|
CN112008082A
|
|
Method for preparing hollow fan blade powder by hot isostatic pressing near-net-shape forming
|
|
CN110795886A
|
|
Method for determining dimensional allowance, method for forming dimensional allowance, forming device, and readable storage medium
|
|
CN112276539A
|
|
Device and method for screwing nut of aircraft engine
|
|
CN112280328A
|
|
Engine fan containing casing and preparation method thereof
|
|
CN112240226A
|
|
Rotor assembly, aircraft engine and assembly method of rotor assembly
|
|
CN112240812A
|
|
Residual stress testing device
|
|
CN112229906A
|
|
Aeroengine blade detection device
|
|
CN112211684A
|
|
Casing installation method
|
|
CN112207760A
|
|
Vertical low-pressure turbine unit assembling device and assembling method thereof
|
|
CN112208743A
|
|
Component end structure, method for producing same, aircraft and aircraft component
|
|
CN112287572A
|
|
Complex system and method and device for optimizing and verifying lightning stroke direct effect protection of complex system
|
|
CN112178107A
|
|
Elastic combined piston ring and squeeze film damper thereof
|
|
CN112172192A
|
|
Pre-compacting device and pre-compacting method
|
|
CN112177692A
|
|
Assembling tool and assembling method for low-pressure turbine rotor
|
|
CN112172198A
|
|
Blade cascade forming die and blade cascade forming method
|
|
CN112139646A
|
|
Energy storage spot welder
|
|
CN112146125A
|
|
Fuel nozzle, combustion chamber, gas turbine and method for preventing coking of fuel in fuel nozzle
|
|
CN112127999A
|
|
Control method and device for rotating speed of low-pressure shaft of aircraft engine
|
|
CN112214949A
|
|
Signal simulation circuit and signal simulation device for lubricating oil metal chip sensor
|
|
CN112214948A
|
|
Signal simulation circuit and signal simulation device for lubricating oil metal chip sensor
|
