Patent application number | Description | Published |
20080205763 | Method for fitting part assemblies - Shims used to join part assemblies are automatically designed and fabricated without the need for fitting part assemblies together in order to determine the exact dimensions of voids filled by the shims. The locations of key features on part assemblies are surveyed using a merged photogrammetry and laser tracking technique that generate the dimensions of a virtual shim. The dimensions of the virtual shim are contained in a digital file that can be used to automatically fabricate the shim using automated fabrication equipment such as a CNC machining center. The automated virtual shim design may be modified to reflect the effect of part assembly fit on performance characteristics of the aircraft. | 08-28-2008 |
20080223985 | Splicing Fuselage Sections without Shims - Fuselage sections of an aircraft are joined using splice elements that compensate for gaps caused by mismatches between mating surfaces on the fuselage sections. The fuselage sections are virtually assembled using computer models that are based on non-contact measurements of as-built fuselage sections. The virtually assembled fuselage sections are used to map the gaps between the mating surfaces. The mapped gaps are used to produce tool inserts having profiles that reflect the dimensions of the gaps. The tool inserts are used to manufacture splice elements having profiles that fill the gaps when the fuselage sections are assembled and joined, thereby eliminating the need for shims and spaces to fill the gaps. | 09-18-2008 |
20080300823 | METHODS AND SYSTEMS FOR MANUFACTURING LARGE COMPONENTS - Methods and systems for fabricating a composite structure are provided. The method includes receiving data representing a portion of a surface of the structure, measuring a surface of the structure, the measured surface corresponding to the received surface wherein the measuring is performed with the structure in a flexed condition, and determining a difference in a first and a second direction between the measured surface and the received surface at areas that correspond to the measured surface. The method also includes determining a difference in a third direction, transmitting to a morphing algorithm the determined differences in the first, second, and third directions, and determining a position in the first, second, and third directions of a point on the surface in the flexed condition that corresponds to a respective point on the received surface when the structure is placed in the nominal condition. | 12-04-2008 |
20080307886 | System and method for automated inspection of large-scale part - Systems and methods can automatically inspect a workpiece. Non-destructive inspection sensors are mounted on a frame mounted on a transport device. Position of a first predetermined location of a workpiece is measured with a tracking system. The transport device is moved to position the non-destructive inspection sensors proximate the first predetermined location of a workpiece. A first portion of a workpiece proximate the first predetermined location is non-destructively inspected with the non-destructive inspection sensors. Position of a second predetermined location of a workpiece can be measured with the tracking system. The transport device can be moved to position the non-destructive inspection sensors proximate the second predetermined location of a workpiece, and a second portion of a workpiece proximate the second predetermined location can be non-destructively inspected with the non-destructive inspection sensors. Data can be provided from the sensors to a computing system and analyzed by the computing system. | 12-18-2008 |
20090006031 | COMBINATION LASER AND PHOTOGRAMMETRY TARGET - The invention relates to the use of one or more targets in measuring surfaces. Each of the one or more targets may comprise a first portion adapted to reflect a laser beam towards a laser tracking device, and a second portion adapted to reflect a light beam towards a photogrammetry device. Simultaneous photogrammetry and laser tracking measurements may be taken utilizing the one or more targets. | 01-01-2009 |
20100201972 | CALIBRATING AIRCRAFT SURFACES - Systems and methods to calibrate aircraft surfaces are provided. A particular method includes installing a set of laser targets. The set of laser targets includes at least first laser target and a second laser target. The first laser target is installed on a first side of a first aircraft surface and the second laser target is installed on a second side of the first aircraft surface at a known location relative to the first laser target. The method also includes determining a first position of the first laser target with a first laser device. The method further includes determining a second position of the second laser target with a second laser device. The method includes determining a position of the first aircraft surface based on the first position of the first laser target and the second position of the second laser target. | 08-12-2010 |
20100280648 | Splicing Fuselage Sections Without Shims - Fuselage sections of an aircraft are joined using splice elements that compensate for gaps caused by mismatches between mating surfaces on the fuselage sections. The fuselage sections are virtually assembled using computer models that are based on non-contact measurements of as-built fuselage sections. The virtually assembled fuselage sections are used to map the gaps between the mating surfaces. The mapped gaps are used to produce tool inserts having profiles that reflect the dimensions of the gaps. The tool inserts are used to manufacture splice elements having profiles that fill the gaps when the fuselage sections are assembled and joined, thereby eliminating the need for shims and spaces to fill the gaps. | 11-04-2010 |
Patent application number | Description | Published |
