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INST HIGH SPEED AERODYNAMICS CHINA AERODYNAMICS RES & DEV CT

Overview
  • Total Patents
    236
  • GoodIP Patent Rank
    6,335
  • Filing trend
    ⇧ 59.0%
About

INST HIGH SPEED AERODYNAMICS CHINA AERODYNAMICS RES & DEV CT has a total of 236 patent applications. It increased the IP activity by 59.0%. Its first patent ever was published in 2012. It filed its patents most often in China. Its main competitors in its focus markets measurement, computer technology and transport are AVIC AERODYNAMICS RES INSTITUTE, CHINA ACAD AEROSPACE AERODYNAMICS CAAA and LOW SPEED AERODYNAMIC INST CHINESE AERODYNAMIC RES AND DEV CT.

Patent filings in countries

World map showing INST HIGH SPEED AERODYNAMICS CHINA AERODYNAMICS RES & DEV CTs patent filings in countries
# Country Total Patents
#1 China 236

Patent filings per year

Chart showing INST HIGH SPEED AERODYNAMICS CHINA AERODYNAMICS RES & DEV CTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Tao Yang 34
#2 Zhang Lin 27
#3 Wu Junqiang 27
#4 Lu Bo 25
#5 Yu Li 24
#6 Lin Jun 24
#7 Xiong Neng 24
#8 Guo Hongtao 24
#9 Liu Dawei 22
#10 Liu Guangyuan 22

Latest patents

Publication Filing date Title
CN112098036A Interference force calibration device and method for wind tunnel test blade supporting device
CN112238932A Aircraft flutter suppression device and aircraft thereof
CN112124562A Aircraft and aircraft control method thereof
CN112098035A Aircraft test system
CN111999030A Three-dimensional oil flow VR (virtual reality) online measurement and display system and working method thereof
CN112014064A Wind tunnel complex flow color fluorescent oil flow test method
CN112001991A High-speed wind tunnel dynamic oil flow map image processing method
CN112268676A Supersonic wind tunnel model pitching motion protection device
CN112268675A Intelligent false strut device for high-speed wind tunnel
CN112229598A Water-cooling support rod and machining method thereof
CN112268677A Forced rock test device for high-speed wind tunnel
CN112230669A Method for judging influence of pitching rate of aircraft on rolling motion stability
CN112268678A Free rock test device for high-speed wind tunnel
CN112268682A Method for predicting single-degree-of-freedom rock-roll characteristic of aircraft
CN112229597A Tracer particle generator for large-scale high-speed wind tunnel PIV test
CN112197934A Tracer particle concentration control method for large-scale high-speed wind tunnel PIV test
CN112179611A Device for generating large-scale high-speed wind tunnel PIV tracer particles and remotely controlling flow
CN112171628A Device for replacing solid spray pipe of high-speed wind tunnel
CN112171203A Machining method of microporous spray pipe
CN112113704A Pressure-sensitive paint response time calibration method based on non-electric detonator driving type shock tube