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SHENYANG AERODYNAMICS RES INST AVIATION IND CORP OF CHINA

Overview
  • Total Patents
    20
  • GoodIP Patent Rank
    83,406
About

SHENYANG AERODYNAMICS RES INST AVIATION IND CORP OF CHINA has a total of 20 patent applications. 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 macromolecular chemistry and polymers are SHENYANG AERODYNAMICS RES INST AVIATION IND CORP CHINA, ELECTRO SCAN INC and ATC INC.

Patent filings in countries

World map showing SHENYANG AERODYNAMICS RES INST AVIATION IND CORP OF CHINAs patent filings in countries
# Country Total Patents
#1 China 20

Patent filings per year

Chart showing SHENYANG AERODYNAMICS RES INST AVIATION IND CORP OF CHINAs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Zhao Ronghuan 5
#2 Zhong Hongjie 5
#3 Shang Jinkui 5
#4 Wang Peng 5
#5 Zhao Min 5
#6 Wang Tianxu 4
#7 Zhang Huaming 3
#8 Yang Ximing 3
#9 Wang Meng 3
#10 Pan Jinzhu 3

Latest patents

Publication Filing date Title
CN106706261A Balance measuring device used for rolling rotation derivative experiment
CN106768816A A kind of pitching dynamic derivative experimental provision of tail vibration
CN106675298A Novel temperature-sensitive coating for temperature measurement and preparation method
CN106752583A A kind of porous type simple component fast-response pressure sensitive coating formula and compound method
CN106768600A A kind of simple component fast-response pressure sensitive coating and matching method
CN106679923A Pressure decoupling apparatus for high-speed jet-flow impact force-measuring model
CN106679925A High-precision control device and control method for micro-mass jet flow rate
CN106768815A A kind of real-time multi-axis synchronized control measuring system
CN106525381A Mach number adjusting mechanism suitable for trans-supersonic wind tunnel
CN106768801A A kind of double rotary shaft yaw angle converting means of high accuracy for wind tunnel test
CN106768800A A kind of model supporting device for multiple aircraft formation wind tunnel test
CN106525386A Conventional loading head inner sleeve position adjusting device for strain balance calibration
CN106404339A Clipping wallboard device for transonic-speed test section
CN106706260A System for precisely controlling total temperature of continuous transonic wind tunnel
CN106501227A Measuring method based on pressure sensitive coating probe molecule fluorescence lifetime
CN106289713A The data collecting system measured for revolving part Life method PSP
CN106218904A Runner type Push-pull Flow dynamic control device in a kind of supersonic inlet
CN106218865A A kind of aircraft precursor eddy current dynamic control device
CN106441785A Support mechanism for small propulsion device inlet engine compatibility test in intermittent wind tunnel
CN105527070A Device for stabilizing atmospheric pressure for wind tunnel gauge pressure sensor and method for stabilizing air pressure