Learn more

SHENYANG AIRCRAFT DESIGN & RES INST AVIC

Overview
  • Total Patents
    510
  • GoodIP Patent Rank
    2,967
  • Filing trend
    ⇧ 160.0%
About

SHENYANG AIRCRAFT DESIGN & RES INST AVIC has a total of 510 patent applications. It increased the IP activity by 160.0%. Its first patent ever was published in 2015. It filed its patents most often in China. Its main competitors in its focus markets transport, computer technology and measurement are SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINA, XI'AN AIRCRAFT DESIGN INST OF AVIATION INDUSTRY CORPORATION OF CHINA and XI AN AIRCRAFT DESIGN INST AVIATION IND CORP CHINA.

Patent filings in countries

World map showing SHENYANG AIRCRAFT DESIGN & RES INST AVICs patent filings in countries
# Country Total Patents
#1 China 510

Patent filings per year

Chart showing SHENYANG AIRCRAFT DESIGN & RES INST AVICs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Wu Bin 29
#2 Wang Xiangming 27
#3 Sun Zhixiao 24
#4 He Qianqiang 20
#5 Zhang Shaoqing 19
#6 Yuan Qiangbo 18
#7 Li Zhipeng 17
#8 Xing Bendong 17
#9 Bi Shiquan 17
#10 Zhang Xuefei 16

Latest patents

Publication Filing date Title
CN112215499A Method for determining availability of use of unmanned aerial vehicle group, electronic device, and readable access medium
CN112200470A Configuration method for transition airplane support equipment
CN112230674A Multi-machine collaborative route planning method and system based on niche particle swarm algorithm
CN112214930A Multi-machine collaborative route planning method and system based on collaborative particle swarm optimization algorithm
CN112254734A Economic navigation resolving method based on efficient sequencing algorithm
CN112179350A Cruise calculation method based on efficient sequencing algorithm
CN112229406A Redundancy guide full-automatic landing information fusion method and system
CN112215414A Multi-machine collaborative route planning method and system based on similarity model
CN112173122A Unmanned aerial vehicle aerial recovery device and method
CN112213070A Device for simulating suspension clearance of plug-in under flutter wind tunnel test wing
CN112045192A Manufacturing method of outer cylinder of aircraft landing gear
CN112027056A Band plate and skin connecting structure thereof
CN112027058A Self-rotating pull rod structure
CN112197034A One-way throttle valve
CN112045193A Outer cylinder of aircraft landing gear and landing gear thereof
CN112027053A Framework structure of frame beam of middle fuselage of airplane
CN112035964A Fuselage reinforcing frame material distribution design method and fuselage reinforcing frame thereof
CN112124571A Outer cylinder of aircraft landing gear, manufacturing method and aircraft landing gear
CN112032230A Method for determining performance of torsion spring with rectangular section
CN112035963A Cabin door structure design method