Automotive headliner development · Draft test plan

A Substrate-Specific Bond Test Plan for Automotive Headliners

Headliner bond evaluation must reflect the actual layer stack and production process. Changes in fabric, foam or supporting material require the relevant interfaces and process conditions to be checked again. Adapt this plan to the customer specification, part design and development stage; it does not set universal acceptance limits.

R-5670 with R-60C can be discussed as a candidate system. Suitability requires current technical data and trials with the actual materials and process. The tables contain no measured results and do not indicate that this system has passed a headliner project.

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Prepared by Relanet New Materials (Guangzhou) Co., Ltd. · Content updated

  1. Define the stack
  2. Record the process
  3. Run separate tests
  4. Review the evidence
Illustrative test workflow, adaptable to the project; not measured results or proof of acceptance.

1. Define representative specimens

Headliner
The accompanying image illustrates an application structure. Confirm the actual materials and adhesive layers for each project.

Map the fabric, foam, supporting layer and each adhesive interface. Identify material grades, suppliers, batches, thicknesses and existing surface treatments. Omit a foam layer if the real assembly has none.

Specify sampling location, direction, dimensions, replicates and conditioning. Strip specimens help compare interfaces; curved, edge or assembly samples examine holding and deformation in representative geometry. Neither replaces the other.

  • Keep unaged controls and separate trial groups when changing materials, cleaning or surface treatment.

2. Record the process before comparing adhesives

Record adhesive and companion-component names and batches, document revision, weighing method, mixing start, application method and coat weight. Use the current applicable technical data for mixing and use conditions.

Document the environment, drying, activation, pressing and release. Separate equipment settings from measured adhesive-layer or substrate temperatures. Distinguish water removal from heat activation. Mark unknown settings for confirmation.

  • Link the operation sequence, unusual observations and photographs to each sample group.

3. Separate the three strength stages

Initial tack describes immediate grab under defined contact conditions. Green strength concerns early handling or holding before full strength develops. Final strength is assessed after specified cure and conditioning. Give each stage its own timing, method and acceptance requirement.

Record peel geometry, speed, specimen width and failure location. Foam or fabric failure changes how a reading is interpreted. A typical one-minute peel value cannot replace the final-strength evaluation for this project.

4. Schedule five evaluation checkpoints

Define requirements and methods before collecting results. Different checkpoints may need different specimens. Agree acceptance values through the applicable customer specification or project test agreement. Keep results marked “Pending test” until traceable records are available.

CheckpointEvaluationConditions to recordResult
Initial tack and green strengthEvaluate immediate grab and early transfer/release hold separatelyStack, contact/pressing, elapsed time and methodPending test
Coating sag resistanceMovement, pooling or coverage change in the wet coatingCoat weight, viscosity method, orientation, environment and observation timePending test
Heat resistance and assembly creepDisplacement, sag and bond retention under defined heat and loadTemperature, duration, load, orientation, geometry and failure criteriaPending test
Humidity aging and hydrolysis riskBond changes after conditioning; hydrolysis needs relevant evidenceCure, humidity/water exposure, temperature, duration and controlsPending test
Final bond strengthStrength and failure mode after specified cure, conditioning and required agingCure/conditioning, peel geometry, speed, width and failure locationPending test

5. Compare aging results and failure locations

Coating sag occurs before bonding; assembly sag or creep occurs within a bonded structure. Viscosity or thixotropic behavior alone cannot establish headliner shape retention under heat and load. Record these evaluations separately.

After humidity aging, compare strength, appearance, displacement and failure mode. Water uptake, material changes and interface conditions can affect results. Humidity aging alone does not prove a hydrolysis mechanism; define the question and evidence needed.

  • Classify interface, adhesive, foam or fabric failure and link photographs.
  • Keep anomalous results; do not pool trials with incompatible conditions.

6. Decide the next trial or project step

Connect each result to its requirement, evidence record and decision basis. Missing results or limits remain pending. Possible decisions include further screening, retesting one adjusted variable or advancing to another sample stage.

Share the layer stack, process, failure photographs, customer test requirements and project stage with RELANET. For R-5670 with R-60C, request current TDS/SDS and sample information. Record sample evaluation separately from later production approval.

Questions and answers

Is this plan a headliner acceptance standard?

No. It organizes specimen, process and result records. Confirm methods, sampling, limits and decisions against the customer specification or project agreement.

Does a non-sagging wet coating prevent assembly sag?

Not necessarily. Wet coating behavior and bonded-assembly creep occur at different stages and need separate coating and assembly evaluations.

Has R-5670 passed the headliner tests described here?

This article makes no such claim. R-5670 with R-60C is a candidate for discussion; suitability needs current technical data and traceable project results.

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Tell us about your bonding project

Email your layer stack, material grades, production process, test targets, company name and business contact details. You can also request the current TDS, SDS or samples.

Email your project requirements →

info@relanet.com.cn

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