Environmental Test Experience For An Antenna Application
The device being tested is a hybrid structure that combines the mechanical robustness of an AM bare metal structure with the electronic performance of a printed electronic AME structure inlay.
Summary Test Checklist for Hybrid AM-Structure With AME-Structure
The hybrid structure is subjected to extracts of the standard RTCA/DO-160F and RTCA/DO-160G tests for airborne equipment.
The following sections provide an overview of the tests performed to demonstrate the potential of additively manufactured samples under operational test conditions.
RTCA/DO-160F
Contamination Test
Fluids
- Hydraulic Fluid
- De-Icing Fluid
- Cleaning + solving
Climate Test
Severe Humidity Environment
- Humidity
- Temperature Variation
Normal Salt Fog
RTCA/DO-160G
Mechanical Test
- Standard Random Vibration
- Robust Vibration
- Shock
1. Contamination Test on 3D-AME Structure With Fluids
The tests are performed with:
- Hydraulic fluid (H544H544 Synthetic)
- De-Icing fluid (Aviform L50 and Killfrost ABC)
- Cleaning and solving (Isopropanol)
Result: The 3D-AME structure was able to withstand the contamination test without loss of performance.
2. Climate Test on Hybrid DUT AM Bare Metal and 3D-AME
Severe Humidity Environment:
Humidity Test
- Temperature range: +38°C/+65°C
- Humidity: 85% RH/95%
- Duration: 10 cycles/24 hours per cycle
Result: The tested hybrid structure was able to withstand without deterioration or damage.
Temperature Variation
Temperatures
- Ground survival low temperature: -55°C
- High operational temperature: +55°C
- Ground survival high temperature: +85°C
Temperature change rate
- 10°C/min
Duration
- 2 cycles with a duration of 12 hours per cycle
Result: The tested hybrid structure was able to withstand without deterioration or damage.
Performance of Normal Salt Fog:
Salt Fog Test
- Temperature: +35°C
- Salt Solution: 5%
- Duration: 2 cycles with a duration of 24 hours per cycle
- Drying room temperature: 2 cycles with a duration of 24 hours per cycle
Result: The tested AME structure inlay showed no degradation.
3. Mechanical Test on Hybrid DUT AM Bare Metal and 3D-AME
Standard Random Vibration
Standard Random Vibration Test Curves for Equipment Installed in Fixed Wing Aircraft with Turbojet or Turbofan Engines
Result: A visual inspection of the tested hybrid structure did not show any defects.
Robust Vibration
Robust Vibration Test Curves for Equipment Installed in Fixed Wing Aircraft with Turbojet or Turbofan Engines
Result: A visual inspection of the tested hybrid structure did not show any defects.
Shock
- Acceleration: 6g, 20g, 40g
- Duration of shock: 1ms
- Number of shocks: 54, 18 per axis
- Number of axes: 3, (X, Y, Z)
- Number of directions: 6, (+X,-X, +Y,-Y,+Z,-Z)
- Test category: non-operational test
Result: A visual inspection of the tested hybrid structure did not show any defects.