Patents by Inventor Richard J. Bacon

Richard J. Bacon 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: 7407133
    Abstract: Methods of operating a multi-engine jet-aircraft. According to one embodiment of the present invention, a first jet engine and a second jet engine are provided. One of the jet engines has a lesser maximum thrust capability than the other jet engine as a result of limiting the former's maximum thrust capability, but the two jet engines are otherwise equally powered. During various segments of flight, both the first jet engine and second jet engine are utilized. A thrust differential between the first jet engine and the second jet engine is created during one or more flight segments by continuing to run either the first jet engine or second jet engine, but running the other at a reduced power.
    Type: Grant
    Filed: March 9, 2005
    Date of Patent: August 5, 2008
    Assignee: 3x Jet Aircraft Company
    Inventor: Richard J. Bacon
  • Patent number: 6921046
    Abstract: A centerline mounted overbalanced multiple main jet engine configuration. The multiple jet engines are centerline mounted rather than parallel offset. While each jet engine is a “main” engine, capable of safely operating the aircraft in the event of a failure of the other engines, the engines are overbalanced in the sense that at least one of the main engines has substantially greater thrust than the other main engines. All of the main engines operate at critical periods of flight, but only one or the other of the main engines operates at other periods. The configuration of this invention combines the efficiency and performance of a single engined aircraft with enhanced safety advantages.
    Type: Grant
    Filed: July 24, 2001
    Date of Patent: July 26, 2005
    Assignee: 3X Jet Aircraft Company
    Inventor: Richard J. Bacon
  • Publication number: 20020074453
    Abstract: A centerline mounted overbalanced multiple main jet engine configuration. The multiple jet engines are centerline mounted rather than parallel offset. While each jet engine is a “main” engine, capable of safely operating the aircraft in the event of a failure of the other engines, the engines are overbalanced in the sense that at least one of the main engines has substantially greater thrust than the other main engines. All of the main engines operate at critical periods of flight, but only one or the other of the main engines operates at other periods. The configuration of this invention combines the efficiency and performance of a single engined aircraft with enhanced safety advantages.
    Type: Application
    Filed: July 24, 2001
    Publication date: June 20, 2002
    Inventor: Richard J. Bacon
  • Patent number: 5855340
    Abstract: A centerline mounted overbalanced multiple main jet engine configuration. The multiple jet engines are centerline mounted rather than parallel offset. While each jet engine is a "main" engine, capable of safely operating the aircraft in the event of a failure of the other engines, the engines are overbalanced in the sense that at least one of the main engines has substantially greater thrust than the other main engines. All of the main engines operate at critical periods of flight, but only one or the other of the main engines operates at other periods. The configuration of this invention combines the efficiency and performance of a single engined aircraft with enhanced safety advantages.
    Type: Grant
    Filed: June 22, 1995
    Date of Patent: January 5, 1999
    Inventor: Richard J. Bacon
  • Patent number: 5480107
    Abstract: A centerline mounted overbalanced multiple main jet engine configuration. The multiple jet engines are centerline mounted rather than parallel offset. While each jet engine is a "main" engine, capable of safely operating the aircraft in the event of a failure of the other engines, the engines are overbalanced in the sense that at least one of the main engines has substantially greater thrust than the other main engines. All of the main engines operate at critical periods of flight, but only one or the other of the main engines operates at other periods. The configuration of this invention combines the efficiency and performance of a single engined aircraft with enhanced safety advantages.
    Type: Grant
    Filed: April 11, 1994
    Date of Patent: January 2, 1996
    Inventor: Richard J. Bacon