Method and apparatus for producing composite structures

Information

  • Patent Grant
  • 8986482
  • Patent Number
    8,986,482
  • Date Filed
    Monday, July 6, 2009
    14 years ago
  • Date Issued
    Tuesday, March 24, 2015
    9 years ago
Abstract
A composite part is formed by a composite tape application machine that lays up a plurality of tapes on a substrate. The lateral position of the tapes may be adjusted as the tapes are being laid up.
Description
TECHNICAL FIELD

This disclosure generally relates to automated machines and methods for laying up composite tape.


BACKGROUND

Composite structures such as those used in the automotive, marine, and aerospace industries may be fabricated using automated composite material application machines, commonly referred to as automated fiber placement (AFP) machines. AFP machines may be used in the aircraft industry, for example, to fabricate structural shapes and skin assemblies by laying up relatively narrow strips of composite tape or “tows,” collimated into a wider band, on a manufacturing tool. The AFP machine aligns and places a plurality of tape strips, typically six or more, in continuous edge-to-edge contact forming a single conformal band which is placed on and compacted against the tool.


In order to fabricate large complex laminated assemblies, current AFP machines using fiber placement heads may have a relatively high degree of operational flexibility. For example, current placement heads may have the ability to add, drop-off, or cut any or all of the contiguous tape strips independently of all others by providing separate, independently controllable cutters for each tape strip.


While both highly flexible and efficient, current AFP machines may have limitations in terms of their productivity. For example, current AFP machines employ a single head having multiple tape supplies that lay down aligned tape courses edge-to-edge to form a single bandwidth. In those applications where head speed has been optimized, additional increases in productivity, i.e., the amount of tape laid down per unit time, may require the provision of additional tape supplies on the head in order to increase the bandwidth. Adding tape supplies not only result in a larger and more complicated head, but may limit flexibility in some applications due, for example, to difficulties in steering a larger head.


Accordingly, there is a continuing need for improved methods and apparatus that increase the laydown rate of composite tape.


SUMMARY

According to a number of disclosed embodiments, a method is provided of laying tape to form a composite part. The method comprises adjusting the lateral position of at least one tape control module in a plurality of the tape control modules as tape is being laid by the modules. Adjusting the lateral position of the tape control module is performed such that the distance between adjacent tapes is altered, the lateral position being substantially orthogonally oriented to a direction of travel of the plurality of tape control modules. Adjusting the lateral position of the tape control module may be performed automatically according to a preprogrammed set of instructions.


According a number of other embodiments, a method is provided of forming a composite part by laying up a plurality of composite tapes. The lateral position of at least one of the tapes is automatically adjusted and the tapes are aggregated into a bandwidth of tape during lay-up. Automatically adjustment of the lateral position is performed using a programmed control system. The adjusting step may comprise adjusting the lateral position of two adjacent tapes.


According to still other embodiments, a method is provided of applying bands of composite tape over a substrate. The method includes moving a tape application head over the substrate and laying down multiple courses of composite tape on the substrate from positions on the head that are staggered in the direction of travel of the head. The lateral positions of at least certain of the courses are adjusted as the head is moving over the substrate. Adjusting the lateral positions of the courses is performed automatically according to a set of pre-programmed instructions, and by adjusting the lateral positions of tape control modules on the tape application head.


According to other embodiments, a tape layup machine is provided for forming a composite part. The machine comprises a plurality of tape control modules for laying up tape, and means coupled with the modules for adjusting the lateral position of at least certain of the modules. The machine further comprises a control system and a program used by the control system to adjust the lateral position of the at least certain modules as tape is being laid up by the modules.


According to another embodiment, a tape application machine is provided for laying up composite tape on a substrate. The machine comprises a head movable over the substrate in a direction of travel, and a carrier mounted on the head. A plurality of tape control modules are mounted on the carrier for laying up courses of tape on the substrate. A motor is mounted on the head, and a drive coupled between the motor and the modules is operable for adjusting the lateral position of at least certain of the modules on the head.


Other features and advantages of the present invention will become apparent to those skilled in the art from a consideration of the following detailed description taken in conjunction with the accompanying drawings.





DESCRIPTION OF THE ILLUSTRATIONS


FIG. 1 is an illustration of an overall block diagram of a system for producing composite laminates.



FIG. 2 is an illustration of a perspective view of a pair of tape application heads mounted on an automatically controlled gantry.



FIG. 3 is an illustration of a functional block diagram of a system for producing laminates using a gantry of the type shown in FIG. 2.



FIG. 4 is an illustration of a functional block diagram showing the relationship between a tape control module and other components of the application head.



FIG. 5 is an illustration of a perspective view of a set of tape control modules, including an alternate form of a tape control module for laying down a band of narrow tape strips.



FIG. 6 is an illustration of a plan view of tape courses forming a single band, and showing the offset between the staggered groups of tape control modules.



FIG. 7 is an illustration similar to FIG. 6 but showing the addition of a tape module laying down a band formed from narrow strips of tape.



FIG. 8 is an illustration of a perspective view of a tape application head having staggered tape control modules.



FIG. 9 is an illustration of a plan view showing tape courses laid down by an application head having sixteen tape control modules.



FIG. 10 is an illustration of a front view of three tape control modules which may form part of the tape application head illustrated in FIG. 8.



FIG. 11 is an illustration of a block diagram of a system for adjusting the lateral positions of the tape control modules.



FIG. 12 is an illustration of a flow chart showing the steps of a method of laying up composite tape.





DETAILED DESCRIPTION

Referring particularly to FIGS. 1 and 2 of the drawings, a number of embodiments relate to an apparatus generally indicated by numeral 50 for producing composite components or structures, for example, a laminate structure 57, by applying bands 87 of composite tape 86 over a tool 59 or other substrate. In many embodiments, the composite fabrication apparatus 50 may be configured to produce composite structures, also sometimes referred to herein as a “part” 57, by adjusting tape position in response to a contour (not shown) of a part 57 being fabricated.


The apparatus 50 may include one or more tape application heads 58, each of which includes at least first and second groups of tape control modules 60a, 60b. Each of the application heads 58 is mounted on a manipulator 52 capable of moving the corresponding head 58 along one or more axes in order to guide the direction in which the bands of tape are applied. The manipulator 52 may be mounted on a machine tool system 54 for movement along multiple axes, which may comprise any of various known systems commonly used to displace tools along multiple axes. The manipulators 52, machine tool system 54 and application heads 58 may be controlled by one or more control systems 56 which may comprise, for example and without limitation, NC or CNC controllers.


