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Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Beihang University has sought patent for Aircraft High-attack-angle Maneuvering Control Method Based on Angular Acceleration Estimator and Incremental Nonlinear Model Predictive Control. This invention was developed by Ling Ruonan, Zhang Zirui, Sun Liguo, Pan Yonghao, Liu Yuanji, Tan Wenqian and Shao Kan. T..

State Intellectual Property Office of China Releases Univ PLA Naval Aviation Patent Application for Student Score Category Prediction Method, System and Device Based on Knowledge G..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released Univ PLA Naval Aviation patent application for Student Score Category Prediction Method, System and Device Based on Knowledge Graph, Medium and Product. This invention was developed by Yu Yingfu, Liu Kai, Fang Wei, Xu Tao, Zhang Bingqiang and Wang Meng. ..

State Intellectual Property Office of China Releases Unit 93213 Of PLA Patent Application for Aircraft Ice Accretion Model Training Method, Prediction Method, Product, Equipment an..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released Unit 93213 Of PLA patent application for Aircraft Ice Accretion Model Training Method, Prediction Method, Product, Equipment and Medium. This invention was developed by Hu Yanbing, Wang Yuqi, Liang Danqing, Wang Xiaoting and Li Sen. The patent applica..

Kaile Cangqiong Aviation Tech Shanghai Co Ltd and Lanse Xiangliang Intelligent Tech Hangzhou Co Ltd Apply for Patent on Electric Energy Distribution Method and Equipment for Low-al..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Kaile Cangqiong Aviation Tech Shanghai Co Ltd and Lanse Xiangliang Intelligent Tech Hangzhou Co Ltd have applied Chinese patent for Electric Energy Distribution Method and Equipment for Low-altitude Aircraft and Medium. Zhang Xu, Wang Liduan, Chen Qiang, Kong Deqiang, Wu Qiong and Li Mingye developed it. Th..

Xi'an Jiaotong University and Beijing Reshu Technology Submit Chinese Patent Application for Hydrogen Energy Aircraft Fuel Stack Thermal Management System and Skin Heat Exchanger D..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Xi'an Jiaotong University and Beijing Reshu Technology have submitted a patent application for Hydrogen Energy Aircraft Fuel Stack Thermal Management System and Skin Heat Exchanger Design Method. This invention was developed by Lu Yuhao, Wang Hui, Lu Guolong, Lian Hongkui and Qu Zhiguo. The patent applicati..

China Aero-Polytechnology Establishment and China Helicopter Research And Development Institute Submit Chinese Patent Application for Aviation Equipment Environmental Adaptability ..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Aero-Polytechnology Establishment and China Helicopter Research And Development Institute have submitted a patent application for Aviation Equipment Environmental Adaptability Demand Analysis Method Based on Model. This invention was developed by Chen Yu, Zhu Yichao, Xu Lu, Peng Wangshu, Zhang Xiaojuan, ..

Beihang University and Beijing Aerospace Automatic Control Research Institute Submit Chinese Patent Application for Electronic Product Health Status Assessment Method Based on Comp..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Beihang University and Beijing Aerospace Automatic Control Research Institute have submitted a patent application for Electronic Product Health Status Assessment Method Based on Component Degradation Data. This invention was developed by Chen Juan, Han Feng, Cao Yuxuan, Yang Yuantong, Xiang Gang, Lin Ruishi, Q..

China Academy Of Aerospace Tech and Nanjing University of Aeronautics and Astronautics Apply for Patent on Method for Evaluating Vibration Fatigue Life of Liquid-filled Composite R..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Academy Of Aerospace Tech and Nanjing University of Aeronautics and Astronautics have applied Chinese patent for Method for Evaluating Vibration Fatigue Life of Liquid-filled Composite Rocket Storage Tank. Yi Min, Pan Gang, Gao Weijian, He Junqing, Shen Zhihai, Zhang Xing, Sun Renguohao and Xue Wei devel..

China Academy Of Aerospace Tech and Nanjing University of Aeronautics and Astronautics Submit Patent Application for Method for Constructing Load Spectrum of Rocket Tank

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Academy Of Aerospace Tech and Nanjing University of Aeronautics and Astronautics have submitted a patent application for Method for Constructing Load Spectrum of Rocket Tank. Yi Min, Pan Gang, Gao Weijian, He Junqing, Shen Zhihai, Zhang Xing, Sun Renguohao and Xue Wei developed the invention. The pate..

State Grid Corporation of China, State Grid Hunan Electric Power Co Limited Electric Power Science Research Institute and State Grid Hunan Electric Power Co Limited Submit Chinese ..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Grid Corporation of China, State Grid Hunan Electric Power Co Limited Electric Power Science Research Institute and State Grid Hunan Electric Power Co Limited have submitted a patent application for Unmanned Aerial Vehicle Autonomous Tower-winding Route Planning Method and Device Based on Three-dimension..

Hubei Luojia Laboratory and Wuhan University Submit Chinese Patent Application for Regional Real-time High-credibility Satellite Orbit and Clock Error Correction Product Generation..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Hubei Luojia Laboratory and Wuhan University have submitted a patent application for Regional Real-time High-credibility Satellite Orbit and Clock Error Correction Product Generation Method. This invention was developed by Kong Jian, Peng Wenjie, Yao Yibin, Chu Ruitao, Xu Chaoqian and Zhang Qi. The patent a..

