CN106762813A
|
|
A kind of fan blade
|
CN107013941A
|
|
Combustion chamber fuel nozzle arrangement
|
CN106988787A
|
|
Rotor blade and turbomachine
|
CN106945302A
|
|
Fiber-reinforced composite fan blade and its manufacture method
|
CN106934074A
|
|
Global optimum's fanjet air intake duct noise abatement method for designing
|
CN106919724A
|
|
Fanjet by-pass air duct noise abatement method for designing
|
CN106917931A
|
|
The remove device of Aero-engine Bearing chamber ventilation duct wall lubricating oil
|
CN106908245A
|
|
Aero Engine Testing device stable state TT&C system and its data sharing method
|
CN106907242A
|
|
Aero-engine impeller
|
CN106884873A
|
|
Rolling bearing and aero-engine
|
CN106882390A
|
|
Airplane air entraining precooling heat regenerative system
|
CN106874526A
|
|
The generation method and device of the production coordinate of turbine blade
|
CN106834992A
|
|
TiAl alloy casting and its handling process
|
CN106812723A
|
|
blade, turbine and compressor
|
CN106812555A
|
|
Turbo blade
|
CN106677834A
|
|
Bolt connecting structure and method connecting low-pressure turbine disc and rotor supporting conical arm
|
CN106555618A
|
|
The tip clearance control system of gas turbine and its method
|
CN106557418A
|
|
For the method and apparatus of software test
|
CN106555675A
|
|
Fan inlet cone and aviation turbofan engine gas handling system
|
CN106555619A
|
|
The control device and method in gas turbine blade gap
|