CN106240842A
|
|
A kind of asymmetric fuselage bulkhead four-point bending test method and device
|
CN106154827A
|
|
A kind of servo-control signal compensation method
|
CN106202699A
|
|
A kind of sensitivity method for solving under many displacement constraints
|
CN106240841A
|
|
A kind of gear test charger
|
CN106240840A
|
|
A kind of wing-box assay device of bending loading
|
CN106248322A
|
|
A kind of wing-box assay device of curved scissors loading
|
CN106168603A
|
|
A kind of temperature compensation in Lamb wave monitoring structural health conditions
|
CN106058792A
|
|
Openable flat cable outlet assembly
|
CN106153721A
|
|
A kind of crack in bolt detection method and screw thread crack detection device
|
CN106168556A
|
|
A kind of anti-unstability device for docking wall strength test
|
CN105857638A
|
|
Wing load applying device
|
CN106015762A
|
|
Wire sealing device
|
CN106114901A
|
|
A kind of noise and pitotstatic charger
|
CN106153735A
|
|
A kind of fatigue crack manual simulation method of bolt reference block
|
CN106153080A
|
|
A kind of packaged type piezoelectric transducer and using method
|
CN106081157A
|
|
A kind of vertical following loading device
|
CN105606357A
|
|
Aircraft static strength test loading device
|
CN105728068A
|
|
Environmental chamber with pressure balance control function
|
CN105843996A
|
|
Optimization method of heat-proof structure
|
CN105836155A
|
|
Double-layer floor beam loading device for aircraft structural strength test
|