<html><head></head><body><h2 id="isPasted">Overview</h2><p>This blog describes a development project to evaluate the efficiency and benefits of automated fiber placement technology through the design, prototyping, and testing of composite bars.&nbsp;</p><p>Discussions focus on the concept of “design-for-manufacturing” and provide an overview of the process going through selecting project objectives, material choices, processes and compensations, engineering and structural considerations, and the set of parts and accessories.</p><p><br></p><p data-hook="rcv-block2" type="paragraph"><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAyODY1MDMwLTE2NTk2MDI4NjUwMzAucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 301.987px;"></p><p><br></p><h2>Why automate helicopter production?</h2><p data-hook="rcv-block6" type="h2">Recurring costs have become an important factor in helicopter design, and although composite materials are widely used in aircraft parts, in many cases, manual manufacturing processes impede profitability.&nbsp;</p><p data-hook="rcv-block6" type="h2">Automatic manufacturing techniques can not only reduce production costs but can also provide repeatable, high-quality parts, digital traceability of defects, lower worker costs, and help achieve higher production rates helping lower the cost even further. The introduction of automation in industrial processes affects not only how parts are manufactured, but also how they are designed.</p><p data-hook="rcv-block7" type="paragraph"><br></p><p data-hook="rcv-block7" type="paragraph"><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAyODY1Mzc0LTE2NTk2MDI4NjUzNzQucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 304.651px;"></p><h2><br></h2><h2>Design for “X”</h2><p data-hook="rcv-block10" type="h2">As discussed in the <a data-hook="linkViewer" href="https://www.addcomposites.com/post/best-step-by-step-guide-for-composites-design#viewer-6ghdi" rel="noopener noreferrer" target="_blank"><u>previous design guide</u></a> "steps in the process flow of designing the composites part", the first step is to <strong>Set out a program objective</strong><strong>.</strong> In this conceptual design phase, the selected criteria are as follows</p><ul><li><p>Customer satisfaction</p></li><li><p>Cost, weight</p></li><li><p>Product readiness</p></li><li><p>Manufacturing (automated)</p></li><li><p>Producibility.&nbsp;</p></li></ul><h3><br></h3><h2>Design for Customer satisfaction and maintainability</h2><p data-hook="rcv-block17" type="h3">Design constraints related to customer satisfaction include the number of man-hours, downtime, and specialized tooling associated with scheduled and unscheduled maintenance and part replacement. The composite tail boom was evaluated at scheduled “gates” by customer support representatives to highlight and debate maintainability issues throughout the evolution of the design.</p><div data-hook="rcv-block19" type="empty-line"><br></div><h2>Design for Cost</h2><p>The airframe structure can account for as much as 25% of the non-recurring cost of a typical commercial light helicopter, and manufacturing cost is a primary driver for the design of aerospace structures. Two main approaches are compact automated fiber placement (AFP) and combine parts.</p><h3 data-hook="rcv-block21" type="paragraph"><br></h3><h3 data-hook="rcv-block21" type="paragraph">Compact Automated Fiber Placement (AFP) head rental</h3><p data-hook="rcv-block23" type="h4">A typical business case based on sales per calendar year for the introduction of this kind of component into the commercial helicopter market can justify a significant non-recurring. A compact AFP solution on a monthly subscription plan with high material and shape flexibility is chosen to reduce the significant non-recurring cost. Additionally, flexibility with material enables the production of ready blanks of dry per-form, thermoset prepregs for complex geometries hand layups.&nbsp;</p><h3 data-hook="rcv-block25" type="empty-line"><br></h3><h3 data-hook="rcv-block25" type="empty-line">Combine parts</h3><p data-hook="rcv-block26" type="h4">Reducing the total number of parts by either combining parts into one or deleting the unnecessary component. A thorough analysis of all the parts that can be combined into a single part is done and an example of such is shown in the image below.</p><p data-hook="rcv-block26" type="h4"><br></p><p><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAyODk5MjM3LTE2NTk2MDI4OTkyMzcucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 341.343px;"></p><p><br></p><h2>Design for weight</h2><h3 data-hook="rcv-block30" type="h3">Parasitic weight (No control)</h3><p data-hook="rcv-block31" type="h4">The weight of a composite tail boom is driven by two major factors. The first is the need to satisfy electrical wiring, avionics shielding, current return, HIRF, and lightning strike requirements.</p><p><br></p><h3 data-hook="rcv-block32" type="paragraph">Fatigue-based design (Can be optimized)</h3><p>The other important influence on structural weight is associated with structural and fatigue design criteria. Compared to metallic airframe design, composite have a very high fatigue tolerance. The lack of data for the tail boom fatigue test may require extensive testing of the produced prototype.</p><p><br></p><h2>Design for automated composite manufacturing</h2><p>Automated manufacturing processes, such as AFP, used to require design and analysis engineers to develop and orient the design specifically for AFP. However, now with the advent of open access software for AFP planning and simulation, the process has become extremely simple.