Abstract: The present invention describes a method and system for monitoring safety parameters of an airplane in compliance with the airplane safety parameters. The system includes an airplane safety device which may obtain a status information corresponding to a current state of the plurality of airplane components (118) via a plurality of sensors (114) associated with each of a plurality of airplane components (118). The system receives the status information from the plurality of sensors (114) associated with the plurality of airplane components (118). Analyze the status information, based on one or more safety-parameters to determine an anomaly in the current state of one or more airplane components. The system triggers a corresponding action to reset the current state of one or more non-compliant airplane components. The action includes displaying an alert message via the user interface (330a) and controlling the corresponding actuators associated with each of the non-compliant airplane components. (To be published with FIG. 1)
Description:PLEASE REFER THE ATTACHMENT , Claims:PLEASE REFER THE ATTACHMENT
| # | Name | Date |
|---|---|---|
| 1 | 202241052048-STATEMENT OF UNDERTAKING (FORM 3) [12-09-2022(online)].pdf | 2022-09-12 |
| 2 | 202241052048-PROOF OF RIGHT [12-09-2022(online)].pdf | 2022-09-12 |
| 3 | 202241052048-POWER OF AUTHORITY [12-09-2022(online)].pdf | 2022-09-12 |
| 4 | 202241052048-FORM 1 [12-09-2022(online)].pdf | 2022-09-12 |
| 5 | 202241052048-DRAWINGS [12-09-2022(online)].pdf | 2022-09-12 |
| 6 | 202241052048-DECLARATION OF INVENTORSHIP (FORM 5) [12-09-2022(online)].pdf | 2022-09-12 |
| 7 | 202241052048-COMPLETE SPECIFICATION [12-09-2022(online)].pdf | 2022-09-12 |
| 8 | 202241052048-FORM 18 [20-10-2023(online)].pdf | 2023-10-20 |
| 9 | 202241052048-FER.pdf | 2025-11-10 |
| 1 | 202241052048_SearchStrategyNew_E_SearchHistoryE_12-08-2025.pdf |