Patents by Inventor Mark Joseph Robuck

Mark Joseph Robuck 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: 11719326
    Abstract: A demister for a gearing system includes a main body having an inner annular rim coupled to an outer annular rim through a first wall and a second wall opposite from the first wall. The main body is configured to be rotated about a central longitudinal axis to create centrifugal forces that separate oil mist particles from air. First fluid passages extend radially between and through the inner annular rim and the outer annular rim. The first fluid passages include a fluid inlet opening in the outer annular rim and a fluid outlet opening in the inner annular rim. The fluid inlet opening is configured to accept incoming air. The fluid outlet opening is configured to discharge filtered air.
    Type: Grant
    Filed: October 15, 2021
    Date of Patent: August 8, 2023
    Inventors: Mark Joseph Robuck, Patrick M. Ridgley, Craig W. Eiser
  • Publication number: 20220333678
    Abstract: A demister for a gearing system includes a main body having an inner annular rim coupled to an outer annular rim through a first wall and a second wall opposite from the first wall. The main body is configured to be rotated about a central longitudinal axis to create centrifugal forces that separate oil mist particles from air. First fluid passages extend radially between and through the inner annular rim and the outer annular rim. The first fluid passages include a fluid inlet opening in the outer annular rim and a fluid outlet opening in the inner annular rim. The fluid inlet opening is configured to accept incoming air. The fluid outlet opening is configured to discharge filtered air.
    Type: Application
    Filed: October 15, 2021
    Publication date: October 20, 2022
    Applicant: THE BOEING COMPANY
    Inventors: Mark Joseph Robuck, Patrick M. Ridgley, Craig W. Eiser
  • Patent number: 11125314
    Abstract: A demister for a gearing system includes a main body shaped as a disk having an inner annular rim coupled to an outer annular rim through a first wall and a second wall opposite from the first wall. A central opening is defined by the inner annular rim and extends between and through the first wall and the second wall. The main body is configured to be rotated about a central longitudinal axis to create centrifugal forces that separate oil mist particles from air. At least one fluid passage extends radially between and through the inner annular rim and the outer annular rim. The fluid passage(s) includes a fluid inlet opening in the outer annular rim and a fluid outlet opening in the inner annular rim. The fluid inlet opening is configured to accept incoming air. The fluid outlet opening is configured to discharge filtered air.
    Type: Grant
    Filed: October 16, 2019
    Date of Patent: September 21, 2021
    Assignee: THE BOEING COMPANY
    Inventors: Mark Joseph Robuck, Patrick M. Ridgley
  • Publication number: 20210116013
    Abstract: A demister for a gearing system includes a main body shaped as a disk having an inner annular rim coupled to an outer annular rim through a first wall and a second wall opposite from the first wall. A central opening is defined by the inner annular rim and extends between and through the first wall and the second wall. The main body is configured to be rotated about a central longitudinal axis to create centrifugal forces that separate oil mist particles from air. At least one fluid passage extends radially between and through the inner annular rim and the outer annular rim. The fluid passage(s) includes a fluid inlet opening in the outer annular rim and a fluid outlet opening in the inner annular rim. The fluid inlet opening is configured to accept incoming air. The fluid outlet opening is configured to discharge filtered air.
    Type: Application
    Filed: October 16, 2019
    Publication date: April 22, 2021
    Applicant: THE BOEING COMPANY
    Inventors: Mark Joseph Robuck, Patrick M. Ridgley
  • Patent number: 9709136
    Abstract: Planetary gear systems, transmissions, and apparatuses include a plurality of compound planet gears, each having three gear stages, a first non-fixed annular gear, a second non-fixed annular gear, a fixed annular gear, and a non-fixed sun gear. A rotational input to the non-fixed sun gear results in opposite rotational outputs of the first non-fixed annular gear and the second non-fixed annular gear. Compound planet gears and carriers for planetary gear systems are also disclosed.
