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R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT CO LTD

Overview
  • Total Patents
    32
  • GoodIP Patent Rank
    49,306
About

R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT CO LTD has a total of 32 patent applications. Its first patent ever was published in 2014. It filed its patents most often in China. Its main competitors in its focus markets transport, measurement and control are SUZHOU XLPOWER ELECTRONIC TECH CO LTD, XDYNAMICS LTD and SIKORSKY AIRCRAFT CORP.

Patent filings in countries

World map showing R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT CO LTDs patent filings in countries
# Country Total Patents
#1 China 32

Patent filings per year

Chart showing R&D INST OF CHINA AVIATION IND GENERAL AIRCRAFT CO LTDs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Zeng Xiaomiao 7
#2 Zhang Wei 5
#3 Yang Jianwei 4
#4 Wu Hao 4
#5 Shi Lei 4
#6 Li Renpeng 4
#7 Liu Haitao 4
#8 Shao Junxin 3
#9 Zhao Yonghong 3
#10 Liang Wangsheng 3

Latest patents

Publication Filing date Title
CN106681342A Airplane search and rescue method
CN106672203A Hybrid composite panel-beam type structure and machining method thereof
CN106639701A Cabin door limiting and locking mechanism
CN106646082A Airplane wire harness conduction detection device based on wireless router
CN106855600A A kind of aircraft wire harness conducting wireless detection device based on RFID
CN106707857A Intelligent control system for avionics system test configuration
CN106628240A Repairing method of airplane composite material foam interlayer structure
CN106769302A A kind of method for preparing composite material defect testpieces
CN106828883A The longitudinally controlled augmentation control rule of amphibious aircraft
CN106828879A A kind of composite jointing
CN106828926A Can folding and unfolding hull bottom faulted-stage radome fairing
CN106828948A Aircraft pressure filling house steward fuel emission designs device
CN106837953A A kind of bolt connection form
CN106840620A A kind of device suitable for composite wing slow test loading
CN106828954A It is a kind of with exhibition to position stability characteristic (quality) wing pylon
CN106828884A The method that amphibious aircraft flight control system installs control augmentation stability system additional
CN106828918A A kind of Three-wing-surface vertically taking off and landing flyer
CN106840560A A kind of Novel fuel tank shakes pilot system of shaking
CN105716827A Amphibious aircraft blown flap wind tunnel test model
CN105710211A Spherical punching point closing-in die suitable for single face or double faces of paired bearings