The present invention relates in general to manufacturing, and in particular, to a pneumatic manifold-based flexible tooling system.
Computer numerical control (CNC) machines are used in many industries, including aerospace manufacturing, and often require specialized tooling to hold the parts being manufactured. Due to the complexity of requiring part specific tooling for large numbers of parts, flexible tooling systems, which can be configured to hold multiple different parts for manufacture, were created. These flexible tooling systems typically consist of a combination of structure and mechanism that enable the positioning of multiple individual tooling elements such as hard stops or vacuum fixtures at known positions in space that are derived from the shape of the part needed to be held by the flexible tooling system.
Typical installed systems use a set of individual driven actuators, each one positioning one of these individual tooling elements, to form a larger flexible tooling system. They are used to rigidly hold contoured or flat panels made of metal or composites for a variety of manufacturing operations (i.e. trimming, drilling, waterjet cutting, inspection, laser scribing, and assembly). These systems are computer controlled, and use specialized software programs that control the operations of the system components.
Existing flexible tooling systems generally have multiple design features that limit their usefulness during the CNC machining that may render them unusable during particular projects:
Despite these challenges, a number of flexible tooling systems have been created, installed, and used in the manufacture of parts. In practice, many parts that could benefit from flexible tooling for machining have less than a 12″ contour to them, while a significant number of CNC machines have a 48″ z-axis height.
One prior art flexible tooling system, manufactured by CNA Manufacturing Systems, Inc. of Renton, Wash. (“CNA”), is shown with reference to
The linear actuators described above are self contained assemblies that generate motion along a linear translational path relative to the frame of the linear actuator assembly. The specific actuator embodiment described above consists of a servo motor connected to a screw drive which moves a rod guided by the frame. The rod and frame each have mounting hardware designed to let the rod be axially loaded. Such actuators are available as commercial products, and are often used as replacements for pneumatic cylinders.
CNA developed a second generation flexible tooling system, shown with reference to
This second generation system, while functional, did have a number of drawbacks: the individual actuators still had a large minimum height, limiting the practicality of mounting them under many machine tools. They also had a limited minimum space between actuators, limiting the support able to be provided to the parts held. The actuation and clamping system was sensitive enough to thermal variations some climate control was required, and some facilities preferred not to have any hydraulic components installed in any manufacturing system installed at their location.
Accordingly, there is a need for a flexible tooling system that can address these challenges.
The low profile of the flexible tooling system disclosed below allows for flexible tooling to be added to nearly all CNC machines with an accommodating z-axis height—without major retrofits to the CNC machine, or lowering the flexible tool into a pit—which is the typical arrangement for current flexible tooling systems. Because of the low profile height of the flexible tooling system, the system can be moved from one CNC machine to another. The system includes one or more pods. Each of the pods of the system include four variable position assemblies that replicate the function of four actuators used in earlier systems built in a single pod structure, and sharing some common structure and components. Each pod functions as a multi-point variable positioning system, capable of moving and holding in place 4 tooling end effectors, and each pod then being mounted to a larger tooling table as part of an installed flexible tooling system.
Arranging the variable position assemblies into groups of four allows for greater density of individual tooling elements compared to spacing needed to install similar performance individual actuators used in prior systems, reduces cable requirements, maintains the network architecture that lets a central control system command large numbers of point positioning systems to operate the flexible tool system, and allows for air, vacuum, and vacuum sensor requirements for the contained variable position assemblies to be localized in each pod. The pod design allows for variable position assemblies to be spaced as close as 6″ in the x and y axis with the current components (with the possibility of even closer spacing using off the shelf components that reduce the rated axial load rating which can be applied to the individual tooling elements), which allows for greater density of support beneath thin parts. An increased variable position assembly density allows for greater flexibility to hold complicated parts by having tooling elements in more places than would otherwise be possible in prior systems where actuator spacing density is limited to 8″ or more.
