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SHENYANG ENGINE DESIGN & RES INST AVIAT IND CORP CHINA

Overview
  • Total Patents
    79
About

SHENYANG ENGINE DESIGN & RES INST AVIAT IND CORP CHINA has a total of 79 patent applications. Its first patent ever was published in 2009. It filed its patents most often in China. Its main competitors in its focus markets environmental technology are GONCHAROV ALEKSEJ IVANOVICH, SHENYANG HUAJU TECH CO LTD and BENXI IRON & STEEL GROUP CO LT.

Patent filings in countries

World map showing SHENYANG ENGINE DESIGN & RES INST AVIAT IND CORP CHINAs patent filings in countries
# Country Total Patents
#1 China 79

Patent filings per year

Chart showing SHENYANG ENGINE DESIGN & RES INST AVIAT IND CORP CHINAs patent filings per year from 1900 to 2020

Focus industries

Focus technologies

Top inventors

# Name Total Patents
#1 Jia Duo 10
#2 Zhao Chunsheng 8
#3 Gao Dongwu 7
#4 Ning Huaisong 6
#5 Mao Hongtu 6
#6 An Zhe 5
#7 Jin Wendong 4
#8 Su Zhuang 4
#9 Yu Li 4
#10 Xu Su 4

Latest patents

Publication Filing date Title
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