CN111922676A
|
|
Aero-engine fuel nozzle decomposition device
|
CN111673683A
|
|
Method for quickly disassembling and assembling nut of turbine support heat shield
|
CN111922980A
|
|
Two-stage nozzle decomposition tool and decomposition method
|
CN111810249A
|
|
W-shaped sealing ring and design method thereof
|
CN111780162A
|
|
Binary channels fuel nozzle of adjustable valve
|
CN112097260A
|
|
Novel high-precision air swirler and manufacturing method thereof
|
CN111805119A
|
|
Cylindrical plug-in welding structure and positioning method thereof
|
CN111693292A
|
|
Detection system and method for engine gas turbine starter
|
CN111608839A
|
|
System and method for plateau starting of engine
|
CN111538318A
|
|
Digital regulator single module detecting system
|
CN111678046A
|
|
Unloading cavity air supply system
|
CN111380490A
|
|
High-precision depth dimension measuring device and method
|
CN111468966A
|
|
Universal clamp for bent pipe parts and use method thereof
|
CN111531234A
|
|
Method for removing burrs of head and tail threads by numerical control lathe
|
CN111331298A
|
|
Combined machining process equipment for large-size thin-wall welding part in aircraft engine
|
CN111360583A
|
|
Special inner diameter measuring tool for exhaust assembly in aircraft engine and using method thereof
|
CN110411321A
|
|
Any two straight lines angle bisector fast accurate positioning device and method in a kind of plane
|
CN110411739A
|
|
A kind of rubber seal oil resistance verifying device and method
|
CN109396884A
|
|
A kind of tooling and processing method of multistation processing fuel nozzle shell
|
CN109128234A
|
|
A kind of soft pawl mandrel adjuster
|