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INST OF HIGH-SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENTER

Overview
  • Total Patents
    43
  • GoodIP Patent Rank
    35,750
  • Filing trend
    ⇩ 100.0%
About

INST OF HIGH-SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENTER has a total of 43 patent applications. It decreased the IP activity by 100.0%. Its first patent ever was published in 2015. It filed its patents most often in China. Its main competitors in its focus markets measurement, control and transport are LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTER, LUOYANG XIYUAN VEHICLE & POWER INSPECTION INST CO LTD and SHENYANG AERODYNAMICS RES INST AVIATION IND CORP CHINA.

Patent filings in countries

World map showing INST OF HIGH-SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENTERs patent filings in countries
# Country Total Patents
#1 China 43

Patent filings per year

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

Top inventors

# Name Total Patents
#1 Zhao Zhongliang 9
#2 Wu Junqiang 8
#3 Li Yuping 7
#4 Ma Shang 7
#5 Yu Li 7
#6 Yang Haiyong 7
#7 Du Ning 6
#8 Zhang Zhengyu 6
#9 Wang Xiaobing 6
#10 Li Ping 6

Latest patents

Publication Filing date Title
CN106918435A A kind of integrated blow cylinder device
CN106837924A A kind of blow cylinder device
CN106918438A The measuring method and system of a kind of multi -components power and torque
CN106908214A The collocation method and experiment finish of high-speed wind tunnel oil stream experiment finish
CN106840576A High-speed wind tunnel oil stream test method
CN106693876A Supersonic nozzle
CN106743674A A kind of device that solid powder is sent into high velocity air
CN106767940A A kind of method for suppressing frequency of supply interference
CN106768810A A kind of high-speed wind tunnel eccentric equipment air cushion transporter and method
CN106644367A Compound large-resistance wind-tunnel strain balance
CN106815428A A kind of wind tunnel balance calibration data processing method based on intelligent optimization algorithm
CN106596037A Wind tunnel test model flow density projection field video measurement method
CN106527519A Method for controlling adjusting dynamic pressure flow field for large direct-current blow-down supersonic wind tunnel
CN106500952A The measurement apparatus of wing flexibility matrix
CN106706255A Multi-degree-of-freedom test mechanism linkage frequency phase synchronous control method
CN106644362A Mach number sensitivity analysis method for supersonic cavity flow
CN106644356A Variable Reynolds number device suitable for cavity flow wind tunnel experimental study and variable Reynolds number method thereof
CN106768797A A kind of linkage frequency plot sync control device of wind-tunnel dynamic multiple degrees of freedom test mechanism
CN106840596A One kind is applied to Asia across supersonic Cavity Flow model in wind tunnel
CN106423698A Atomizing jet method and device based on vertex ring structure