Patents by Inventor Andrew J. Bayliss

Andrew J. Bayliss 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).

  • Non-propulsive utility power (NPUP) generation system for providing secondary power in an aircraft
    Patent number: 10737802
    Abstract: An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system.
    Type: Grant
    Filed: October 10, 2017
    Date of Patent: August 11, 2020
    Assignee: The Boeing Company
    Inventors: David S. Krug, Kamiar J. Karimi, Thomas F. Currier, Andrew J. Bayliss, George M. Roe, Mark E. Liffring, Mark W. Lesyna, Christopher M. Severns, Andrew Johnson
  • NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT
    Publication number: 20190023412
    Abstract: An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system.
    Type: Application
    Filed: October 10, 2017
    Publication date: January 24, 2019
    Inventors: David S. Krug, Kamiar J. Karimi, Thomas F. Currier, Andrew J. Bayliss, George M. Roe, Mark E. Liffring, Mark W. Lesyna, Christopher M. Severns, Andrew Johnson
  • Non-propulsive utility power (NPUP) generation system for providing full-time secondary power during operation of an aircraft
    Patent number: 9815564
    Abstract: An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system.
    Type: Grant
    Filed: December 4, 2013
    Date of Patent: November 14, 2017
    Assignee: The Boeing Company
    Inventors: David S. Krug, Kamiar J. Karimi, Thomas F. Currier, Andrew J. Bayliss, George M. Roe, Mark E. Liffring, Mark W. Lesyna, Christopher M. Severns, Andrew Johnson
  • NON-PROPULSIVE UTILITY POWER (NPUP) GENERATION SYSTEM FOR PROVIDING SECONDARY POWER IN AN AIRCRAFT
    Publication number: 20150151847
    Abstract: An aircraft may include at least one secondary power system requiring secondary power, at least two main engines, and at least three non-propulsive utility power (NPUP) generation systems. The NPUP generation systems may each be configured to provide full-time secondary power during operation of the aircraft. The NPUP generation systems may be configured to provide at least a portion of the secondary power required by the secondary power system.
    Type: Application
    Filed: December 4, 2013
    Publication date: June 4, 2015
    Applicant: The Boeing Company
    Inventors: David S. Krug, Kamiar J. Karimi, Thomas F. Currier, Andrew J. Bayliss, George M. Roe, Mark E. Liffring, Mark W. Lesyna, Christopher M. Severns, Andrew Johnson
  • Independent power generation in aircraft
    Patent number: 8950703
    Abstract: A method includes generating thrust at one or more engines of an aircraft. The method includes generating first electricity at a first power unit concurrently with generating second electricity at a second power unit. The first power unit and the second power unit are independent of the one or more engines of the aircraft. The first electricity has a first set of electrical characteristics and the second electricity has a second set of electrical characteristics, where the first set of electrical characteristics is different than the second set of electrical characteristics.
    Type: Grant
    Filed: October 17, 2013
    Date of Patent: February 10, 2015
    Assignee: The Boeing Company
    Inventors: Andrew J. Bayliss, John T. Paterson, Kevin Retz
  • INDEPENDENT POWER GENERATION IN AIRCRAFT
    Publication number: 20150014479
    Abstract: A method includes generating thrust at one or more engines of an aircraft. The method includes generating first electricity at a first power unit concurrently with generating second electricity at a second power unit. The first power unit and the second power unit are independent of the one or more engines of the aircraft. The first electricity has a first set of electrical characteristics and the second electricity has a second set of electrical characteristics, where the first set of electrical characteristics is different than the second set of electrical characteristics.
    Type: Application
    Filed: October 17, 2013
    Publication date: January 15, 2015
    Applicant: The Boeing Company
    Inventors: Andrew J. Bayliss, John T. Paterson, Kevin Retz
  • Independent power generation in aircraft
    Patent number: 8657227
    Abstract: Systems and methods of independent power generation are disclosed. A particular system includes an aircraft having at least one engine and a plurality of independent power units. Each power unit of the plurality of independent power units generates electricity independently of the at least one engine. The plurality of independent power units include at least a first independent power unit that generates first electricity having a first set of electrical characteristics and a second independent power unit that generates second electricity having a second set of electrical characteristics concurrently with the first power unit generating the first electricity. The first set of electrical characteristics is different than the second set of electrical characteristics.
    Type: Grant
    Filed: September 11, 2009
    Date of Patent: February 25, 2014
    Assignee: The Boeing Company
    Inventors: Andrew J. Bayliss, John T. Paterson, Kevin Retz