CN103485896A
|
|
Anti-siphon structure in oil suction inlet of lubricating oil pump
|
CN103485895A
|
|
Ultrahigh rotation speed centrifugal ventilator
|
CN103470339A
|
|
Integrated oil filter
|
CN103440381A
|
|
Thermal compensation design method for high-temperature air pipeline
|
CN103410617A
|
|
Method for determining position of hoops on engine pipelines
|
CN103422935A
|
|
Bypass valve realizing segmented overflow
|
CN103411785A
|
|
Method for measuring performance of centrifugal ventilator
|
CN103423024A
|
|
Control and suspension mechanism for binary spray pipe contraction section
|
CN103423030A
|
|
Tapered plug mechanism realizing axial symmetry spray pipe all-direction vector regulation
|
CN103411510A
|
|
Two-dimensional nozzle bottleneck height measuring mechanism
|
CN103437852A
|
|
Filter screen-integrated chip annunciator structure
|
CN103423027A
|
|
Two-dimensional thrust vectoring nozzle expanding section control mechanism
|
CN103423028A
|
|
Two-dimensional nozzle throat area control mechanism
|
CN103423026A
|
|
Vector cascade mechanism capable of enhancing stealth of S-shaped bent two-dimensional nozzle
|
CN103423768A
|
|
Bleed air purging system of dual-fuel combustor nozzle itself
|
CN103423025A
|
|
Convergent nozzle
|
CN103364191A
|
|
Large tester remote data exchange and control method
|
CN103397913A
|
|
Low-pressure turbine balancing method achieved by means of stator
|
CN103334850A
|
|
Connecting rod type two-dimensional jet pipe contraction section control mechanism
|
CN103334849A
|
|
Double-sliding beam type two-dimensional convergent-divergent nozzle control mechanism for single actuator systems
|