Referring particularly now to FIG. 2, the apparatus 50 may comprise, for example and without limitation, a gantry system 55 comprising a gantry beam 62 having its opposite ends mounted on elevated rails 68 for linear movement thereon. The gantry beam 62 may include motors 70 provided with geared drives (not shown) for powering the gantry beam 62 along the rails 68. One or more manipulators 52 may be operatively and movably mounted on the gantry beam 62, with each manipulator 52 being provided a tape application head 58. In the example illustrated in FIG. 2, two manipulators 52 and heads 58 are mounted on opposite sides of a single gantry beam 62. The manipulator(s) 52 may be powered by motors (not shown) that drive the manipulator 52 along the gantry beam 62. Various electrical and other lines and cables (not shown) may be enclosed within conduits (not shown) in order to connect the motors, the manipulators 52, and the application heads 58 to the control system 56 of FIG. 1 and/or to other systems (not shown).


Attention is now directed to FIG. 3 which illustrates in block diagram form additional components of the apparatus 50. In many embodiments, the application head 58 may broadly include a material delivery system 58a and a tape alignment and application head 58b. The material delivery system 58a delivers tape or slit tape known as tows to the tape alignment and application head 58b, which applies the slit tape to a substrate, thereby forming a laminate bandwidth 74. As used herein, “composite fiber tape,” “fiber tape,” “tape,” and “tape strips” are intended to include a wide range of tapes and tows of various widths. Composite tape is supplied to the material delivery system 58a from a suitable raw material supply 76. As previously mentioned, the operations of the gantry system 54a and the tape alignment and application head 58b are controlled by the control systems 56 (FIG. 1).


Additional details are the tape alignment and application head 58b are shown in FIG. 4. Each of the tape alignment and application heads 58b may include a plurality of tape control modules 84 which output a tape course 86 (see FIG. 6) onto a substrate (not shown). As will be described later in more detail, each of the tape control modules 84 may be removably mounted on the tape alignment and application head 58b, allowing quick change out of the modules 84. Each of the modules 84 may be coupled to suitable power, control and sensor connections 94 by any suitable means. Each of the tape control modules 84 may also be connected by a coupling 96 to a rethread drive 88 or independent servo drive which functions to rethread the module 84 with tape supplied by the material delivery system 58a. Examples of tape control modules 84 may be found in U.S. Pat. No. 4,699,683 and U.S. Patent Publication No. 2007/0029030A1, the entire contents of both of which are incorporated by reference herein.


Referring now to FIGS. 5, 6, and 7, as will be described later in more detail, in accordance with the disclosed embodiments, the tape control modules 84 are arranged in two alternating groups 84a, 84b that are staggered or offset in the direction of travel 110 of the application head 58 (see FIG. 2). As shown in FIG. 5, the modules 84 in group 84a are substantially aligned along a first axis 121 that extends in a direction 126 transverse to the direction of travel 110, while the modules 84 in group 84b are substantially aligned along a second axis 123 that extends substantially parallel to the first axis 121. As a result of this alignment and the offset relationship between the two groups of modules 84, as best seen in FIG. 6, the centerlines “A” and “B” of the compaction rollers 112a, 112b associated with the corresponding modules 84a, 84b are separated by a distance “d” in the direction of travel 110. The amount of offset or staggering (distance “d”) between adjacent tape control modules 84 may be automatically adjusted by the previously discussed control system 56 (FIG. 1) using pre-programmed values.


The groups of modules 84a, 84b may apply courses of tape 86a, 86b in substantially edge-to-edge alignment to form a tape band 87 (FIG. 7) having a bandwidth “W”. As a result of staggering the groups 84a, 84b of tape control modules 84, an advanced number 86a of the tape courses are laid up spatially advanced from a trailing number 86b of tape courses, and a bandwidth 87 of the tapes is laid up as an aggregate of the plurality of tape courses 86 at a trailing edge 119 of the trailing number of tape courses 86.



FIG. 7 illustrates an alternate embodiment wherein one or more tape control modules 84c (FIG. 5) may be mounted on the tape alignment and application head 58b, aligned with either module group 84a, 84b. The tape control module 84c applies a bandwidth 114 of tape segments 116 each having a width less than the tape courses 86a, 86b. The narrower, individual tape segments 116 allow a higher resolution profile 117 to be achieved on either end of the tape band 87.


Attention is now directed to FIG. 8 which illustrates an alternate form of the tape application head 58 wherein the distance between the centerlines 125 of two or more of the tape control modules 84, also referred to as “pitch”, may be adjusted to control the aggregate bandwidth and thus aid in “steering” of the tape courses 86 or for other purposes. In the illustrated embodiment, the application head 58 includes two groups 84a, 84b of tape control modules 84 that are staggered in the direction of travel 110 of the head 58 and respectively apply tape courses 86a, 86b, similar to the groups 84a, 84b of tape control modules 84 shown in FIG. 5. The application head 58 may include a suitable tape module adjustment system 120 connected to one or more of the tape control modules 84 that may be controlled and operated by the control system 56 (FIG. 1). As will be discussed below, the tape module adjustment system 120 may comprise any of various known mechanical and/or electromechanical devices and/or assemblies that function to laterally displace one or more of the tape control modules 84 in a transverse direction 126, thereby adjusting the transverse position of one or more of the tape courses 86, wherein the transverse direction 126 is substantially orthogonal to the direction of travel 110 of the application head 58. Lateral displacement of one or more of the tape control modules 84 correspondingly alters the lateral position of the tape courses 86a, 86b. In one of several embodiments, the groups 84a, 84b of tape control modules 84 are automatically laterally adjustable relative to each other by the adjustment mechanism 120 based on a set of pre-programmed instructions forming part of the control system 56 (FIG. 1), while in other embodiments, the tape control modules 84 in either or both of the groups 84a, 84b may be separately laterally adjustable. The pitch between the tape modules 84 may be automatically adjusted prior to a bandwidth 87 being laid down, and/or may be dynamically adjusted “on-the-fly” as a bandwidth 87 is being laid down.


