Patents Assigned to Rosemount Aerospace Inc.
  • Patent number: 11292191
    Abstract: An embodiment of a method for operating a direct write device includes operating a first pump to deliver a first fluid feedstock to a first inlet of a multiaxial needle and operating a second pump to deliver a second feedstock to a second inlet of the multiaxial needle. At least the first and second feedstocks are simultaneously drawn or injected through respective first and second axial passages in the multiaxial needle. At least the first and second feedstocks are combining to a common outlet of the multiaxial needle, forming a single multicomponent deposition material having multiple discrete phases without applying external heat to the first or second feedstocks within the needle. The multicomponent deposition material is deposited from the common outlet onto a substrate.
    Type: Grant
    Filed: June 15, 2018
    Date of Patent: April 5, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Wayde R. Schmidt, Callum Bailey
  • Patent number: 11293815
    Abstract: A system for correcting an air temperature (AT) reading can include a water content sensor configured to measure a water content in an airflow and to output a water content signal indicative thereof, an AT sensor configured to measure an air temperature and output an AT signal indicative thereof, and a correction module operatively connected to the water content sensor and the AT sensor. The correction module can be configured to receive the water content signal and the AT signal and to correct the AT signal based on the water content to output a corrected AT signal.
    Type: Grant
    Filed: July 20, 2018
    Date of Patent: April 5, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: John D. Winter, Wesley J. Schwartz, Darren G. Jackson
  • Patent number: 11279492
    Abstract: A method for managing icing conditions on a rotary aircraft via one or more ice protection controllers. The method includes steps for receiving an icing condition signal from an icing rate sensor at an ice protection controller, determining, in response to the icing condition signal, a de-icing signal based at least in part a liquid water content (LWC). The method further includes steps for transmitting, via a digital communication bus disposed in at least part of a slip ring assembly, the de-icing signal to a upper distributor to cause the upper distributor to transmit power to one or more heating elements for a respective rotor blade.
    Type: Grant
    Filed: November 14, 2019
    Date of Patent: March 22, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Harold Edward Garnett, Matthew Michael Webb, Jason Lee Skoglund
  • Patent number: 11280846
    Abstract: A system for monitoring the quality of voltage supplied by a power supply includes a voltage variation detection module and a controller. The voltage variation detection module has one or more level detection circuits that each receive a signal indicating the supplied voltage, thereby producing an amplitude signal representing a temporal variation in the voltage during a capture interval. The controller determines the capture interval, provides a capture control signal that causes the level detection circuit(s) to receive the voltage during the capture interval, receives the respective amplitude signal(s) from each of the level detection circuit(s), and produces one or more output signals, each representing the amplitude signal(s) and the associated capture interval, thereby providing an indication of the voltage quality. A method of using the system is also disclosed.
    Type: Grant
    Filed: September 3, 2020
    Date of Patent: March 22, 2022
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventor: Dennis A. Quy
  • Patent number: 11262227
    Abstract: A pitot tube includes an outer tube extending from a first tube end to second tube end. The second tube end defines a tip portion of the pitot tube. A tube sleeve is located inside of the outer tube and defines a tube passage extending from the first tube end to the second tube end. A heating element is located between the outer tube and the tube sleeve. The heating element is isolated from airflow into the tube passage. A method of forming a pitot tube includes installing a heating element to an outer surface of a tube sleeve, the tube sleeve defining a tube passage of the pitot tube. The tube sleeve is secured in an outer tube such that the heating element is between the tube sleeve and the outer tube and is isolated from airflow through the tube passage.
    Type: Grant
    Filed: September 23, 2019
    Date of Patent: March 1, 2022
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
  • Patent number: 11237183
    Abstract: A probe head for an air data probe includes a ceramic body and a heater embedded within the ceramic body.
    Type: Grant
    Filed: December 13, 2019
    Date of Patent: February 1, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Christopher Sanden, Scott D. Isebrand, Greg Allen Seidel
  • Patent number: 11237031
    Abstract: An air data probe includes an air data probe body and an additively manufactured heater on the air data probe body, the heater including a first heater layer and a first dielectric layer on the first heater layer. The first dielectric layer makes up an exterior surface of the heater.
