Patents by Inventor Henry Claeys

Henry Claeys 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: 11202987
    Abstract: A gas compression system includes a system inlet to receive a gas stream containing a first component and a second component, a vapor system outlet to discharge the gas stream, and a plurality of compression stages coupled in series between the system inlet and the vapor system outlet. Each of the plurality of compression stages includes a compressor, a condenser coupled to the compressor, and a gravity-independent phase separator coupled to the condenser. The compressor is configured to receive the gas stream from either the system inlet or another of the plurality of compression stages and compress the gas stream. The condenser is configured to condense the second component from the gas stream. The gravity-independent phase separator is configured to remove the second component from the gas stream and discharge the gas stream to either the system outlet or another of the plurality of compression stages.
    Type: Grant
    Filed: October 18, 2018
    Date of Patent: December 21, 2021
    Assignee: Honeywell International Inc.
    Inventors: Phoebe Henson, Stephen Yates, Henry Claeys, David Loeffelholz
  • Publication number: 20200122084
    Abstract: A gas compression system includes a system inlet to receive a gas stream containing a first component and a second component, a vapor system outlet to discharge the gas stream, and a plurality of compression stages coupled in series between the system inlet and the vapor system outlet. Each of the plurality of compression stages includes a compressor, a condenser coupled to the compressor, and a gravity-independent phase separator coupled to the condenser. The compressor is configured to receive the gas stream from either the system inlet or another of the plurality of compression stages and compress the gas stream. The condenser is configured to condense the second component from the gas stream. The gravity-independent phase separator is configured to remove the second component from the gas stream and discharge the gas stream to either the system outlet or another of the plurality of compression stages.
    Type: Application
    Filed: October 18, 2018
    Publication date: April 23, 2020
    Inventors: Phoebe Henson, Stephen Yates, Henry Claeys, David Loeffelholz
  • Patent number: 10427797
    Abstract: In one embodiment, a method is provided. The method comprises: receiving, in a vehicle, at least one pollution parameter; and adjusting at least one fluid flow regulating mechanism position, to regulate an intake of pollutants into an environmental control system of the vehicle, based upon the at least one pollution parameter.
    Type: Grant
    Filed: January 20, 2017
    Date of Patent: October 1, 2019
    Assignee: Honeywell International Inc.
    Inventors: Dinkar Mylaraswamy, C. Arthur Dins, Qixiang Li, Eric Blumer, Garry H Lee, Henry Claeys, Michael Easley
  • Publication number: 20180257785
    Abstract: In one embodiment, a method is provided. The method comprises: receiving, in a vehicle, at least one pollution parameter; and adjusting at least one fluid flow regulating mechanism position, to regulate an intake of pollutants into an environmental control system of the vehicle, based upon the at least one pollution parameter.
    Type: Application
    Filed: January 20, 2017
    Publication date: September 13, 2018
    Inventors: Dinkar MYLARASWAMY, C. Arthur DINS, Qixiang LI, Eric BLUMER, Garry H LEE, Henry CLAEYS, Michael EASLEY
  • Publication number: 20070113579
    Abstract: An environmental control system for an aircraft cabin includes a plurality of electrically-driven ported shroud cabin air compressors, each cabin air compressor compressing ram air received from the aircraft exterior, a heat exchange circuit comprising a primary heat exchanger receiving airflow from at least one of the cabin air compressors, and the secondary heat exchanger supplying airflow to the aircraft cabin, and an air cycle machine comprising a compressor adapted to receive airflow from the primary heat exchanger and supply compressed air to the secondary heat exchanger. The environmental control system may further comprise an air recirculation system, having an aft recirculation fan adapted to receive a portion of recirculation air from the aircraft cabin, and a recirculation heat exchanger, disposed in the heat exchange circuit in series with the primary and secondary heat exchangers, and adapted to receive airflow from the aft recirculation fan.
    Type: Application
    Filed: July 29, 2005
    Publication date: May 24, 2007
    Inventors: Henry Claeys, Katherine Clarke, David Elpern