As discussed above, the automated adjustability of the lateral position of the tape control modules 84 allows relatively precise control over the lateral positions of the corresponding tape courses 86a, 86b in each band 87. For example as shown in FIG. 9, automated adjustment of the pitch between the tape modules 84 may be carried out in order to adjust the distance between the centerlines 127 of adjacent tape courses 86a, 86b such that the edges of the tape courses 86a 86b are essentially contiguous. Automated control of the lateral positions of adjacent tape courses 86a, 86b through dynamic adjustment of the pitch between the tape modules 84 may improve the ability to “steer” the band 87, particularly over surfaces having complex contours. Thus, the lateral or transverse positions of the tape control modules 84 may be adjusted to adapt to a contour of a part 57 being laid up, or for a variety of other purposes. The compression force applied by the tape control modules 84 through the compaction rollers 112 may be preset, while in other embodiments the pressure may adjusted based on one or more contours of the substrate where tape courses 86 are being laid down.



FIG. 10 illustrates the directions in which the tape control modules 84 may be automatically and independently adjusted. A tape control module 84b forming part of a first group 84b is axially offset or staggered relative to two tape control modules 84a forming part of a second group 84a. The modules 84a are laterally adjustable in either direction (X, −X) along a first common X axis 122 while the module 84b is laterally displaceable in either direction (XX, −XX) along an XX axis 124 that is offset from the X axis 122 in the direction of travel 110 of the tape application head 58 (FIG. 8). As mentioned above, the tape control modules 84 may be laterally adjusted, dynamically, on-the-fly as the tape courses 86 are being applied in order to aid in steering the applied tape band 87 (FIG. 5) and/or to cover complex substrate shapes and/or contours.


Attention is now directed to FIG. 11 which illustrates further details of a system used to automatically adjust the lateral positions of the tape control modules 84. In the illustrated example, two staggered groups 84a, 84b of tape control modules 84 are shown, however, in other embodiments, automated lateral adjustment of the pitch between tape modules 84 may be advantageously employed where only a single group of tape control modules 84 is used.


Each group 84a, 84b of tape control modules 84 is mounted on the head 58 (FIGS. 1 and 2) for lateral adjustment on a corresponding carrier 128a, 128b. Each of the carriers 128a, 128b may comprise, without limitation, any of a variety of known types of mechanical supports, trays, tracks, rails or similar devices that mount and support the tape control modules for lateral movement on the head 58, substantially transverse to the direction of travel 110 (FIG. 5) of the head 58. Each of the tape module adjustment systems 120a, 120b is mounted on the head 58 and comprises a motor 130a, 130b coupled with a corresponding mechanical drive 132a, 132b. Each of the motors 132a, 132b may be, without limitation, pneumatic, hydraulic or electric, such as a stepper or servo motor (not shown). Each of the mechanical drives 132a, 132b may comprise, without limitation, a screw drive, a gear drive, a linkage assembly or any of various other known mechanical drive mechanisms. The motors 130a, 130b may be controlled and operated by the control system 56 or other programmed controller (not shown).


The control system 56, or other controller, controls and adjusts the lateral position of the tape control modules 84 based on a set of programmed instructions forming part of a control program 134. These programmed instructions may be based in part on the geometry and/or ply make-up of the composite structure 57 (FIG. 1) being fabricated. Each of the mechanical drives 132a, 132b is coupled with the tape control modules 84 in the corresponding group 84a, 84b. Each of the adjustment systems 120a, 120b may adjust the lateral position of one or more of the tape control modules 84 in the group 84a, 84b, either individually, or as a group. As mentioned above, the lateral positions of one or more of the tape control modules 84 may be adjusted dynamically as a bandwidth 87 of the tape courses 86 is being laid down.



FIG. 12 shows the steps of a method of laying up composite tape using the technique previously described. At 136, courses of tape 86 are laid up using the tape control modules 84 mentioned above. At 138, the lateral position of at least one of the modules 84 is adjusted as the tape courses are being laid, thereby adjusting the lateral position of at least one of the tape courses 86.


Embodiments of the disclosure may find use in a variety of potential applications, particularly in the transportation industry, including for example, aerospace, marine and automotive applications. Those skilled in the art will understand that the preceding embodiments of the present invention provide the foundation for numerous alternatives and modifications thereto. These other modifications are also within the scope of the present invention. Accordingly, the present invention is not limited to that precisely as shown and described in the present invention.