Beihang University and Shenyang Aircraft Design & Research Institute AVIC Apply for Patent on Radar Distance Ambiguity Resolution Implementation Method Based on GPU

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Beihang University and Shenyang Aircraft Design & Research Institute AVIC have applied Chinese patent for Radar Distance Ambiguity Resolution Implementation Method Based on GPU. Zhang Peng, Wang Chaoyu, Hong Tao, Gan Lei, Zhang Min, Chen Jingxian, Tian Chen, Guo Qingchao, Guan Yangyang and Ju Liang developed i..

Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft File Chinese Patent Application for Method, System and Storage Medi..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft have filed a patent application for Method, System and Storage Medium for Cursor Jump of Electronic Checklist of Aircraft. This invention was developed by Wang Jiachen, Zhang Bo, Chu Jiangping, Hu J..

Zhuhai Lichuang Kexin Investment Partnership Enterprise Lp and Zhuhai Beihut City Dawan District Innovation Research Institute Apply for Patent on Unmanned Aerial Vehicle Anti-inte..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Zhuhai Lichuang Kexin Investment Partnership Enterprise Lp and Zhuhai Beihut City Dawan District Innovation Research Institute have applied Chinese patent for Unmanned Aerial Vehicle Anti-interference Passive Positioning Method and System Based on GRU and Particle Filter Fusion. Cui Tong, Zheng Dezhi, Cui Jiaw..

Zhongke Zhiyan Shandong Tech Development Co Ltd and Shandong University of Science and Technology Seek Patent for Unmanned Aerial Vehicle System in Satellite Signal Rejection Area

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Zhongke Zhiyan Shandong Tech Development Co Ltd and Shandong University of Science and Technology have sought patent for Unmanned Aerial Vehicle System in Satellite Signal Rejection Area. This invention was developed by Sun Shangqu, Du Xuzhe, Wang Kun, Li Hui and Liu Xingguang. The patent application number..

Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft Submit Patent Application for Head-up Display Image Compensation Sy..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft have submitted a patent application for Head-up Display Image Compensation System and Method for Curved Windshield. Feng Zhixiang, Zhu Xinyang, Wang Zhijia, Jin Zhefeng, Jiang Jun and Kim Ja Sung de..

State Grid Hunan Electric Power Co Ltd Information Communication Branch, State Grid Corporation of China and State Grid Hunan Electric Power Co Limited Submit Patent Application fo..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- State Grid Hunan Electric Power Co Ltd Information Communication Branch, State Grid Corporation of China and State Grid Hunan Electric Power Co Limited have submitted a patent application for Method and System for Positioning Electric Power Beidou Communication Terminal Based on Receiving Two Satellites. Zhang..

Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft Submit Chinese Patent Application for Lubricating Oil Detection Pro..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Shanghai Aircraft Design And Research Institute Commercial Aircraft Corporation Of China and Commercial Aircraft have submitted a patent application for Lubricating Oil Detection Probe Rod and Intelligent Lubricating Oil Monitoring System Comprising Same. This invention was developed by Shen Shilei, Jiang Chan..

Green Transition Alliance BV Submits WIPO Patent Application for Aircraft with Hybrid Propulsion System

Aerospace

| Wed 01 Jul 2026

Geneva, July 2 -- Green Transition Alliance BV has submitted a patent application for Aircraft with Hybrid Propulsion System. This invention was developed by Nüsseler Martin and Pischedda Luciano. The patent application number is WO2025EP85267 20251203. The patent publication number is WO2026131126 (A1). International Patent..

Henan Aerospace Fluid Control Technology Submits Patent Application for Power-level Two-way Hydraulic Control Main Valve

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Henan Aerospace Fluid Control Technology has submitted a patent application for Power-level Two-way Hydraulic Control Main Valve. Deng Tengfei, Chen Panpan, Dai Yibo, Zhang Ge, Li Cong, Cao Le, Li Yunhe, Guo Gang, Ye Wenhai and Wang Yuxian developed the invention. The patent application number is CN20251197..

Huazhi Zhuoyue Quality Tech Service Beijing Co Ltd and China Aero-Polytechnology Establishment Submit Chinese Patent Application for Aviation O-shaped Sealing Ring Service Life Pre..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Huazhi Zhuoyue Quality Tech Service Beijing Co Ltd and China Aero-Polytechnology Establishment have submitted a patent application for Aviation O-shaped Sealing Ring Service Life Prediction Method and Structure Optimization Method. This invention was developed by Bian Zhi, Wang Xiaojia, Han Zhanjie and Xu Yiha..

China Academy of Space Technology and Beijing University File Chinese Patent Application for Spacecraft Simulation Model Fidelity Verification Method Based on Behavior Comparison

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Academy of Space Technology and Beijing University have filed a patent application for Spacecraft Simulation Model Fidelity Verification Method Based on Behavior Comparison. This invention was developed by Wang Yue, Li Zewen, Chen Zihan, Zhang Xi, Yu Longjiang and Wang Ziqi. The patent application num..

Aerospace Hi Tech Holding Group Co Ltd Submits Patent Application for Uuid Configuration Method Based on Intelligent Verification

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Aerospace Hi Tech Holding Group Co Ltd has submitted a patent application for Uuid Configuration Method Based on Intelligent Verification. Huang Mingsen, Hu Xiaodong, Zhong Guangjin and Zhang Fumin developed the invention. The patent application number is CN202511918388 20251218. The patent publication numb..

