Thermoplastic composite IR welding spec

Spec notes for IR welding of TPC, with figures traced to NTRS.

Earlier published engineering notes

As shown here, a composite part with the epoxy layer is easily penetrated.

Using Kubota Research's P-Wave™ IR radiation system and ImpacGard™ process to consolidate a P-Wave™ Pseudo -prepreg onto the surface of a reinforced composite preserves the integrity of the high tenacity fiber.

A single layer of ImpacGard™ increases impact absorption of composite materials up to 40%, and dramatically improves shatter and spalling containment.

ImpacGard™ is a patent pending composite facing that absorbs impact energy to reduce the risk of major structural damage, and minimize the potential for hazardous debris.

Report language on this query

Fusion bonding, or welding, refers to heating a thermoplastic joint at the bondline, providing time and pressure as required for polymer chain reptation across the weld interface, and cooling under pressure to solidify the joint.

Several methods for welding thermoplastic composites are available however the three often used in aerospace include resistance, induction, and ultrasonic welding.

The goal of this work is to evaluate the requirements, benefits, and constraints of these three welding methods to join four candidate thermoplastic composite material systems.

Lap shear coupons were welded by each method on a per coupon basis.

The weld area was limited to the 2.54 by 2.54 cm coupon overlap region to provide an assessment of the reproducibility of each weld process and the influence of edge effects.

ly heated above the processing temperature range to the point of degradation.

The regions with dry fibers (no resin) apparently experienced temperatures high enough to vaporize the resin.

Therefore, these results suggest significant temperature gradients occurred during the welding process.

6 Concluding Remarks Thermoplastic composite welding is a candidate for future in -space and on -surface structural join ing applications.

TDEA has contributed toward this long-term objective through hundreds of welding trials and evaluations.

This report summarized the key findings from these welding trials.

Strong welds are possible as demonstrated at the coupon and subelement scale .

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Spec notes for IR welding of TPC, with figures traced to NTRS. Verify every figure against the original report before a drawing release.

Source titles on this pass: NASA TM thermoplastic joining resistance induction ultrasonic; NASA TM TDEA thermoplastic composite welding; An Assessment of the Use of a Carbon Fiber Heating Element in Resistance Welding for PPS, PEI, LM-PAEK, and PEKK Thermop; Manufacture, Characterization, and Fusion Welding of Thermoplastic Composites for Space Applications; Finite Element Thermal Model for Ultrasonic Welding of Thermoplastic Composites; Thermoplastic Composite High Rate Fuselage Manufacturing Demonstrator.

Figures taken from the reports

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Figures traced to cited documents
DocumentStated figureSource
NASA TM thermoplastic joining resistance induction ultrasonic54 by 2.54 cm coupon overlap region to provide an assessment of the reproducibility of each weld process and the influence of edge effects.20250006527
NASA TM TDEA thermoplastic composite welding6 Concluding Remarks Thermoplastic composite welding is a candidate for future in -space and on -surface structural join ing applications.20250008644
An Assessment of the Use of a Carbon Fiber Heating Element in Resistance Welding for PPS, PEI, LM-PAEK, and PEKK ThermopThermoplastic Resistance Welding with a Carbon Fiber Heating Element Phase II An assessment of the use of a Carbon Fiber Heating Element in Resistance Welding for PPS, PEI, LM-PAEK, and PEKK Thermoplastic Composite June.20250001324
Manufacture, Characterization, and Fusion Welding of Thermoplastic Composites for Space Applications3 MPa 14 Process Development for Ultrasonic Welding DOE Results- Ultrasonic Welding/ PEI Run 6: 12.20240012394
Finite Element Thermal Model for Ultrasonic Welding of Thermoplastic Compositesigate… Sample 1 Sample 1 non-destructive evaluation (NDE) 5 Ultrasonic testing (UT) Peak UT reflection from weld plane Pore Peak UT transmission thru specimen Assumed “good” bond area 48% [4] Shi, Huajie, Irene Fernandez Villegas, and Harald EN Bersee.20240005126
Thermoplastic Composite High Rate Fuselage Manufacturing Demonstratormoplastic composites, specifically fastener-less assembly, and reformability of interfacing parts during welding. AFP of the skin did not meet rate targets however the repairability of the process and no material.20250005727
Innovations in Continuous Ultrasonic Welding of Thermoplastic Composites and Evaluation for Space Applications1 1 Innovations in Continuous Ultrasonic Welding of Thermoplastic Composites and Evaluation for Space Applications Sandi Miller1, Joseph Pinakidis1, Robert Bryant2, Christopher Lang2, Andrew Bergan3, Ken Segal4 1 NASA.20240002138
Thermoplastic Aircraft Manufacturing Modele above its melt temperature to around 330oC to get enough tack.20240000967

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Sources for this page

Every figure above traces to the reports below. Check the original document before using a number in a live design.

Figures stated in the cited documents
DocumentStated figure
NASA TM thermoplastic joining resistance induction ultrasonic54 by 2.54 cm coupon overlap region to provide an assessment of the reproducibility of each weld process and the influence of edge effects.
Manufacture, Characterization, and Fusion Welding of Thermoplastic Composites for Space Applications3 MPa 14 Process Development for Ultrasonic Welding DOE Results- Ultrasonic Welding/ PEI Run 6: 12.
Manufacture, Characterization, and Fusion Welding of Thermoplastic Composites for Space Applications3 MPa Run #53 15 K15 Weldability Evaluation: Commercially Available Materials The purpose of this milestone was to generate single lap shear data for thermoplastic composite adherends welded by resistance welding (RW), ultrasonic welding (UW), and induction welding (IW).
Finite Element Thermal Model for Ultrasonic Welding of Thermoplastic Compositesigate… Sample 1 Sample 1 non-destructive evaluation (NDE) 5 Ultrasonic testing (UT) Peak UT reflection from weld plane Pore Peak UT transmission thru specimen Assumed “good” bond area 48% [4] Shi, Huajie, Irene Fernandez Villegas, and Harald EN Bersee.

Drawn from the cited NASA/NIST/EPA source documents for the query “thermoplastic composite ir welding spec”.

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