Patents by Inventor Mei DING

Mei DING 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).

  • Publication number: 20230110203
    Abstract: The present disclosure relates to methods of treating patients suffering from interleukin (IL)-33-mediated disorders and methods for determining whether a patient is at increased risk of suffering from an IL-33-mediated disorder or determining whether a patient suffering from a disorder has an increased chance of responding to an anti-IL-33 therapy.
    Type: Application
    Filed: March 11, 2021
    Publication date: April 13, 2023
    Inventors: Adam Samuel PLATT, Hans Daniel MUTHAS, Monica Lynn GAVALA, Jingya WANG, Benjamin Felix GEORGI, Mei DING
  • Patent number: 10815002
    Abstract: The present disclosure relates to a structural component of an aircraft wing body and an aircraft including the structural component. According to an aspect of the present disclosure, a structural component of an aircraft wing body is provided. The structural component includes a body part and a profile. The body part includes an edge portion formed by end portions of a first skin and a second skin of the body part superposed together. The profile is attached to the edge portion. The profile has an outer profile conforming to an outer profile of the body part such that the structural component, as a whole, exhibits an aerodynamic outer profile after the profile is attached to the edge portion. The profile is attached to the edge portion via a plurality of separate intermediate members or by contacting the edge portion.
    Type: Grant
    Filed: May 22, 2017
    Date of Patent: October 27, 2020
    Assignee: AIRBUS (S.A.S.)
    Inventor: Mei Ding
  • Publication number: 20170341774
    Abstract: The present disclosure relates to a structural component of an aircraft wing body and an aircraft including the structural component. According to an aspect of the present disclosure, a structural component of an aircraft wing body is provided. The structural component includes a body part and a profile. The body part includes an edge portion formed by end portions of a first skin and a second skin of the body part superposed together. The profile is attached to the edge portion. The profile has an outer profile conforming to an outer profile of the body part such that the structural component, as a whole, exhibits an aerodynamic outer profile after the profile is attached to the edge portion. The profile is attached to the edge portion via a plurality of separate intermediate members or by contacting the edge portion.
    Type: Application
    Filed: May 22, 2017
    Publication date: November 30, 2017
    Inventor: Mei DING