Shanghai Civil Aviation Electronic System Co Ltd Submits Patent Application for Automatic Pilot Parameter Design Method Based on Linear Quadratic Regulator

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Shanghai Civil Aviation Electronic System Co Ltd has submitted a patent application for Automatic Pilot Parameter Design Method Based on Linear Quadratic Regulator. Yao Tianyu, Ma Hangshuai, Li Boya, Chen Xiliang and Tu Zixuan developed the invention. The patent application number is CN202511965970 20251224..

Univ Pittsburgh Commonwealth Sys Higher Education and Vest Inc Submit Patent Application for Devices, Systems, and Methods for Remotely Controlling Water Controls

Aerospace

| Wed 01 Jul 2026

Geneva, July 2 -- Univ Pittsburgh Commonwealth Sys Higher Education and Vest Inc have submitted a patent application for Devices, Systems, and Methods for Remotely Controlling Water Controls. Pearlman Jonathan, Hargroder Todd, Villacreces Paulina, Chovan Chris, Roy Zachary and Fadness Joel developed the invention. The patent ..

Aerospace Tianmu Chongqing Satellite Tech Co Ltd Submits Patent Application for Satellite-borne Gnss-r Sea Surface Wind Speed Fusion Method Based on Three-dimensional Variational A..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Aerospace Tianmu Chongqing Satellite Tech Co Ltd has submitted a patent application for Satellite-borne Gnss-r Sea Surface Wind Speed Fusion Method Based on Three-dimensional Variational Assimilation. Tang Qi, Zhou Yi, Hu Shuhan and Yin Yan'an developed the invention. The patent application number is CN2025..

Guangzhou Civil Aviation College Submits Chinese Patent Application for Broadband Doppler Sonar Signal Processing Method and System

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Guangzhou Civil Aviation College has submitted a patent application for Broadband Doppler Sonar Signal Processing Method and System. This invention was developed by Min Ying, Zhu Fang, Ye Baoyu and Tian Ju. The patent application number is CN20251255681 20251231. The patent publication number is CN121741715..

Xian Aircraft Design Institute Aviation Industry Corporation China Submits Patent Application for Skin Corner Connection Strength Determination Method and Device Based on Temperatu..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Xian Aircraft Design Institute Aviation Industry Corporation China has submitted a patent application for Skin Corner Connection Strength Determination Method and Device Based on Temperature Influence. Xue Yingju, Yin Li, Wang Bintuan, Li Mingqiang, Liu Yanjie and Zheng Qi developed the invention. The paten..

Shanghai Aircraft Manufacturing Files Chinese Patent Application for Part Assembly Connection Structure Batch Simulation Method, Device and Equipment and Storage Medium

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Shanghai Aircraft Manufacturing has filed a patent application for Part Assembly Connection Structure Batch Simulation Method, Device and Equipment and Storage Medium. This invention was developed by Ge Ende, Ke Yulin, Lu Hu, Wang Wei, Shi Weihui, Xing Hongwen and Lyu Lindong. The patent application number ..

State Intellectual Property Office of China Receives Northwestern Polytechnical University Patent Application for Airfoil Aerodynamic Optimization Method Based on Large-model Multi..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has received Northwestern Polytechnical University patent application for Airfoil Aerodynamic Optimization Method Based on Large-model Multi-agent System Collaboration. Sun Yu, Mi Baigang and Banwake developed the invention. The patent application number is CN2025..

State Intellectual Property Office of China Publishes Futaba Denshi Kogyo Patent Application for Attitude Control Device

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published Futaba Denshi Kogyo patent application for Attitude Control Device. The invention was developed by Tanaka Masahiro. The patent application number is CN202511346014 20250919. The patent publication number is CN121742508 (A). International Patent Class..

Wuhan Infoearth Information Submits Chinese Patent Application for Composite Cable and Unmanned Aerial Vehicle Cable Descending System

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Wuhan Infoearth Information has submitted a patent application for Composite Cable and Unmanned Aerial Vehicle Cable Descending System. This invention was developed by Hu Quanbin, Wei Ruxiang, Liu Cong, Tan Xing, Ju Ping, Yang Rui, Li Xingxing and Zeng Peng. The patent application number is CN20261029252 20..

China Helicopter Research And Development Institute Seeks Patent for Method for Verifying Performance of Key Non-metallic Material for Helicopter

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has sought patent for Method for Verifying Performance of Key Non-metallic Material for Helicopter. This invention was developed by Xu Lu, Wang Yingcong, Ai Jianbo, Zhu Bensheng, Wu Jianguo, Zheng Linfeng, Xu Tianyu, Cao Yaoqin and Liu Wenjing. The patent ..

China Academy of Aerospace Aerodynamics Submits Chinese Patent Application for Method for Predicting Surface Catalytic Ablation Coupled Aerodynamic Heat of Carbon-carbon Heat-proof..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Academy of Aerospace Aerodynamics has submitted a patent application for Method for Predicting Surface Catalytic Ablation Coupled Aerodynamic Heat of Carbon-carbon Heat-proof Material. This invention was developed by Zhou Jingyun, He Dongfeng, Jin Xuhong, Liu Yihao, Ai Bangcheng, Nie Rongxu and Miao Wenb..

China Academy of Aerospace Aerodynamics Submits Patent Application for Method and System for Calculating Sweating and Cooling Mass Flow Rate of Ablative Material

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Academy of Aerospace Aerodynamics has submitted a patent application for Method and System for Calculating Sweating and Cooling Mass Flow Rate of Ablative Material. Luo Xiaoguang, Chen Zhi, Song Liye, Gao Junjie, Ai Bangcheng, Deng Daiying, Yu Jijun and Nie Rongxu developed the invention. The patent app..

