Inventor · disambiguated record
Yingdong Song
Also filed as: SONG YINGDONG
7 granted patents·5 pending applications·3 citations·filing 2002–2024
70Inventor score
Top patents by PatentIndex Score
12 records- 0186US12163860B1Methods for structural damage monitoring for whole-machine life test of small turboshaft enginesUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2024·Granted Dec 10, 2024·2 cites·8 claims
- 0258US2023184648A1Method for predicting creep damage and deformation evolution behavior with timeUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2023·Application pending·0 cites
- 0353US2024126948A1Numerical simulation optimization method of impact damage based on laser mapped solid meshUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Application pending·0 cites
- 0452US12060300B2Method for calculating gaseous diffusion and oxidation evolution of ceramic matrix composite (CMC) structureUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Granted Aug 13, 2024·0 cites·7 claims
- 0551US11965861B2Equivalent acceleration method of creep loads based on consistent failure modeUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Granted Apr 23, 2024·0 cites·6 claims
- 0651US11650143B2Method for compiling equivalent acceleration spectrum of creep under variable temperatures and loadsUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Granted May 16, 2023·0 cites·6 claims
- 0747US11644382B2High-temperature biaxial strength tester for ceramic matrix composite (CMC) turbine vane and test method thereofUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Granted May 9, 2023·0 cites·9 claims
- 0843US2023038640A1Method for calculating service life of material under action of thermal shock loadUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2022·Application pending·0 cites
- 0942US12481808B2Optimized designing method for laminate preform of ceramic matrix compositeUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2021·Granted Nov 25, 2025·0 cites·10 claims
- 1039US2022245313A1Method for calculating fluid-structure interaction response of ceramic matrix compositesUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2020·Application pending·0 cites
- 1135US2022277112A1Structural integrated design method for ceramic matrix composite bolt preformUNIV NANJING AERONAUTICS & ASTRONAUTICS·Filed 2020·Application pending·0 cites
- 1231US6798388B2Stubby, multi-band, antenna having a large-diameter high frequency radiating/receiving element surrounding a small-diameter low frequency radiating/receiving elementCENTURION WIRELESS TECH INC·Filed 2002·Granted Sep 28, 2004·1 cites·24 claims
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