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AVIC AERODYNAMICS RES INST

Overview
  • Total Patents
    60
  • GoodIP Patent Rank
    32,390
About

AVIC AERODYNAMICS RES INST has a total of 60 patent applications. Its first patent ever was published in 2009. It filed its patents most often in China. Its main competitors in its focus markets measurement, control and transport are FEDERALNOE GOSUDARSTVENNOE UNITARNOE PREDPRIYATIE SIBIRSKIJ NAUCHNO ISSLEDOVATELSKIJ INST AVIATSII I, FEDERALNOE GOSUDARSTVENNOE UNITARNOE PREDPRIYATIE TSENTRALNYJ AEROGIDRODINAMICHESKIJ INST IMENI PROF and DYNAMIC ENG INC.

Patent filings in countries

World map showing AVIC AERODYNAMICS RES INSTs patent filings in countries
# Country Total Patents
#1 China 60

Patent filings per year

Chart showing AVIC AERODYNAMICS RES INSTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Liu Guozheng 13
#2 Duo Meng 12
#3 Zhang Wei 11
#4 Zhang Guoyou 9
#5 Ming Qiang 9
#6 Zhou Wen 8
#7 Cui Lidong 8
#8 You Liang 8
#9 Yu Jinge 8
#10 Niu Zhongguo 7

Latest patents

Publication Filing date Title
CN106525385A Model integrated type flat/vertical fin aerodynamic force measurement device
CN106788328A A kind of external trigger signal switched filter for wind tunnel test acquisition system
CN106500950A A kind of efficient large scale injection piping installation of air intake test
CN106768630A Mono-pendulum type guided missile model rotation inerttia mechanism and its measuring method
CN106240797A A kind of wing improving band sawtooth swept-back wing transonic speed maneuvering characteristics
CN106275387A A kind of band sawtooth swept-back wing that improves transonic speed is fallen off the wing of characteristic
CN106240799A A kind of wing improving band sawtooth swept-back wing transonic speed horizontal flight quality
CN105300653A Test section upper and lower rotating disk offset induction apparatus
CN105353764A Motion sensing type operating instrument for wind tunnel free flying test
CN105277333A Fusion-type muffler corner apparatus
CN105486481A Low-speed wind tunnel expansion section tensioning mechanism
CN105352703A Curved knife slide block angle-varying mechanism based on bevel pulley guiding and angle-varying method
CN105486453A Test equipment for measuring inertial load of aircraft under vacuum condition
CN105387992A Airfoil profile support device and support method
CN105242707A Temperature remote monitoring alarm system based on multi-point acquisition
CN105203253A Multi-range pressure measuring segmentation collecting control method suitable for wind tunnel experiment
CN105181292A Multi-measuring range pressure measurement device with purging function
CN105021337A Propeller driving rotation force measuring apparatus and force measuring method
CN105021370A Low speed high Reynolds number wind tunnel semi model force balance and force-measuring method
CN105021367A Portable tracer particle generator apparatus based on pressure atomization and generation method