Beijing Andawell Aviation Equipment Submits Chinese Patent Application for Active Noise Reduction System and Method for Aircraft and Storage Medium

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- Beijing Andawell Aviation Equipment has submitted a patent application for Active Noise Reduction System and Method for Aircraft and Storage Medium. This invention was developed by Shen Peng, Wang Wentao, Yang Yu, Liu Hui and Wang Zhen. The patent application number is CN20261021844 20260108. The patent publi..

Chinese Aeronautical Radio Electronics Research Institute Applies for Patent on Software Fault-tolerant Design Method and System Based on End-to-end Monitoring

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Chinese Aeronautical Radio Electronics Research Institute has applied Chinese patent for Software Fault-tolerant Design Method and System Based on End-to-end Monitoring. Zhu Yifeng, Su Yu, Min Xin, Zhou Yuanhui, Fu Rongxin, Geike, Chen Du, Wang Jingbin, Chen Jianwei and Zhou Xinzhou developed it. The patent..

China Star Net Network System Research Institute Co Ltd Submits Patent Application for Test Method, Device and Equipment of Satellite Task Scheduling Algorithm, Medium and Product

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- China Star Net Network System Research Institute Co Ltd has submitted a patent application for Test Method, Device and Equipment of Satellite Task Scheduling Algorithm, Medium and Product. Zhou Kangyan, Cui Yue, Cui Bo and Wang Yao developed the invention. The patent application number is CN202511984595 202..

China Electronics Technology Group Corporation No. 14 Research Institute Submits Chinese Patent Application for Multi-radar Synchronous Satellite Orbit Determination Resource Sched..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- China Electronics Technology Group Corporation No. 14 Research Institute has submitted a patent application for Multi-radar Synchronous Satellite Orbit Determination Resource Scheduling Method Based on Reinforcement Learning. This invention was developed by Li Shikang, Li Pin, Cheng Qiang, Xu Xianzhe, Wang Yaf..

Chinese Aeronautical Radio Electronics Research Institute Seeks Patent for Multi-flight Scene Avionics Service Dynamic Scheduling Method and System

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Chinese Aeronautical Radio Electronics Research Institute has sought patent for Multi-flight Scene Avionics Service Dynamic Scheduling Method and System. This invention was developed by Luan Jianze. The patent application number is CN202511841673 20251209. The patent publication number is CN121764616 (A). I..

Avic Chengdu Aircraft Design & Research Institute Files Chinese Patent Application for Heterogeneous System Migration and Double-track Operation Method

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Avic Chengdu Aircraft Design & Research Institute has filed a patent application for Heterogeneous System Migration and Double-track Operation Method. This invention was developed by Yang Sixun, Long Bin, Luo Xiaoqi, Wu Pengwei, Li Jiajun, Geng Chenming and Zhu Yuhong. The patent application number is CN202..

Beijing Aerospace Automatic Control Research Institute Submits Chinese Patent Application for Method and Device for Creating Real-time Operating System Task, Electronic Equipment a..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Beijing Aerospace Automatic Control Research Institute has submitted a patent application for Method and Device for Creating Real-time Operating System Task, Electronic Equipment and Medium. This invention was developed by Wang Qi, Tong Xin, Liu Jian, Zhang Shu, Zhong Yu, Pang He, Lyu Yuepeng, Han Xiangyu and ..

AVIC Chengdu Aircraft Design & Research Institute Submits Chinese Patent Application for Document Automatic Generation Method Based on Hierarchical Cue Word and Rule Engine

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- AVIC Chengdu Aircraft Design & Research Institute has submitted a patent application for Document Automatic Generation Method Based on Hierarchical Cue Word and Rule Engine. This invention was developed by Cheng Xi, Ma Bo, Zhu Rui, Zhou Yan and Han Lili. The patent application number is CN202511700753 20251..

AVIC Chengdu Aircraft Design & Research Institute Submits Patent Application for Software Development Work Auxiliary System Suitable for Multi-person Assistance

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- AVIC Chengdu Aircraft Design & Research Institute has submitted a patent application for Software Development Work Auxiliary System Suitable for Multi-person Assistance. Guo Peng, Shi Jingjing, Zhang Xiaohui, Long Jinyun, Wang Jian and Zhang Chi developed the invention. The patent application number is CN20..

AVIC Chengdu Aircraft Design & Research Institute Seeks Patent for C + + Mock Class Automatic Generation Method Based on Reflection Memory Agent and Contrast Knowledge Graph

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- AVIC Chengdu Aircraft Design & Research Institute has sought patent for C + + Mock Class Automatic Generation Method Based on Reflection Memory Agent and Contrast Knowledge Graph. This invention was developed by Shi Jingjing, Guo Dong, Song Yanxiang, Xu Xiaojie, Ma Kexin and Li Chang. The patent application..

AVIC Chengdu Aircraft Design & Research Institute Submits Chinese Patent Application for Framework Component for Software Development and Construction Method Thereof

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- AVIC Chengdu Aircraft Design & Research Institute has submitted a patent application for Framework Component for Software Development and Construction Method Thereof. This invention was developed by Guo Peng, Shi Jingjing, Song Yanxiang, Zhang Chi, Ma Kexin and Li Chang. The patent application number is CN2..

