Patents Assigned to ADAMS RITE AEROSPACE
  • Patent number: 11781299
    Abstract: A touchless faucet includes a faucet body having a first compartment and a second compartment, where the second compartment has a mixing chamber for mixing fluid and a flow passage. The faucet also includes an aerator coupled to the faucet body and configured to receive fluid from the flow passage, a control board disposed in the first compartment, a solenoid disposed in the second compartment and communicatively coupled to the control board, and an IR sensor disposed in the first compartment for sensing a presence of a user.
    Type: Grant
    Filed: May 19, 2021
    Date of Patent: October 10, 2023
    Assignee: ADAMS RITE AEROSPACE, INC.
    Inventors: Matthew Timsit, Nera-Lee Herzig-Patel, Enoch Hwang, Juan Pena, Chris Selstad, Dan Lau
  • Patent number: 11384585
    Abstract: A shock absorber includes a first end configured to be mechanically fastened to a first component, a second end configured to be mechanically fastened to a second component, a main body, a main shaft, and a primary piston. The primary piston configured to move within the main body and further configured to provide a first damping force by movement of a fluid through the primary piston while the main shaft moves a first distance. The shock absorber also includes a deformable solid material arranged in the main body. The primary piston configured to further move within the main body and further configured to provide a second damping force by deforming the deformable solid material after the main shaft moves the first distance.
    Type: Grant
    Filed: January 17, 2019
    Date of Patent: July 12, 2022
    Assignee: ADAMS RITE AEROSPACE INC.
    Inventors: Morteza Yadollahi, Alan Manara
  • Publication number: 20110297333
    Abstract: An aircraft window shade assembly is provided. The assembly includes an inboard shade, an outboard shade, a housing and a cover. The inboard and outboard shades each include a plurality of holes disposed along one side. The housing includes a transparent inboard panel, a transparent outboard panel, a pair of inboard guide slots to receive the inboard shade, a pair of outboard guide slots to receive the outboard shade, an inboard motor and an outboard motor. The inboard motor is coupled to a drive gear sprocket having a cylindrical outer surface and a plurality of teeth extending radially therefrom that mesh with the plurality of holes in the inboard shade, and moves the inboard shade between open and closed positions. The outboard motor is coupled to a drive gear sprocket having a cylindrical outer surface and a plurality of teeth extending radially therefrom that mesh with the plurality of holes in the outboard shade, and moves the outboard shade between open and closed positions.
    Type: Application
    Filed: August 15, 2011
    Publication date: December 8, 2011
    Applicant: ADAMS RITE AEROSPACE, INC.
    Inventors: Thomas J. Sievers, Morteza Yadollahi, John F. Leary, Darrell L. James, Marek S. Brzeski, Elmon D. Sotto, John Edward Cheever
  • Publication number: 20110201262
    Abstract: A system for monitoring pressure change within at least one compartment of an aircraft is provided. The system includes a primary pressure sensor for providing a signal corresponding to a pressure within a primary compartment of the aircraft, a primary monitoring channel coupled to the primary pressure sensor, and an output driver coupled to the primary monitoring channel. The primary monitoring channel includes a band pass filter for receiving and filtering the primary pressure signal, a pressure change circuit for determining a change in the filtered pressure signal and for providing a pressure change output signal corresponding to the change in pressure, and a threshold logic circuit for determining whether the pressure change output signal meets a predetermined threshold and for providing a threshold output signal indicating that a decompression event has occurred if the pressure change output signal meets the predetermined threshold.
    Type: Application
    Filed: March 9, 2009
    Publication date: August 18, 2011
    Applicant: ADAMS RITE AEROSPACE
    Inventor: Michael Lehmann
  • Publication number: 20090118876
    Abstract: A decompression vent latching apparatus, includes a flap placed on a door opening to a first area from a second area, a housing fastened to the flap on the door, a plunger mounted within the housing, having rotational and lateral movement within the housing, a stop block connected to the plunger, a pair of tip blocks having movement restricted by the stop block connected to the plunger when contacting the stop block, the tip blocks being controlled to be a predetermined distance away from the stop block, and a locking unit connected to the pair of tip blocks providing a closed or open position.
    Type: Application
    Filed: November 3, 2008
    Publication date: May 7, 2009
    Applicant: ADAMS RITE AEROSPACE
    Inventor: Morteza Yadollahi