CN112033337A
|
|
Quick detection device of plunger sphere circularity
|
CN112069756A
|
|
Programmable logic verification architecture and implementation method thereof
|
CN112068430A
|
|
Electro-hydraulic proportional valve dead zone compensation algorithm and compensation system
|
CN112069122A
|
|
General computer architecture for two-by-two and two-out and implementation method thereof
|
CN112054309A
|
|
Multi-frequency-band electromagnetic wave absorption structure and method
|
CN112073068A
|
|
Input/output circuit of general analog signal and using method thereof
|
CN112068985A
|
|
NORFLASH memory ECC (error correction code) error detection and correction method and system with programming instruction identification function
|
CN112104489A
|
|
High-speed real-time data capturing method without interference to communication
|
CN112068867A
|
|
On-line loading architecture and loading method for multifunctional board software in flight control computer
|
CN112122428A
|
|
Device and method for finishing orifice of tiny part
|
CN112077791A
|
|
Device and method for controlling assembly precision of tiny precise component
|
CN111898980A
|
|
Method for automatically issuing electronic files and printing and issuing paper files in batches
|
CN111980982A
|
|
Positive displacement hydraulic safety device
|
CN111930036A
|
|
Main-standby control switching system and method for civil aircraft actuator
|
CN111930096A
|
|
Flight control system servo valve connection fault diagnosis method
|
CN111959799A
|
|
Stall protection method for civil passenger plane
|
CN111988364A
|
|
Servo control electronic system and REU instruction conversion method thereof
|
CN111976955A
|
|
Method and device for processing single-side jamming fault of civil aviation flight control double-steering-column disk
|
CN111947869A
|
|
Servo flutter test system and safety protection method for flight control system in flutter test
|
CN111980977A
|
|
Cross power control valve for duplex hydraulic pump and duplex hydraulic pump
|