|
CN112216181A
|
|
System and method capable of realizing single-shot training of double-shot helicopter
|
|
CN110920868A
|
|
Steering engine mounting device of automatic pilot
|
|
CN110989660A
|
|
Automatic flight control system's balancing adapter
|
|
CN110901951A
|
|
Multifunctional tail rotor test system
|
|
CN110901950A
|
|
Automatic detection test platform for helicopter electrical system
|
|
CN110905302A
|
|
Helicopter cabin door latch mechanism
|
|
CN111215930A
|
|
Finish machining positioning device and method for composite material blade fatigue test piece
|
|
CN110803297A
|
|
Airworthiness test method for single-shot performance of CCAR29 helicopters
|
|
CN110850869A
|
|
Precise positioning method and device for AGV transferring part
|
|
CN110815862A
|
|
Laying method of full-height foam sandwich airfoil surface layer
|
|
CN110804734A
|
|
Composite passivation method for stainless steel material
|
|
CN110758767A
|
|
Helicopter rotor blade simulation transparent ice structure and integration method
|
|
CN110815877A
|
|
Repair method for penetrating damage of thin-wall composite laminated structure with curvature
|
|
CN110699533A
|
|
Heat treatment furnace convenient for temperature measurement and capable of reducing temperature measurement errors
|
|
CN110823163A
|
|
Device for measuring rudder rotation angle
|
|
CN110789724A
|
|
Flexible towing nacelle retracting and releasing mechanism and method
|
|
CN110686628A
|
|
Supporting device
|
|
CN110793434A
|
|
Calibration device and calibration method for target base of laser tracker
|
|
CN110789708A
|
|
Helicopter rear horizontal tail wing structure with support rod
|
|
CN110837882A
|
|
Aircraft test flight test marking device and marking method
|