    Type: Grant
    Filed: August 20, 2019
    Date of Patent: February 1, 2022
    Assignee: Rosemount Aerospace Inc.
    Inventors: Scott Wigen, Greg Allen Seidel, Ram Ranjan, Timothy Thomas Golly, Wayde R. Schmidt, Sameh Dardona, Slade R. Culp
  • Publication number: 20220024602
    Abstract: An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in the forward tip. A first conduit is in fluid communication with the port opening to guide fluid flow from the port opening to a first chamber. The first chamber is downstream from the port opening. A second conduit, offset radially and circumferentially from the first conduit, is in fluid communication with the first chamber to guide fluid flow from the first chamber to a second chamber. The second chamber is downstream from the first chamber. The offset between the first and second conduits is configured to prevent particle ingestion from the port opening from entering the second conduit.
    Type: Application
    Filed: October 7, 2021
    Publication date: January 27, 2022
    Applicant: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Greg A. Seidel, Paul Robert Johnson
  • Patent number: 11209330
    Abstract: A corrosion resistant apparatus for an air data probe with a sleeve being cylindrical in shape with a first end and a second end, at least one circumferentially extending groove on an outside of the sleeve configured to accommodate coils of a heater, and a bore at a center of the sleeve and extending between the first end and the second end configured to provide a pneumatic pathway that allows atmospheric conditions to reach measurement equipment of the air data probe.
    Type: Grant
    Filed: July 1, 2020
    Date of Patent: December 28, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
  • Patent number: 11193951
    Abstract: An air data probe includes a faceplate, a body connected to the faceplate, and a heating system comprising a coil, the coil being connected to the faceplate. The coil generates an electromagnetic field that couples with the body to heat the body.
    Type: Grant
    Filed: November 8, 2019
    Date of Patent: December 7, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Mark Buenz, Greg Allen Seidel
  • Patent number: 11179808
    Abstract: A method is disclosed for additive manufacturing a three-dimensional object layer-by-layer including depositing a layer of material on a bed surface or a previously deposited layer of the object to form the object layer-by-layer; providing energy to the material after each layer is deposited with the energy being provided by an energy source that forms an energized beam directed at the material; altering a property of a gas surrounding the material and through which the energized beam extends to alter a property of the object constructed from the material; melting the material with the energized beam to form a melted pool of liquefied material; and allowing the material to solidify to bond the material to a previous layer of material of the object.
    Type: Grant
    Filed: July 11, 2018
    Date of Patent: November 23, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Mark Stephen Lopac, Ryan Chou
  • Patent number: 11181505
    Abstract: A method of determining an amount of imperfection in an additively manufactured material is disclosed herein. The method includes forming a sample piece constructed from the material during a same additive manufacturing cycle as a design piece constructed from the material, introducing a first electrical current to the sample piece while maintaining the sample piece at a reference temperature, and determining the amount of imperfection in the material depending on the measured resistance and the reference temperature of the sample piece.
    Type: Grant
    Filed: July 13, 2018
    Date of Patent: November 23, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Rudy Pitera, Greg Allen Seidel, Scott Wigen
  • Patent number: 11181807
    Abstract: Apparatus and associated methods relate to ranging of objects in a scene based on difference images indicative of only objects in the scene that have ranges within a subrange. The difference images are calculated by taking differences of two images, each of which captures light reflected by objects in the scene that have ranges within range domains that are different from one another. Thus, each of the difference images includes light reflected by only those objects located at ranges that are included in one of the range domains but not the other. These range domains are controlled by the timing of operation of a fast shutter. In some embodiments, the fast shutter includes an electro-optical modulator between two polarizing filters. The electro-optical modulator can rapidly change the polarization of the light transmitted therethrough such that the second polarizing filter either transmits or blocks the light.
