Patents by Inventor Jiaju WU

Jiaju WU has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • SYSTEM AND METHOD FOR MONITORING LUBRICANT OF AN ENGINE
    Publication number: 20150068289
    Abstract: The present invention relates to a system and method for monitoring lubricant of an engine. The system for monitoring lubricant of an engine comprises: a lubricant sensor, which measures lubricant quantity of the engine; a data acquisition unit, which collects the lubricant quantity of the engine from the lubricant sensor at a fixed time interval; and a message generation unit, which generates lubricant quantity monitoring messages according to the lubricant quantity of the engine collected by the data acquisition unit.
    Type: Application
    Filed: July 23, 2014
    Publication date: March 12, 2015
    Inventors: Dechao Zhong, Zhuping Gu, Huifeng Ding, Jiaju Wu, Lei Huang, Bingzheng Wang, Hongtao Ma, Lei Chen, Yi Zhu
  • Method for detecting whether performance of aircraft components is in the deterioration period
    Patent number: 8798848
    Abstract: The present application discloses a method for detecting whether performance of an aircraft component is in a decline period, comprising: obtaining one or more detection parameters reflecting operation status of the aircraft component; comparing data of the one or more detection parameters with respective desired values; and determining whether the performance of the aircraft component is in the decline period based on a comparison result.
    Type: Grant
    Filed: July 6, 2012
    Date of Patent: August 5, 2014
    Assignee: Air China Limited
    Inventors: Zhuping Gu, Huifeng Ding, Fengliang Zheng, Yubin Wu, Jiaju Wu, Yi Zhu, Bingzheng Wang, Hongtao Ma, Lei Huang
  • METHOD FOR DETECTING PERFORMANCE OF AN AIRCRAFT BASED ON A CUSTOMIZED MESSAGE
    Publication number: 20130197721
    Abstract: The present invention relates to a method for detecting the performance of the aircraft comprising: collecting data reflecting operation status of the aircraft; generating the customized message based on the collected data, wherein, the customized message is configured to include one or more main parameters related to the operation status of the aircraft; storing or transmitting the customized message; and detecting the performance of the aircraft based on the customized message.
    Type: Application
    Filed: July 26, 2012
    Publication date: August 1, 2013
    Applicant: AIR CHINA LIMITED
    Inventors: Zhuping GU, Jiaju WU, Fengliang ZHENG, Lei HUANG, Minjie TANG
  • METHOD FOR DETECTING WHETHER PERFORMANCE OF AIRCRAFT COMPONENTS IS IN THE DETERIORATION PERIOD
    Publication number: 20130179028
    Abstract: The present application discloses a method for detecting whether performance of an aircraft component is in a decline period, comprising: obtaining one or more detection parameters reflecting operation status of the aircraft component; comparing data of the one or more detection parameters with respective desired values; and determining whether the performance of the aircraft component is in the decline period based on a comparison result.
    Type: Application
    Filed: July 6, 2012
    Publication date: July 11, 2013
    Applicant: AIR CHINA LIMITED
    Inventors: Zhuping GU, Huifeng DING, Fengliang ZHENG, Yubin WU, Jiaju WU, Yi ZHU, Bingzheng WANG, Hongtao MA, Lei HUNAG
  • METHOD FOR DETECTING THE LANDING QUALITY OF AN AIRCRAFT
    Publication number: 20130030614
    Abstract: The present invention relates to a method for detecting landing quality of an aircraft, comprising: determining whether a vertical speed rate is greater than a first preset value or a vertical acceleration is greater than a second value when the aircraft landing; collecting landing data; generating a landing message based on collected landing data in response to that the vertical speed rate is greater than the first preset value or the vertical acceleration is greater than the second value when the aircraft landing; storing or transmitting the landing message; and determining the landing quality of the aircraft based on the landing data in the landing message.
    Type: Application
    Filed: July 26, 2012
    Publication date: January 31, 2013
    Applicant: AIR CHINA LIMITED
    Inventors: Huifeng DING, Jiaju WU, Yubin WU, Yi ZHU, Minjie TANG, Zhiping HUANG, Lei CHEN, Jiang YUAN