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AECC AERO ENGINE CONTROL SYSTEM INST

Overview
  • Total Patents
    43
  • GoodIP Patent Rank
    35,693
  • Filing trend
    0.0%
About

AECC AERO ENGINE CONTROL SYSTEM INST has a total of 43 patent applications. It increased the IP activity by 0.0%. Its first patent ever was published in 2017. It filed its patents most often in China. Its main competitors in its focus markets computer technology, control and mechanical elements are BEIJING DWIN TECH CO LTD, GUANGDONG ELECTRONICS INDUSTRY INST LTD and DSPACE GMBH.

Patent filings in countries

World map showing AECC AERO ENGINE CONTROL SYSTEM INSTs patent filings in countries
# Country Total Patents
#1 China 43

Patent filings per year

Chart showing AECC AERO ENGINE CONTROL SYSTEM INSTs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Shi Binbin 5
#2 Chu Songlin 5
#3 Li Xiaolei 5
#4 Shao Tengfei 5
#5 Zhang Wei 5
#6 Zhou Xiong 5
#7 Zhu Haolin 5
#8 Liu Nian 4
#9 Fang Geng 4
#10 Zhu Ye 4

Latest patents

Publication Filing date Title
CN111880787A Configuration development method for distributed IO (input/output) component of gas turbine control software
CN111966341A Gas turbine monitoring software event configuration method supporting event sequence customization
CN111885160A Gas turbine control software time sequence task scheduling method based on network communication
CN111880830A Automatic compiling, linking and loading method for distributed control software source code
CN111678604A Temperature field monitoring device for selective laser melting forming process
CN111322975A Device, system and method for measuring diameter of nozzle of spray pipe
CN111380691A Total pressure distortion generator
CN111190598A Gas turbine monitoring software picture configuration method based on control library drag-type development
CN111124384A JSON-based IO and control logic configuration integration method
CN110889239A Aviation gas turbine engine modeling method based on flight parameter data identification
CN110850788A Multi-electric distributed control system architecture for aircraft engine
CN110886891A Multistage valve core and solenoid valve based on flexible collision
CN110889232A Weighted average voting method for multi-system redundancy signals considering priority
CN110874503A Rapid development method for aero-engine control system product
CN110780606A Vortex shaft guide vane synchronous ring loading mechanism based on torque loading
CN110778572A Reliability and service life testing device for hydraulic valve matching parts
CN110793599A High-pressure high-low temperature fuel flow measuring system
CN110145472A A kind of impeller and spiral case gap measuring apparatus
CN110030231A A kind of online debugging device of electrohydraulic servo valve
CN109660256A The A/D error correcting circuit and modification method of preset parameter