The present disclosure relates to locating positions on components, for example for proper placement of strain gages on test specimens for aerospace components.
Proper placement of gages for monitoring mechanical components presents challenges. For example, installing a strain gage on a mechanical component that has a complex geometry can present challenges. For example, it can be difficult to determine the proper location for the strain gage, as tolerances for strain gage position can be as narrow. In a manufacturing setting where multiple specimens of a component need strain gages, repeatability of strain gage placement is difficult. Reasons for these difficulties include lack of convenient hard points from which to measure location, difficulties in interpreting complicated drawing views and dimensions, and geometries that limit visibility and/or access for measurement devices. As a result, traditional techniques for placement of gages involve relatively labor intensive processes.
Such conventional methods and systems have generally been considered satisfactory for their intended purpose. However, there is still a need in the art for improved location. The present disclosure provides a solution for this need.
A method of locating position on a component includes engaging a template with a component and marking a location on the component using marking features of the template.
Marking a location can include marking a plurality of locations on the component using a plurality of respective marking features of the template. Each marking feature of the template can include a corner formed where at least two edges meet on the template. Marking each respective location on the component can include marking two line segments that cross at an intersection point, wherein the two line segments follow the edges of the template at each respective corner, to mark the respective location on the component at the intersection of the two respective line segments. For example, marking each location can include marking a center point location for a strain gage, as well as the horizontal and vertical orientation.
Engaging the template with the component can include engaging the template with at least two hard points of the component for positive location of the template relative to the component. Engaging the template can include sliding the template into place along a first hard point until meeting a second hard point that stops the template in position. At least one of the hard points can include at least one of a corner, hole, or stud of the component.
The method can further include forming the template using a solid model of the template, repeating engaging and marking until the template is worn down, and forming a replacement template using the solid model of the template. It is also contemplated that the method can include using the replacement template for engaging and marking until the replacement template is worn down. Forming the template and forming the replacement can include using the solid model to print the template and replacement template in an additive manufacturing process.
A template for locating position on a component includes a template body including mating features configured to engage corresponding hard points on a component, and a marking feature configured to locate a location on the component with the template body engaged with the hard points of the component. Each marking feature of the template can include a corner formed where at least two edges meet on the template. It is contemplated that the template body can include a plurality of marking features. It is also contemplated that the template body can be formed by an additive manufacturing process.
These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings.
So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a template in accordance with the disclosure is shown in
Template 100 for locating position on component 102 includes a template body 104 including mating features 106 that engage corresponding hard points 108 on component 102. The dashed lines in
A method of locating position on a component, e.g., component 102, includes engaging a template, e.g., template 100, with the component and marking a location on the component using marking features, e.g., marking features 110, of the template. In the example shown in
With reference again to
With reference now to
Templates 100 and 200 can be formed using a solid model of the template, as in a computer numerical controlled (CNC) type solid model. The procedures for engaging the template and marking the component can be repeated until the template is worn down. Using the same solid model, a replacement template can be formed. The replacement template can be used in the same manner until worn out, and it can in turn be replaced using the same solid model. For example, the templates as described herein can be formed using any suitable additive or subtractive manufacturing processes using the respective solid model. The additive or subtractive process should have tolerances within the acceptable tolerance for location of positions on the given component. For example, a template for placing strain gages on a component can be produced with an additive manufacturing process the tolerances of which are within the tolerance limit for the strain gage placement. Each replacement template can simply be printed, in an additive process for example. Since each replacement template is based on the same model, long term repeatability of locating gages on the respective component is facilitated.
While described herein in the exemplary context of placement of strain gages, those skilled in the art will readily appreciate that any other suitable type of gage or instrument can be placed on a component as described herein. For example, piezoelectric instruments, accelerometers, or the like could also be placed using the techniques described herein for component health monitoring purposes. It is also contemplated that flaws or other features such as stress risers can be placed in components in addition to or in lieu of placing gages without departing from the scope of this disclosure. The techniques described herein can be used for any suitable application requiring location of specific positions on components.
Potential advantages include reduced technician labor hours, reduction or elimination of rework due to misplaced gages and the like, and improved repeatability across multiple specimens. The methods and systems of the present disclosure, as described above and shown in the drawings, provide for locating positions on components with superior properties including improved facility, accuracy, and/or repeatability of location of positions on components relative to traditional techniques. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.
The subject application claims the benefit of priority from U.S. Provisional Application No. 62/199,005, filed Jul. 30, 2015, the entire disclosure of which is incorporated herein by reference in its entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/US2016/043848 | 7/25/2016 | WO | 00 |
Number | Date | Country | |
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62199005 | Jul 2015 | US |