Custom Aviation Thermal Shock Test Chambers for Aerospace Parts and Materials
Product Description:
Our thermal shock test chambers are specifically designed to evaluate the durability and reliability of aerospace parts and materials subjected to rapid and extreme temperature changes. These chambers simulate the harsh thermal environments encountered in aerospace applications, ensuring your components can withstand the stresses of flight and space exploration.
Key Features:
Precise Temperature Control: Our chambers maintain accurate and stable temperatures in both hot and cold zones.
Rapid Temperature Transition: The chambers feature a high-speed transfer mechanism to quickly move test samples between hot and cold zones, minimizing the time it takes to complete a test cycle.
Programmable Control System: The chambers have a user-friendly programmable control system that allows you to set test parameters such as temperature, dwell time, and cycle count.
Data Logging: Our chambers can record and store test data for analysis and reporting purposes.
Safety Features: The chambers include safety features such as over-temperature protection and door interlocks to ensure safe operation.
3. Specifications
Model
TSC-49-3
TSC-80-3
TSC-150-3
TSC-216-3
TSC-512-3
TSC-1000-3
Inside dimension(W x D x H) mm
40 x 35 x 35
50 x 40 x 40
65x 50 x 50
60 x 60 x 60
80 x 80 x 80
100 x 100 x 100
Outside dimension(W x D x H) mm
128x 190 x 167
138 x 196 x 172
149 x 192 x 200
158 x 220 x 195
180 x 240 x 210
220 x 240x 220
Internal material
#304 Stainless Steel
External material
Powder coated #304 Stainless Steel
High temperature range
60 ℃ ~ 200 ℃
Low temperature range
0 ℃ ~ -70 ℃
Test temperature range
60 ℃ ~ 180 ℃ / 0 ℃ ~ -70 ℃
Temperature recovery time
1-5min
Temperature stability ℃
±2
Cylinder switching time
10s
High temperature ℃
150
150
150
150
150
150
Heating time (min)
20
30
30
30
30
30
Low temperature
-40, -50, -65
-40, -50, -65
-40, -50, -65
-40, -50, -65
-40, -50, -65
-40, -50, -65
Cooling time (min)
40, 50, 60
40, 50, 60
40, 50, 60
40, 50, 60
40, 50, 60
40, 50, 60
Air circulation system
Mechanical convection system
Cooling system
Imported compressor, fin evaporator, gas condenser
Heating system
Fin heating system
Humidification system
Steam Generator
Humidification water supply
Reservoir, Sensor-controller solenoid valve, recovery-recycle system
Controller
Touch panel
Electrical power requirements
3 phase 380V 50/60 Hz
Safety device
Circuit system load protection, compressor load protection, control system load protection, humidifier load protection, overtemperature load protection, fault warning light
Applications
5.1 Wing Components
Wing Spars and Ribs: Test wing spars and ribs to ensure they can withstand the complex loading and thermal conditions during flight. Thermal stress can affect the structural integrity of these components, and the chamber can simulate the temperature variations they experience at different altitudes and during different flight phases.
Wing Skin Panels: Evaluate the performance of wing skin panels to ensure they can maintain their aerodynamic shape and structural integrity under extreme temperature changes. The chamber can test for issues such as buckling, delamination, and fatigue cracks caused by thermal stress.
5.2 Fuselage Components
Fuselage Frames and Stringers: Test fuselage frames and stringers to ensure they can support the weight of the aircraft and withstand the thermal stresses during flight. The chamber can simulate the temperature variations inside the fuselage, which can be affected by factors such as cabin heating and cooling systems.
Fuselage Skin Panels: Evaluate the performance of fuselage skin panels to ensure they can provide a secure and airtight enclosure for the aircraft's interior. The chamber can test for issues such as thermal expansion, contraction, and corrosion that can affect the integrity of the skin panels.
5.3 Engine Components
Engine Mounts: Test engine mounts to ensure they can support the weight of the engine and withstand the extreme heat and vibration generated during engine operation. The chamber can simulate the temperature variations experienced by engine mounts, which can be crucial for their long - term reliability.
Engine Cowlings: Evaluate the performance of engine cowlings to ensure they can protect the engine from external elements and withstand the high temperatures generated by the engine. The chamber can test for issues such as heat resistance, fire resistance, and structural integrity under thermal stress.
Benefits:
Identifies potential failure points in aerospace parts and materials
Ensures product reliability and durability in extreme temperature environments
Accelerates product development and validation processes
Reduces the risk of field failures and warranty claims
Meets industry standards and customer requirements
Why Choose Us:
We have years of experience in designing and manufacturing thermal shock test chambers. Our chambers are built to the highest standards and are backed by our commitment to customer satisfaction.
Call to Action:
Contact us today to learn more about our thermal shock test chambers and how they can benefit your business.