Patents by Inventor Michael Babu

Michael Babu 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: 20240132509
    Abstract: Disclosed are quinoline and quinazoline compounds which modulate the activity of the gated ion channels. Compounds that modulate these gated ion channels are useful in the treatment of diseases and disorders related to pain, inflammation, the neurological system, the gastrointestinal system and genitourinary system. Preferred compounds include quinoline or quinazoline derivatives substituted at the 4-position via N(H), C(O) or O moieties.
    Type: Application
    Filed: November 13, 2023
    Publication date: April 25, 2024
    Inventors: Nadiya Sydorenko, Md Rauful Alam, Michael A. Arnold, Suresh Babu, Anuradha Bhattacharyya, Guangming Chen, Aleksey I. Gerasyuto, Gary Mitchell Karp, Andrew J. Kassick, Anthony R. Mazzotti, Young-Choon Moon, Jana Narasimhan, Jigar Patel, Anthony Turpoff, Matthew G. Woll, Wuming Yan, Nanjing Zhang
  • Publication number: 20240109514
    Abstract: Systems and methods are provided for recording video of a driver in a vehicle and a surrounding visual field of the driver. The system includes a detachable body coupled to a windshield of a vehicle. The system further includes three or more cameras coupled to the detachable body. The three or more cameras are configured to capture surrounding views from the detachable body. One of the three or more cameras faces a driver seat of the vehicle in response to the detachable body being coupled to the windshield of the vehicle. The video may be processed by the system, the cloud, or a combination of them.
    Type: Application
    Filed: December 13, 2023
    Publication date: April 4, 2024
    Applicant: NETRADYNE, INC.
    Inventors: David Jonathan JULIAN, Sandeep PANDYA, Adam David KAHN, Michael CAMPOS, Avneesh AGRAWAL, Venkata Sreekanta Reddy ANNAPUREDDY, Lance Steven HETHERINGTON, Tejeswara Rao GUDENA, Suresh Babu YANAMALA, Arun VALIAPARAMBIL
  • Publication number: 20240099213
    Abstract: Provided here are methods of using a mutated patatin-like phospholipase II? (“pPLAII?,” renamed here MATRILINEAL) to induce haploid induction in plants, cloning a pPLAII? to induce haploid induction in plants, and genetically engineering a plant to contain a mutated pPLAII?. Also provided are methods of applying topical and spray chemicals, lipids, and RNAi molecules to plants during pollination in order to induce haploid production. Further provided are methods of chemically treating plants during pollination to induce haploids while also reducing embryo abortion and increasing seed set.
    Type: Application
    Filed: November 30, 2023
    Publication date: March 28, 2024
    Applicant: Syngenta Participations AG
    Inventors: Timothy Kelliher, Satya Chintamanani, Brent Delzer, Michael L Nuccio, Robert Arthur Dietrich, Suresh Babu Kadaru, Todd Lee Warner, William Paul Bullock
  • Patent number: 9243675
    Abstract: A brake disc of a rotor brake is provided including a generally cylindrical body having a first planar surface, a second, opposite planar surface, and a central opening extending there through. A plurality of first connection members extend generally outwardly from the first planar surface. The first connection members are generally equidistantly spaced about a diameter of the first planar surface. A plurality of second connection members extend generally outwardly from the second planar surface. The second connection members are generally equidistantly spaced about a diameter of the second planar surface.
    Type: Grant
    Filed: October 30, 2013
    Date of Patent: January 26, 2016
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Michael Babu, Yuriy Gmirya, Justin Gouveia
  • Publication number: 20150114772
    Abstract: A brake disc of a rotor brake is provided including a generally cylindrical body having a first planar surface, a second, opposite planar surface, and a central opening extending there through. A plurality of first connection members extend generally outwardly from the first planar surface. The first connection members are generally equidistantly spaced about a diameter of the first planar surface. A plurality of second connection members extend generally outwardly from the second planar surface. The second connection members are generally equidistantly spaced about a diameter of the second planar surface.