Claims
  • 1. A method of laying composite tape to form a composite part, the method comprising: moving a gantry carrier in a direction of travel that is substantially linear;applying a first set of tape courses aligned in the direction of travel from a first set of tape control modules on a tool, the first set of tape control modules moveably connected to the gantry carrier;applying a second set of tape courses in the direction of travel from a second set of tape control modules on the tool, the second set of tape control modules moveably connected to the gantry carrier;controlling a position of each tape control module independent of a position of the other tape control modules while applying the plurality of tape courses;adjusting a lateral position of the first set of tape control modules with respect to the second set of tape control modules while tape is being laid by the first set and the second set of tape control modules on the tool, in response to a change in a varied contour of the composite part, so as to maintain the first set of tape courses and the second set of tape courses substantially adjacent to each other in an edge to edge alignment, adjusting the lateral position including moving at least one of the first or second tape control modules on the gantry carrier in a transverse direction with respect to the substantially linear direction of travel of the gantry carrier; andadjusting a compression force applied by the first set of tape control modules and the second set of tape control modules in response to the change in the varied contour of the composite part.
  • 2. The method of claim 1 wherein the adjusting step further comprises adjusting the lateral position of the first set of tape control modules and the second set of tape control modules such that a distance between a course of tape from a module in the first set of tape control modules is altered with respect to a course of tape from a module in the second set of tape control modules, the lateral position being substantially transverse to the direction of travel of the plurality of tape control modules.
  • 3. The method of claim 2 wherein adjusting the lateral position is performed automatically according to a set of programmed instructions.
  • 4. The method of claim 1 further comprising adjusting a stagger of the first set of tape control modules with respect to the second set of tape control modules while adjusting the lateral position, the stagger being substantially in a direction of travel of the first tape control module and the second tape control module.
  • 5. A method of forming a composite part, the method comprising: moving a gantry carrier in a direction of travel that is substantially linear;laying up a first composite tape in the direction of travel, the first composite tape comprising a plurality of substantially evenly spaced tape segments, the first composite tape applied from a first tape control module moveably connected to the gantry carrier;laying up a second composite tape in the direction of travel, the second composite tape comprising a plurality of substantially evenly spaced tape segments, the second composite tape applied from a second tape control module moveably connected to the gantry carrier, and the first composite tape is laid up spatially advanced in the direction of travel with respect to the second composite tape;automatically adjusting a lateral position of the first composite tape with respect to the second composite tape while laying up the first composite tape and the second composite tape, the automatically adjusting a lateral position of the first composite tape being independent of the second composite tape, the adjusting in response to a change in a varied contour of the composite part and so as to maintain the first set of tape courses and the second set of tape courses substantially adjacent to each other in an edge to edge alignment, adjusting the lateral position including moving at least one of the first or second tape control module on the gantry carrier in a transverse direction with respect to the substantially linear direction of travel of the gantry carrier;adjusting a compression force applied to the first composite tape and the second composite tape in response to the change in the varied contour of the composite part; andaggregating the first composite tape and the second composite tape into a bandwidth of tape during lay-up.
  • 6. The method of claim 5 wherein automatically adjusting the lateral position is performed using a programmed control system.
  • 7. The method of claim 6 wherein the adjusting step comprises adjusting the lateral position of the first composite tape and the second composite tape in response to laying the first composite tape and the second composite tape over a complex contour.
  • 8. The method of claim 5 wherein the plurality of tapes are aggregated into the bandwidth of the tapes.
  • 9. The method of claim 5, further comprising a plurality of tapes are laid up advanced with respect to a plurality of trailing tapes respectively include advanced tapes in a direction that is substantially orthogonal to the direction of travel.
  • 10. A method of applying bands of composite tape over a substrate to form a composite part with a complex contour, comprising: moving a gantry carrier in a direction of travel over a surface of the substrate that is substantially linear;moving a tape application head over a complex contour of a substrate in a direction of travel;laying down a first course of composite tape on the complex contour in the direction of travel, the first course of composite tape applied from a first tape control module moveably connected to the gantry carrier;laying down a second course of composite tape on the complex contour in the direction of travel, the second course of composite tape applied from a second tape control module moveably connected to the gantry carrier, and wherein the first composite tape is laid up spatially advanced in the direction of travel with respect to the second composite tape;adjusting a lateral position of the first course of composite tape with respect to the second course of composite tape as the head is moving over the substrate, the adjusting the lateral position of the first course of composite tape being independent of the second course of composite tape, in response to a change in a varied contour of the composite part, so as to maintain the first course and the second course substantially adjacent to each other in an edge to edge alignment, adjusting the lateral position including moving at least one of the first or second tape control module on the gantry carrier in a transverse direction with respect to the substantially linear direction of travel of the gantry carrier, and adjusting the lateral positions of the courses is performed by laterally displacing staggered groups of tape control modules on the tape application head; andadjusting a compression force applied to the first course of composite tape and the second course of composite tape in response to the change in the varied contour of the composite part.
  • 11. The method of claim 10, wherein adjusting the lateral positions of the courses is performed automatically according to a set of programmed instructions.
  • 12. The method of claim 11, wherein adjusting the lateral positions of the courses is performed by adjusting the lateral positions of tape control modules on the tape application head.
  • 13. A tape layup machine for forming a composite part, comprising: a gantry carrier configured to move in a direction of travel that is substantially linear over a surface of the composite part;a first set of tape control modules and a second set of tape control modules for laying up tape in a direction of travel, the first set of tape control modules and the second set of tape control modules moveably connected to the gantry carrier;means coupled with the modules for adjusting a lateral position of at least certain of the modules independently of the other modules, while the certain modules are laying up tape, and the means configured to adjust the lateral position by moving at least one of the first or second tape control modules on the gantry carrier in a transverse direction with respect to the substantially linear direction of travel of the gantry carrier;a control system; and,a program used by the control system to adjust the lateral position of the at least certain modules as tape is being laid up by the modules over a varied surface contour, in response to a change in a varied contour of the composite part, so as to maintain a first course of tape and a second course of tape substantially adjacent to each other in an edge to edge alignment, and to adjust a compression force applied to the at least certain modules in response to the change in the varied contour of the composite part.