    Type: Grant
    Filed: May 26, 2015
    Date of Patent: July 18, 2017
    Assignee: The Boeing Company
    Inventors: Scott Hendrik Bouwer, Christopher C. Pierce, Mark Joseph Robuck
  • Patent number: 9255626
    Abstract: Planetary gear systems, transmissions, and apparatuses include at least one non-fixed annular gear, at least one non-fixed sun gear, at least one compound planet gear meshed between the at least one non-fixed annular gear and the at least one non-fixed sun gear, and at least one fixed gear meshed with the at least one compound planet gear. Rotational input to one of the at least one non-fixed annular gear and the at least one non-fixed sun gear results in an opposite rotational output of the other of the at least one non-fixed annular gear and the at least one non-fixed sun gear.
    Type: Grant
    Filed: June 10, 2014
    Date of Patent: February 9, 2016
    Assignee: The Boeing Company
    Inventors: Scott Hendrik Bouwer, Mark Joseph Robuck
  • Publication number: 20150354668
    Abstract: Planetary gear systems, transmissions, and apparatuses include at least one non-fixed annular gear, at least one non-fixed sun gear, at least one compound planet gear meshed between the at least one non-fixed annular gear and the at least one non-fixed sun gear, and at least one fixed gear meshed with the at least one compound planet gear. Rotational input to one of the at least one non-fixed annular gear and the at least one non-fixed sun gear results in an opposite rotational output of the other of the at least one non-fixed annular gear and the at least one non-fixed sun gear.
    Type: Application
    Filed: June 10, 2014
    Publication date: December 10, 2015
    Applicant: The Boeing Company
    Inventors: Scott Hendrik Bouwer, Mark Joseph Robuck
  • Publication number: 20150354672
    Abstract: Planetary gear systems, transmissions, and apparatuses include a plurality of compound planet gears, each having three gear stages, a first non-fixed annular gear, a second non-fixed annular gear, a fixed annular gear, and a non-fixed sun gear. A rotational input to the non-fixed sun gear results in opposite rotational outputs of the first non-fixed annular gear and the second non-fixed annular gear. Compound planet gears and carriers for planetary gear systems are also disclosed.
    Type: Application
    Filed: May 26, 2015
    Publication date: December 10, 2015
    Applicant: The Boeing Company
    Inventors: Scott Hendrik Bouwer, Christopher C. Pierce, Mark Joseph Robuck
  • Patent number: 6889808
    Abstract: A positive locking overrunning clutch mechanism comprising an inner clutch member, an outer clutch member, and a locking mechanism. The clutch members are adapted to rotate about a clutch axis. The locking mechanism has a plurality of lock portions adapted to transfer torque load from the inner clutch member to the outer clutch member. The locking mechanism is moveable between a locked position and an unlocked position. In the locked position, the lock portions simultaneously engage the inner and outer clutch members in a manner to cause the outer clutch member to rotate with the inner clutch member upon rotation of the inner clutch member about the clutch axis in a first rotational direction. In the unlocked position, the lock portions are positioned relative to the inner and outer clutch members in a manner to permit rotation of the outer clutch member relative to the inner clutch member in the first rotational direction.
    Type: Grant
    Filed: December 20, 2002
    Date of Patent: May 10, 2005
    Assignee: The Boeing Company
    Inventor: Mark Joseph Robuck
  • Publication number: 20040118654
    Abstract: A positive locking overrunning clutch mechanism comprising an inner clutch member, an outer clutch member, and a locking mechanism. The clutch members are adapted to rotate about a clutch axis. The locking mechanism has a plurality of lock portions adapted to transfer torque load from the inner clutch member to the outer clutch member. The locking mechanism is moveable between a locked position and an unlocked position. In the locked position, the lock portions simultaneously engage the inner and outer clutch members in a manner to cause the outer clutch member to rotate with the inner clutch member upon rotation of the inner clutch member about the clutch axis in a first rotational direction. In the unlocked position, the lock portions are positioned relative to the inner and outer clutch members in a manner to permit rotation of the outer clutch member relative to the inner clutch member in the first rotational direction.
    Type: Application
    Filed: December 20, 2002
    Publication date: June 24, 2004
    Inventor: Mark Joseph Robuck