Patents by Inventor George Bates

George Bates 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).

  • Patent number: 11992692
    Abstract: This document describes an automated external defibrillator comprising a control configured to switch between a pediatric operating mode and an adult operating mode, wherein each operating mode comprises a mode-specific energy configuration and a mode-specific user configuration; an indicator configured to provide an indication of the operating mode in use during a resuscitation process; one or more processors configured to switch to the mode-specific energy configuration and the mode-specific user configuration upon a change of operating mode between the pediatric operating mode and the adult operating mode such that the automated external defibrillator delivers a defibrillating shock to a patient based on the mode-specific energy configuration; and an interface of the automated external defibrillator provides resuscitation instructions to a user based on the mode-specific user configuration.
    Type: Grant
    Filed: December 14, 2021
    Date of Patent: May 28, 2024
    Assignee: ZOLL Medical Corporation
    Inventors: Melissa M. Dascoli, Charles E. Sawyer, Jr., Bill Gastrock, Dustin Boutet, Gary A. Freeman, James Wilson, Brian Stonecipher, Ian Durrant, George Reilly, Mark Bates
  • Patent number: 11948055
    Abstract: Record clustering is performed for a collection of records using training rules, training-rule labels, training data created from a sample of pairs of records, a pair-wise classifier, and a clustering algorithm. Record clustering is also performed for a collection of records using prediction rules, prediction-rule labels, a pair-wise classifier, and a clustering algorithm.
    Type: Grant
    Filed: March 1, 2023
    Date of Patent: April 2, 2024
    Assignee: TAMR, INC.
    Inventors: George Anwar Dany Beskales, Nikolaus Bates-Haus, Ihab F. Ilyas
  • Patent number: 10927845
    Abstract: A seal assembly for a gas turbine engine employs a first seal forming an oil chamber around a bearing. The first seal is configured to maintain the oil chamber at a first pressure. A second seal forms a ventilating cavity around the oil chamber. The second seal is configured to maintain the ventilating cavity at a second pressure, the second pressure being less than the first pressure and less than an ambient pressure of a primary flow path in the engine. A pressure reducing device is coupled to the ventilating cavity. The pressure reducing device is configured to maintain the second pressure.
    Type: Grant
    Filed: May 24, 2017
    Date of Patent: February 23, 2021
    Assignee: The Boeing Company
    Inventors: Chao-Hsin Lin, Raymond H. Horstman, George Bates, III
  • Patent number: 10377496
    Abstract: An airflow control system for use in a vehicle is provided. The airflow control system includes a manifold and a recirculation duct in flow communication with the manifold. The recirculation duct includes a fan and a recirculation valve. The system additionally includes a ventilation duct coupled in flow communication with the recirculation duct between the fan and the recirculation valve. The ventilation duct is in flow communication with an ambient environment surrounding the vehicle and includes at least one ventilation valve.
    Type: Grant
    Filed: July 30, 2013
    Date of Patent: August 13, 2019
    Assignee: THE BOEING COMPANY
    Inventors: Luong Hoang Le, George Bates, III, Myles Edward Brown, Brian P. Berryessa, Ryan S. Perham
  • Patent number: 10215442
    Abstract: A diverter duct for a ventilation system includes a main body defining an inner surface, a first portion including an inlet, a second portion located downstream of the first portion, a third portion including an outlet, an opening located between the first portion and the third portion, and an air deflector positioned within the main body downstream of the first portion to deflect a portion of the air from the inlet of the main body towards the opening. A first contoured section is formed in the first portion of the main body. The first contoured section may direct air received from the inlet towards the opening at a first operating condition. A method of installing the diverter duct includes coupling the inlet with an upstream fan, and coupling the outlet with an outlet fan, such that selective operation of the inlet and outlet fans cause vary airflow though the outlet or the opening.
    Type: Grant
    Filed: July 30, 2014
    Date of Patent: February 26, 2019
    Assignee: The Boeing Company
    Inventors: Scott Peterson Ellsworth, George Bates, III
  • Publication number: 20180340546
    Abstract: A seal assembly for a gas turbine engine employs a first seal forming an oil chamber around a bearing. The first seal is configured to maintain the oil chamber at a first pressure. A second seal forms a ventilating cavity around the oil chamber. The second seal is configured to maintain the ventilating cavity at a second pressure, the second pressure being less than the first pressure and less than an ambient pressure of a primary flow path in the engine. A pressure reducing device is coupled to the ventilating cavity. The pressure reducing device is configured to maintain the second pressure.
