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SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINA

Overview
  • Total Patents
    192
  • GoodIP Patent Rank
    7,682
  • Filing trend
    ⇩ 100.0%
About

SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINA has a total of 192 patent applications. It decreased the IP activity by 100.0%. Its first patent ever was published in 2013. It filed its patents most often in China. Its main competitors in its focus markets computer technology, measurement and transport are BIOS CORP, KOMPETENZZENTRUM DAS VIRTUELLE FAHRZEUG FORSCHUNGSGESELLSCHAFT MBH and SUZHOU HANNENG NETWORK TECH CO LTD.

Patent filings in countries

World map showing SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINAs patent filings in countries
# Country Total Patents
#1 China 192

Patent filings per year

Chart showing SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINAs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Qiu Tao 11
#2 Yu Jiaxin 8
#3 Yang Xu 7
#4 Huang Jinchang 7
#5 Wang Xiangming 7
#6 Liu Liyang 6
#7 Bi Shiquan 5
#8 Yan Zhibin 5
#9 Zhang Dong 5
#10 He Xiaofan 5

Latest patents

Publication Filing date Title
CN106934130A A kind of electronic equipment Quantitative Reliability appraisal procedure
CN106899325A Pilot system when one kind is based on IRIG B yards of hardware pair
CN106934129A A kind of Engineering Structure Optimum method based on reliability
CN106406240A Negative entity modeling method
CN106529097A Airplane wiring harness laying method
CN106788743A A kind of fiber buss network system of photoelectricity mixed architecture
CN106741843A A kind of quick-release hanging point lid mechanism
CN106741975A A kind of full electric drive inlet ramp regulation and control system
CN106503411A A kind of method for designing of fuselage primary load bearing reinforcing frame
CN106741961A A kind of aircraft hanger
CN106596003A Composite aircraft fuselage section pressurizing test method
CN106769533A A kind of composite bulkhead structure four-point bending test method
CN106529096A Analyzing method for temperature field of integral fuel tank
CN106788892A multi-source heterogeneous test flight data processing method and multi-source heterogeneous test flight data processing system
CN106741834A Hanging point attachment means are carried at a kind of thin wing
CN106626434A Method for manufacturing and designing composite material bulkhead structure of airplane
CN106769089A Unmanned plane during flying performance evaluation and the flight quality integrated method for real-time monitoring of assessment
CN106774903A A kind of spare part based on gesture interaction please lead system and method
CN106709984A L-extrusion profile three-dimensional modeling method used for establishing faying surface as complex surface
CN106599486A Method for establishing aircraft wing deformable model