In one embodiment, a pneumatic manifold-based flexible tooling system is provided. The system includes one or more pods attached to a table frame. Each of the pods includes: a top plate shaped to attach to the table frame, the top plate including one or more pass through shaft guides; a lower plate; a plurality of structural elements connecting the top plate to the lower plate; and one or more integrated motor and screw modules connected to the lower plate, each including: a motor co-axial with one of the pass through shaft guides; an encoder configured to detect the motor being in one of a plurality of positions; a motor controller configured to command the motor to take one of the positions using feedback from the encoder; a drive screw mechanically coupled to an output of the motor, wherein the drive screw is moved upon the motor moving from one of the positions to another one of the positions; an anti-rotation linear guide including a nut element that mounts onto the drive screw and a linear guide element that is attached to the nut element and that prevents rotation of the nut element, wherein the movement of the drive screw causes a linear motion of the nut element along a length of the drive screw; and a hollow shaft mounted onto the nut element, the hollow shaft extending through one of the pass through shaft guides and configured to connect to a tooling element including an end effector configured to hold a load. Each pod further includes a pneumatic manifold which provides air and vacuum to the end effectors, wherein the vacuum is used to secure the load to the end effectors, and the air is used to release the load from the end effectors. The pneumatic manifold further includes: a manifold block; air fittings connecting the manifold block to a supply of the air and a supply of the vacuum; and a plurality of pairs of valves attached to the manifold block, wherein flow of the vacuum or the air through a plurality of exit pneumatic ports of the manifold block is controlled by the pairs of the valves.
Still other embodiments of the present invention will become readily apparent to those skilled in the art from the following detailed description, wherein is described embodiments of the invention by way of illustrating the best mode contemplated for carrying out the invention. As will be realized, the invention is capable of other and different embodiments and its several details are capable of modifications in various obvious respects, all without departing from the spirit and the scope of the present invention. Accordingly, the drawings and detailed description are to be regarded as illustrative in nature and not as restrictive.
Each pod 2 includes a plurality of connections to hold individual tooling elements 3, and the moving shaft structure, actuation mechanisms, supporting structure, and supporting electronics required to position those tooling elements 3 in space. While in the description below, the tooling elements 3 are referred to as “end effectors,” the end effectors are particular kinds of tooling elements 3 and other kinds of tooling elements are possible, such as tooling balls, locating pins, or custom tooling surfaces held in space by a combination of three positioned shafts. Each pod 2 has its own control board, and valving that can individually control air 102 and vacuum 103 feeds for each end effector connected to the pod 2. Power, communication, air, and vacuum are routed inside the table frame 1 to each individual pod 2. Air and vacuum are provided from a central manifold location. Power and controls come from a centrally located human-machine interface (“HMI”) with a system controller, such as a PC computer, though other kinds of controllers or computing devices are possible. The controller is in turn interfaced to a source of power, such as but not limited to a generator, a stored power source (such as a battery), or an electrical outlet. Each end effector's 3 location is individually controlled from the HMI through a communication network run over the cables connecting it to the pods 2, which allows for each end effector to be set to individual heights by positioning the moving shaft the end effector 3 is attached to (within the limit of the stroke of the mechanism) to be able to conform to the shape of the part being held by the flexible tooling system 100. When the flexible tooling system 100 has conformed to the shape of a part that needs to be held in place, and the part has been placed onto the flexible tooling system 100, the part is held in place in contact with the end effectors 3 using vacuum force that is controlled individually for each end effector 3 employed in the pattern for the part. Once the machining process of the part has been completed, vacuum supply 103 for each of the end effectors 3 is turned off and air supply 102 for each is turned on so as to break the vacuum force holding the part and to allow the part to be removed from the flexible tooling system 100. In one embodiment, a separate power cable and a separate network communication cable (via which control commands are provided and data is received) originate from the HMI and connect to the table 1. At the table 1, the power and network signals are routed such that they are united together into separate conductors in a single cable for each pod 2. The united cable connects to the pod 2 where the cable splits up into separate power and communication cables for each motor module 8 in the pod 2. The power and communication signals are common to each motor module 8 in the table 1. Motor modules 8 use an internal network address system to determine if the module 8 is the recipient of any given command. Other configurations of the cables are possible. Data from the motor module 8 (such as pressure level at end effector 3) can be provided to the HMI via the same cable provides communication to that motor module 8. The power and communication cables could connect ports 11 on the module 8, though other ways to connect the cables are possible.”
Due to each motor module 8 being individually addressable by the HMI, the HMI can cause a movement of each of the motors 9 (and consequently coaxial tooling elements, such as an end effector 3) that is independent of other motors 9 but that can be concurrent with movement of other motors 9 (“asynchronous independent movement).
