CN112199785A
|
|
Method and device for acquiring fatigue life of ship bottom skin of amphibious aircraft
|
CN112193399A
|
|
Spherical airtight end frame with large opening
|
CN112278295A
|
|
Airplane lubricating oil tank capable of recovering oil gas
|
CN112238940A
|
|
A flotation pontoon structure for amphibious aircraft
|
CN112193400A
|
|
Supercharging rear end frame with large opening
|
CN112173162A
|
|
Propeller flexible installation device
|
CN111745985A
|
|
Full-composite material aileron glue joint method and full-composite material aileron
|
CN111762336A
|
|
Full-composite material flap and gluing method thereof
|
CN110744835A
|
|
Sand grain pressurizing auxiliary method for composite material fiber ship body
|
CN110608707A
|
|
Online testing system and method for attack angle sensor
|
CN110626493A
|
|
Electric retraction control system based on large aircraft landing gear
|
CN110672001A
|
|
Method and device for measuring thickness of non-ferromagnetic material on surface of ferromagnetic material
|
CN110815864A
|
|
Forming process method for composite material part with complex profile
|
CN110803298A
|
|
Device and method for determining neutral position of control surface of airplane
|
CN110815662A
|
|
Method for designing mould of composite profiled pipe
|
CN110657923A
|
|
Test device and method for detecting water tightness of airplane body
|
CN110861157A
|
|
Auxiliary tool for dimple of part
|
CN110543161A
|
|
Static test device for control box of airplane direct current generator
|
CN110530575A
|
|
A kind of amphibious aircraft watertight test verifying system of large size and verification method
|
CN110207684A
|
|
A kind of airborne radio direction finder outfield automated calibration system and method
|