    Type: Application
    Filed: October 30, 2013
    Publication date: April 30, 2015
    Applicant: Sikorsky Aircraft Corporation
    Inventors: Michael Babu, Yuriy Gmirya, Justin Gouveia
  • Patent number: 8015796
    Abstract: A gas turbine engine includes a compressor section, a combustor section and a turbine section, all arranged about a central axis. A turbine rotor drives a driveshaft for rotation on the central axis. The driveshaft in turn drives at least two fan rotors on axes parallel to, but spaced from, the central axis. The fan rotors each deliver a portion of the air they move into a central inlet for delivering the air to the compressor section. In addition, the majority of the air moved by the plurality of fan rotors passes between a cowl and an outer periphery of a housing for the central core of the engine. This bypass air provides propulsion as is known in the turbojet art.
    Type: Grant
    Filed: June 5, 2007
    Date of Patent: September 13, 2011
    Assignee: United Technologies Corporation
    Inventors: Michael Babu, Richard E. Domonkos, Philip Shacter
  • Patent number: 7743600
    Abstract: A sensor assembly for a gas turbine engine includes a telemetry module mounted at a rotor bearing compartment for sensing engine operational parameters and a cooling system for cooling the telemetry module separate from a rotor bearing lubricant flow.
    Type: Grant
    Filed: April 4, 2006
    Date of Patent: June 29, 2010
    Assignee: United Technologies Corporation
    Inventors: Michael Babu, Michael Ian Walker, William G. Sheridan, Richard E. Domonkos, Michael T. Chelte
  • Publication number: 20100011741
    Abstract: A gas turbine engine includes a compressor section, a combustor section and a turbine section, all arranged about a central axis. A turbine rotor drives a driveshaft for rotation on the central axis. The driveshaft in turn drives at least two fan rotors on axes parallel to, but spaced from, the central axis. The fan rotors each deliver a portion of the air they move into a central inlet for delivering the air to the compressor section. In addition, the majority of the air moved by the plurality of fan rotors passes between a cowl and an outer periphery of a housing for the central core of the engine. This bypass air provides propulsion as is known in the turbojet art.
    Type: Application
    Filed: June 5, 2007
    Publication date: January 21, 2010
    Inventors: Michael Babu, Richard E. Domonkos, Philip Shacter
  • Publication number: 20070233415
    Abstract: A sensor assembly for a gas turbine engine includes a telemetry module mounted at a rotor bearing compartment for sensing engine operational parameters and a cooling system for cooling the telemetry module separate from a rotor bearing lubricant flow.
    Type: Application
    Filed: April 4, 2006
    Publication date: October 4, 2007
    Applicant: United Technologies Corporation
    Inventors: Michael Babu, Michael Walker, William Sheridan, Richard Domonkos, Michael Chelte
  • Patent number: 6764282
    Abstract: A blade for a turbine engine having a centerline. The blade comprises: a root section extending at an angle relative to the centerline; and an airfoil section extending from the root section. The root section is directly adjacent said airfoil section. In other words, the blade is neckless. The blade is part of a rotor assembly, and is preferably a fan blade.
    Type: Grant
    Filed: November 14, 2001
    Date of Patent: July 20, 2004
    Assignee: United Technologies Corporation
    Inventors: Gabriel L. Suciu, Michael Babu, James R. Murdock
  • Publication number: 20040062651
    Abstract: A blade for a turbine engine having a centerline. The blade comprises: a root section extending at an angle relative to the centerline; and an airfoil section extending from the root section. The root section is directly adjacent said airfoil section. In other words, the blade is neckless. The blade is part of a rotor assembly, and is preferably a fan blade.
    Type: Application
    Filed: November 14, 2001
    Publication date: April 1, 2004
    Inventors: Gabriel L. Suciu, Michael Babu, James R. Murdock