AVIC Chengdu Aircraft Design & Research Institute Files Chinese Patent Application for Human-computer Interaction Task Failure Evolution Path Identification Method Based on Binary ..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- AVIC Chengdu Aircraft Design & Research Institute has filed a patent application for Human-computer Interaction Task Failure Evolution Path Identification Method Based on Binary Decision Diagram. This invention was developed by Tan Chengpeng, Zhai Qi, Deng Wei, Yang Chunbo, He Mingjun, Zhou Rui and Fan Zeng. ..

Shanghai Aerospace Control Technology Institute Submits Chinese Patent Application for Magnetic Torquer Magnetic Current Driving Real-time Compensation Method and System

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Shanghai Aerospace Control Technology Institute has submitted a patent application for Magnetic Torquer Magnetic Current Driving Real-time Compensation Method and System. This invention was developed by Zhai Xinghui, Yang Zhen, Sun Shang, Yang Yulong, Li Shengwen and Zhang Yanzhao. The patent application nu..

Ziguang Tianji Nanjing Tech Co Ltd Submits Patent Application for Unmanned Aerial Vehicle Battery Temperature Control Method, System, Device and Equipment and Storage Medium

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Ziguang Tianji Nanjing Tech Co Ltd has submitted a patent application for Unmanned Aerial Vehicle Battery Temperature Control Method, System, Device and Equipment and Storage Medium. Wang Haoyu developed the invention. The patent application number is CN202511927349 20251219. The patent publication number i..

Shanghai Institute Space Propulsion Submits Chinese Patent Application for Ground Automatic Test System and Method for Detecting On-orbit Temperature Control Function of Spacecraft

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Shanghai Institute Space Propulsion has submitted a patent application for Ground Automatic Test System and Method for Detecting On-orbit Temperature Control Function of Spacecraft. This invention was developed by Zhu Yemao, Yang Yang, Liu Shenghao, Zhang Cheng, Ji Feixiang and Cao Yaokai. The patent applic..

State Intellectual Property Office of China Releases Xi'an Chenhang Zhuoyue Tech Co Ltd Patent Application for Unmanned Aerial Vehicle Path Prediction Method, Device, Equipment and..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released Xi'an Chenhang Zhuoyue Tech Co Ltd patent application for Unmanned Aerial Vehicle Path Prediction Method, Device, Equipment and Medium. This invention was developed by Pan Quan, Liu Chenhui, Lyu Yang and Ye Liang. The patent application number is CN20..

State Intellectual Property Office of China Releases CN Academy Launch Vehicle Tech Patent Application for Variable Configuration Aircraft Control Law Intelligent Optimization Meth..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released CN Academy Launch Vehicle Tech patent application for Variable Configuration Aircraft Control Law Intelligent Optimization Method Based on Reinforcement Learning. This invention was developed by Ma Shaojie, Qiu Gongwang, Chen Keqin, Wang Haoliang, Yang B..

Changchun Changguang Boxiang Uav Co Ltd Applies for Patent on Unmanned Aerial Vehicle Guidance Method

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Changchun Changguang Boxiang Uav Co Ltd has applied Chinese patent for Unmanned Aerial Vehicle Guidance Method. Bai Yue, Wang Fan, Pei Xinbiao, Qiao Zheng and Wang Dong developed it. The patent application number is CN20251219428 20251230. The patent publication number is CN121764170 (A). International Pate..

Power Emergency Center Of State Grid Sichuan Electric Power Corp Submits Chinese Patent Application for Unmanned Aerial Vehicle Lost Multi-phased Array Fusion Homeward Voyage Contr..

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Power Emergency Center Of State Grid Sichuan Electric Power Corp has submitted a patent application for Unmanned Aerial Vehicle Lost Multi-phased Array Fusion Homeward Voyage Control Method and System. This invention was developed by Deng Chuang, Ming Ziqiang, Zhou Wei, Li Guo, Qing Dong and Nie Peng. The p..

Byd Co Limited Submits Chinese Patent Application for Unmanned Aerial Vehicle Landing Control Method, System and Related Device

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Byd Co Limited has submitted a patent application for Unmanned Aerial Vehicle Landing Control Method, System and Related Device. This invention was developed by Fan Daowei, Xu Yawen, Zhao Hongbo and Lin Guizhang. The patent application number is CN202510325590 20250318. The patent publication number is CN12..

Hualu Yiyun Tech Co Ltd Applies for Patent on Unmanned Aerial Vehicle Adaptive Obstacle Avoidance Control Method and System Based on Environment Perception

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Hualu Yiyun Tech Co Ltd has applied Chinese patent for Unmanned Aerial Vehicle Adaptive Obstacle Avoidance Control Method and System Based on Environment Perception. Zhao Chuchen, Zhao Xinyong, Gu Huinan, Zhou Wen and Ma Xuguang developed it. The patent application number is CN202610252861 20260303. The pat..

Ziguang Tianji Nanjing Tech Co Ltd Submits Chinese Patent Application for Unmanned Aerial Vehicle Garage Humidity Control Method and Device, Air Conditioner, Medium and Product

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Ziguang Tianji Nanjing Tech Co Ltd has submitted a patent application for Unmanned Aerial Vehicle Garage Humidity Control Method and Device, Air Conditioner, Medium and Product. This invention was developed by Wang Haoyu. The patent application number is CN202511857849 20251210. The patent publication numbe..

