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ULTRA HIGH SPEED AERODYNAMICS INST CHINA AERODYNAMICS RES & DEVELOPMENT CT

Overview
  • Total Patents
    292
  • GoodIP Patent Rank
    4,994
  • Filing trend
    ⇧ 925.0%
About

ULTRA HIGH SPEED AERODYNAMICS INST CHINA AERODYNAMICS RES & DEVELOPMENT CT has a total of 292 patent applications. It increased the IP activity by 925.0%. Its first patent ever was published in 2016. It filed its patents most often in China. Its main competitors in its focus markets measurement, computer technology and mechanical elements are LOW SPEED AERODYNAMICS INSTITUTE OF CHINA AERODYNAMICS RES AND DEVELOPMENT CENTER, SHENYANG AERODYNAMICS RES INST AVIATION IND CORP CHINA and SUZHOU CHANGLING MEASUREMENT TECH CO LTD.

Patent filings in countries

World map showing ULTRA HIGH SPEED AERODYNAMICS INST CHINA AERODYNAMICS RES & DEVELOPMENT CTs patent filings in countries
# Country Total Patents
#1 China 292

Patent filings per year

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

Top inventors

# Name Total Patents
#1 Xu Xiaobin 49
#2 Lyu Zhiguo 41
#3 Zhao Rongjuan 38
#4 Zhu Tao 34
#5 Yang Yanguang 32
#6 Qiu Huacheng 31
#7 Liao Zhenyang 30
#8 Liu Sen 29
#9 Zhong Yong 27
#10 Min Fu 25

Latest patents

Publication Filing date Title
CN112222669A Welding seam structure and manufacturing method thereof
CN112128441A High-pressure gas quick valve
CN112197051A Pipeline protection device
CN112229595A Device and method for improving local vacuum degree of pulse wind tunnel
CN112215830A Method for judging impact damage characteristic types of aerospace heat-proof materials
CN112284676A Model supporting device applied to wind tunnel test
CN112233099A Reusable spacecraft surface impact damage characteristic identification method
CN112284674A Electromagnet hanging and throwing device for hypersonic wind tunnel model free flight test
CN112213069A Flow field calibration and measurement bent frame with cooling structure for hypersonic high-temperature wind tunnel
CN112158362A Resistance-reducing and heat-reducing device and method for spacecraft
CN112179607A Wind tunnel diaphragm clamping device
CN112093701A Jacking structure and jacking device
CN111947882A Transient heat flow sensor and testing method thereof
CN112179522A Aircraft surface temperature sensor testing system and testing method
CN112067193A Aircraft surface pressure sensor testing device and testing method
CN112066749A Double-row blade air inlet distributor for vacuum high-temperature equipment
CN112066019A Horizontal vacuum baffle valve
CN112016627A Visual detection and evaluation method for micro-impact damage of on-orbit spacecraft
CN112037211A Damage characteristic identification method for dynamically monitoring small space debris impact event
CN112016628A Space debris impact damage interpretation method based on dynamic multi-target prediction