|
CN112276331A
|
|
Welding method for double-spoke-plate turbine disk
|
|
CN112284720A
|
|
Acoustic test-based fault diagnosis method for central transmission bevel gear of aircraft engine
|
|
CN112097073A
|
|
Roller adapter capable of being vertically installed and locked
|
|
CN112211678A
|
|
Long-life turbine rotor front baffle
|
|
CN112284751A
|
|
Distortion test device with adjustable distortion characteristic
|
|
CN112228558A
|
|
Hole detector plugging head assembly and casing plugging method
|
|
CN112199848A
|
|
Fatigue life evaluation method for low-pressure turbine shaft
|
|
CN112229640A
|
|
Rigidity test device and measurement method for aircraft engine tail nozzle adjusting mechanism
|
|
CN112229238A
|
|
Woven fin heat exchange structure arranged in corrugated mode and heat exchanger
|
|
CN112182939A
|
|
Dynamic strength evaluation method for engine bearing frame
|
|
CN112228557A
|
|
Blocking assembly and hole detecting and blocking structure
|
|
CN112287477A
|
|
Turbine guide device large and small blade layout method based on airflow excitation
|
|
CN112050251A
|
|
Steady flow pressure regulating device for combustion chamber of aircraft engine
|
|
CN112228243A
|
|
Hydraulic push type cam mechanism for variable state adjustment of combined spray pipe
|
|
CN112128440A
|
|
Diaphragm type internal ballast overpressure relief device
|
|
CN112284546A
|
|
Tail nozzle temperature field visualization device based on binocular vision and identification method thereof
|
|
CN112228226A
|
|
Aircraft engine turbine rotor cooling thermal management system
|
|
CN112199796A
|
|
Method for designing composite material culvert casing layering
|
|
CN112280472A
|
|
Formula and use method of colored oil flow suitable for medium-high speed blowing test
|
|
CN112228162A
|
|
Boosting turbofan engine radar and infrared comprehensive stealth structure
|