State Intellectual Property Office of China Releases Xi'an Baotong Defense Tech Co Ltd Patent Application for Unmanned Aerial Vehicle Design Optimization Method and System for Low-..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released Xi'an Baotong Defense Tech Co Ltd patent application for Unmanned Aerial Vehicle Design Optimization Method and System for Low-altitude Logistics. This invention was developed by Zhang Hang, Zhong Jingyang, Kang Zhaozhao and Zhao Gang. The patent appl..

China Helicopter Research And Development Institute Submits Patent Application for Verification Method for Single-engine Failure Training Mode of Double-engine Civil Helicopter

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Verification Method for Single-engine Failure Training Mode of Double-engine Civil Helicopter. Zhang Zhiming, Feng Hui, Zhou Lingling, Qiu Liangjun, Xu Yumao and Sun Donghong developed the invention. The patent applic..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Unmanned Aerial Vehicle Atmosphere Data Resolving Me..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Unmanned Aerial Vehicle Atmosphere Data Resolving Method and System. This invention was developed by Chen Yangming, Huang Xiankai, Duan Biao and Sun Chuanliang. The patent appl..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Helicopter Pneumatic Surface Non-uniformly Distribut..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Helicopter Pneumatic Surface Non-uniformly Distributed Load Fine Loading Method. This invention was developed by Liu Zhichao, Liu Hai, Zhang Yanhui, Wu Tangzhen, Zha Dingping, Wan..

China Helicopter Research And Development Institute Submits Chinese Patent Application for Simulation Evaluation Method for Water Emergency Evacuation Time of Personnel in Helicopt..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Simulation Evaluation Method for Water Emergency Evacuation Time of Personnel in Helicopter Cockpit. This invention was developed by Jiang Bin, Huang Lei, Xi Jinjian, Shi Chunqin and Zhao Yue. The patent application n..

State Intellectual Property Office of China Publishes China Helicopter Research And Development Institute Patent Application for Online Evaluation Data Processing Method and Device..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published China Helicopter Research And Development Institute patent application for Online Evaluation Data Processing Method and Device Based on Real-time Simulation Deduction. The invention was developed by Zhao Jun, Zhang Zemin, Du Yicong and Bai Lerong. Th..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Helicopter Coating Color Matching Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Helicopter Coating Color Matching Method. This invention was developed by Xu Yuan, Zou Yanzhang, Zhang Linfeng, Yin Jing, Zhao Kailin, Huang Lei, Zhang Jieyu and Shi Chunqin. T..

China Helicopter Research And Development Institute Seeks Patent for Method for Acquiring Body Modal Parameters of Helicopter in Sliding or Running Process

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has sought patent for Method for Acquiring Body Modal Parameters of Helicopter in Sliding or Running Process. This invention was developed by Huang Yuping, Wang Wentao, Wu Sihan, Ma Songlin, Wang Ying, Zhou Hua and Wang Zheren. The patent application numbe..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Rotor Shaft and Guide Cylinder Gap Design Method Bas..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Rotor Shaft and Guide Cylinder Gap Design Method Based on Impact Response Simulation. This invention was developed by Yu Guorui, Kong Dekui, Zhang Yingqi, Cao Zhe, Wang Weite and ..

State Intellectual Property Office of China Publishes China Aero-Polytechnology Establishment and China Helicopter Research And Development Inst Patent Application for Helicopter S..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published China Aero-Polytechnology Establishment and China Helicopter Research And Development Inst patent application for Helicopter Support System Demand Capturing Method Based on RFLP Architecture. The invention was developed by Liu Zhaoxing, Li Chunxiu, Liu ..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Scene-oriented Helicopter Low-altitude Flight Capabi..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Scene-oriented Helicopter Low-altitude Flight Capability Comprehensive Evaluation Method. This invention was developed by Li Chonghui, Wang Yang, He Tao, Li Jin, Xu Changshen and ..

China Helicopter Research And Development Institute Submits Patent Application for Loading Gravity Center Envelope Design Method of Transport Helicopter

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Loading Gravity Center Envelope Design Method of Transport Helicopter. Li Yanan, Liu Zheng, Liu Qiaoxia, Ji Guangdong, Zhang Wei, Huang Li and Feng Shengquan developed the invention. The patent application number is C..

China Helicopter Research And Development Institute Seeks Patent for Helicopter Landing Load Analysis Method Based on Model Test

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has sought patent for Helicopter Landing Load Analysis Method Based on Model Test. This invention was developed by Duan Guohe, Hua Yiqun, Han Chong, Jiang Bin and Huang Lei. The patent application number is CN202511842506 20251209. The patent publication n..

State Intellectual Property Office of China Publishes China Helicopter Research And Development Institute Patent Application for Helicopter Cockpit Control Panel Arrangement Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published China Helicopter Research And Development Institute patent application for Helicopter Cockpit Control Panel Arrangement Method. The invention was developed by Xu Yuan, Zou Yanzhang, Jiang Naiwen, Yin Jing, Huang Lei, Xi Jinjian and Shi Chunqin. The p..

China Helicopter Research And Development Institute Files Chinese Patent Application for Calculation Method for Balance Weight Required for Hanging Flag on Helicopter

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Calculation Method for Balance Weight Required for Hanging Flag on Helicopter. This invention was developed by Niu Song, Tian Bo, Tian Xu and Xu Ming. The patent application number is CN202511842491 20251209. The patent p..

