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公开(公告)号：US10826626B2
公开(公告)日：2020-11-03
申请号：US16427626
申请日：2019-05-31
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Ashutosh Kumar Jha , Divakara Rao Vadada , Naveen Kumar Veerabhadrappa , Jordan William Nelson
Abstract: Systems and methods for operating sensors in an aircraft are provided. Aspects include receiving, by a processor associated with a sensor, a first request to test a transmitter function of the sensor, transmitting a test message to one or more other sensors associated with the aircraft, and listening to a transmitter associated with each of the one or more other sensors to determine a transmitter status of the sensor, wherein the transmitter status of the sensor is a pass status based on receiving a confirmation from at least one of the one or more other sensors. Aspects also include transmitting air data parameters and health status parameters associated with the air data probe to the one or more other air data probes.
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公开(公告)号：US20190331710A1
公开(公告)日：2019-10-31
申请号：US16395759
申请日：2019-04-26
Applicant: Rosemount Aerospace Inc.
Inventor： Ashutosh Kumar Jha , Jordan William Nelson
Abstract: A monitoring device is provided herein. The monitoring device is in communication with one or more air data systems. The monitoring device includes a processor and a memory storing program instructions thereon. The program instructions executable by the processor to implement a model. The model includes a monitoring and comparing layer utilizing parameters from the one or more air data systems to measure a performance and determine a drift. The model includes an estimating layer providing a degradation model determining a degradation of health parameters of the one or more air data systems. The model includes a predicting layer monitoring changes and patterns in the drift and the degradation of health parameters.
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Patent Agency Ranking
公开(公告)号：US11866147B2
公开(公告)日：2024-01-09
申请号：US17357438
申请日：2021-06-24
Applicant: Rosemount Aerospace Inc.
Inventor： Mahesh Ainapure , Nitin Kumar Goyal , Ashutosh Kumar Jha , Michael William Madsen
CPC classification number: B64C1/1484 , B60S1/08 , B60S1/3404 , B60S1/44 , B60S1/0402
Abstract: A windshield wiper system for use on an aircraft includes a controller and a wiper assembly including a wiper arm, a wiper blade, and a moving block. Further, the windshield wiper system includes a rail assembly including a rail assembly rack, a plurality of electromagnets, and an electrical interface. The electrical interface and the plurality of electromagnets induce a force on the moving block of the wiper assembly, causing the wiper assembly to sweep across the windshield of the aircraft. The controller is coupled to the rail assembly and the controller is configured to direct the motion of the wiper assembly through command signals to the rail assembly.
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公开(公告)号：US11414216B2
公开(公告)日：2022-08-16
申请号：US16788391
申请日：2020-02-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Ashutosh Kumar Jha , Mahesh Ainapure , Praveen Valiyaparambil , Cal Roeske , Rameshkumar Balasubramanian
Abstract: Provided are embodiments for a method for monitoring a wiper system, the method includes reading a radio frequency identification (RFID) tag embedded in a wiper blade using a reader, comparing the read RFID tag to stored wiper blade information, determining a blade usage ratio for the wiper blade based on determining whether the wiper blade has been replaced, and providing 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.
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公开(公告)号：US20220033052A1
公开(公告)日：2022-02-03
申请号：US17357438
申请日：2021-06-24
Applicant: Rosemount Aerospace Inc.
Inventor： Mahesh Ainapure , Nitin Kumar Goyal , Ashutosh Kumar Jha , Michael William Madsen
IPC: B64C1/14
Abstract: A windshield wiper system for use on an aircraft includes a controller and a wiper assembly including a wiper arm, a wiper blade, and a moving block. Further, the windshield wiper system includes a rail assembly including a rail assembly rack, a plurality of electromagnets, and an electrical interface. The electrical interface and the plurality of electromagnets induce a force on the moving block of the wiper assembly, causing the wiper assembly to sweep across the windshield of the aircraft. The controller is coupled to the rail assembly and the controller is configured to direct the motion of the wiper assembly through command signals to the rail assembly.
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公开(公告)号：US20210179296A1
公开(公告)日：2021-06-17
申请号：US16788391
申请日：2020-02-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Ashutosh Kumar Jha , Mahesh Ainapure , Praveen Valiyaparambil , Cal Roeske , Rameshkumar Balasubramanian
IPC: B64F5/60 , G07C5/00 , G07C5/08 , B64C1/14 , G06K19/077
Abstract: Provided are embodiments for a method for monitoring a wiper system, the method includes reading a radio frequency identification (RFID) tag embedded in a wiper blade using a reader, comparing the read RFID tag to stored wiper blade information, determining a blade usage ratio for the wiper blade based on determining whether the wiper blade has been replaced, and providing 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.
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公开(公告)号：US20200304217A1
公开(公告)日：2020-09-24
申请号：US16427626
申请日：2019-05-31
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： Ashutosh Kumar Jha , Divakara Rao Vadada , Naveen Kumar Veerabhadrappa , Jordan William Nelson
Abstract: Systems and methods for operating sensors in an aircraft are provided. Aspects include receiving, by a processor associated with a sensor, a first request to test a transmitter function of the sensor, transmitting a test message to one or more other sensors associated with the aircraft, and listening to a transmitter associated with each of the one or more other sensors to determine a transmitter status of the sensor, wherein the transmitter status of the sensor is a pass status based on receiving a confirmation from at least one of the one or more other sensors. Aspects also include transmitting air data parameters and health status parameters associated with the air data probe to the one or more other air data probes.
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