Returning to
Each integrated motor and screw module 8 has an integrated controller that that receives commands from the HMI and returns data to the HMI. The motor controller uses feedback from the encoder to control the electrical motor so the mechanisms of the pod will move the hollow shaft 22 to the position commanded by the HMI. Data including status and errors is returned to the HMI. In this implementation the electrical motor 9 is a stepper motor with an integral encoder, and integral controls, enabling the motor controller 8 to command the electrical motor 9 to seek a rotary position with a specific encoder count which corresponds to a hollow shaft 22 position. Each motor module 8 has integrated ports 11 for power, communications, and input/output of data signals. The input/output signals can be controlled automatically by the motor controller firmware or controlled by commands to the motor module 8 from an outside system controller 101. In one embodiment, the ports 11 can be located on the motor controller, although other locations are also possible. In one embodiment, the motor module 8 can be a Lexium MDrive® Linear Actuator (NEMA 23 integrated 1.8° 2-phase stepper motor with external shaft) produced by Schneider Electric SE, headquartered in Rueil-Malmaison, France. In a further embodiment, other kinds of motors are also possible. In a still further embodiment, the motor controller could be physically separate from the motor and connected to the motor via a wired or wireless connection. The integrated motor and screw module 8 can be interfaced to three cables (power, communications, and inputs/outputs). The integrated motor and screw module 8 can have connectors compatible with Phoenix Contact SPEEDCOM connection, with the cables interfaced being cables provided by Phoenix Contact of Blomberg, Germany, though other kind of cables are also possible. The connectors can be right angle connectors to reduce the height requirement of the pod 2, though other kinds of connector are also possible. The motor controller being built into the integrated motor and screw module 8 allows for localization of functionality (valves and vacuum sensor mounting to the pod's bottom plate 4) to the integrated motor and screw module 8 rather than distributing components throughout the system or in a system enclosure. This reduces cable lengths and allows the pod 2 to only need one cable for communications and power from the system
Returning to
Also attached to the bottom plate 6, is a pneumatic manifold 13.
Returning to
Attached to the top of this hollow shaft 22 is an end effector adaptor 23 that holds tooling elements 3, such as end effectors 3, with an end effector 3 including a precisely positioned spherical pivot that links to combination of a locating surface and a vacuum cup which holds parts to that locating surface. In a further embodiment, instead of an end effector 23 adaptors, a cap (not shown) on which tooling elements can be constructed can be attached to an end of the hollow shaft 22 to which the end effector adaptor 3 otherwise attaches.
Returning to
Corner guards 24 are attached to the underside of the upper plate 4 and continue to the corners of the lower plate 6 that is slightly smaller than the holes of the table 1 that the pod 2 is lowered into to prevent damage to the actuation mechanisms.
Attached to the pneumatic manifold 13 is one internal pneumatic tube 25 for each supported end effector 3. Each internal pneumatic tube 25 also connects to a bulkhead pneumatic fitting 26 that penetrates the top plate 4. Also attached to this bulkhead pneumatic fitting 26 is an external pneumatic tube 27, which also connects to the end effector adaptor 23 that is co-axial with the motor module 8 that supplied the output switch signals for that valve 19 pair. This air and vacuum supply is used to control the suction status of the vacuum cup of the mounted end effector 3.
As mentioned above,
While the invention has been particularly shown and described as referenced to the embodiments thereof, those skilled in the art will understand that the foregoing and other changes in form and detail may be made therein without departing from the spirit and scope of the invention.
