公开(公告)号：EP4224264A1

公开(公告)日：2023-08-09

申请号：EP23154558.3

申请日：2023-02-01

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BALASUBRAMANIAN, Rameshkumar ,  ROESKE, Cal

IPC: G05B23/02

Abstract: A coordinator for use in a system for monitoring a vehicle-borne probe includes a first communication interface (48) configured to exchange data with at least one edge device (18) of a plurality of edge devices, a second communication interface (48) configured to exchanged data with a cloud infrastructure (26) and at least one vehicle system, and a processing unit (40). The processing unit (40) is configured to analyze synthesized data comprising first data outputs from at least one edge device (18) of the plurality of edge devices, second data outputs from at least one edge device (18) of the plurality of edge devices, and data from the at least one vehicle system. The processing unit (40) is further configured to implement a data processing application to analyze the synthesized data to generate a third data output, and incorporate the synthesized data and the third data output into a data package.

公开(公告)号：EP3835147A1

公开(公告)日：2021-06-16

申请号：EP20213920.0

申请日：2020-12-14

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： JHA, Ashutosh Kumar ,  AINAPURE, Mahesh ,  VALIYAPARAMBIL, Praveen ,  ROESKE, Cal ,  BALASUBRAMANIAN, Rameshkumar

IPC: B60S1/38

Abstract: Provided are embodiments for a method for monitoring a wiper system, the method includes reading (804) a radio frequency identification (RFID) tag embedded in a wiper blade using a reader, comparing (806) the read RFID tag to stored wiper blade information, determining (808) a blade usage ratio for the wiper blade based on determining whether the wiper blade has been replaced, and providing (810) an indication of a status of the wiper blade based at least in part on the blade usage ratio. Also provided are embodiments for a system for monitoring the health of the wiper system.

公开(公告)号：EP4224172A1

公开(公告)日：2023-08-09

申请号：EP23155445.2

申请日：2023-02-07

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BALASUBRAMANIAN, Rameshkumar ,  ROESKE, Cal

IPC: G01P5/16 ,  B64D15/12 ,  G01P5/165 ,  G01P21/02

Abstract: A system for monitoring a vehicle-borne probe (12) includes a first edge device (18) in communication with the probe and configured to sense data related to a characteristic of a heating element (14) of the probe, a coordinator in communication with the first edge device and configured to receive a first data output from the first edge device and to incorporate the first data output into a data package, a cloud infrastructure in communication with the coordinator via a data gateway and configured to analyze the data package to estimate a remaining useful life and predict a failure of the probe, and a ground station (28) in communication with the cloud infrastructure and configured to refine remaining useful life estimation and failure prediction techniques of the system.

公开(公告)号：EP3985400A1

公开(公告)日：2022-04-20

申请号：EP21202743.7

申请日：2021-10-14

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BALASUBRAMANIAN, Rameshkumar ,  ROESKE, Cal

IPC: G01P5/165 ,  G01P13/02 ,  B64D43/02 ,  H05B3/56

Abstract: A sensor assembly for monitoring a heater system for an aircraft probe sensor includes a current sensor module (36) with a current sensor core (38) and a high electromagnetically permeable enclosure (40) around the current sensor core. An input wire pathway (28) extends through the current sensor core and is configured to receive a heater input wire (22). A return wire pathway (30) extends through the current sensor core and is configured to receive a heater return wire (24). A high electromagnetically permeable tube (52, 54) extends through the current sensor core and is configured to extend around one of the input wire and the heater return wire.

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).

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

IPC: G01P5/16 ,  B64D15/12 ,  G01P5/165 ,  G01P21/02

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.

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

IPC: G01P21/02 ,  G01P5/165 ,  G01N21/95 ,  G06K9/46 ,  G06T7/00 ,  G06T7/70 ,  B64D43/02

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.