Patents by Inventor Mark M. Gmerek

Mark M. Gmerek 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: 11712872
    Abstract: A duct includes a foam-filled honeycomb core structure having a tubular shape. The duct further includes an air-impermeable duct wall coupled to an exterior surface of the foam-filled honeycomb core structure.
    Type: Grant
    Filed: August 20, 2018
    Date of Patent: August 1, 2023
    Assignee: THE BOEING COMPANY
    Inventors: Douglas D. Maben, Bryce A. Vandyke, Mark M. Gmerek, David R. C. Cannal
  • Publication number: 20230010222
    Abstract: Described herein are noise attenuating ducts and vehicles using these ducts for environmental control systems. A duct comprises an exoskeleton structure and a sound-absorbing structure, disposed within and conforming to the exoskeleton structure. The exoskeleton structure provides external mechanical support to the sound-absorbing structure thereby helping to maintain the tubular shape of the sound-absorbing structure. This external support does not interfere with the airflow inside the sound-absorbing structure. Furthermore, the external positioning of the exoskeleton structure allows the integration of various support mounting features for the installation of the duct in a vehicle. In some examples, the exoskeleton structure comprises a plurality of enclosed openings to reduce the weight of the exoskeleton structure and provide additional flexibility.
    Type: Application
    Filed: July 12, 2021
    Publication date: January 12, 2023
    Applicant: The Boeing Company
    Inventors: Bryce A. Vandyke, Douglas D. Maben, Dale Hastings, Mark M. Gmerek, Xin Han
  • Patent number: 10891934
    Abstract: Described are methods and systems for broad-band active reduction of noise in target spaces, such as spaces around headrests in aircraft cabins. Systems describe herein are effective over wide frequency ranges without causing undesirable amplification at any subrange ranges. Specifically, a system comprises a speaker and a resonator, both coupled to an enclosure. The interior space of the resonator is in fluid communication with the enclosed space of the enclosure, allowing the resonator to reduce the amplitude of unwanted amplification by the audio reducing sound generated by the speaker. The amplitude is reduced in a selected frequency range, which may correspond to an expected amplification for this particular system. The resonator may partially extend into the enclosure or may be completely incorporated into the enclosure. Some examples of the resonator include a Helmholtz resonator, a passive radiator, a quarter wave resonator, a pipe resonator, and an acoustic metamaterial.
    Type: Grant
    Filed: October 18, 2019
    Date of Patent: January 12, 2021
    Assignee: The Boeing Company
    Inventors: Steven F. Griffin, Adam R. Weston, Mark M. Gmerek
  • Publication number: 20200056727
    Abstract: A duct includes a foam-filled honeycomb core structure having a tubular shape. The duct further includes an air-impermeable duct wall coupled to an exterior surface of the foam-filled honeycomb core structure.
    Type: Application
    Filed: August 20, 2018
    Publication date: February 20, 2020
    Inventors: Douglas D. Maben, Bryce A. Vandyke, Mark M. Gmerek, David R. C. Cannal
  • Publication number: 20200051543
    Abstract: Described are methods and systems for broad-band active reduction of noise in target spaces, such as spaces around headrests in aircraft cabins. Systems describe herein are effective over wide frequency ranges without causing undesirable amplification at any subrange ranges. Specifically, a system comprises a speaker and a resonator, both coupled to an enclosure. The interior space of the resonator is in fluid communication with the enclosed space of the enclosure, allowing the resonator to reduce the amplitude of unwanted amplification by the audio reducing sound generated by the speaker. The amplitude is reduced in a selected frequency range, which may correspond to an expected amplification for this particular system. The resonator may partially extend into the enclosure or may be completely incorporated into the enclosure. Some examples of the resonator include a Helmholtz resonator, a passive radiator, a quarter wave resonator, a pipe resonator, and an acoustic metamaterial.
    Type: Application
    Filed: October 18, 2019
    Publication date: February 13, 2020
    Applicant: The Boeing Company
    Inventors: Steven F. Griffin, Adam R. Weston, Mark M. Gmerek
  • Patent number: 10453438
    Abstract: Described are methods and systems for broad-band active reduction of noise in target spaces, such as spaces around headrests in aircraft cabins. Systems describe herein are effective over wide frequency ranges without causing undesirable amplification at any subrange ranges. Specifically, a system comprises a speaker and a resonator, both coupled to an enclosure. The interior space of the resonator is in fluid communication with the enclosed space of the enclosure, allowing the resonator to reduce the amplitude of unwanted amplification by the audio reducing sound generated by the speaker. The amplitude is reduced in a selected frequency range, which may correspond to an expected amplification for this particular system. The resonator may partially extend into the enclosure or may be completely incorporated into the enclosure. Some examples of the resonator include a Helmholtz resonator, a passive radiator, a quarter wave resonator, a pipe resonator, and an acoustic metamaterial.
    Type: Grant
    Filed: May 30, 2018
    Date of Patent: October 22, 2019
    Assignee: The Boeing Company
    Inventors: Steven F. Griffin, Adam R. Weston, Mark M. Gmerek
  • Patent number: 10350863
    Abstract: A panel includes a structural substrate and a damping element including a viscoelastic material (VEM) layer coupleable to the structural substrate of the aircraft, and a constraining layer coupled to the VEM layer. The VEM layer is configured to dampen a vibration of the structural substrate. The constraining layer is configured to apply a shear force to the VEM layer.
    Type: Grant
    Filed: July 30, 2014
    Date of Patent: July 16, 2019
    Assignee: The Boeing Company
    Inventors: Alan E. Landmann, Mark A. Negley, Jaffar S. Iqbal, Bret A. Voss, Mark M. Gmerek, Giacomo Licciardi
  • Publication number: 20160031195
    Abstract: A panel includes a structural substrate and a damping element including a viscoelastic material (VEM) layer coupleable to the structural substrate of the aircraft, and a constraining layer coupled to the VEM layer. The VEM layer is configured to dampen a vibration of the structural substrate. The constraining layer is configured to apply a shear force to the VEM layer.
    Type: Application
    Filed: July 30, 2014
    Publication date: February 4, 2016
    Inventors: Alan E. Landmann, Mark A. Negley, Jaffar S. Iqbal, Bret A. Voss, Mark M. Gmerek, Giacomo Licciardi