  • 14. The machine of claim 13, wherein the tape control modules include first and second groups thereof staggered relative to each other in a direction of travel of the modules.
  • 15. The machine of claim 14 wherein the tape control modules in the first and second staggered groups thereof are alternately arranged in a direction transverse to the direction of travel of the modules.
  • 16. The machine of claim 13, wherein the adjusting means includes: a motor, anda drive coupling the motor with the at least certain modules, anda programmed control system for controlling the operation of the motor.
  • 17. A tape application machine for laying up composite tape on a substrate, comprising: a head movable over the substrate in a direction of travel;a gantry carrier mounted on the head configured to move in a direction of travel that is substantially linear over a surface of the substrate;a plurality of tape control modules mounted on the carrier for laying up courses of tape on the substrate in the direction of travel, the plurality of tape control modules configured to move in a transverse direction with respect to the direction of travel by moving on the gantry carrier;a motor mounted on the head; anda drive coupled between the motor and the modules for adjusting a lateral position of at least one of the plurality of tape control modules on the head, such that a first tape control module is moved in the transverse direction with respect to a second tape control module while the first tape control module and the second tape control module lay down tape on the substrate, in response to a change in a varied contour of the substrate, the first tape control module moved independently of the second tape control module so as to maintain a first course of tape from the first tape control module and a second course of tape from the second tape control module substantially adjacent to each other in an edge to edge alignment, the drive further adjusting a compression force applied by the first set of tape control modules and the second set of tape control modules in response to the change in the varied contour of the substrate.
  • 18. The machine of claim 17, wherein: the plurality of tape control modules are arranged in first and second groups that are staggered relative to each other in the direction of travel of the head.
  • 19. The machine of claim 18, wherein the tape control modules in the first and second groups thereof are alternately arranged in a direction substantially transverse to the direction of travel of the head.
  • 20. The machine of claim 17, further comprising: a control system for controlling the operation of the motor; anda program used by the control system for adjusting the lateral position of the first tape control module and the second tape control module.
  • 21. A method of applying bands of composite tape over a substrate, comprising: moving a gantry carrier in a direction of travel over a surface of the substrate that is substantially linear;moving a tape application head connected to the gantry carrier over the substrate in the direction of travel, the tape application head comprising a first set of tape application modules and a second set of tape application modules, each tape application module configured to apply a course of tape onto the substrate, each course of tape comprising a plurality of tape segments substantially equally spaced, the first set of tape application modules and the second set of tape application modules moveably connected to the gantry carrier;simultaneously applying multiple courses of tape as a band to the substrate from the first set of tape application modules and the second set of tape application modules as the head moves over the substrate;positioning the first set of tape application modules substantially aligned with a first axis and positioning the second set of tape application modules substantially aligned with a second axis, the first and the second axis substantially transverse to the direction of travel, and the first axis and the second axis separated by a distance; andautomatically adjusting the lateral position of the first set of tape application modules as the head moves over the substrate using pre-programmed instructions, the automatically adjusting being independent of the second set of tape application modules in response to a change in a varied contour of the substrate so as to maintain a first course of tape from the first tape control module and a second course of tape from the second tape control module substantially adjacent to each other in an edge to edge alignment, adjusting the lateral position including moving at least one of the first or second tape application modules on the gantry carrier in a transverse direction with respect to the substantially linear direction of travel of the gantry carrier; andadjusting a compression force applied by the first set of tape application modules and the second set of tape application modules in response to the change in the varied contour of the substrate.
  • 22. A machine for applying composite tape over a substrate, comprising: a gantry carrier configured to move in a direction of travel that is substantially linear over a surface of the substrate;a tape application head connected to the gantry carrier and adapted to travel over the substrate;a first and a second group of tape application modules, each module operable for applying a course of composite tape to the substrate the composite tape comprising a plurality tape segments substantially evenly spaced, the first and the second groups of modules being staggered in the direction of travel of the gantry carrier such that the first group of tape application modules substantially aligns along a first axis and the second group of tape application modules substantially aligns along a second axis, the modules in the first group of tape application modules and the second group of tape application modules alternately arranged in side-by-side relationship such that the tape applied by the modules form a substantially continuous band, and wherein alternating courses of the tape are respectively applied by the tape control modules in the first and second groups thereof;means for mounting the first and the second groups of tape application modules for movement relative to each other in a direction substantially traverse to the substantially linear direction of travel of the gantry carrier;a first and a second adjustment system mounted on the head and respectively associated with the first and second groups of modules for adjusting the lateral positions of the modules, such that a transverse spacing between courses of tape may be adjusted, the transverse spacing of each module being independent of the other modules, each of the adjustment systems including a motor and a drive coupling the motor with the respectively associated group of modules for laterally displacing the modules, the first and the second adjustment systems configured to adjust the first and second groups of modules, in response to a change in a varied contour of the substrate, so as to maintain a first course of tape from the first group of modules and a second course of tape from the second group of modules substantially adjacent to each other in an edge to edge alignment;a control system for controlling the operation of each of the adjustment systems; anda program used by the control system for controlling the operation of each of the adjustment systems while a tape application module is applying a course of composite tape and adjusting a compression force applied by the first group of tape control modules and the second group of tape control modules in response to the change in the varied contour of the substrate.
CROSS REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of Provisional U.S. Patent Application No. 61/134,308 filed Jul. 8, 2008, which is incorporated by reference herein in its entirety.

