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CHINA ACAD AEROSPACE AERODYNAMICS CAAA

Overview
  • Total Patents
    413
  • GoodIP Patent Rank
    3,617
  • Filing trend
    ⇧ 44.0%
About

CHINA ACAD AEROSPACE AERODYNAMICS CAAA has a total of 413 patent applications. It increased the IP activity by 44.0%. Its first patent ever was published in 2015. It filed its patents most often in China. Its main competitors in its focus markets measurement, transport and computer technology are INST HIGH SPEED AERODYNAMICS CHINA AERODYNAMICS RES & DEV CT, CHINA ACADEMY AEROSPACE AERODYNAMICS CAAA and AVIC AERODYNAMICS RES INSTITUTE.

Patent filings in countries

World map showing CHINA ACAD AEROSPACE AERODYNAMICS CAAAs patent filings in countries
# Country Total Patents
#1 China 413

Patent filings per year

Chart showing CHINA ACAD AEROSPACE AERODYNAMICS CAAAs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Chen Xing 35
#2 Yu Jijun 32
#3 Ou Dongbin 31
#4 Ai Bangcheng 29
#5 Chen Siyuan 27
#6 Chen Lianzhong 26
#7 Luo Xiaoguang 21
#8 Zhang Jiang 19
#9 Chen Junmou 19
#10 Dong Jingang 19

Latest patents

Publication Filing date Title
CN112235891A Arc striking circuit and arc striking method for electric arc wind tunnel heater
CN112284675A Wind tunnel for multi-body separation dynamics research
CN112197655A Rolling control method and control device for rotating missile
CN112193408A Tail wheel follow-up mechanism for solar aircraft
CN112268680A Method for improving test accuracy of rotary balance
CN112229600A Towing tank test device and method for underwater power generation kite
CN112169723A Method for preparing high-temperature high-pressure gas and application
CN112067233A Six-degree-of-freedom motion capture method for wind tunnel model
CN112124593A Small-size carry input mechanism to I heavy-duty suspended object lug
CN112124567A Folding propeller capable of bearing high-speed airflow blowing
CN112173082A Micro-vortex generating device with auxiliary control of airflow
CN112067243A Flow field temperature measuring method for high-enthalpy shock tunnel
CN112265651A Solar airplane ultra-light leading edge structure and preparation method thereof
CN112014059A Back support mechanism for wind tunnel experiment
CN112067232A Hypersonic wind tunnel test system and method for simulating rocket sled ground effect
CN112129483A Ablation ground simulation test device and method based on ablation backset compensation
CN112067241A High-enthalpy shock tunnel total temperature measurement method
CN111907731A Wing rudder surface variable parameter experiment simulation method
CN112014062A Pose measurement system and measurement method for wind tunnel free flight test model
CN112067240A Method for determining surface recovery enthalpy of flat model under arc wind tunnel condition