</p><h4><br></h4><h4>Tooling design</h4><p>A CAD model of a tail boom approx 3-4 m in length and less than 0.5 m in diameter is drawn as an example here. If the starting point is a metallic structure with holes and other sub-assemblies the work of building mold becomes more tedious as it requires cleaning up of the provided part.&nbsp;</p><p><br></p><p><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAzNDcxODU2LTE2NTk2MDM0NzE4NTYucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 195.261px;"></p><p><br></p><p>In order to make a cleaner mold following points are proposed to clear a tool design:</p><ol><li><p>Remove any holes from the fan blade surface</p></li><li><p>Extend the open edges of the surface by up to 50-100 mm, up to 150mm if possible</p></li><li><p>Plan for the trimming allowance and draw an outer boundary</p></li><li><p>Sperate the layup and the boundary area by splitting the surface</p></li><li><p>Add mounting and alignment points for placement in AFP robotic cell</p></li><li><p>Consider markings or orientation points for fiber orientation definition</p></li><li><p>Now output the CAD in either step model</p></li></ol><h4><br></h4><p><br></p><h4>Planning the layup</h4><p>Planning the layup on a 3D mold shape has been made very simple and accessible thanks to our 3D Programming Software - <a data-hook="linkViewer" href="https://www.addcomposites.com/post/addpath-installation-instruction" rel="noopener noreferrer" target="_blank"><u>AddPath</u></a>. A step-by-step process of planning via AddPath is depicted in the picture below. The process also allows user to define their own paths by simply drawing a curve in the chosen CAD modeling software and importing it.&nbsp;</p><p><br></p><h4><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAzNDk3MDk5LTE2NTk2MDM0OTcwOTkucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 297.612px;"></h4><h4><br></h4><h4>Production simulation</h4><p>Simulating the process via 3D Programming Software - <a data-hook="linkViewer" href="https://www.addcomposites.com/post/addpath-installation-instruction" rel="noopener noreferrer" target="_blank"><u>AddPath</u></a> is very critical to make sure the following items are being met without error:</p><ol><li><p>Mold is positioned correctly</p></li><li><p>The robot can reach the entire layup area without overextending or reaching a point of singularity.</p></li><li><p>In the given setup a linear axis onto which the robot is set up so that the AFP can reach the entire layup area.</p></li><li><p>Motion sync between robot and mold is smooth and without error</p></li><li><p>No collisions are occurring</p></li><li><p>Fiber is being placed where you designed them to be among others...</p></li></ol><p><br></p><p>AddPath allows for modification of mold position to optimize the planned layup placement, thus enabling the part to be optimally designed. Below is the video showcasing the simulation in the finalized position. This case study can be downloaded from the <a data-hook="linkViewer" href="https://www.addcomposites.com/post/addpath-installation-instruction#viewer-56st9" rel="noopener noreferrer" target="_blank"><u>AddPath repository</u></a>&nbsp;</p><div data-hook="rcv-block66" type="paragraph"><br></div><p><u>Key learning from the simulation</u></p><ul id="isPasted"><li><p>Fiber steering is under the limit of given fiber width-GSM combinations</p></li><li><p>Time and estimated material for creating a business case for the production/pricing&nbsp;</p></li><li><p>Overlap/ gaps analysis for the certain fiber orientations and performing right width of AFP with ply drop strategies</p></li></ul><p><br></p><h2>Design for productibility</h2><p data-hook="rcv-block72" type="h3">The AFP tail boom is designed as a one-piece cone in order to provide an optimum surface of revolution for efficient AFP processing. The resulting one-piece tail boom skin structure requires a different philosophy for manufacturing and assembly. The tail boom's internal structure consists of 6 full frames fastened to the inside of the tail boom skin.</p><p data-hook="rcv-block73" type="paragraph">IML tooling (shown in the picture below) for the tail boom cone provides a tool-controlled surface on the interior of the part.</p><p data-hook="rcv-block74" type="paragraph"><br></p><p data-hook="rcv-block74" type="paragraph"><img src="https://images.wevolver.com/eyJidWNrZXQiOiJ3ZXZvbHZlci1wcm9qZWN0LWltYWdlcyIsImtleSI6ImZyb2FsYS8xNjU5NjAzNDcwNDQ4LTE2NTk2MDM0NzA0NDgucG5nIiwiZWRpdHMiOnsicmVzaXplIjp7IndpZHRoIjo5NTAsImZpdCI6ImNvdmVyIn19fQ==" width="624" id="isPasted" class="fr-fic fr-dii" style="width: 756px; height: 383.245px;"></p><div data-hook="imageViewer" tabindex="0"><br></div><h2>Sources</h2><div data-hook="post-description" id="isPasted"><article><div data-rce-version="8.72.16"><div data-id="rich-content-viewer" dir="ltr"><p>1.&nbsp;<a data-hook="linkViewer" href="https://iopscience.iop.org/article/10.1088/1757-899X/26/1/012016/pdf" rel="noopener noreferrer" target="_blank"><u>Design for Manufacturing – One-Piece, FibrePlaced Composite Helicopter Tailboom</u></a><a data-hook="linkViewer" href="https://iopscience.iop.org/article/10.1088/1757-899X/26/1/012016/pdf" rel="noopener noreferrer" target="_blank"></a><strong><a data-hook="linkViewer" href="https://iopscience.iop.org/article/10.1088/1757-899X/26/1/012016/pdf" rel="noopener noreferrer" target="_blank"></a>&nbsp;</strong></p></div></div></article></div><div data-hook="post-main-actions-desktop"><br></div></body></html>

Automatic manufacturing techniques can not only reduce production costs but can also provide repeatable, high-quality parts, digital traceability of defects, lower worker costs, and help achieve higher production rates helping lower the cost even further.

Design for Manufacturing via Automated Fiber Placement (AFP) Simulation - Composite Helicopter Tail Boom

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