Patents by Inventor Anita Fink

Anita Fink 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: 9835511
    Abstract: A method for forming a pressure sensor includes forming a base of a sapphire material, the base including a cavity formed therein; forming a sapphire membrane on top of the base and over the cavity; forming a lower electrode on top of the membrane; forming a piezoelectric material layer on an upper surface of the lower electrode, the piezoelectric material layer being formed of aluminum nitride (AIN); and forming at least one upper electrode on an upper surface of the piezoelectric material layer.
    Type: Grant
    Filed: May 8, 2015
    Date of Patent: December 5, 2017
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Weibin Zhang, Anita Fink, Kimiko Childress, Odd Harald Steen Eriksen
  • Publication number: 20160327445
    Abstract: A method for forming a pressure sensor includes forming a base of a sapphire material, the base including a cavity formed therein; forming a sapphire membrane on top of the base and over the cavity; forming a lower electrode on top of the membrane; forming a piezoelectric material layer on an upper surface of the lower electrode, the piezoelectric material layer being formed of aluminum nitride (AIN); and forming at least one upper electrode on an upper surface of the piezoelectric material layer.
    Type: Application
    Filed: May 8, 2015
    Publication date: November 10, 2016
    Inventors: Weibin Zhang, Anita Fink, Kimiko Childress, Odd Harald Steen Eriksen
  • Patent number: 9464950
    Abstract: A capacitive pressure sensor includes a substrate wafer and a diaphragm wafer. The substrate wafer defines a substrate recess with a first recess. The diaphragm wafer defines a diaphragm recess with a second recess. The diaphragm wafer is bonded to the substrate wafer such that the substrate and diaphragm recesses form a height differentiated pressure chamber.
    Type: Grant
    Filed: February 20, 2014
    Date of Patent: October 11, 2016
    Assignee: Rosemount Aerospace Inc.
    Inventors: Weibin Zhang, Anita Fink, Saeed Fahimi, Kimiko J. Childress
  • Patent number: 9261425
    Abstract: A pressure sensor assembly includes a pressure sensor having a pressure sensing transducer connected to a plurality of electrode pins via a plurality of electrode pads disposed on the transducer, an inner casing configured to hold the pressure sensing transducer including a plurality of inner casing electrode pin channels having the electrode pins disposed therein. The pressure sensor further includes an outer casing holding the inner casing therein having a capsule header with a plurality of capsule header electrode pin channels defined therein which can include a ceramic seal disposed therein such that the capsule header electrode pin channels engage the electrode pins in an insulating sealed relationship. The outer casing further includes an isolator plate including an isolator plate fluid port defined therein and a pressure isolator disposed on the isolator plate and configured to deflect in response to a change in ambient pressure.
    Type: Grant
    Filed: February 28, 2014
    Date of Patent: February 16, 2016
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Saeed Fahimi, Odd Harald Steen Eriksen, Charles Little, Anita Fink
  • Publication number: 20150276512
    Abstract: A capacitive pressure sensor includes a substrate wafer and a diaphragm wafer. The substrate wafer defines a substrate recess with a first recess. The diaphragm wafer defines a diaphragm recess with a second recess. The diaphragm wafer is bonded to the substrate wafer such that the substrate and diaphragm recesses form a height differentiated pressure chamber.
    Type: Application
    Filed: February 20, 2014
    Publication date: October 1, 2015
    Applicant: ROSEMOUNT AEROSPACE INC.
    Inventors: Weibin Zhang, Anita Fink, Saeed Fahimi, Kimiko J. Childress
  • Publication number: 20150185103
    Abstract: A pressure sensor assembly includes a pressure sensor having a pressure sensing transducer connected to a plurality of electrode pins via a plurality of electrode pads disposed on the transducer, an inner casing configured to hold the pressure sensing transducer including a plurality of inner casing electrode pin channels having the electrode pins disposed therein. The pressure sensor further includes an outer casing holding the inner casing therein having a capsule header with a plurality of capsule header electrode pin channels defined therein which can include a ceramic seal disposed therein such that the capsule header electrode pin channels engage the electrode pins in an insulating sealed relationship. The outer casing further includes an isolator plate including an isolator plate fluid port defined therein and a pressure isolator disposed on the isolator plate and configured to deflect in response to a change in ambient pressure.
    Type: Application
    Filed: February 28, 2014
    Publication date: July 2, 2015
    Applicant: Rosemount Aerospace Inc.
    Inventors: Saeed Fahimi, Odd Harald Steen Eriksen, Charles Little, Anita Fink
  • Patent number: 8656778
    Abstract: A system for determining in-plane acceleration of an object. The system includes an in-plane accelerometer with a substrate rigidly attached to an object, and a proof mass—formed from a single piece of material—movably positioned a predetermined distance above the substrate. The proof mass includes a plurality of electrode protrusions extending downward from the proof mass to form a gap of varying height between the proof mass and the substrate. The proof mass is configured to move in a direction parallel to the upper surfaces of each of the plurality of substrate electrodes when the object is accelerating, which results in a change in the area of the gap, and a change in capacitance between the substrate and the proof mass. The in-plane accelerometer can be fabricated using the same techniques used to fabricate an out-of-plane accelerometer and is suitable for high-shock applications.
    Type: Grant
    Filed: December 30, 2010
    Date of Patent: February 25, 2014
    Assignee: Rosemount Aerospace Inc.
    Inventors: Shuwen Guo, Alexander Spivak, Anita Fink
  • Publication number: 20120167685
    Abstract: A system for determining in-plane acceleration of an object. The system includes an in-plane accelerometer with a substrate rigidly attached to an object, and a proof mass—formed from a single piece of material—movably positioned a predetermined distance above the substrate. The proof mass includes a plurality of electrode protrusions extending downward from the proof mass to form a gap of varying height between the proof mass and the substrate. The proof mass is configured to move in a direction parallel to the upper surfaces of each of the plurality of substrate electrodes when the object is accelerating, which results in a change in the area of the gap, and a change in capacitance between the substrate and the proof mass. The in-plane accelerometer can be fabricated using the same techniques used to fabricate an out-of-plane accelerometer and is suitable for high-shock applications.
    Type: Application
    Filed: December 30, 2010
    Publication date: July 5, 2012
    Applicant: Rosemount Aerospace Inc.
    Inventors: Shuwen Guo, Alexander Spivak, Anita Fink