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CHINA AERO ENGINE RES INSTITUTE

Overview
  • Total Patents
    34
  • GoodIP Patent Rank
    46,326
  • Filing trend
    ⇧ 140.0%
About

CHINA AERO ENGINE RES INSTITUTE has a total of 34 patent applications. It increased the IP activity by 140.0%. Its first patent ever was published in 2017. It filed its patents most often in China. Its main competitors in its focus markets engines, pumps and turbines, computer technology and measurement are HUNAN HANGXIANG GAS TURBINE CO LTD, SZYDLOWSKI JOSEPH and CHAIR R S DE.

Patent filings in countries

World map showing CHINA AERO ENGINE RES INSTITUTEs patent filings in countries
# Country Total Patents
#1 China 34

Patent filings per year

Chart showing CHINA AERO ENGINE RES INSTITUTEs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Jia Zhigang 7
#2 Yan Wenhui 4
#3 Yang Qian 4
#4 Shao Dong 4
#5 Yuan Shanhu 4
#6 Miao Hui 4
#7 Zhang Changxian 3
#8 Xu Jinchun 3
#9 Zhang Xuening 3
#10 Zhu Jiangnan 3

Latest patents

Publication Filing date Title
CN111577466A Ice-proof bleed air preheating and turbine cooling bleed air precooling system for aircraft engine
CN111577467A Spliced heat exchanger for high-speed air suction type engine
CN110953187A Transonic compressor plane cascade with bionic sawtooth tail edge structure
CN110985410A Transonic compressor plane cascade with bionic wavy structure leading edge
CN110449309A A kind of fluidic oscillator array and its frequency synchronization method
CN110259883A The damping structure Vibration Absorption Designing method of integral blade disk
CN110259600A Double outer adaptive cycle engines of culvert
CN110276125A Aero-engine overall performance slump evaluations and prediction technique based on data
CN110108577A Thin-wall construction axial bending loading device
CN110131208A The fan propeller of variable-diameter and established angle based on hydraulic-driven
CN110131207A Using the engine blower and its diameter adjustment method of the variable-diameter of hydraulic-driven
CN110107426A Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky
CN110107401A Across medium flight device power device based on empty water flow passage compact layout
CN109973224A Aircraft engine oil cooling system and method
CN110131048A Self contained internal combustion wave rotor igniter and method
CN110107917A The conduit gas curtain extinguishing combustion chamber of radial fuel oil classification
CN110107915A Main chamber triple channel dump diffuser
CN108891595A Across the medium flight device power device sealed using medium sensing device and duct
CN108984874A Obtain the method for numerical simulation in the flow field of potential flows
CN108799199A The design method of high load capacity allowance camber is adjustable tandem cascade