Case Studies

Cabin Wireless Access Point (CWAP): PEI Enclosure Design for In-Flight Connectivity Systems

JBRplas delivered a single-cavity submarine-gate injection mold for a Cabin Wireless Access Point enclosure in PEI — 160×242×6mm at 126g, achieving ±0.08mm boss tolerance, 0.06mm long-axis flatness, UL94 V-0 certification, and full DO-160G Category A compliance for a Tier 1 avionics systems integrator.

Cabin Wireless Access Point (CWAP): PEI Enclosure Design for In-Flight Connectivity Systems
Industry: Aerospace & Avionics Material: PEI (Polyetherimide) 1-cavity Steel: H13 (52±2 HRC) 200,000 shots 32 days to T1

Project Overview

A leading avionics systems integrator approached JBRplas requiring a precision injection mold for a Cabin Wireless Access Point (CWAP) housing—a critical component installed within aircraft cabin walls to provide passenger connectivity and in-flight entertainment systems. The CWAP must operate reliably across extreme temperature differentials, high-altitude pressure variations, and demanding electromagnetic environments unique to commercial aviation.

Challenge: The client’s previous supplier delivered housing prototypes that exhibited unacceptable dimensional variance exceeding ±0.3mm across the long axis, and failed both UL94 V-0 flame retardancy verification and DO-160G environmental testing protocols. PEI material selection required specialized processing knowledge—excessive barrel temperatures risked thermal degradation, while insufficient cooling promoted warping and fiber orientation inconsistencies in the directional flow pattern.


Part Specifications

ParameterSpecification
Part Dimensions160 × 242 × 6mm
Nominal Wall Thickness2.5mm
MaterialPEI (Polyetherimide)
Surface FinishSPI A2 (cosmetic-grade exterior)
Critical Tolerances±0.15mm on connector mounting bosses
Flammability RatingUL94 V-0 (validated)
Aeronautical StandardDO-160G Category A environmental testing
Operating Temperature-55°C to +85°C continuous
Part Weight126g
Annual Volume48,000 units

Engineering Approach

Root Causes of Previous Failures

Our Design for Manufacturability (DFM) analysis identified three critical deficiencies in the prior supplier’s tooling:

  1. PEI Processing Mismanagement — inadequate barrel temperature control (316–318°C instead of required 340–360°C) created incomplete polymer chain extension, resulting in brittleness during pressurization cycling and visible stress-whitening on the 242mm long edges.

  2. Single-Point Gate Location — gate positioned at the short end (160mm side) created asymmetric melt flow across the 242mm length, producing anisotropic shrinkage and warping exceeding 0.4mm on the flat face after 24-hour post-mold conditioning.

  3. Inadequate Cooling Architecture — conventional cooling channels lacked thermal balance between the broad cavity face and narrow core face, causing non-uniform crystallinity development in the PEI structure and inconsistent surface quality across the connector mounting bosses.

Solution: Optimized PEI Process + Conformal Cooling + Dual-Gate Valve System

Material Processing Protocol:

  • Barrel temperatures: 350–365°C with 8°C ±2°C gradients across heating zones
  • Mold temperature: 170–180°C (critical for PEI flow control and UL94 V-0 certification)
  • Injection pressure: 95–110 MPa with dynamic pressure hold to maintain dimensional stability
  • Cooling hold-time: 22 seconds minimum to allow complete crystallization before ejection

Gating Strategy: We implemented a submarine gate system positioned at the geometric center of the 242mm axis, with gate diameter of 2.2mm. This creates symmetrical melt advancement from the centerline outward, neutralizing the differential shrinkage patterns that plagued the previous design. Moldflow simulation confirmed a fill time of 4.8 seconds with balanced pressure distribution (variance <3%) across all four mounting boss zones.

Cooling Design:

  • Core-side conformal cooling channels following the narrow 6mm profile with 8mm pitch, maintaining ±2°C thermal uniformity
  • Cavity-side conventional cooling with flow rates optimized for the broad 160×242mm surface
  • Differential coolant temperatures: Core-side 175°C, cavity-side 172°C to counteract heat retention in the thick boss geometry

Validation & Results:

  • Moldflow simulation predicted warping of 0.08mm on the long axis; actual T1 measurement: 0.06mm
  • UL94 V-0 flame retardancy: Pass (no after-flame, no dripping, no afterglow)
  • DO-160G thermal shock testing (-55°C to +85°C, 10 cycles): Pass (zero dimensional change >0.05mm)
  • Connector mounting boss positioning: ±0.08mm (exceeds ±0.15mm requirement)

Tooling Details

ParameterDetail
Mold TypeSingle-cavity, submarine gate, precision cooling
Mold BaseLKM standard, 450 × 380mm
Core / Cavity SteelH13, hardened to 52±2 HRC
Gate SystemSubmarine gate, 2.2mm diameter at center flow point
CoolingConformal on core; sequential zone cooling on cavity
Surface FinishSPI A2 (polished), cavity and core
Ejection6× Ø4mm ejector pins, balanced distribution
Venting8× 0.025mm vacuum vents at parting line
Mold Weight1,420kg

Timeline

MilestoneDuration
DFM report & PEI processing analysis issuedDay 3
Mold design complete (CAD + Moldflow)Day 14
Customer aerospace engineering approvalDay 18
Steel procurement completedDay 21
Machining & EDMDay 26
Conformal cooling commissioningDay 30
T1 trial with PEI validationDay 32
UL94 & DO-160G testing initiatedDay 36
Aerospace certification approvalDay 48
Production tooling releasedDay 52

Results

MetricRequirementAchieved
Long-axis flatness≤0.20mm0.06mm
Boss positioning tolerance±0.15mm±0.08mm
UL94 V-0 flammabilityRequired✅ Certified
DO-160G environmentalCategory A✅ Certified
T1 lead time35 days32 days
Production Cpk (critical dims)≥1.671.94
First-piece yield>95%98.2%

The program achieved full aerospace qualification within 52 days and entered production at a Tier 1 avionics supplier. The mold has since produced over 156,000 cycles with zero dimensional drift and 100% pass rate on all DO-160G periodic re-validation testing. PEI parts maintain UL94 V-0 certification compliance across all production lots, validating the precision thermal control architecture implemented in the mold design.


This case study demonstrates JBRplas’s specialized capability in aerospace-grade polymer tooling, where material mastery, conformal cooling precision, and adherence to DO-160G environmental protocols are non-negotiable requirements for cabin safety systems.

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