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公开(公告)号：US20180170572A1
公开(公告)日：2018-06-21
申请号：US15897537
申请日：2018-02-15
Applicant: Rosemount Aerospace Inc.
Inventor： Kaare Josef Anderson , Brian Daniel Matheis , Derrick D. Hongerholt , William Kunik
Abstract: In one example, a method includes receiving, over an aircraft data communications bus, a plurality of non-pneumatic inputs corresponding to aircraft operational parameters. The method further includes processing the plurality of non-pneumatic inputs through an artificial intelligence network to generate an air data output value, and outputting the air data output value to a consuming system for use when a pneumatic-based air data output value is determined to be unreliable.
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公开(公告)号：US20180149501A1
公开(公告)日：2018-05-31
申请号：US15882068
申请日：2018-01-29
Applicant: Rosemount Aerospace, Inc.
Inventor： Paul Robert Johnson , Aaron A. Cusher , Timothy Thomas Golly , Brian Daniel Matheis , Greg Seidel
Abstract: An air data probe has a pitot tube with a tap at a forward end that defines an inner flow path. The inner flow path decreases in the cross-sectional area until reaching a throat. The inner flow path has cross-sections that are generally cylindrical and also has sections of removed material. Other embodiment have unique shapes.
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公开(公告)号：US09696187B2
公开(公告)日：2017-07-04
申请号：US14789598
申请日：2015-07-01
Applicant: Rosemount Aerospace Inc.
Inventor： Mackenzie Whalen , Brian Daniel Matheis
Abstract: A device is disclosed for measuring total pressure of a fluid flow comprises a tubular member having an inlet chamber with an inlet opening at a first end of the tubular member. The tubular member also comprises an outlet chamber having an outlet opening at a second end of the tubular member. The inlet opening has a diameter transverse to the longitudinal axis and the outlet opening has a second diameter transverse to the longitudinal axis. The ratio of the first diameter to the second diameter is from 3:1 to 10:1. The tubular member also includes a transitional chamber between the inlet chamber and the outlet chamber. Total pressure can be measured in the inlet chamber.
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公开(公告)号：US11851193B2
公开(公告)日：2023-12-26
申请号：US16953807
申请日：2020-11-20
Applicant: Rosemount Aerospace Inc.
Inventor： Jaime Sly , Brian Daniel Matheis , Kaare Josef Anderson
Abstract: An optical ice detector and airspeed probe includes an ice detection module and an airspeed module. The ice detection module detects the presence or absence of ice, water, or ice and water particles, and the airspeed module determines a line-of-sight speed along a directional vector, each based on backscatter light returns emitted from a common collimated light source. An electronics module determines an airspeed of an aircraft based on the line-of-sight speed determined by the airspeed module and at least one aircraft parameter received from the air data system.
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公开(公告)号：US11422147B2
公开(公告)日：2022-08-23
申请号：US16694303
申请日：2019-11-25
Applicant: Rosemount Aerospace Inc.
Inventor： Brian Hawley , Jaime Sly , Brian Daniel Matheis
Abstract: Apparatus and associated methods relate to detecting turbulence of an airstream over an airfoil surface of an aircraft using a sequence of acoustic transducers attached to the airfoil surface of the aircraft along a path. Each of the sequence of acoustic transducers is configured to detect acoustic waves indicative of airstream condition proximate the acoustic transducer. A processor is configured to determine, for each of the sequence of acoustic transducers, a level of turbulence of the airstream proximate the acoustic transducer.
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Patent Agency Ranking
公开(公告)号：US20220161933A1
公开(公告)日：2022-05-26
申请号：US16953807
申请日：2020-11-20
Applicant: Rosemount Aerospace Inc.
Inventor： Jaime Sly , Brian Daniel Matheis , Kaare Josef Anderson
Abstract: An optical ice detector and airspeed probe includes an ice detection module and an airspeed module. The ice detection module detects the presence or absence of ice, water, or ice and water particles, and the airspeed module determines a line-of-sight speed along a directional vector, each based on backscatter light returns emitted from a common collimated light source. An electronics module determines an airspeed of an aircraft based on the line-of-sight speed determined by the airspeed module and at least one aircraft parameter received from the air data system.
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公开(公告)号：US20200300882A1
公开(公告)日：2020-09-24
申请号：US16361005
申请日：2019-03-21
Applicant: Rosemount Aerospace Inc.
Inventor： Brian Daniel Matheis , Daniel W. Shannon , Sudarshan N. Koushik
Abstract: An acoustic air data sensing system includes an acoustic transmitter, a plurality of acoustic receivers, and a skin friction sensor. The acoustic transmitter is located to transmit an acoustic signal into airflow about an exterior of a vehicle. Each of the acoustic receivers is located at a respective angle from a wind angle reference line and a respective distance from the acoustic transmitter. The skin fiction sensor is positioned in a boundary layer region of the airflow that interacts with the acoustic receivers and transmitter. Based on time of flight values of the acoustic signal from the transmitter to each of the receivers and a skin friction measurement from the skin friction sensor as inputs to a transformation matrix, the acoustic air data sensing system outputs, from the transformation matrix, the true airspeed, the relative wind angle, and the speed of sound for operational control of the vehicle.
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公开(公告)号：US10281303B2
公开(公告)日：2019-05-07
申请号：US14665007
申请日：2015-03-23
Applicant: Rosemount Aerospace, Inc.
Inventor： Paul Robert Johnson , Aaron A Cusher , Timothy Thomas Golly , Brian Daniel Matheis , Greg Seidel
Abstract: An air data probe has a pitot tube with a tap at a forward end that defines an inner flow path. The inner flow path decreases in the cross-sectional area until reaching a throat. The inner flow path has cross-sections that are generally cylindrical and also has sections of removed material.
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公开(公告)号：US09932127B2
公开(公告)日：2018-04-03
申请号：US14962137
申请日：2015-12-08
Applicant: Rosemount Aerospace Inc.
Inventor： Kaare Josef Anderson , Brian Daniel Matheis , Derrick D. Hongerholt , William Kunik
CPC classification number: B64D43/02 , G01C21/165 , G01P5/16 , G01P13/025 , G01P21/025 , G06N3/04 , G07C5/0808
Abstract: In one example, a method includes receiving, over an aircraft data communications bus, a plurality of non-pneumatic inputs corresponding to aircraft operational parameters. The method further includes processing the plurality of non-pneumatic inputs through an artificial intelligence network to generate an air data output value, and outputting the air data output value to a consuming system for use when a pneumatic-based air data output value is determined to be unreliable.
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公开(公告)号：US20180017591A1
公开(公告)日：2018-01-18
申请号：US15649873
申请日：2017-07-14
Applicant: Rosemount Aerospace Inc.
Inventor： Charles Jae Doolittle , Mackenzie Whalen , James Barron Egberg , Aaron A. Cusher , Brian Daniel Matheis
CPC classification number: G01P5/165 , G01L19/0007 , G01L19/02 , G01L19/14 , G01P13/025
Abstract: An air data probe includes a probe body and an air data sensing port disposed in the probe body. The probe body includes a barrel region, a tapered head region extending forward from the barrel region, and a tip at a forward-most end of the tapered head region. The air data sensing port is disposed in the probe body at a port location aft of the tip. The probe body has a turbulence-producing geometry originating at the tip that produces a turbulent boundary layer of airflow that extends from the tip to the port location.
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