    Type: Grant
    Filed: July 14, 2020
    Date of Patent: November 23, 2021
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventor: Mark Ray
  • Patent number: 11181545
    Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.
    Type: Grant
    Filed: November 28, 2017
    Date of Patent: November 23, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
  • Patent number: 11173878
    Abstract: A windshield wiper assembly for a dual sweep angle and indexable wiper system is provided. The system includes a wiper motor and a wiper arm for sweeping a surface of a windshield coupled to a first eccentric, the first eccentric comprising a primary eccentric and an indexable eccentric plate, wherein the indexable eccentric plate determines an eccentric offset of the wiper arm coupled to the first eccentric. The system further includes an output wiper shaft coupled to the wiper arm, a second eccentric coupled to a cam shaft, and a link coupled to the first eccentric and the second eccentric, the link having a first effective link arm length between the first eccentric and the second eccentric for driving the first eccentric to operate the wiper arm when operated in a first direction.
    Type: Grant
    Filed: April 15, 2019
    Date of Patent: November 16, 2021
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Amar Patel, Ramanathan Malaichamy
  • Patent number: 11172580
    Abstract: The proposed masking dam protects ball grid array integrated circuit components from conformal coating overflow, preventing joint breakage and thermal mismatch. The masking dam includes a frame with an integrated seal, a cover, and a fastening mechanism. The frame is sealed to a circuit board surround a component, the cover is attached to the frame, and the masking dam is secured to protect the component.
    Type: Grant
    Filed: July 24, 2017
    Date of Patent: November 9, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventor: James R. Gaertner, II
  • Patent number: 11168883
    Abstract: A vented module includes a housing portion having a drainage side and a drainage port within the drainage side. The module further includes a flame arrestor including a first surface having a fluid inlet, a second surface having at least one fluid outlet, a labyrinth channel extending from the fluid inlet to the fluid outlet, and at least one mesh screen disposed within the labyrinth channel. The flame arrestor is attached to the housing portion such that the drainage port is aligned with the fluid inlet.
    Type: Grant
    Filed: September 29, 2017
    Date of Patent: November 9, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Kevin Benning, Aaron Wesser, Scott Wigen, Andrew Sherman
  • Patent number: 11169173
    Abstract: A system includes a laser air data sensor and an acoustic air data sensor. The laser air data sensor is configured to emit directional light into airflow about an aircraft exterior and to generate first air data parameter outputs for the aircraft based on returns of the emitted directional light. The acoustic air data sensor is configured to emit acoustic signals into the airflow about the aircraft exterior, sense the acoustic signals, and generate second air data parameter outputs for the aircraft based on the sensed acoustic signals.
    Type: Grant
    Filed: May 15, 2019
    Date of Patent: November 9, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Jaime Sly, Mark Sherwood Miller
  • Patent number: 11167727
    Abstract: A windshield wiper system (WWS) is provided and includes a brushless direct current (BLDC) motor with a motor output shaft gear, a gear train and an internally cut sector gear. The gear train includes a first gear, which has a first diameter and engages with the motor output shaft gear, and a second gear, which has a second diameter that is shorter than the first diameter and rotates with the first gear. The internally cut sector gear is coupled with an output shaft and formed to define an internal geared groove that engages with the second gear.
    Type: Grant
    Filed: January 11, 2019
    Date of Patent: November 9, 2021
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Nouduri Phani Srinivas, Srivatsa Santyar
  • Patent number: 11167861
    Abstract: An air data probe includes a probe head defining a longitudinal axis between a forward tip and aft base. A port opening is defined in a side of the probe head and opening at an angle with respect to the longitudinal axis. A bulkhead within the probe head has a chamber in fluid communication with the port opening. The chamber includes a single chamber inlet having an elongated cross-sectional shape. The single elongated chamber inlet is in fluid communication with two downstream pressure conduits to provide redundancy in case one of the two pressure conduits is blocked.
    Type: Grant
    Filed: March 13, 2020
    Date of Patent: November 9, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy T. Golly, Paul R. Johnson, Greg Seidel