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LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTER

Overview
  • Total Patents
    211
  • GoodIP Patent Rank
    6,906
  • Filing trend
    ⇧ 571.0%
About

LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTER has a total of 211 patent applications. It increased the IP activity by 571.0%. Its first patent ever was published in 2017. It filed its patents most often in China. Its main competitors in its focus markets measurement, transport and computer technology are SHENYANG AERODYNAMICS RES INST AVIATION IND CORP CHINA, AVIC AERODYNAMICS RES INSTITUTE and SUZHOU CHANGLING MEASUREMENT TECH CO LTD.

Patent filings in countries

World map showing LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTERs patent filings in countries
# Country Total Patents
#1 China 211

Patent filings per year

Chart showing LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTERs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Yi Xian 26
#2 Zhang Weiguo 25
#3 Xiong Jianjun 24
#4 Lai Qingren 24
#5 Zhang Rongping 22
#6 Liu Qinglin 21
#7 Lu Xiangyu 21
#8 Jiang Yubiao 20
#9 Zhao Weiming 20
#10 Zhao Xianli 20

Latest patents

Publication Filing date Title
CN112268684A Variable azimuth angle surface pressure measuring system and method for low-speed wind tunnel rotor model
CN112197933A Width-adjustable opening jet flow wind tunnel chamber and opening jet flow wind tunnel test method
CN112197713A Device and method for synchronously measuring deformation and surface pressure of helicopter rotor blade
CN112197932A Surface temperature correction method and measurement method for airplane anti-icing and deicing test model
CN112197721A Water film thickness measuring method
CN112129485A Single-vector loading method for wind tunnel mechanical balance
CN112113740A Pressure measuring device, pressure measuring method and wind tunnel local airflow deflection angle measuring method
CN112098040A Measuring device and measuring method for mounting angle of directional dynamic pressure probe
CN112066912A Synchronous measurement method and measurement device for three-dimensional surface profile and surface pressure of model
CN112014063A A stores pylon for wind-tunnel test
CN111999029A Supporting device for propeller test
CN111929026A Low-frequency pressure pulsation suppression method for wind tunnel 3/4 opening test section
CN111929025A Hot gas supply system and method for anti-icing and deicing test
CN112291025A Rotating signal equal-direction synchronous triggering acquisition method based on optical fiber slip ring
CN111929024A Icing wind tunnel air intake and height simulation system and method
CN112229596A Coaxial rigid rotor wing lift force offset wind tunnel test method and system
CN111795796A Icing wind tunnel ice prevention and removal test method and system
CN112197826A Air inlet mass flow measuring device and measuring method for aircraft engine
CN111811770A Wind tunnel model supporting device and adapter based on internal balance
CN112211726A Continuous air entraining system based on turbojet engine