US Referenced Citations (239)
Number Name Date Kind
799374 Gray et al. Sep 1905 A
920776 Pohl May 1909 A
1132837 Eggleston Mar 1915 A
1195554 Bourdin Aug 1916 A
1370339 Midgley Mar 1921 A
1420271 McLane Jun 1922 A
1464632 Wayne Aug 1923 A
1512096 Hopkinson Oct 1924 A
1930733 Tomlin Oct 1933 A
2182358 Sherts et al. Dec 1939 A
2220760 Gates et al. Nov 1940 A
2345541 Scholze, Jr. Mar 1944 A
2722590 Engler Nov 1955 A
2871716 Stade Feb 1959 A
3037898 Zumofen Jun 1962 A
3137452 Winders Jun 1964 A
3329181 Buss et al. Jul 1967 A
3574040 Chitwood et al. Apr 1971 A
3602416 Basche et al. Aug 1971 A
3684278 Takahaski Aug 1972 A
3695977 Kandelaki et al. Oct 1972 A
3775219 Karlson et al. Nov 1973 A
3810805 Goldsworthy May 1974 A
3844822 Boss et al. Oct 1974 A
3910522 Lee et al. Oct 1975 A
3970831 Hegyi Jul 1976 A
3992240 Kuehn, Jr. Nov 1976 A
4091979 Browder May 1978 A
4100004 Moss et al. Jul 1978 A
4133711 August et al. Jan 1979 A
4135447 Barnes et al. Jan 1979 A
4186861 Steinhilber Feb 1980 A
4208238 August et al. Jun 1980 A
4234374 Frank Nov 1980 A
4241884 Lynch Dec 1980 A
4259144 Ballentine Mar 1981 A
4267951 Grant et al. May 1981 A
4285752 Higgins Aug 1981 A
4292108 Weiss et al. Sep 1981 A
4328061 Off et al. May 1982 A
4351688 Weiss et al. Sep 1982 A
4351992 Crouch Sep 1982 A
4382836 Frank May 1983 A
4419170 Blad Dec 1983 A
4432828 Siempelkamp et al. Feb 1984 A
4461669 Dontscheff Jul 1984 A
4462551 Bloch Jul 1984 A
4491493 Eaton Jan 1985 A
4506969 Baker Mar 1985 A
4508584 Charles Apr 1985 A
4531992 Eaton Jul 1985 A
4541886 Marlow et al. Sep 1985 A
4557783 Grone et al. Dec 1985 A
4557790 Wisbey Dec 1985 A
4560433 Frank Dec 1985 A
4569716 Pugh Feb 1986 A
4574029 Murray Mar 1986 A
4588466 Eaton May 1986 A
4591402 Evans et al. May 1986 A
4627886 Grone et al. Dec 1986 A
4636276 Nozaka Jan 1987 A
4680806 Bolza-Schunemann Jul 1987 A
4696707 Lewis et al. Sep 1987 A
4699683 McCowin Oct 1987 A
4706442 Riemenschneider Nov 1987 A
4707212 Hailey et al. Nov 1987 A
4750965 Pippel et al. Jun 1988 A
4781782 Luhman et al. Nov 1988 A
4799981 Stone et al. Jan 1989 A
4842215 Takami Jun 1989 A
4867834 Alenskis et al. Sep 1989 A
4877471 McCowin et al. Oct 1989 A
4878984 Bourrieres Nov 1989 A
4880488 Matsuo et al. Nov 1989 A
4909880 Kittelson et al. Mar 1990 A
4938824 Youngkeit Jul 1990 A
4943338 Wisbey Jul 1990 A
4978417 Grimshaw et al. Dec 1990 A
4990213 Brown et al. Feb 1991 A
5000397 Darrieux Mar 1991 A
5041179 Shinno et al. Aug 1991 A
5045147 Benson et al. Sep 1991 A
5100493 Leclere et al. Mar 1992 A
5110395 Vaniglia May 1992 A
5114519 Grimshaw et al. May 1992 A
5120976 Clayton et al. Jun 1992 A
5148572 Wells et al. Sep 1992 A
5197198 Onozato Mar 1993 A
5200018 Gill et al. Apr 1993 A
5213646 Zsolnay et al. May 1993 A
5249120 Foley Sep 1993 A
5290386 Trudeau Mar 1994 A
5290389 Shupe et al. Mar 1994 A
5294803 Pahr Mar 1994 A
5345399 Collins Sep 1994 A
5397415 Manabe et al. Mar 1995 A
5431749 Messner Jul 1995 A
5448505 Novak Sep 1995 A
5480508 Manabe et al. Jan 1996 A
5482589 Shin et al. Jan 1996 A
5560942 Curry Oct 1996 A
5562788 Kitson et al. Oct 1996 A
5627647 Baan et al. May 1997 A
5645677 Cahuzac et al. Jul 1997 A
5659229 Rajala Aug 1997 A
5698066 Johnson et al. Dec 1997 A
5700347 McCowin Dec 1997 A
5725175 Thundathil Mar 1998 A
5879505 Fujisawa et al. Mar 1999 A
5954917 Jackson et al. Sep 1999 A
6041840 Ogawa Mar 2000 A
6073670 Koury Jun 2000 A
6096164 Benson et al. Aug 2000 A
6100986 Rydningen Aug 2000 A
6112792 Barr et al. Sep 2000 A
6164477 Druckman et al. Dec 2000 A
6215553 Rider et al. Apr 2001 B1
6240333 McGee May 2001 B1
6262814 Furukawa Jul 2001 B1
6312247 Kassuelke et al. Nov 2001 B1
6315235 Breyer et al. Nov 2001 B1
6325568 Druckman et al. Dec 2001 B1
6391436 Xu et al. May 2002 B1
6436528 Kulper et al. Aug 2002 B1
6441905 Tojyo et al. Aug 2002 B1
6451152 Holmes et al. Sep 2002 B1
6459494 Kurokawa et al. Oct 2002 B1
6474389 Steelman et al. Nov 2002 B1
6520234 Anderson et al. Feb 2003 B1
6544367 Fujimoto et al. Apr 2003 B1
6638388 Nagata et al. Oct 2003 B2
6675688 Ostini Jan 2004 B2
6706131 Steelman et al. Mar 2004 B2
6748836 Vivirito et al. Jun 2004 B2
6752190 Boll et al. Jun 2004 B1
6764754 Hunter et al. Jul 2004 B1
6767426 Yamamoto Jul 2004 B1
6773537 Erickson et al. Aug 2004 B2
6799081 Hale et al. Sep 2004 B1
6799619 Holmes et al. Oct 2004 B2
6823342 Wallen et al. Nov 2004 B2
6860957 Sana et al. Mar 2005 B2
6900547 Polk, Jr. et al. May 2005 B2
6966966 Koizumi et al. Nov 2005 B2
6968971 Ely Nov 2005 B2
6979501 Merton Dec 2005 B2
6984429 Thunhorst et al. Jan 2006 B2
7010544 Wallen et al. Mar 2006 B2
7048024 Clark et al. May 2006 B2
7063118 Hauber et al. Jun 2006 B2
7137182 Nelson Nov 2006 B2
7206665 Groppe Apr 2007 B2
7213629 Ledet et al. May 2007 B2
7282107 Johnson et al. Oct 2007 B2
7293590 Martin Nov 2007 B2
7326312 Rust et al. Feb 2008 B1
7337818 Briese et al. Mar 2008 B2
7341086 Nelson et al. Mar 2008 B2
7376480 Hagen et al. May 2008 B2
7407556 Oldani et al. Aug 2008 B2
7419031 Liguore et al. Sep 2008 B2
7455740 Bostanjoglo et al. Nov 2008 B2
7455742 Ledet et al. Nov 2008 B2
7472736 Kisch et al. Jan 2009 B2
7478780 Wilding et al. Jan 2009 B2
7517426 Mano et al. Apr 2009 B2
7527084 Kaczkowski May 2009 B2
7536242 Ledet et al. May 2009 B2
7591294 Wampler et al. Sep 2009 B2
7643970 Drumheller et al. Jan 2010 B2
7681615 McCowin Mar 2010 B2
7717151 Wampler et al. May 2010 B2
7747421 Tang et al. Jun 2010 B2
7748425 Tingley Jul 2010 B2
7766063 Lauder et al. Aug 2010 B2
