Patents Assigned to Rosemount Aerospace Inc.
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Patent number: 11319086Abstract: Apparatus and associated methods relate to aligning a taxi-assist camera such that each image frame of real-time video that the camera generates has a standard presentation format. The taxi-assist camera is configured to be mounted on an aircraft and oriented such that each image frame includes both a specific feature of the aircraft and of nearby objects external to the aircraft. The specific feature of the aircraft is detected and a location within the image frame of the specific feature is determined. The determined location within the image frame is compared with a reference location. A transformation operator is generated to transform the image frame such that the specific feature of the aircraft will be located within the image at a location corresponding to the reference location. The transformation operator is then applied to each of the image frames of the real-time video that the camera generates.Type: GrantFiled: May 23, 2016Date of Patent: May 3, 2022Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Travis W. Fleck, Gerald L. Brown
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Patent number: 11292191Abstract: 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: GrantFiled: June 15, 2018Date of Patent: April 5, 2022Assignee: Rosemount Aerospace Inc.Inventors: Wayde R. Schmidt, Callum Bailey
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Patent number: 11292435Abstract: A windshield wiper system (WWS) blade assembly is provided. The WWS blade assembly includes a composite frame and a blade that has a length which is normally shorter than a corresponding length of the composite frame. The blade includes first and second ends attachable to corresponding first and second ends of the composite frame, respectively.Type: GrantFiled: February 28, 2019Date of Patent: April 5, 2022Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Nouduri Phani Srinivas, Venkata Anil Kumar Mothe, Sujoy Khanra, Elbert Jeyapaul
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Patent number: 11293995Abstract: A system and method for monitoring leakage current in a heater connected to a heater power supply by a power cable having a first power lead conducting an inlet current defining an inlet current direction and a second power lead conducting an outlet current defining an outlet current direction that is opposite the inlet current direction. The system includes a differential current electromagnetic sensor having a magnetic core with a center region that the power cable passes through one or more times. The magnetic core has an air gap in which a magnetic flux sensing device is positioned and configured to provide a signal that is representative of magnetic flux across the air gap, which is indicative of a difference between the inlet current and the outlet current. This difference defines the leakage current.Type: GrantFiled: March 23, 2020Date of Patent: April 5, 2022Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Magdi A. Essawy, Cuong Tho Huynh, Marvin G. Onken
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Patent number: 11293815Abstract: 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: GrantFiled: July 20, 2018Date of Patent: April 5, 2022Assignee: Rosemount Aerospace Inc.Inventors: John D. Winter, Wesley J. Schwartz, Darren G. Jackson
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Patent number: 11279492Abstract: 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: GrantFiled: November 14, 2019Date of Patent: March 22, 2022Assignee: Rosemount Aerospace Inc.Inventors: Harold Edward Garnett, Matthew Michael Webb, Jason Lee Skoglund
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Patent number: 11280846Abstract: 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: GrantFiled: September 3, 2020Date of Patent: March 22, 2022Assignee: ROSEMOUNT AEROSPACE INC.Inventor: Dennis A. Quy
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Patent number: 11262227Abstract: 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: GrantFiled: September 23, 2019Date of Patent: March 1, 2022Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Robin Jacob, Guru Prasad Mahapatra, Paul Robert Johnson
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Patent number: 11237183Abstract: A probe head for an air data probe includes a ceramic body and a heater embedded within the ceramic body.Type: GrantFiled: December 13, 2019Date of Patent: February 1, 2022Assignee: Rosemount Aerospace Inc.Inventors: Christopher Sanden, Scott D. Isebrand, Greg Allen Seidel
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Patent number: 11237031Abstract: 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: GrantFiled: August 20, 2019Date of Patent: February 1, 2022Assignee: Rosemount Aerospace Inc.Inventors: Scott Wigen, Greg Allen Seidel, Ram Ranjan, Timothy Thomas Golly, Wayde R. Schmidt, Sameh Dardona, Slade R. Culp
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Publication number: 20220024602Abstract: 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: ApplicationFiled: October 7, 2021Publication date: January 27, 2022Applicant: Rosemount Aerospace Inc.Inventors: Timothy Thomas Golly, Greg A. Seidel, Paul Robert Johnson
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Patent number: 11209330Abstract: 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: GrantFiled: July 1, 2020Date of Patent: December 28, 2021Assignee: Rosemount Aerospace Inc.Inventors: Timothy Thomas Golly, Paul Robert Johnson, Greg Seidel
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Patent number: 11193951Abstract: 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: GrantFiled: November 8, 2019Date of Patent: December 7, 2021Assignee: Rosemount Aerospace Inc.Inventors: Mark Buenz, Greg Allen Seidel
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Patent number: 11179808Abstract: 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: GrantFiled: July 11, 2018Date of Patent: November 23, 2021Assignee: Rosemount Aerospace Inc.Inventors: Mark Stephen Lopac, Ryan Chou
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Patent number: 11181545Abstract: 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: GrantFiled: November 28, 2017Date of Patent: November 23, 2021Assignee: Rosemount Aerospace Inc.Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
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Patent number: 11181807Abstract: 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: GrantFiled: July 14, 2020Date of Patent: November 23, 2021Assignee: ROSEMOUNT AEROSPACE INC.Inventor: Mark Ray
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Patent number: 11181505Abstract: 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: GrantFiled: July 13, 2018Date of Patent: November 23, 2021Assignee: Rosemount Aerospace Inc.Inventors: Rudy Pitera, Greg Allen Seidel, Scott Wigen
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Patent number: 11173878Abstract: 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: GrantFiled: April 15, 2019Date of Patent: November 16, 2021Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Amar Patel, Ramanathan Malaichamy
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Patent number: 11167727Abstract: 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: GrantFiled: January 11, 2019Date of Patent: November 9, 2021Assignee: ROSEMOUNT AEROSPACE INC.Inventors: Nouduri Phani Srinivas, Srivatsa Santyar
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Patent number: 11169173Abstract: 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: GrantFiled: May 15, 2019Date of Patent: November 9, 2021Assignee: Rosemount Aerospace Inc.Inventors: Jaime Sly, Mark Sherwood Miller