Custom test engineering · Chengdu
Custom validation equipment, component test rigs and environmental chambers for civil aviation engineering — designed around the test object, measurement chain and acceptance method.
We develop purpose-built verification systems that combine mechanical structures, actuation, fluid power, instrumentation, controls and software. The scope is defined around your test objective rather than a fixed catalogue configuration.
Servo-controlled loading platforms for actuator, steering and structural verification, configured to reproduce representative operating loads and dynamic response.
Integrated benches for critical-stage inspection, fine adjustment and characteristic evaluation under controlled hydraulic and thermal conditions.
Hydraulic and electromechanical motion systems for attitude, trajectory and motion-response verification, from compact platforms to large integrated installations.
Real-time simulation and interface equipment that connects physical hardware with controlled models, signals, loads and fault scenarios during development verification.
Project photographs illustrate engineering categories only. Each delivered system is configured to the agreed test object, interfaces and acceptance method; detailed specifications are discussed directly under the project scope.
From compact qualification chambers to walk-in installations, each system is configured against the specimen, test profile, facility utilities and applicable standard.
Bench and walk-in systems for steady-state and cyclic climate exposure.
Accelerated thermal cycling and environmental stress screening profiles.
Two-zone and three-zone architectures for abrupt temperature transitions.
Controlled condensation and icing conditions for component resilience studies.
Cabinets and rooms for elevated-temperature endurance and burn-in.
Compressor-free, salt fog, dust, battery safety and anaerobic test configurations.
Dedicated pneumatic, hydraulic and lubrication-oil test platforms for aircraft doors, nacelle airflow, flow measurement and accessory verification.
Five platforms covering aircraft-door actuation, high-temperature gas flow and engine-nacelle airflow.
Loading and fuel-nozzle test platforms configured around the component and its test procedure.
A dedicated platform for lubrication-oil accessory test work.
Share the test object, operating medium, pressure and temperature range, duty cycle, measurement channels and acceptance procedure so the configuration can be scoped accurately.
A disciplined handoff from requirement to commissioning reduces avoidable changes and gives your team a clear technical counterpart throughout the project.
Test object, operating envelope, load cases, signals, interfaces and applicable procedure.
Mechanical, fluid-power, controls, instrumentation, safety logic and facility interfaces.
Technical review, assembly, internal commissioning and acceptance criteria alignment.
Shipment coordination, installation guidance, operator training and after-sales response.
Test equipment should fit the work around it. We focus configurations on the way aviation engineering, MRO and training teams actually validate parts and processes.
Specify the standard, section, specimen and profile in your inquiry. We will respond with an initial configuration path and the technical questions needed to scope it correctly.
DO-160 §4DO-160 §5DO-160 §6DO-160 §12DO-160 §14Technical inquiry
Include the test object, operating conditions, load cases, interfaces, measurement requirements, acceptance method, facility utilities and destination. We will use that to start a focused technical discussion.