Patents by Inventor Mohammad TABESH

Mohammad TABESH 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: 20230271708
    Abstract: An insert for an air intake of a suction duct, the insert including an inner portion configured to extend within the suction duct, a mating portion configured for sealingly engaging the air intake, and an outer portion configured for extending outside of the suction duct. The inner portion includes a conduit having a central axis extending along an inlet direction at the inlet end and along an outlet direction at the outlet end, the inlet and outlet directions being non-parallel. The outlet end has a smaller cross-sectional area than that of the suction duct. The insert includes an inlet in fluid communication with the inlet end of the conduit. The outer portion includes a curved lip surrounding at least part of an inlet opening of the inlet, the lip configured to direct a flow into the inlet opening and toward the inlet end of the conduit.
    Type: Application
    Filed: February 16, 2023
    Publication date: August 31, 2023
    Inventors: Manuel ETCHESSAHAR, Eric HANSEN, Mohammad TABESH, Vincent POINTEL, Stephen COLAVINCENZO, Alexis CARON-L'ECUYER
  • Patent number: 11608180
    Abstract: An insert for an air intake of a suction duct, the insert including an inner portion configured to extend within the suction duct, a mating portion configured for sealingly engaging the air intake, and an outer portion configured for extending outside of the suction duct. The inner portion includes a conduit having a central axis extending along an inlet direction at the inlet end and along an outlet direction at the outlet end, the inlet and outlet directions being non-parallel. The outlet end has a smaller cross-sectional area than that of the suction duct. The insert includes an inlet in fluid communication with the inlet end of the conduit. The outer portion includes a curved lip surrounding at least part of an inlet opening of the inlet, the lip configured to direct a flow into the inlet opening and toward the inlet end of the conduit.
    Type: Grant
    Filed: April 9, 2018
    Date of Patent: March 21, 2023
    Assignee: BOMBARDIER INC.
    Inventors: Manuel Etchessahar, Eric Hansen, Mohammad Tabesh, Vincent Pointel, Stephen Colavincenzo, Alexis Caron-L'Ecuyer
  • Patent number: 11591068
    Abstract: A wing assembly includes a swept wing body, a leading edge of the wing body extending outward and rearward from a wing root to a wing edge; a first slat selectively movably connected to the wing body; and a second slat selectively movably connected to the wing body, the second slat being disposed outboard of the first slat, a flexible sealing member disposed and connected between the first slat and the second slat; at least a portion of the first slat, at least a portion of the second slat, and at least a portion of the flexible sealing member defining a slat gap therebetween, at least a majority of the slat gap being substantially parallel to a predetermined local airflow direction. An aircraft is also disclosed which includes a fuselage; and two oppositely disposed wing assemblies connected to the fuselage.
    Type: Grant
    Filed: June 9, 2020
    Date of Patent: February 28, 2023
    Assignee: BOMBARDIER INC.
    Inventors: Stephen Colavincenzo, Robby Lapointe, Mohammad Tabesh
  • Publication number: 20200385102
    Abstract: A wing assembly includes a swept wing body, a leading edge of the wing body extending outward and rearward from a wing root to a wing edge; a first slat selectively movably connected to the wing body; and a second slat selectively movably connected to the wing body, the second slat being disposed outboard of the first slat, a flexible sealing member disposed and connected between the first slat and the second slat; at least a portion of the first slat, at least a portion of the second slat, and at least a portion of the flexible sealing member defining a slat gap therebetween, at least a majority of the slat gap being substantially parallel to a predetermined local airflow direction. An aircraft is also disclosed which includes a fuselage; and two oppositely disposed wing assemblies connected to the fuselage.
    Type: Application
    Filed: June 9, 2020
    Publication date: December 10, 2020
    Inventors: Stephen COLAVINCENZO, Robby LAPOINTE, Mohammad TABESH
  • Publication number: 20200094971
    Abstract: An insert for an air intake of a suction duct, the insert including an inner portion configured to extend within the suction duct, a mating portion configured for sealingly engaging the air intake, and an outer portion configured for extending outside of the suction duct. The inner portion includes a conduit having a central axis extending along an inlet direction at the inlet end and along an outlet direction at the outlet end, the inlet and outlet directions being non-parallel. The outlet end has a smaller cross-sectional area than that of the suction duct. The insert includes an inlet in fluid communication with the inlet end of the conduit. The outer portion includes a curved lip surrounding at least part of an inlet opening of the inlet, the lip configured to direct a flow into the inlet opening and toward the inlet end of the conduit.
    Type: Application
    Filed: April 9, 2018
    Publication date: March 26, 2020
    Inventors: Manuel ETCHESSAHAR, Eric HANSEN, Mohammad TABESH, Vincent POINTEL, Stephen COLAVINCENZO, Alexis CARON-L'ECUYER