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公开(公告)号：EP3179254B1
公开(公告)日：2018-09-05
申请号：EP16201353.6
申请日：2016-11-30
Applicant: Rosemount Aerospace Inc.
CPC classification number: B64D43/02 , G01C21/165 , G01P5/16 , G01P13/025 , G01P21/025 , G06N3/04 , G07C5/0808
Abstract: The method according to the invention 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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Patent Agency Ranking
公开(公告)号：EP3336558A1
公开(公告)日：2018-06-20
申请号：EP17207656.4
申请日：2017-12-15
Applicant: Rosemount Aerospace Inc.
Inventor： MILLER, Mark Sherwood , NASLUND, Brian Brent , KUNIK, William
CPC classification number: G01P13/025 , B64D43/02 , G01K13/028 , G01P5/14 , G01P5/165 , G01P5/26 , G01P21/025
Abstract: A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel of a first multi-function probe (MFP) (12A) that is electrically coupled with a first electronics channel of a second MFP (12B) to receive static pressure data from the second MFP (12B). A second air data system for providing second aircraft air data parameter outputs is formed by a second electronics channel of the second MFP (12B) that is electrically coupled with a second electronics channel of the first MFP (12A) to receive static pressure data from the first MFP (12A). A third air data system for providing third aircraft air data parameter outputs is formed by a laser air data sensor that is configured to emit directional light into airflow about the aircraft exterior and to generate the third aircraft air data parameter outputs based on returns of the emitted directional light.
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公开(公告)号：EP3179254A1
公开(公告)日：2017-06-14
申请号：EP16201353.6
申请日：2016-11-30
Applicant: Rosemount Aerospace Inc.
CPC classification number: B64D43/02 , G01C21/165 , G01P5/16 , G01P13/025 , G01P21/025 , G06N3/04 , G07C5/0808
Abstract: The method according to the invention 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.
Abstract translation: 根据本发明的方法包括通过飞行器数据通信总线接收与飞行器操作参数相对应的多个非气动输入。 该方法还包括通过人造智能网络处理多个非气动输入，以产生空气数据输出值，并将空气数据输出值输出到消耗系统，以在将基于气动的空气数据输出值确定为 不可靠
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公开(公告)号：EP3926346A1
公开(公告)日：2021-12-22
申请号：EP21180693.0
申请日：2021-06-21
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： ROESKE, Cal , KUNIK, William , NASLUND, Brian Brent , BALASUBRAMANIAN, Rameshkumar
Abstract: A method of inspecting an air data (10) probe for damage or misalignment on a mounting surface includes retrieving reference data for the air data probe from a database, capturing images of the air data probe via a camera (30) and generating dimensions from the captured images of the air data probe via a feature extractor (50). An alignment calculator (52) analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify misalignment of the air data probe, and analyzes the generated dimensions from the captured images of the air data probe and the reference data for the air data probe from the database to identify damage of the air data probe. A maintenance recommendation for the air data probe is generated and outputted, based on the identified misalignment or damage of the air data probe.
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公开(公告)号：EP3730947A1
公开(公告)日：2020-10-28
申请号：EP19214956.5
申请日：2019-12-10
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： SLY, Jamie , SHANNON, Daniel W. , MATHEIS, Brian Daniel , ELL, Todd A. , KUNIK, William , KOUSHIK, Surdarshan N.
Abstract: An ultrasonic air data system (100) can include a pole (103) having a length (103) longer than a boundary layer thickness (105) of a boundary layer flow (107) such that at least a distal end of the pole is configured to extend outwardly from an aircraft surface to be at least partially outside of the boundary layer flow. The system can include a transmitter (111) disposed on or in the pole at or near the distal end of the pole such that the transmitter is located at least partially outside of the boundary layer flow when in use, wherein the transmitter is configured to output a transmitter signal. The system can include one or more receivers (115) disposed downstream of the pole as defined by the boundary layer flow and configured to receive the transmitter signal.
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公开(公告)号：EP3677922A1
公开(公告)日：2020-07-08
申请号：EP19218977.7
申请日：2019-12-20
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： KUNIK, William , NASLUND, Brian Brent , BRAUN, Scott J.
IPC: G01P5/165 , G01P21/02 , G06K9/78 , G06T7/00 , G01N21/956
Abstract: Inspecting an air data probe for physical degradation includes generating a silhouette (64) of the air data probe (12) based on an identification of the air data probe to be inspected. The silhouette is simultaneously displayed with an image (66) of the air data probe produced by a camera (18), and the displayed image of the air data probe is caused to conform to the silhouette on the display (20). An image of the air data probe is captured while the displayed image of the air data probe conforms to the silhouette on the display. The captured image is analyzed to identify physical degradation of the air data probe. A maintenance recommendation for the air data probe is generated based on the identified physical degradation.
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