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Stainless Steel Thermal Shock Test Chamber For Aerospace Parts And Materials

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Stainless Steel Thermal Shock Test Chamber For Aerospace Parts And Materials

Brand Name : PRECISION

Model Number : TSC-150

Certification : ISO

Place of Origin : CHINA

MOQ : 1

Price : $6000

Payment Terms : T/T

Supply Ability : 100/month

Delivery Time : 15 working days

Packaging Details : Standard export packaging

Customized support : OEM ODM

Temp range : +150~-70℃

Internal material : 304 Stainless Steel

External material : Powder coated #304 Stainless Steel

Temperature Uniformity ℃ : 0.01

Humidity Uniformity % R. H. : 0.1

Temperature stability ℃ : ±0.3

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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.

Stainless Steel Thermal Shock Test Chamber For Aerospace Parts And MaterialsStainless Steel Thermal Shock Test Chamber For Aerospace Parts And Materials

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.


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