|
CN112196674A
|
|
Aviation air turbine starter transmission system
|
|
CN111829788A
|
|
Test method for verifying thermal state cleaning effect of aero-engine
|
|
CN111734689A
|
|
Two-stage thermal-state cleaning device for aircraft engine and working method of two-stage thermal-state cleaning device
|
|
CN111749967A
|
|
Fixing bolt for aero-engine case and using method thereof
|
|
CN111734679A
|
|
Aeroengine compressor inner casing with air vent and machining method thereof
|
|
CN111734496A
|
|
Centrifugal impeller assembly of aviation turbine starter and assembly method of centrifugal impeller assembly
|
|
CN111734672A
|
|
Tangential injection lubricating system for turboshaft engine and using method thereof
|
|
CN111716061A
|
|
Clamp for welding screw base of radial diffuser and using method of clamp
|
|
CN111750147A
|
|
Aero-engine combustion chamber oil discharge valve and use method thereof
|
|
CN111734673A
|
|
Lubricating system for shaft of aircraft engine and using method of lubricating system
|
|
CN110285927A
|
|
A kind of axial flow compressor leading portion static state oil seal experimental rig and test method
|
|
CN108406374A
|
|
Process two grade blade recruitment dress of aero-engine free turbine
|
|
CN108381188A
|
|
The repairing of aero-engine output shaft centre bore grinds with tooling and its repaiies and grind working method
|
|
CN109807702A
|
|
The threaded top adapter of one kind and its application method
|
|
CN109807411A
|
|
A kind of shunting disk processing electric pulse fixture and its application method
|
|
CN107824920A
|
|
Suitable for saving the fixture of production cost
|
|
CN107511755A
|
|
A kind of centrifugal impeller abrasive Flow fixture
|
|
CN108252955A
|
|
Compressor tubular diffuser
|
|
CN107313983A
|
|
A kind of compressor blade diffuser component and its assembly method
|
|
CN107313982A
|
|
A kind of new radial diffuser component and its manufacture method
|
