Learn more

BEIJING KONGTIAN TECH RESEARCH INSTITUTE

Overview
  • Total Patents
    63
  • GoodIP Patent Rank
    23,387
  • Filing trend
    ⇩ 31.0%
About

BEIJING KONGTIAN TECH RESEARCH INSTITUTE has a total of 63 patent applications. It decreased the IP activity by 31.0%. Its first patent ever was published in 2016. It filed its patents most often in China. Its main competitors in its focus markets measurement, computer technology and environmental technology are SHENYANG AIRCRAFT DESIGN INST AVIATION IND CORP CHINA, STATE KEY LABORATORY OF AERODYNAMICS and XI AN AIRCRAFT DESIGN INST AVIATION IND CORP CHINA.

Patent filings in countries

World map showing BEIJING KONGTIAN TECH RESEARCH INSTITUTEs patent filings in countries
# Country Total Patents
#1 China 63

Patent filings per year

Chart showing BEIJING KONGTIAN TECH RESEARCH INSTITUTEs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Luo Jinling 16
#2 Song Yue'E 15
#3 Li Jing 14
#4 Kang Honglin 14
#5 Wu Ningning 13
#6 Zhou Dan 13
#7 Zhu Guoxiang 13
#8 Ma Yinwei 13
#9 Zhang Fan 11
#10 Cao Jie 11

Latest patents

Publication Filing date Title
CN109850167A A kind of two-way oil valve and its design method
CN109900486A A kind of winged hot aeroperformance acquisition methods of aircraft of band
CN109918765A Thermal environment couples Precise computation in a kind of high-speed aircraft cabin
CN109595076A A kind of air intake duct protective cover
CN109488484A Three-level is entered the orbit Reusable Launch Vehicles and its application method
CN109632886A Fine hot certification test system and method in a kind of high-speed aircraft cabin
CN109612676A Aerodynamic parameter reverse calculation algorithms based on test flight data
CN109460626A Punching engine performance parameter calculation method
CN109592035A High speed information platform and its application method can be suspended
CN109955392A A kind of heat insulation structural method for repairing and mending
CN109975205A A kind of adhesive asserably performance estimating method
CN109611572A Gas pressure reducer
CN109612675A The full servo full bridge aero-elastic model that plays verifies ground experiment method
CN109583067A High-speed aircraft based on equalized temperature turns to twist position measurement sensor design method
CN109367795A Fuselage bilateral air inlet high-speed aircraft aerodynamic arrangement
CN109238634A Hypersonic aircraft model in wind tunnel rudder-face device
CN109131821A A kind of slidable connection structure
CN109026924A Cold and hot slidable connection structure
CN109299499A Consider the multi-step optimum structure design method and aircraft of modifying factor
CN108827588A Rocket prizes design method and rocket sled