State Intellectual Property Office of China Receives China Helicopter Research And Development Institute Patent Application for Rotor Wing Load Transfer Calculation Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has received China Helicopter Research And Development Institute patent application for Rotor Wing Load Transfer Calculation Method. Liu Haiqing, Yuan Xi, Yu Ruoyan and Chen Kuo developed the invention. The patent application number is CN202511842481 20251209. The..

China Helicopter Research And Development Institute Files Chinese Patent Application for Model-based Off-line Helicopter Cross-hierarchy Architecture Collaborative Modeling Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Model-based Off-line Helicopter Cross-hierarchy Architecture Collaborative Modeling Method. This invention was developed by Zhao Jun, Guo Yuqiang and Qi Keke. The patent application number is CN202511842475 20251209. The ..

China Helicopter Research And Development Institute Submits Chinese Patent Application for Helicopter Cockpit Intersection Data Design and Rapid Verification Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Helicopter Cockpit Intersection Data Design and Rapid Verification Method. This invention was developed by Zou Yanzhang, Zhang Yingying, Yin Jing, Huang Lei, Li Zheng and Fu Zhiyi. The patent application number is CN2..

China Helicopter Research And Development Institute Applies for Patent on Flexible Blade Structure Dynamics System Calculation Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has applied Chinese patent for Flexible Blade Structure Dynamics System Calculation Method. Zhou Yun, Zhou Wen, Qiu Zhixiang, Sun Bangkun, Cui Wei and Gao Bochen developed it. The patent application number is CN202511842199 20251209. The patent publication..

China Helicopter Research And Development Institute Applies for Patent on Low-resistance Propeller Hub Fairing Aerodynamic Configuration Optimization Design Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has applied Chinese patent for Low-resistance Propeller Hub Fairing Aerodynamic Configuration Optimization Design Method. Yang Yongfei, Sun Pengpeng, Gao Bochen, Tian Xu and Huang Shuilin developed it. The patent application number is CN202511842187 202512..

State Intellectual Property Office of China Publishes China Helicopter Research And Development Institute Patent Application for Multi-trailing Edge Flap Active Control Rotor Aerod..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published China Helicopter Research And Development Institute patent application for Multi-trailing Edge Flap Active Control Rotor Aerodynamic Noise Rapid Calculation Method. The invention was developed by Tian Zhongqu, Cao Yaxiong, Li Zhibin, Sun Wei, Fan Fangru..

China Helicopter Research And Development Institute Submits Patent Application for Method for Calculating Shear Deformation Component of Rectangular Sandwich Panel with Four Simply..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Method for Calculating Shear Deformation Component of Rectangular Sandwich Panel with Four Simply Supported Sides Under Normal Force. Liu Zhichao, Su Feng, Liu Qianqian, Qiao Ge and Kang Tingwei developed the invention. ..

State Intellectual Property Office of China Publishes China Helicopter Research And Development Institute Patent Application for Electric Lap Joint Design Method and Device for Com..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has published China Helicopter Research And Development Institute patent application for Electric Lap Joint Design Method and Device for Composite Mounting Plate. The invention was developed by Wang Jihuan, Sheng Chao, Wang Jun, Wan Mingjuan and Zhao Guowen. The p..

China Helicopter Research And Development Institute Seeks Patent for Sleigh Undercarriage Landing Running Dynamics Analysis Method and Device

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has sought patent for Sleigh Undercarriage Landing Running Dynamics Analysis Method and Device. This invention was developed by Huang Jianxin, Lu Zhilong, Yang Yun, Fang Jianyi, Ai Jianbo, Liu Song, Tao Zhouliang and Peng Haifeng. The patent application nu..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Method and Device for Acquiring Landing Load of Semi..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Method and Device for Acquiring Landing Load of Semi-rocker Arm Type Undercarriage. This invention was developed by Lu Zhilong, Chen Xiang, Xie Xiaoping, Li Qi and Tao Zhouliang. ..

China Helicopter Research And Development Institute Submits Chinese Patent Application for Helicopter Emergency Floating System Buoy Cabin Safety Analysis Method and System

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Helicopter Emergency Floating System Buoy Cabin Safety Analysis Method and System. This invention was developed by Shang Hao, Gao Dunlin, Wang Huaji, Li Yongliang, Xue Meiping, Jiang Bin, Ai Jianbo, Xu Longqi, Yan Liang,..

China Helicopter Research And Development Institute Submits Chinese Patent Application for Integrated Blade Root Skin Fatigue Life Analysis Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Integrated Blade Root Skin Fatigue Life Analysis Method. This invention was developed by Zhang Jiaqi, He Dingni, Tao Xianbin, Chen Dandan, Liu Junzeng and Xiong Xin. The patent application number is CN202511841763 202..

China Helicopter Research And Development Institute Applies for Patent on Tension-shear Separation Design Method for Uniaxial Load Bearing Connector and Load Connector

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has applied Chinese patent for Tension-shear Separation Design Method for Uniaxial Load Bearing Connector and Load Connector. Liu Zhichao, Zhang Xin, Ming Dehan, Wang Lipeng, Zha Dingping, Yang Chan, Wang Jiao, Wang Zhaoyong, Ma Fengfei and Li Linjie develope..

China Helicopter Research And Development Institute Files Chinese Patent Application for Method for Synthesizing Actual Measurement Load Spectrum Resultant Bending Moment of Helico..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Method for Synthesizing Actual Measurement Load Spectrum Resultant Bending Moment of Helicopter. This invention was developed by Zhang Xingguang, Yu Jianjian, Lyu Mingyue, Wang Yutang, Zhang Wei, Chen Yaping, Yang Chang and ..

