDICOES LEGAIS. |

优先权:

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申请号 | 申请日 | 专利标题

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US13/198,418|US8808490B2|2011-08-04|2011-08-04|Methods for laminating composites|

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US13/198,418|2011-08-04|

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PCT/US2012/045369|WO2013019356A1|2011-08-04|2012-07-03|Method and apparatus for laminating composites|

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