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Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation

This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with addi...

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Published in:Computation 2024-05, Vol.12 (5), p.105
Main Authors: Sedelnikov, Andry, Kurkin, Evgenii, Smelov, Vitaliy, Chertykovtseva, Vladislava, Alekseev, Vyacheslav, Gavrilov, Andrey, Kishov, Evgenii, Zvyagincev, Maksim, Chernyakin, Sergey
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container_issue 5
container_start_page 105
container_title Computation
container_volume 12
creator Sedelnikov, Andry
Kurkin, Evgenii
Smelov, Vitaliy
Chertykovtseva, Vladislava
Alekseev, Vyacheslav
Gavrilov, Andrey
Kishov, Evgenii
Zvyagincev, Maksim
Chernyakin, Sergey
description This paper discusses an approach to estimating the parameters of the cohesive zone model (CZM) by mode II by extruding the bushing along the lug axis. This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.
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This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.</description><identifier>ISSN: 2079-3197</identifier><identifier>EISSN: 2079-3197</identifier><identifier>DOI: 10.3390/computation12050105</identifier><language>eng</language><publisher>Basel: MDPI AG</publisher><subject>Adhesion ; Adhesives ; Aerospace industry ; Aircraft ; Analysis ; Bearing strength ; Bond strength ; Bushings ; Carbon fiber reinforced plastics ; Carbon fibers ; Composite materials ; contact ; Contact melting ; Contact stresses ; Crack propagation ; CZM model ; Dynamic testing ; Extrusion process ; Fiber reinforced polymers ; Influence ; Injection molding ; Lasers ; Load ; Load carrying capacity ; Lugs ; Manufacturing ; Materials ; Methods ; PA6 ; Parameters ; Polyamide resins ; Polyamides ; Polymers ; Properties ; Roughness ; Sandblasting ; SFRP ; Short fibers ; SLM ; Tensile strength ; Testing ; Ti-6Al-4V ; Titanium alloys ; Titanium base alloys ; Vibratory finishing</subject><ispartof>Computation, 2024-05, Vol.12 (5), p.105</ispartof><rights>COPYRIGHT 2024 MDPI AG</rights><rights>2024 by the authors. 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This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. 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This method of evaluation requires small samples, which is particularly relevant when investigating short fiber-reinforced polymers (SFRPs) with additively manufactured embedded elements. Adhesion is investigated on the example of 30% carbon fiber-reinforced polyamide-6 molded to Ti-6Al-4V (VT6) selective laser-melted (SLM) alloy bushing in cases of a roughness Ra = 2.66 μm (vibratory finishing), Ra = 8.79 μm (sandblasting), and Ra = 10.02 (directly from SLM). The values of the maximum equivalent tangential contact stress were in a range from 1.1 MPa to 9.5 MPa, while the critical fracture energy for tangential slip was estimated at 15 N/mm for all cases. Experimental validation of the obtained CZM mode II was carried out by evaluating the load-carrying capacity of the lugs with different bushings. In both the experiment and the calculation, greater bushing roughness provides greater lug load-bearing capacity. The ribbed bushings added significant strength in the experiments, which confirmed the importance of considering the tangential mode in the contact model. The presented models can be used for the preliminary evaluation of short fiber-reinforced polyamide-6 parts with titanium-embedded elements bearing capacity.</abstract><cop>Basel</cop><pub>MDPI AG</pub><doi>10.3390/computation12050105</doi><orcidid>https://orcid.org/0000-0003-2698-1348</orcidid><orcidid>https://orcid.org/0000-0002-0893-9878</orcidid><orcidid>https://orcid.org/0000-0002-6893-1894</orcidid><orcidid>https://orcid.org/0000-0001-9556-6290</orcidid><oa>free_for_read</oa></addata></record>
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ispartof Computation, 2024-05, Vol.12 (5), p.105
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source Publicly Available Content (ProQuest)
subjects Adhesion
Adhesives
Aerospace industry
Aircraft
Analysis
Bearing strength
Bond strength
Bushings
Carbon fiber reinforced plastics
Carbon fibers
Composite materials
contact
Contact melting
Contact stresses
Crack propagation
CZM model
Dynamic testing
Extrusion process
Fiber reinforced polymers
Influence
Injection molding
Lasers
Load
Load carrying capacity
Lugs
Manufacturing
Materials
Methods
PA6
Parameters
Polyamide resins
Polyamides
Polymers
Properties
Roughness
Sandblasting
SFRP
Short fibers
SLM
Tensile strength
Testing
Ti-6Al-4V
Titanium alloys
Titanium base alloys
Vibratory finishing
title Short Fiber-Reinforced Polymer Polyamide 6 Lugs and Selective Laser-Melted Ti-6Al-4V Bushing Contact Cohesive Zone Model Mode II Parameters’ Evaluation
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