Selected Achievements
Selected Achievements
XS23-ZLXXXA - Small Shock Tubes for Impact Loads (Basic Research Type) Caliber φ30-90mm
XS-SC01 - Integrated Data Acquisition and Control System
Customizable 8 to 256 data acquisition channels, up to 16 synchronous control channels
XS25-ZL/SLXXX - Large Shock Tube/Shock Wind Tunnel (Engineering Test Type), Caliber φ150-300mm
XS23-ZLXXXB Small Flow Visualization Shock Tube, Caliber φ30-90mm
XS24-ZLXXXM Medium Shock Tube / Shock Wind Tunnel (Research Type), Caliber φ100-220mm
XS24-ZLXXXM Medium Shock Tube / Shock Wind Tunnel (Research Type), Caliber φ100-220mm
Physical photo of the diaphragm test bench
Customizable bursting pressure range: 0.2–25.0 MPa, rupture disc diameter: 30–300 mm
XSA-SDXXXA Split Simple Schlieren Instrument
Integrated Schlieren Instrument XSA-SDXXXB
Radar Floor
High-pressure turbine casing
High-pressure turbine casing
Nuclear reactor core products
aircraft skin
Aerospace Components
Actual Renderings of the Fluid Power Machinery Laboratory
Actual Renderings of Fluid Power Machinery Laboratory
Actual renderings of the Fluid Power Machinery Laboratory
Manufacturing and construction capacity as well as equipment operation and maintenance technical services
Construction Plan of Fluid Power Machinery Laboratory
XS23-ZLXXXA - Small Shock Tubes for Impact Loads (Basic Research Type) Caliber φ30-90mm
XS24-ZLXXXM Medium Shock Tube / Shock Wind Tunnel (Research Type), Caliber φ100-220mm
Actual renderings of the Fluid Power Machinery Laboratory
XS-SC01 - Integrated Data Acquisition and Control System
Physical photo of the diaphragm test bench
XSA-SDXXXA Split Simple Schlieren Instrument
Aerospace Components
Radar Floor
High-pressure turbine casing
Manufacturing and construction capacity as well as equipment operation and maintenance technical services
Customizable 8 to 256 data acquisition channels, up to 16 synchronous control channels
XS25-ZL/SLXXX - Large Shock Tube/Shock Wind Tunnel (Engineering Test Type), Caliber φ150-300mm
XS23-ZLXXXB Small Flow Visualization Shock Tube, Caliber φ30-90mm
Customizable bursting pressure range: 0.2–25.0 MPa, rupture disc diameter: 30–300 mm
Integrated Schlieren Instrument XSA-SDXXXB
High-pressure turbine casing
Nuclear reactor core products
aircraft skin
Construction Plan of Fluid Power Machinery Laboratory
Actual Renderings of the Fluid Power Machinery Laboratory
Manufacturing and construction capacity as well as equipment operation and maintenance technical services
Actual Renderings of Fluid Power Machinery Laboratory
Manufacturing and construction capacity as well as equipment operation and maintenance technical services
XS23-ZLXXXA - Small Shock Tubes for Impact Loads (Basic Research Type) Caliber φ30-90mm
XS-SC01 - Integrated Data Acquisition and Control System
Customizable 8 to 256 data acquisition channels, up to 16 synchronous control channels
XS25-ZL/SLXXX - Large Shock Tube/Shock Wind Tunnel (Engineering Test Type), Caliber φ150-300mm
XS23-ZLXXXB Small Flow Visualization Shock Tube, Caliber φ30-90mm
XS24-ZLXXXM Medium Shock Tube / Shock Wind Tunnel (Research Type), Caliber φ100-220mm
Physical photo of the diaphragm test bench
Customizable bursting pressure range: 0.2–25.0 MPa, rupture disc diameter: 30–300 mm
XSA-SDXXXA Split Simple Schlieren Instrument
Integrated Schlieren Instrument XSA-SDXXXB
Radar Floor
High-pressure turbine casing
Aircraft spar
Nuclear reactor core products
Aerospace Components
Construction Plan of Fluid Power Machinery Laboratory
Actual renderings of the Fluid Power Machinery Laboratory
Actual Renderings of Fluid Power Machinery Laboratory
Actual Renderings of the Fluid Power Machinery Laboratory
Manufacturing and construction capacity as well as equipment operation and maintenance technical services