20090138126 | Controlled Application of External Forces to a Structure for Precision Leveling and Securing - Methods and systems provide for the controlled application of forces to a structure during leveling and securing procedures. According to embodiments described herein, a force distribution system includes a number of force application devices that are communicatively linked to a computing system. The computing system controls the force application devices to apply calculated forces to the structure, monitor the forces, and adjust the forces when deviations occur. According to one embodiment, the force application devices include jack assemblies and the system is operative to level a structure and maintain the level position when the structure shifts. According to another embodiment, the force application devices include clamp assemblies and the system is operative to apply and maintain a constant and uniform pressure on a structure to secure the structure during machining. Other embodiments include using force application devices to secure a structure during transport. | 05-28-2009 |
20110190941 | Systems and Methods for Structure Contour Control - Systems and methods provide for the controlled application of forces to a structure during assembly, machining, manufacturing, and/or transportation operations. According to embodiments described herein, a contour control system includes a number of force control modules that are communicatively linked to a control system. The control system receives or retrieves data indicating the shape of the structure and a shape associated with a desired structure, and determines if the structure is consistent with the design specifications and any associated tolerances. The control system controls the force control modules to apply calculated forces to the structure to control the contours of the structure and/or to maintain the structure in a desired configuration. According to embodiments, the force control modules include support cradles, air cushion pads, vacuum cups, and/or other structures for selectively applying dynamic and/or static forces to the structure. | 08-04-2011 |
20120196254 | METHODS AND SYSTEMS FOR CONCURRENT TEACHING OF ASSEMBLY PROCESSES AT DISPARATE LOCATIONS - A method for teaching an aircraft assembly method to students at locations separate from the location of an instructor is described. The method includes providing, from the instructor location, a first video feed based on a line of sight of the instructor and a second video feed being a field view of the assembly area. The video feeds are received at the disparate locations for display within a line of sight of the students such that the students may view the instructor performing the assembly method concurrent with the students performing the assembly method. Like video feeds are provided from the student locations such that the instructor may view at least one of the students performing the assembly method concurrent with the instructor performing the assembly method. | 08-02-2012 |
20140222171 | Controlled Application Of External Forces To A Structure For Precision Leveling And Securing - Methods provide for the controlled application of forces to a structure during leveling and securing procedures. According to embodiments described herein, a structure is supported at a number of support locations. An upward force is applied to the structure by the force application devices to counteract an equivalent downward force from the structure at each support location. The forces applied by the force application devices are monitored to detect whenever one or more of the upward forces deviates outside of a threshold range of force values, which includes a quantity of force sufficient to counteract internal forces within a material of the structure. Each force may be adjusted to ensure no deviation outside of the allowed threshold range. | 08-07-2014 |
Patent application number | Description | Published |
20100106678 | MONITORING AGENT PROGRAMS IN A DISTRIBUTED COMPUTING PLATFORM - Methods, systems, and computer-readable media for monitoring information passed from instances of role(s) of a service application installed on a distributed computing platform and for indexing and analyzing the information within a data store are provided. Monitoring involves a monitoring agent that is integrated within an operating system of computing devices that make up the distributed computing platform. In operation, the monitoring agent retrieves information from the role instances and converts the information into parameters that are assembled to documents. Generally, the parameters are assembled to a uniform-structured format in accordance with a schema imposed by the distributed computing platform. Accordingly, each of the documents across the platform have a common format that promotes processing and analysis without a need for reconfiguration. Accordingly, the health of the service application, although dispersed throughout the distributed computing environment, may be observed and evaluated in a consistent manner. | 04-29-2010 |
20130024564 | MONITORING AGENT PROGRAMS IN A DISTRIBUTED COMPUTING PLATFORM - Methods, systems, and computer-readable media for monitoring information passed from instances of role(s) of a service application installed on a distributed computing platform and for indexing and analyzing the information within a data store are provided. Monitoring involves a monitoring agent that is integrated within an operating system of computing devices that make up the distributed computing platform. In operation, the monitoring agent retrieves information from the role instances and converts the information into parameters that are assembled to documents. Generally, the parameters are assembled to a uniform-structured format in accordance with a schema imposed by the distributed computing platform. Accordingly, each of the documents across the platform have a common format that promotes processing and analysis without a need for reconfiguration. Accordingly, the health of the service application, although dispersed throughout the distributed computing environment, may be observed and evaluated in a consistent manner. | 01-24-2013 |