This non-provisional patent application is a continuation of U.S. Pat. No. 11,022,953, issued Jun. 1, 2021, which claims priority under 35 U.S.C. § 119(e) to U.S. Provisional Patent application, Ser. No. 62/844,682, filed May 7, 2019, the disclosure of which is incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
2471921 | Ashdown | May 1949 | A |
3542354 | Fitzpatrick | Nov 1970 | A |
3599279 | McDonald | Aug 1971 | A |
3853313 | Appenzeller et al. | Dec 1974 | A |
3926447 | Cox, Jr. | Dec 1975 | A |
4080716 | Vom Dorp | Mar 1978 | A |
4088312 | Frosch et al. | May 1978 | A |
4200272 | Godding | Apr 1980 | A |
4317577 | Cameron | Mar 1982 | A |
4432559 | Rasmussen | Feb 1984 | A |
4491306 | Eickhorst | Jan 1985 | A |
4527783 | Collora et al. | Jul 1985 | A |
4638984 | Puisais et al. | Jan 1987 | A |
4684113 | Douglas | Aug 1987 | A |
4693458 | Lewecke et al. | Sep 1987 | A |
4736957 | Bischopink | Apr 1988 | A |
4883312 | Kulis | Nov 1989 | A |
4946149 | Greene | Aug 1990 | A |
5110239 | Riley et al. | May 1992 | A |
5139245 | Bruns et al. | Aug 1992 | A |
5143360 | Wilken et al. | Sep 1992 | A |
5163793 | Martinez | Nov 1992 | A |
5230594 | Pilkington | Jul 1993 | A |
5279493 | Halder | Jan 1994 | A |
5316276 | Heinle | May 1994 | A |
5318005 | Mayer | Jun 1994 | A |
5364083 | Ross et al. | Nov 1994 | A |
5372357 | Blaimschein | Dec 1994 | A |
5427363 | Rink | Jun 1995 | A |
5457868 | Blaimschein | Oct 1995 | A |
5546784 | Haas et al. | Aug 1996 | A |
5551677 | Puettmer et al. | Sep 1996 | A |
5562276 | Blick | Oct 1996 | A |
5722646 | Soderberg | Mar 1998 | A |
5846464 | Hoffman | Dec 1998 | A |
6024392 | Blatt | Feb 2000 | A |
6032348 | Haas et al. | Mar 2000 | A |
6209188 | Soderberg et al. | Apr 2001 | B1 |
6250619 | Cook | Jun 2001 | B1 |
8322700 | Saberton et al. | Dec 2012 | B2 |
8469345 | Samac et al. | Jun 2013 | B2 |
10562157 | Rinaldi | Feb 2020 | B2 |
20060017298 | Osten | Jan 2006 | A1 |
20070069436 | Zarske | Mar 2007 | A1 |
20090057971 | Bumgarner | Mar 2009 | A1 |
20110018185 | Samac | Jan 2011 | A1 |
20110037213 | Marrinan | Feb 2011 | A1 |
20140199153 | Reinhold | Jul 2014 | A1 |
20160152507 | Brown | Jun 2016 | A1 |
20180215540 | Tanaka | Aug 2018 | A1 |
20190210217 | Bolton et al. | Jul 2019 | A1 |
Number | Date | Country |
---|---|---|
9906917 | Feb 1999 | WO |
2005042204 | Dec 2005 | WO |
Entry |
---|
Retrieved from https://www.aerospacemanufacturinganddesign.com/product/kostyrka-uhf-chucking-device-38291/ (retrieved May 20, 2020). Publication date—Jul. 17, 2014. |
http://infinitetool.com/turnkey-automated-systems-portfolio/flexible-tooling-system/ . Cached on Aug. 18, 2018. |
https://dk8mx37zdr9bp.cloudfront.net/metal-cutting-composites/PDF_Fives_Line_Machines/Liné%20Machines%20FLEXITOOL%20-Light.pdf . Copyright 2014. |
https://www.mtorres.es/en/aeronautics/products/metallic/torrestool. Cached on Jan. 8, 2019. |
https://ph.parker.com/us/en/lcb-series-lcb040-belt-driven-slider-bearing-rodless-linear-actuator . Cached on Aug. 23, 2017. |
Centralized Flexible Manufacturing Center. Original publication date unavailable. Saved as of Sep. 8, 2015. |
CNA Manufacturing Systems, POGO Actuator. Original publication date unavailable. Saved as of Aug. 21, 2014. |
https://www.parker.com/Literature/Electromechanical%20North%20America/SERVICE-USER%20GUIDES/ETH%20Manual%20192-550002N2.pdf, revised Nov. 21, 2018. |
ETP Hydro-Grip brochure, cashed on Mar. 12, 2016. |
Merriam-Webster Dictionary (Year: 2020). |
https://www.mmsonline.com/articles/abrasive-waterjet-helps-make-composites--affordable-for-boeing. Aug. 5, 2008. |
Number | Date | Country | |
---|---|---|---|
20210286336 A1 | Sep 2021 | US |
Number | Date | Country | |
---|---|---|---|
62844682 | May 2019 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 16866374 | May 2020 | US |
Child | 17334476 | US |