|
CN111774616A
|
|
Three-dimensional projection auxiliary assembly tool
|
|
CN111791305A
|
|
Carbon fiber composite material hole making method
|
|
CN111774613A
|
|
Dimple tool for surface machining of curved surface U-shaped groove part
|
|
CN110756868A
|
|
Milling system and method
|
|
CN110793456A
|
|
Airplane cabin door component measuring method
|
|
CN110775293A
|
|
Method for establishing measurement reference coordinate system of lower station of aircraft nose component frame
|
|
CN110842987A
|
|
Method for removing sealing adhesive bonding part on airplane
|
|
CN110816951A
|
|
Transportation mechanism for packaging and dispatching aircraft parts and method for packaging and dispatching aircraft parts
|
|
CN108994349A
|
|
Plate nut rivet hole drill jig
|
|
CN109262013A
|
|
Pilot hole device
|
|
CN108044189A
|
|
The Sandwich assemblies method for drilling of carbon fiber-containing composite material
|
|
CN108068161A
|
|
Drill dust suction auxiliary tool and drilling dust collection method
|
|
CN108057915A
|
|
/V hole guiding device
|
|
CN108032052A
|
|
Fuselage wallboard assembly jig of the cross section radian more than π and its removal method
|
|
CN108032262A
|
|
Reversible, which is repaiied to cut bracket and repair, cuts bracket group
|
|
CN107301286A
|
|
The bent jaw clamp relative rotation design method of covering longitudinal stretching shaping
|
|
CN107150136A
|
|
Multilayer module positioning drilling die
|
|
CN107161842A
|
|
Barrel-shaped skinpiston group parts lift transporter
|
|
CN106697327A
|
|
Aircraft panel butt joint structure
|
|
CN106737384A
|
|
Large-scale bushing removes device and large-scale bushing method for dismounting
|