7769481 Tang et al. Aug 2010 B2
7809454 Hu et al. Oct 2010 B2
7824512 Lauder et al. Nov 2010 B2
7842145 Hogg Nov 2010 B2
7849903 Vaniglia Dec 2010 B2
7867352 Johnson et al. Jan 2011 B2
7922856 Hagman et al. Apr 2011 B2
8029642 Hagman Oct 2011 B2
8147637 Kisch et al. Apr 2012 B2
8156988 Martinez Apr 2012 B2
8205532 DeVlieg et al. Jun 2012 B2
20030015298 Steelman et al. Jan 2003 A1
20030102070 Black et al. Jun 2003 A1
20030145932 Holmes et al. Aug 2003 A1
20040026025 Sana et al. Feb 2004 A1
20040112534 Koizumi et al. Jun 2004 A1
20040226651 Ledet et al. Nov 2004 A1
20050016671 Sharp et al. Jan 2005 A1
20050039842 Clark et al. Feb 2005 A1
20050039843 Johnson et al. Feb 2005 A1
20050194210 Panossian Sep 2005 A1
20050227124 Merton Oct 2005 A1
20050247396 Oldani et al. Nov 2005 A1
20060073309 Hogg Apr 2006 A1
20060090856 Nelson et al. May 2006 A1
20060106507 Ledet et al. May 2006 A1
20060118244 Zaballos et al. Jun 2006 A1
20060147669 Mano et al. Jul 2006 A1
20060162143 Nelson et al. Jul 2006 A1
20060180270 Ledet et al. Aug 2006 A1
20060226651 Griswold et al. Oct 2006 A1
20060260751 Lauder et al. Nov 2006 A1
20070029030 McCowin Feb 2007 A1
20070034340 Kaczkowski Feb 2007 A1
20070039434 DeVlieg et al. Feb 2007 A1
20070044896 Tingley Mar 2007 A1
20070044900 Tingley Mar 2007 A1
20070069080 Rassaian et al. Mar 2007 A1
20070077896 Ho et al. Apr 2007 A1
20070102239 Liguore et al. May 2007 A1
20070106407 Drumheller et al. May 2007 A1
20070106418 Hagen et al. May 2007 A1
20070144676 Tang et al. Jun 2007 A1
20070150087 Tang et al. Jun 2007 A1
20070187024 Johnson et al. Aug 2007 A1
20070234907 Torres Martinez Oct 2007 A1
20080277057 Montgomery et al. Nov 2008 A1
20080282863 McCowin Nov 2008 A1
20080302483 Vaniglia Dec 2008 A1
20090025875 Hagman Jan 2009 A1
20090076638 Hu et al. Mar 2009 A1
20090078361 Kisch et al. Mar 2009 A1
20090079998 Anderson et al. Mar 2009 A1
20090082892 Tang et al. Mar 2009 A1
20090166467 Hagman et al. Jul 2009 A1
20090205767 Lauder et al. Aug 2009 A1
20090211698 McCowin Aug 2009 A1
20090301648 Hogg et al. Dec 2009 A1
20100193103 McCowin Aug 2010 A1
20100224716 McCowin Sep 2010 A1
20100230043 Kisch Sep 2010 A1
20110114265 Hagman et al. May 2011 A1
20110277941 Hagman Nov 2011 A1
20130037649 McCowin Feb 2013 A1
Foreign Referenced Citations (34)
Number Date Country
2505223 Aug 1976 DE
20120792 May 2003 DE
10342658 Apr 2005 DE
1775108 Apr 2007 EP
1804146 Jul 2007 EP
1859917 Nov 2007 EP
1977882 Oct 2008 EP
1992473 Nov 2008 EP
2077246 Jul 2009 EP
2228200 Sep 2010 EP
2228333 Sep 2010 EP
2253005 May 2006 ES
2065566 Jul 1981 GB
05126536 May 1993 JP
07182724 Jul 1995 JP
08327330 Dec 1996 JP
09210665 Aug 1997 JP
2006347121 Dec 2006 JP
1019227 May 1983 SU
WO0196223 Dec 2001 WO
WO-03035380 May 2003 WO
WO2005030458 Apr 2005 WO
2005105641 Nov 2005 WO
2006021601 Mar 2006 WO
WO-2006060270 Jun 2006 WO
WO2006060270 Jun 2006 WO
WO2006101379 Sep 2006 WO
WO2006118692 Nov 2006 WO
WO-2006134422 Dec 2006 WO
WO2009038895 Mar 2009 WO
WO2009038943 Mar 2009 WO
2009049850 Jul 2009 WO
WO2009108517 Sep 2009 WO
2010005996 Jan 2010 WO
Non-Patent Literature Citations (77)
Entry
Machine translation of PCT WO 03/035380, date unknown.
USPTO Notice of Allowance, dated Jul. 9, 2012, regarding U.S. Appl. No. 13/012,617, 36 pages.
USPTO Supplemental Notice of Allowance, dated Jul. 31, 2012, regarding U.S. Appl. No. 12/400,600, 4 pages.
International Search Report dated Feb. 5, 2010, regarding Application No. PCT/US2009/049850, 2 pages. (WO 2010/005996).
PCT Application No. PCT/ES2005/000408, filed Jul. 20, 2005, 32 pages.
PCT Application No. PCT/US2009/049850, filed Jul. 7, 2009, 17 pages.
Ashizawa et al., “Manufacturing Technology for Polymer Composite Structures,” JTEC Panel Report on Advanced Manufacturing Technology for Polymer Composite Structures in Japan, Apr. 1994, 20 pages.
Cincinnati Milacron, “Into the Future With Better Ways to Automate the Manufacture of Composite Parts,” Cincinnati Milacron Publication No. SP-152-3, 1998, 22 pages.
Collins, “Measuring Small,” Computer Technology Review, vol. XXV No. 3, 2005, 5 pages.
European Search Report dated Sep. 15, 2008, regarding Application No. EP08008877 (EP1992473), 3 pages.
European Search Report dated Nov. 30, 2010, regarding Application No. EP08173139 (EP2077246), 2 pages.
European Search Report dated Jun. 7, 2010, regarding Application No. EP10250405 (EP2228333), 2 pages.
European Search Report dated Jun. 23, 2010, regarding Application No. EP10250484 (EP2228200), 3 pages.
Evans et al., “Fiber Placement Process Study,” SAMPE 34th Symposium Book of Proceedings, Reno, NV, May 8-11, 1989, pp. 1822-1833.
Guillermin, “Advanced Composite Engineering using MSC.Pantran and FiberSIM.” Composite Design Technologies, Jul. 20, 2004, 15 pages.
International Search Report dated Apr. 1, 2005, regarding Application No. PCT/US2004/015144 (WO2005030458), 2 pages.
International Search Report dated Aug. 30, 2006, regarding Application No. PCT/US2006/010704 (WO2006118692), 3 pages.
International Search Report dated Dec. 3, 2008, regarding Application No. PCT/US2008/072450 (WO2009038895), 3 pages.
International Search Report dated Mar. 2, 2009, regarding Application No. PCT/US2008/074612 (WO2009038943), 4 pages.
International Search Report dated May 28, 2009 regarding Application No. PCT/US2009/034048 (WO2009108517), 2 pages.
Koschmieder et al., “On-Line Tow Width Measurement in Filament Winding,” Proceedings of the 45th International SAMPE Symposium and Exhibition, Long Beach, CA, May 21-25, 2000, pp. 1417-1426.
