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AERODYNAMICS NAT KEY LAB

Overview
  • Total Patents
    13
  • GoodIP Patent Rank
    172,256
About

AERODYNAMICS NAT KEY LAB has a total of 13 patent applications. Its first patent ever was published in 2011. It filed its patents most often in China. Its main competitors in its focus markets measurement are METRICORR APS, ACTIVE IMPULSE SYSTEMS INC and WEINHOLD WOLFGANG.

Patent filings in countries

World map showing AERODYNAMICS NAT KEY LABs patent filings in countries
# Country Total Patents
#1 China 13

Patent filings per year

Chart showing AERODYNAMICS NAT KEY LABs patent filings per year from 1900 to 2020

Focus industries

# Industry
#1 Measurement

Top inventors

# Name Total Patents
#1 Zhou Zhihong 6
#2 Yi Xian 5
#3 Wu Wenhua 5
#4 Duan Yanhui 4
#5 Yu Lei 3
#6 Wang Xunnian 3
#7 Yue Shu 2
#8 Deng Xiaogang 2
#9 Zhu Guolin 2
#10 Chen Xiaodong 2

Latest patents

Publication Filing date Title
CN105333827A Ice thickness real-time measuring device for deicing experiment
CN105277485A Ice and object surface adhesion force measuring device
CN105059530A Sharp vertex osculation tapered wave-rider with controllable sweepback
CN105059531A Osculating cone waverider with curve head and controllable sweepback angle
CN104931228A Double-body super-high aspect ratio aircraft wind tunnel force measurement test supporting device
CN104554739A Air inlet lip for improving and adjusting course stability of double-engine wing-body blending tailless configuration
CN104354867A Design method of big supercooling water droplet icing detector and detector
CN104268399A Computing method of model parameters in icing wind tunnel experiment under supercooled large droplet condition
CN104180980A External wind turbine freezing detector and wind turbine freezing detecting method
CN103407580A Manufacturing method of light aerofoil with super-high aspect ratio and high lift-drag ratio and aerofoil manufactured thereby
CN102880589A Complex configuration flow-around finite difference simulation method for detecting grid quality
CN102750259A Method for simulating flow around complex configuration by utilizing non-equidistant mapping finite difference
CN103177646A Whisker enhanced photosensitive resin aero-elastic high-speed wind tunnel test model