China Helicopter Research And Development Institute Submits Patent Application for Method for Calculating Unsteady Aerodynamic Interference of Multi-component Combined Aircraft

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Method for Calculating Unsteady Aerodynamic Interference of Multi-component Combined Aircraft. Fan Feng, Sun Huixun, Zhang Zihan, Li Zhibin, Jiang Lusheng, Li Shangbin, Wang Xuquan, Sun Wei, Yuan Mingchuan and Niu Qingfe..

State Intellectual Property Office of China Receives China Helicopter Research And Development Institute Patent Application for Rotor Blade Structure Optimization Design Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has received China Helicopter Research And Development Institute patent application for Rotor Blade Structure Optimization Design Method. He Zihao, Jiang Qihuang, Gao Le, Zhang Shiming, Wang Siwen, Zhao Jinrui, Wei Wulei, Yu Zhihao, Cheng Yi and Huang Jian developed ..

China Helicopter Research And Development Institute Seeks Patent for Unified Blade Grid Generation Method and Device

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has sought patent for Unified Blade Grid Generation Method and Device. This invention was developed by Fan Feng, Sun Huixun, Zhang Yuni, Zhang Zihan, Li Zhibin, Jiang Lusheng, Sun Wei, Yuan Mingchuan, Wang Xuehe and Chai Chunshuo. The patent application nu..

China Helicopter Research And Development Institute Files Chinese Patent Application for Rotor Wing Shape Design Method

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Rotor Wing Shape Design Method. This invention was developed by Fan Feng, Li Zhibin, Zhang Zihan, Jiang Lusheng, Li Shangbin, Xing Shilong, Sun Wei, Wang Xuehe, Yuan Mingchuan and Chai Chunshuo. The patent application num..

State Intellectual Property Office of China Releases China Helicopter Research And Development Institute Patent Application for Aircraft Aerodynamic Characteristic Calculation Meth..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- State Intellectual Property Office of China has released China Helicopter Research And Development Institute patent application for Aircraft Aerodynamic Characteristic Calculation Method. This invention was developed by Fan Feng, Sun Huixun, Li Zhibin, Li Shangbin, Jiang Lusheng, Sun Wei, Yuan Mingchuan, Wang ..

China Helicopter Research And Development Institute Files Chinese Patent Application for Nacelle Response Calculation Method and Device for Multi-propeller Tilting Aircraft

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Nacelle Response Calculation Method and Device for Multi-propeller Tilting Aircraft. This invention was developed by He Zihao, Jiang Qihuang, Gao Le, Zhang Shiming, Wang Siwen, Zhao Jinrui, Wei Wulei, Yu Zhihao, Cheng Yi and..

China Helicopter Research And Development Institute Files Chinese Patent Application for Aeroelastic Analysis Method and Device for Multi-propeller Tilting Wing

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Aeroelastic Analysis Method and Device for Multi-propeller Tilting Wing. This invention was developed by He Zihao, Jiang Qihuang, Li Chunhua, Gao Le, Zhang Shiming, Wang Siwen, Zhao Jinrui, Yu Zhihao, Cheng Yi and Huang Jian..

China Helicopter Research And Development Institute Submits Chinese Patent Application for Active Control Aeroelastic Modeling Method and Device for Flap of Half-unfolded Tilt-roto..

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has submitted a patent application for Active Control Aeroelastic Modeling Method and Device for Flap of Half-unfolded Tilt-rotor Aircraft. This invention was developed by He Zihao, Jiang Qihuang, Gao Le, Zhang Shiming, Wang Siwen, Zhao Jinrui, Wei Wulei, Yu ..

China Helicopter Research And Development Institute Files Chinese Patent Application for Helicopter Rotor Aerodynamic Noise Data Acquisition and Processing Method and Device

Aerospace

| Thu 02 Jul 2026

Beijing, July 2 -- China Helicopter Research And Development Institute has filed a patent application for Helicopter Rotor Aerodynamic Noise Data Acquisition and Processing Method and Device. This invention was developed by Zhang Yuni, Li Zhibin, Zhang Zihan, Yang Yongfei, Li Shangbin, Jiang Lusheng, Sun Wei, Niu Qingfeng, Wang ..

World Intellectual Property Organization Releases Gladigau Fabian and Mohr Thomas Patent Application for Smartglasses Having an ESIM and a Satellite Communication Module

Aerospace

| Wed 01 Jul 2026

Geneva, July 2 -- World Intellectual Property Organization has released Gladigau Fabian and Mohr Thomas patent application for Smartglasses Having an ESIM and a Satellite Communication Module. The patent application number is WO2025EP87344 20251216. The patent publication number is WO2026131804 (A1). International Patent Cla..

Changchun Changguang Boxiang Uav Co Ltd Seeks Patent for Unmanned Aerial Vehicle Trajectory Planning Method

Aerospace

| Wed 01 Jul 2026

Beijing, July 2 -- Changchun Changguang Boxiang Uav Co Ltd has sought patent for Unmanned Aerial Vehicle Trajectory Planning Method. This invention was developed by Zhang Xiumei, Bai Yue, Pei Xinbiao, Qiao Zheng, Wang Dong and Zhu Fazheng. The patent application number is CN20251216231 20251230. The patent publication number ..

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