Morrison et al., “Automatic Controlled Apparatus for Producing Tobacco Smoke Filter Rods,” USPTO Defensive Publication No. T941,011, Dec. 2, 1975, 3 pages.
Olsen et al., “Automated Composite Tape Lay-up Using Robotic Devices,” Proceedings of the International Conference on Robotics and Automation, Atlanta, GA, May 1993, pp. 291-297.
USPTO Office Action dated Jan. 11, 2005 regarding U.S. Appl. No. 10/437,067, 10 pages.
USPTO Final Office Action dated Jul. 1, 2005 regarding U.S. Appl. No. 10/437,067, 9 pages.
USPTO Office Action dated Feb. 17, 2006 regarding U.S. Appl. No. 10/437,067, 10 pages.
USPTO Notice of Allowance dated Sep. 13, 2006 regarding U.S. Appl. No. 10/437,067, 7 pages.
USPTO Supplemental Notice of Allowance dated Dec. 27, 2006 regarding U.S. Appl. No. 10/437,067, 4 pages.
USPTO Office Action dated Feb. 6, 2008 regarding U.S. Appl. No. 11/116,222, 13 pages.
USPTO Final Office Action dated Sep. 5, 2008 regarding U.S. Appl. No. 11/116,222, 12 pages.
USPTO Notice of Allowance dated Mar. 27, 2009 regarding U.S. Appl. No. 11/116,222, 4 pages.
USPTO Office Action dated Jun. 6, 2009 regarding U.S. Appl. No. 11/116,222, 11 pages.
USPTO Office Action dated Nov. 24, 2009 regarding U.S. Appl. No. 11/116,222, 9 pages.
USPTO Notice of Allowance dated Mar. 25, 2010 regarding U.S. Appl. No. 11/116,222, 5 pages.
USPTO Office Action dated Feb. 1, 2010 regarding U.S. Appl. No. 12/423,472, 36 pages.
USPTO Office Action dated Jul. 8, 2010 regarding U.S. Appl. No. 12/423,472, 25 pages.
USPTO Notice of Allowance dated Sep. 17, 2010 regarding U.S. Appl. No. 12/423,472, 6 pages.
USPTO Office Action dated Mar. 5, 2008 regarding U.S. Appl. No. 11/196,455, 12 pages.
USPTO Final Office Action dated Jul. 17, 2008 regarding U.S. Appl. No. 11/196,455, 11 pages.
USPTO Office Action dated Jan. 28, 2009 regarding U.S. Appl. No. 11/196,455, 10 pages.
USPTO Final Office Action dated Jul. 9, 2009 regarding U.S. Appl. No. 11/196,455, 8 pages.
USPTO Notice of Allowance dated Nov. 4, 2009 regarding U.S. Appl. No. 11/196,455, 8 pages.
USPTO Office Action dated Aug. 13, 2009 regarding U.S. Appl. No. 11/750,154, 9 pages.
USPTO Office Action dated Dec. 28, 2009 regarding U.S. Appl. No. 11/750,154, 7 pages.
USPTO Office Action dated May 25, 2010 regarding U.S. Appl. No. 11/750,154, 7 pages.
USPTO Final Office Action dated Sep. 14, 2010 regarding U.S. Appl. No. 11/750,154, 5 pages.
USPTO Office Action dated Aug. 21, 2009 regarding U.S. Appl. No. 11/856,372, 21 pages.
USPTO Final Office Action dated Jan. 27, 2010 regarding U.S. Appl. No. 11/856,372, 16 pages.
USPTO Notice of Allowance dated Apr. 30, 2010 regarding U.S. Appl. No. 11/856,372, 4 pages.
USPTO Supplemental Notice of Allowance dated Jul. 21, 2010 regarding U.S. Appl. No. 11/856,372, 2 pages.
USPTO Office Action dated Sep. 15, 2010 regarding U.S. Appl. No. 11/829,525, 11 pages.
USPTO Final Office Action dated Feb. 2, 2011 regarding U.S. Appl. No. 11/829,525, 12 pages.
USPTO Notice of Allowance dated Jun. 21, 2011 regarding U.S. Appl. No. 11/29,525, 8 pages.
USPTO Office Action dated Mar. 31, 2010 regarding U.S. Appl. No. 11/859,745, 18 pages.
USPTO Final Office Action dated Oct. 14, 2010 regarding U.S. Appl. No. 11/859,745, 22 pages.
USPTO Office Action dated Mar. 28, 2011 regarding U.S. Appl. No. 11/859,745, 24 pages.
USPTO Ex Parte Quayle Action dated Jan. 4, 2012 regarding U.S. Appl. No. 11/859,745, 9 pages.
USPTO Notice of Allowance dated Feb. 13, 2012 regarding U.S. Appl. No. 11/859,745, 9 pages.
USPTO Office Action dated Aug. 19, 2010 regarding U.S. Appl. No. 11/968,542, 10 pages.
USPTO Notice of Allowance dated Dec. 17, 2010 regarding U.S. Appl. No. 11/968,542, 9 pages.
USPTO Notice of Allowance dated Apr. 25, 2012 regarding U.S. Appl. No. 13/012,617, 16 pages.
USPTO Office Action dated May 17, 2011 regarding U.S. Appl. No. 12/038,155, 11 pages.
USPTO Final Office Action dated Oct. 19, 2011 regarding U.S. Appl. No. 12/038,155, 9 pages.
USPTO Office Action dated May 10, 2011 regarding U.S. Appl. No. 12/363,749, 11 pages.
USPTO Final Office Action dated Feb. 21, 2012 regarding U.S. Appl. No. 12/363,749, 8 pages.
USPTO Office Action dated Jun. 22, 2011 regarding U.S. Appl. No. 12/404,265, 10 pages.
USPTO Notice of Allowance dated Nov. 10, 2011 regarding U.S. Appl. No. 12/404,265, 9 pages.
USPTO Notice of Allowance dated Feb. 17, 2012 regarding U.S. Appl. No. 12/404,265, 11 pages.
USPTO Office Action dated Apr. 12, 2010 regarding U.S. Appl. No. 12/400,600, 14 pages.
USPTO Final Office Action dated Sep. 17, 2010 regarding U.S. Appl. No. 12/400,600, 18 pages.
USPTO Notice of Allowance dated Mar. 28, 2012 regarding U.S. Appl. No. 12/400,600, 5 pages.
USPTO Notice of Allowance dated Jun. 8, 2012 regarding U.S. Appl. No. 11/859,745, 40 pages.
USPTO Supplemental Notice of Allowance dated Jun. 19, 2012 regarding U.S. Appl. No. 11/859,745, 38 pages.
USPTO Office Action dated Jun. 21, 2012 regarding U.S. Appl. No. 13/169,160, 45 pages.
USPTO Notice of Allowance, dated Jun. 28, 2012, regarding U.S. Appl. No. 12/400,600, 64 pages.
Office Action, dated Feb. 1, 2013, regarding U.S. Appl. No. 12/363,749, 45 pages.
Notice of Allowance, dated Feb. 19, 2013, regarding U.S. Appl. No. 13/189,160, 18 pages.
Related Publications (1)
Number Date Country
20100006205 A1 Jan 2010 US
Provisional Applications (1)
Number Date Country
61134308 Jul 2008 US