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CHINA HELICOPTER RES & DEVELOPMENT INST

Overview
  • Total Patents
    582
  • GoodIP Patent Rank
    2,616
  • Filing trend
    ⇧ 49.0%
About

CHINA HELICOPTER RES & DEVELOPMENT INST has a total of 582 patent applications. It increased the IP activity by 49.0%. Its first patent ever was published in 2017. It filed its patents most often in China and WIPO (World Intellectual Property Organization). Its main competitors in its focus markets transport, computer technology and measurement are XIAN AIRCRAFT DESIGN INST AVIATION IND CORP CHINA, XI AN AIRCRAFT DESIGN INST AVIATION IND CORP CHINA and SHENYANG AIRCRAFT DESIGN & RES INST AVIC.

Patent filings in countries

World map showing CHINA HELICOPTER RES & DEVELOPMENT INSTs patent filings in countries

Patent filings per year

Chart showing CHINA HELICOPTER RES & DEVELOPMENT INSTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Sun Wei 17
#2 Wu Tangzhen 14
#3 Liu Zhengjiang 14
#4 Li Xinmin 14
#5 Chen Huan 14
#6 Zeng Qingji 13
#7 Deng Jinghui 13
#8 Wang Yuqi 13
#9 Zeng Jiuhai 13
#10 Chen Yaofeng 13

Latest patents

Publication Filing date Title
CN112224445A Oversleeve of perspective inspection flexible beam
CN112224437A Vehicle-mounted cabled rotorcraft system
CN112268036A Device for simulating starting load of helicopter APU
CN112213101A Durability test bed for torsion arm swing-proof bearing of helicopter
CN112238948A Quick-release helicopter tail transmission shaft assembly
CN112052608A Integrated method for war deduction simulation and efficiency evaluation
CN112180980A Autorotation landing control method of unmanned helicopter
CN112235914A Display control circuit with lamp for cabin switch plate
CN112268067A Elastic rod end bearing of helicopter rotor damper
CN112245821A Cable descending device and cable descending method
CN112229629A Self-lubricating joint bearing starting torque measuring tool and measuring method
CN112224404A Oversleeve structure for foldable bearingless rotor wing
CN112268799A Static strength and fatigue strength integrated test verification method for composite material structure
CN112213106A Helicopter APU starting load simulation system
CN112224446A High-speed coaxial dual-rotor blade tip distance measuring method based on phase distance measuring principle
CN112255138A Special fire extinguishing agent concentration measurement system inspection and maintenance method
CN112178110A Liquid elastic vibration isolator capable of achieving assembly type frequency modulation
CN112173139A Helicopter fuel pipeline integrated system
CN112214835A Rotor hovering state aerodynamic noise engineering estimation method
CN112052431A Helicopter terminal point time calculation method based on ground speed correction algorithm