US2010037444A1PendingUtilityA1

Reconfigurable flexible rail apparatus and method

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Assignee: REID ERIC MPriority: Aug 15, 2008Filed: Aug 15, 2008Published: Feb 18, 2010
Est. expiryAug 15, 2028(~2.1 yrs left)· nominal 20-yr term from priority
Y10T29/51B23Q 9/0042B64F 5/10B23Q 2210/008B23Q 9/0007
44
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Claims

Abstract

A method and apparatus for performing operations on a work piece comprises a flexible rail system and a multi-axis carriage. The flexible rail system may be capable of being attached to a work surface. The multi-axis carriage may be coupled to the flexible rail system. The multi-axis carriage may be capable of moving along the flexible rail system and may be capable of moving a tool in axes relative to the work surface. The tool may be single use or multi use and may be removably coupled to the frame and or carriage

Claims

exact text as granted — not AI-modified
1 . An apparatus comprising:
 a flexible rail system capable of being attached to a work surface; and   a multi-axis carriage coupled to the flexible rail system, wherein the multi-axis carriage is capable of moving along the flexible rail system and is capable of moving a tool in axes relative to the work surface.   
   
   
       2 . The apparatus of  claim 1  further comprising:
 a tool module capable of being removably coupled to the multi-axis carriage, wherein the tool module comprises a frame and the tool, wherein the tool is mounted on the frame.   
   
   
       3 . The apparatus of  claim 2 , wherein the tool is located on a first side of the tool module further comprising:
 a pressure foot located on the first side and capable of applying pressure to the work surface.   
   
   
       4 . The apparatus of  claim 3 , wherein the flexible rail system comprises a flexible rail, and wherein the tool module further comprises:
 a reaction unit located on a second side of the tool module and capable of stabilizing the multi-axis carriage during operation of the tool.   
   
   
       5 . The apparatus of  claim 4 , wherein the reaction unit is capable of stabilizing the multi-axis carriage while the multi-axis carriage moves along the flexible rail. 
   
   
       6 . The apparatus of  claim 4  further comprising:
 a set of rollers associated with the pressure foot.   
   
   
       7 . The apparatus of  claim 5 , wherein the reaction unit comprises at least one of a set of feet and a set of rollers. 
   
   
       8 . The apparatus of  claim 4 , wherein the multi-axis carriage comprises:
 a first motor that is capable of moving the multi-axis carriage on the flexible rail along an X-axis in the axes.   
   
   
       9 . The apparatus of  claim 8 , wherein the multi-axis carriage further comprises:
 a second motor capable of moving the tool in the tool module along a Y-axis in the axes   
   
   
       10 . The apparatus of  claim 4 , wherein the pressure foot is rotatable about an A-axis that is parallel to the X-axis and is movable to contact the work surface. 
   
   
       11 . The apparatus of  claim 10 , wherein the pressure foot is capable of providing a force that is normal to the work surface. 
   
   
       12 . The apparatus of  claim 1 , wherein the flexible rail system is a flexible vacuum rail system. 
   
   
       13 . The apparatus of  claim 1 , wherein the flexible rail system comprises:
 a plurality of rails.   
   
   
       14 . The apparatus of  claim 1 , wherein the work surface is curved. 
   
   
       15 . The apparatus of  claim 2 , wherein the tool is removably attached to the frame. 
   
   
       16 . The apparatus of  claim 2 , wherein the tool is selected from one of a drill, a measurement probe, a rivet hammer, a router, a trimming saw, a grinding wheel, and a fastener. 
   
   
       17 . The apparatus of  claim 1 , wherein the work surface is a surface of a work piece selected from one of an aircraft fuselage, an aircraft wing, an aircraft door, an aircraft empennage, an aircraft control surface, a spacecraft, a ship, a tank, and a building. 
   
   
       18 . An apparatus for performing operations on an aircraft work piece.
 a flexible vacuum rail capable of being attached to a curved work surface of the work piece;   a multi-axis carriage coupled to the flexible rail system, wherein the multi-axis carriage is capable of moving along the flexible rail system and is capable of moving a tool in axes relative to the curved work surface and wherein the multi-axis carriage comprises:   a first motor capable of moving the multi-axis carriage on the flexible rail along an X-axis in the axes; and   a second motor capable of moving the tool in a tool module along a Y-axis in the axes;   a tool module capable of being removably coupled to the multi-axis carriage and comprising:   a frame;   the tool, wherein the tool is mounted on the frame, wherein the tool is located on a first side of the tool module, and wherein the tool is selected from one of a drill, a measurement probe, a rivet hammer, a router, a trimming saw, a grinding wheel, and a fastener;   a pressure foot located on the first side of the tool module, wherein the pressure foot is capable of applying pressure to the curved work surface, is rotatable about an A-axis that is parallel to the X-axis, and is capable of providing a force that is normal to the curved work surface; and   a reaction unit located on a second side of the tool module and capable of stabilizing the multi-axis carriage during operation of the tool and capable of stabilizing the multi-axis carriage while the multi-axis carriage moves along the flexible rail, wherein the reaction unit comprises at least one of a set of fixed feet and a set of rollers.   
   
   
       19 . A method for performing an operation on a work piece, the method comprising:
 attaching a vacuum rail with a multi-axis carriage coupled to the vacuum rail to a surface of a work piece;   coupling a tool module to the multi-axis carriage, wherein the tool module has a tool capable of performing the operation;   moving the multi-axis carriage along the flexible vacuum rail to a location on the work piece; and   performing the operation at the location.   
   
   
       20 . The method of  claim 19 , wherein the performing step comprises:
 applying a force against the surface with a pressure unit located on a first side of the tool module, wherein the pressure unit is rotatable around an axis parallel to an axis of movement of the multi-axis carriage and wherein force is normal to the surface;   providing a reactive force to the force with a reactive unit located on a second side of the tool module; and   performing the operation after the force and the reactive force are applied.   
   
   
       21 . The method of  claim 20 , wherein the operation is selected from at least one of a drilling operation, a sealing operation, a measuring operation, and a fastening operation. 
   
   
       22 . A method for performing an operation on an aircraft work piece comprising:
 attaching a flexible vacuum rail with a multi-axis carriage coupled to the flexible vacuum rail to a surface of the aircraft work piece;   coupling a tool module to the multi-axis carriage, wherein the tool module has a tool capable of performing the operation;   moving the multi-axis carriage along the flexible vacuum rail to a location on the aircraft work piece; and   applying a force against the surface with a pressure unit located on a first side of the tool module, wherein the pressure unit is rotatable around an axis parallel to an axis of movement of the multi-axis carriage and wherein force is normal to the surface;   providing a reactive force to the force with a reactive unit located on a second side of the tool module; and   performing the operation after the force and the reactive force are applied, wherein the operation is selected from at least one of a drilling operation and a fastening operation.

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