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公开(公告)号：EP4235218A3
公开(公告)日：2024-01-03
申请号：EP23168581.9
申请日：2019-12-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： SLY, Jamie , MILLER, Mark Sherwood
IPC: G01P5/24 , G01P5/26 , G01P13/02 , G01S7/521 , G01S15/60 , G01S15/86 , G01S17/00 , G01S17/58 , B64D43/02 , G01S15/00
Abstract: An air data sensor is described, comprising: an acoustic transmitter (101) configured to output an acoustic signal into an airflow; a plurality of acoustic transducers (105) configured to receive the acoustic signal output by the acoustic transmitter; a light source (107) configured to output a light beam into the airflow; a light receiver (111) configured to receive scattered light from the light beam, wherein the light source (107) and the light receiver (111) are bistatic such that a measurement zone is formed away from the air data sensor (100); a plate body (117); and one or more lenses mounted to the plate body (117) and disposed in optical communication with each the light source (107) and the light receiver (111).
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12.发明公开
公开(公告)号：EP4279887A1
公开(公告)日：2023-11-22
申请号：EP23173475.7
申请日：2023-05-15
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： SABLE, Robert E. , PITERA, Rudy
Abstract: In one embodiment, a cover (12) for an aircraft sensor includes a leading edge (28), the leading edge extending along a longitudinal axis. A first side panel (24) extending from the leading edge in a positive x direction transverse to the longitudinal axis and a second side panel (26) extending from the leading edge in the positive x direction. A first trailing edge (30) on the first side panel, the first trailing edge opposite the leading edge. A second trailing edge (32) on the second side panel, the second trailing edge opposite the leading edge. A first plurality of ridges (34) on an outer surface of the first side panel.
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公开(公告)号：EP4235189A2
公开(公告)日：2023-08-30
申请号：EP23165129.0
申请日：2019-12-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： WIGEN, Scott , Seidel, Greg , RANJAN, Ram , GOLLY, Timothy Thomas
Abstract: An air data probe (10;26;42) includes an air data probe body (12;28;44) and an additively manufactured heater (100-900) on the air data probe body.
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公开(公告)号：EP4224265A1
公开(公告)日：2023-08-09
申请号：EP23155425.4
申请日：2023-02-07
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： BALASUBRAMANIAN, Rameshkumar , ROESKE, Cal
IPC: G05B23/02
Abstract: A method for monitoring a vehicle-borne probe (12) includes receiving, by a first edge device (18) in communication with the probe (12), sensed data related to a characteristic of a heating element (14) of the probe (12), analyzing, by a first application of the first edge device (18), the sensed data to generate a first data output, receiving, by a coordinator (20) in communication with the first edge device (18), the first data output, and incorporating the first data output into a data package, receiving, by a cloud infrastructure (26) in communication with the coordinator (20), the data package via a data gateway (24), and analyzing, by one of the cloud infrastructure (26) and a ground station (28), the data package to estimate a remaining useful life and a failure of the probe (12).
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公开(公告)号：EP4224171A1
公开(公告)日：2023-08-09
申请号：EP23155360.3
申请日：2023-02-07
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： BALASUBRAMANIAN, Rameshkumar , ROESKE, Cal
Abstract: An edge device (18) for use in a system for monitoring a vehicle-borne probe includes a first communication interface (48) configured to receive sensed data related to a characteristic of a heating element of a first probe (12), a core application module (60) configured to host a plurality of core applications (62), a dynamic application module (64) configured to host a plurality of dynamic applications (66), and a processing unit (40) configured to implement the plurality of core applications on the sensed data. The plurality of core applications includes a coarse data processing application configured to monitor and analyze the sensed data to generate a first data output.
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Patent Agency Ranking
公开(公告)号：EP4166449A3
公开(公告)日：2023-07-12
申请号：EP22202217.0
申请日：2022-10-18
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： BALASUBRAMANIAN, Rameshkumar , PESIK, Joseph
Abstract: A vision-based aircraft cabin light monitoring/control system is used to maintain the light intensity level within the aircraft cabin at a desired level. The system uses video cameras (34) to continuously monitor the ambient light entering the passenger cabin windows (28), analyzes the video stream/feed to identify the light intensity level within the cabin, identifies the window whose state should be controlled, and generates commands to control the window through central cabin controllers (14). The system further compensates for light sources internal to the cabin and monitors the phase of flight to ensure compliance to specific light conditions within the aircraft cabin.
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公开(公告)号：EP4184783A1
公开(公告)日：2023-05-24
申请号：EP22209015.1
申请日：2022-11-23
Applicant: Rosemount Aerospace Inc.
Inventor： MURTHY, Muthukumar , THIRUNARAYANA, Ashok Kumar , ARYASOMAYAJULA, Srividya , KUNDANAGAR, Rohini
IPC: H02P3/22 , H02P6/06 , H02P6/08 , H02P6/24 , H02P21/06 , H02P23/06 , H02P23/20 , H02P23/24 , B60S1/08 , B60L1/00 , B60J1/00
Abstract: A windshield wiper system includes a three-phase motor (14), the three-phase inverter (34), a brake circuit (36), and a controller (18). The controller transmits commutation signals to the three-phase inverter to drive the motor according to an inboard-to-outboard speed profile and to drive the motor according to an outboard-to-inboard speed profile. The controller activates the brake circuit based on the inboard-to outboard speed profile, or the outboard-to-inboard speed profile, and a direct current bus voltage.
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公开(公告)号：EP4166449A2
公开(公告)日：2023-04-19
申请号：EP22202217.0
申请日：2022-10-18
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： BALASUBRAMANIAN, Rameshkumar , PESIK, Joseph
Abstract: A vision-based aircraft cabin light monitoring/control system is used to maintain the light intensity level within the aircraft cabin at a desired level. The system uses video cameras (34) to continuously monitor the ambient light entering the passenger cabin windows (28), analyzes the video stream/feed to identify the light intensity level within the cabin, identifies the window whose state should be controlled, and generates commands to control the window through central cabin controllers (14). The system further compensates for light sources internal to the cabin and monitors the phase of flight to ensure compliance to specific light conditions within the aircraft cabin.
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公开(公告)号：EP4163162A1
公开(公告)日：2023-04-12
申请号：EP22200034.1
申请日：2022-10-06
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： SRINIVAS, Nouduri Phani , KUPPUSWAMY, Murugan
IPC: B60S1/52
Abstract: An aircraft windshield wiper system includes a wiper blade (14) with a composite support member (26) and a blade element that interfaces with the windshield of the aircraft to clear the windshield of rain and other debris. The composite support member (26) includes a wash tube (32) integral with the composite support member (26), such that the wash tube (32) receives windshield washing fluid from a fluid reservoir and dispenses the fluid onto the windshield of the aircraft. A plurality of clips can be used to couple the composite support member (26) to the blade element.
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公开(公告)号：EP4134298A1
公开(公告)日：2023-02-15
申请号：EP22190049.1
申请日：2022-08-11
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： PESIK, Joseph , BOER, Jonathan
Abstract: A camera with a field of view toward an external environment of an aircraft is disposed within an aircraft door. A display device is disposed within an interior of the aircraft. A processor is operatively coupled to the camera and to the display device. The processor analyzes image data captured by the camera to provide alerts, automatic guidance, or other outputs that can reduce aircraft crew workload, thereby increasing crew efficiency as well as the safety of the aircraft crew and passengers during aircraft operation.
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