    Type: Application
    Filed: May 24, 2017
    Publication date: November 29, 2018
    Inventors: Chao-Hsin Lin, Raymond H. Horstman, George Bates, III
  • Publication number: 20160033152
    Abstract: A diverter duct for a ventilation system is disclosed. The diverter duct includes a main body defining an inner surface, a first portion including an inlet, a second portion located downstream of the first portion, a third portion including an outlet, and an opening located between the first portion and the third portion. The diverter duct also includes a first contoured section formed in the first portion of the main body. The inner surface of the main body at the first contoured section may be configured to direct air received from the inlet towards the opening at a first operating condition. The diverter duct also includes an air deflector positioned along the inner surface of the main body downstream of the first portion to deflect a portion of the air received from the inlet of the main body towards the opening at the first operating condition.
    Type: Application
    Filed: July 30, 2014
    Publication date: February 4, 2016
    Inventors: Scott Peterson Ellsworth, George Bates, III
  • Publication number: 20150099444
    Abstract: An airflow control system for use in a vehicle is provided. The airflow control system includes a manifold and a recirculation duct in flow communication with the manifold. The recirculation duct includes a fan and a recirculation valve. The system additionally includes a ventilation duct coupled in flow communication with the recirculation duct between the fan and the recirculation valve. The ventilation duct is in flow communication with an ambient environment surrounding the vehicle and includes at least one ventilation valve.
    Type: Application
    Filed: July 30, 2013
    Publication date: April 9, 2015
    Applicant: The Boeing Company
    Inventors: Luong Hoang Le, George Bates, III, Myles Edward Brown, Brian P. Berryessa, Ryan S. Perham
  • Patent number: 7112770
    Abstract: A humidification system and method particularly well adapted for use in commercial aircraft to provide substantially micro-organism free humidified air within a passenger cabin of the aircraft. The system employs a vessel for holding a quantity of water therein. The vessel is disposed within a microwave oven which is used to heat the water within the vessel to the boiling point such that steam is generated therefrom. This steam is directed into an airflow duct and used to humidify an airflow being supplied into a cabin area of the aircraft. The steam is substantially micro-organism free. A controller is used to cycle the filling and draining of the vessel to achieve a desired humidity level for the airflow. Optimally, a vacuum accumulator is employed to assist in rapid draining of the water from the vessel.
    Type: Grant
    Filed: October 3, 2003
    Date of Patent: September 26, 2006
    Assignee: The Boeing Company
    Inventors: Justin H. Doh, George Bates, III
  • Publication number: 20050072776
    Abstract: A humidification system and method particularly well adapted for use in commercial aircraft to provide substantially micro-organism free humidified air within a passenger cabin of the aircraft. The system employs a vessel for holding a quantity of water therein. The vessel is disposed within a microwave oven which is used to heat the water within the vessel to the boiling point such that steam is generated therefrom. This steam is directed into an airflow duct and used to humidify an airflow being supplied into a cabin area of the aircraft. The steam is substantially micro-organism free. A controller is used to cycle the filling and draining of the vessel to achieve a desired humidity level for the airflow. Optimally, a vacuum accumulator is employed to assist in rapid draining of the water from the vessel.
    Type: Application
    Filed: October 3, 2003
    Publication date: April 7, 2005
    Inventors: Justin Doh, George Bates
  • Patent number: 6413159
    Abstract: Passenger cabin ventilation air outlets located in the cabin ceiling blow air downward toward the passengers. An outlet for this location utilizes a series of high velocity jets exiting from a narrow ceiling nozzle to entrain cabin air to form a broad slow moving single jet. Three rows of slots are utilized, the outer rows to initially produce a wide air jet, and the center row to draw the outer jets back together outside of the nozzle. The center jets coalesce the outer jets into a slower moving total air stream.
    Type: Grant
    Filed: June 28, 2000
    Date of Patent: July 2, 2002
    Assignee: The Boeing Company
    Inventors: George Bates, III, Glenn Sitler, Rory C. Keogh