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AVIC AERODYNAMICS RES INSTITUTE

Overview
  • Total Patents
    57
  • GoodIP Patent Rank
    26,041
  • Filing trend
    ⇩ 52.0%
About

AVIC AERODYNAMICS RES INSTITUTE has a total of 57 patent applications. It decreased the IP activity by 52.0%. Its first patent ever was published in 2016. It filed its patents most often in China. Its main competitors in its focus markets measurement, transport and computer technology are LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTER, SHENYANG AERODYNAMICS RES INST AVIATION IND CORP CHINA and EYOTO GROUP LTD.

Patent filings in countries

World map showing AVIC AERODYNAMICS RES INSTITUTEs patent filings in countries
# Country Total Patents
#1 China 57

Patent filings per year

Chart showing AVIC AERODYNAMICS RES INSTITUTEs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Mou Weiqiang 10
#2 Chen Bao 10
#3 Yan Yongchang 9
#4 Wang Jianfeng 9
#5 Shao Tianshuang 8
#6 Yu Jinge 8
#7 Wei Lihui 7
#8 Li Cong 7
#9 Zhou Guocheng 6
#10 Bu Chen 6

Latest patents

Publication Filing date Title
CN112067247A Labview-based pressure measurement system and measurement method
CN112082729A Transverse continuous measurement system and method based on fiber-optic gyroscope
CN112014060A Large-scale low-speed wind tunnel flutter test full-mode supporting device
CN112149366A Gust flow field calibration and measurement method based on flow display technology
CN112033635A Large-scale low-speed wind tunnel buffeting test wing model strutting arrangement
CN112014061A Vibration damper of oscillating blade gust generator
CN112254920A Quick installation clamping device of jumbo size model tail boom and abdomen back boom
CN112125142A Device for improving bearing capacity of mobile lift truck
CN111999031A Sudden change ground effect ground simulation device based on rotary test bed
CN111982455A Drive control device applied to tensile wire oscillation dynamic derivative test
CN112067228A Drive control device applied to 2m magnitude model dynamic derivative test
CN112082727A Control device applied to translational oscillation test of model with automatic variable attack angle
CN111829751A Flight control system and method for wind tunnel virtual flight test
CN111752882A Gyroscope SPI-RS 232 interface system and method based on ARM
CN111930041A Gyroscope RS422 conversion high-precision AO module based on ARM
CN111896215A Model supporting device for releasing two rigid body degrees of freedom of wind tunnel test model
CN112069589A Low-speed wind tunnel aerial refueling hose-taper sleeve dynamic characteristic test method
CN111288028A Low-pressure ejector device applied to Mars wind tunnel
CN111337218A Mars wind tunnel with sand simulation function
CN110793624A Sound source calibrating device used in high-speed airflow