Patents by Inventor Mark David Horn

Mark David Horn 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: 11918794
    Abstract: A button for a drug delivery device with a reduced operating loudness includes a plate-like button body forming a touch surface, wherein the plate-like button body is coupled by an axial supporting member to a noise-generating interface of the drug delivery device and movable into a longitudinal direction of the drug delivery device, wherein the plate-like button body includes a material composite with at least one first component consisting of a first material and at least one second component consisting of a second material different from the first material, wherein the at least one first component and the at least one second component are coupled via at least one coupling plane that is at least sectionwise slanted or perpendicular to the longitudinal direction. Further, the disclosure describes a button assembly for a drug delivery device which is shock resistant.
    Type: Grant
    Filed: October 30, 2018
    Date of Patent: March 5, 2024
    Assignee: Sanofi
    Inventors: Ralph Donald Quentin Collings, James Robert Coop, James Anthony West, Stephen Francis Gilmore, Daniel David Higgins, Mark Digby Teucher, Matthew Meredith Jones, Anthony Paul Morris, Sophie Sladen, William Geoffrey Arthur Marsh, Denny Lustosa Horn, Stefan Blancke, Michael Jugl
  • Publication number: 20230304457
    Abstract: A variable flow area injector for a liquid rocket engine. The injector has a poppet with a variable outer width portion and a housing with a variable inner width portion. An annular flow path is defined between the variable width portions. Increased throttling of the engine passively increases the annular flow area of the injector by forcing the poppet in a distal direction. Decreased throttling allows a restoring spring to move the poppet in a proximal direction to decrease the annular flow area. A bellows can be included to dampen movement of the poppet. The bellows may be in a propellant-filled cavity separate from the main propellant flow path and have a series of openings through which the separate propellant flows.
    Type: Application
    Filed: May 5, 2023
    Publication date: September 28, 2023
    Inventors: Mark David Horn, Adam Keith Norman
  • Patent number: 11643995
    Abstract: A variable flow area injector for a liquid rocket engine. The injector has a poppet with a variable outer width portion and a housing with a variable inner width portion. An annular flow path is defined between the variable width portions. Increased throttling of the engine passively increases the annular flow area of the injector by forcing the poppet in a distal direction. Decreased throttling allows a restoring spring to move the poppet in a proximal direction to decrease the annular flow area. A bellows can be included to dampen movement of the poppet. The bellows may be in a propellant-filled cavity separate from the main propellant flow path and have a series of openings through which the separate propellant flows.
    Type: Grant
    Filed: November 4, 2021
    Date of Patent: May 9, 2023
    Assignee: BLUE ORIGIN, LLC
    Inventors: Mark David Horn, Adam Keith Norman
  • Patent number: 9435204
    Abstract: An engine includes a housing having a single wall, where the wall has a rib and a flange, and the wall provides a primary structure and cooling for the engine. A closeout is attached to an outer surface of the wall, and the closeout and the wall form a cavity. The closeout provides a secondary structure for containing a coolant fluid flow within the cavity. The closeout may be corrugated, and the ribs may be exposed to the cavity.
    Type: Grant
    Filed: March 21, 2011
    Date of Patent: September 6, 2016
    Assignee: United Technologies Corporation
    Inventor: Mark David Horn
  • Patent number: 8689764
    Abstract: A rotary engine which provides a supplemental phase of compression between a first phase of compression and a second phase of compression.
    Type: Grant
    Filed: October 8, 2009
    Date of Patent: April 8, 2014
    Assignee: Aerojet Rocketdyne of De, Inc.
    Inventors: Mark David Horn, Glenn L. Havskjold, Calvin Q. Morrison, Jr.
  • Publication number: 20120315172
    Abstract: A rotary engine includes a first transfer duct between a first rotor section and a second rotor section. A second transfer duct is between the second rotor section and the first rotor section. A supplemental compounding control valve selectively controls communication between the first transfer duct and the second transfer duct.
    Type: Application
    Filed: October 8, 2009
    Publication date: December 13, 2012
    Inventor: Mark David Horn
  • Publication number: 20120240885
    Abstract: An engine includes a housing having a single wall, where the wall has a rib and a flange, and the wall provides a primary structure and cooling for the engine. A closeout is attached to an outer surface of the wall, and the closeout and the wall form a cavity. The closeout provides a secondary structure for containing a coolant fluid flow within the cavity. The closeout may be corrugated, and the ribs may be exposed to the cavity.
    Type: Application
    Filed: March 21, 2011
    Publication date: September 27, 2012
    Applicant: Pratt & Whitney Rocketdyne, Inc.
    Inventor: Mark David Horn
  • Publication number: 20110174261
    Abstract: A shaft for a rotary engine defines an axis of rotation, a first eccentric cam axially displaced from a second eccentric cam along the axis of rotation, the first eccentric cam aligned with the second eccentric cam.
    Type: Application
    Filed: October 8, 2009
    Publication date: July 21, 2011
    Inventors: Glenn L. Havskjold, Mark David Horn, Khin C. Phul
  • Publication number: 20110174262
    Abstract: A rotary engine which provides a supplemental phase of compression between a first phase of compression and a second phase of compression.
    Type: Application
    Filed: October 8, 2009
    Publication date: July 21, 2011
    Applicant: PRATT & WHITNEY ROCKETDYNE, INC.
    Inventors: Mark David Horn, Glenn L. Havskjold, Calvin Q. Morrison, JR.
  • Publication number: 20080299504
    Abstract: An ignition system for a combustion device utilizes an oscillating pressure force in a resonance system to generate thermal energy within a resonance driven glow plug. The resonance driven glow plug stores the thermal energy for transfer to ignitable propellant combinations within a torch assembly and thus within the combustion chamber.
    Type: Application
    Filed: June 1, 2007
    Publication date: December 4, 2008
    Inventor: Mark David Horn
  • Patent number: 6883220
    Abstract: A method for forming an article having a wall that is at least partially fabricated from tubing. The methodology employs a pressurized fluid to deform the tubing such that an outer surface of the tubing substantially conforms to a predetermined first wall configuration, an inner surface of the tubing substantially conforms to a predetermined second wall configuration and each of segment or loop of the tubing is substantially contiguous with at least one other segment or loop between the first and second surfaces.
    Type: Grant
    Filed: July 17, 2002
    Date of Patent: April 26, 2005
    Assignee: The Boeing Company
    Inventor: Mark David Horn
  • Publication number: 20040010900
    Abstract: A method for forming an article having a wall that is at least partially fabricated from tubing. The methodology employs a pressurized fluid to deform the tubing such that an outer surface of the tubing substantially conforms to a predetermined first wall configuration, an inner surface of the tubing substantially conforms to a predetermined second wall configuration and each of segment or loop of the tubing is substantially contiguous with at least one other segment or loop between the first and second surfaces.
    Type: Application
    Filed: July 17, 2002
    Publication date: January 22, 2004
    Inventor: Mark David Horn