image
image
user-login
Patent search/

METHOD FOR ENHANCING AVIATION SAFETY THROUGH STRUCTURAL HEALTH MONITORING (SHM) OF AIRCRAFT COMPONENTS

search

Patent Search in India

  • tick

    Extensive patent search conducted by a registered patent agent

  • tick

    Patent search done by experts in under 48hrs

₹999

₹399

Talk to expert

METHOD FOR ENHANCING AVIATION SAFETY THROUGH STRUCTURAL HEALTH MONITORING (SHM) OF AIRCRAFT COMPONENTS

ORDINARY APPLICATION

Published

date

Filed on 13 November 2024

Abstract

A method (100) for enhancing aviation safety through Structural Health Monitoring (SHM) of aircraft components. deploying a plurality of sensors on critical structural components of an aircraft. Further, the method (100) comprising the steps of continuously collecting real-time data from the deployed sensors regarding structural integrity and operational conditions of the aircraft components during flight. Further, the method (100) comprising the steps of processing the collected data using advanced signal processing algorithms to identify potential damage or degradation in the aircraft components. Further, the method (100) comprising the steps of utilizing a damage propagation model, including the Arrhenius equation, to predict the remaining useful life of the aircraft components based on the processed data. Further, the method (100) comprising the steps of generating maintenance recommendations based on the predicted remaining useful life to facilitate condition-based maintenance of the aircraft components.

Patent Information

Application ID202411087608
Invention FieldPHYSICS
Date of Application13/11/2024
Publication Number48/2024

Inventors

NameAddressCountryNationality
KHENI TARANGKUMAR NARESHBHAILOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
NIKHIL RAKESH PAISADELILOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
GAIKWAD HARSHWARDHAN DATTATRAYLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
NAYAK PARTH KUMAR PRAVESH KUMARLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
MOHAMMED SINANLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
PALLELA ARVINDLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia

Applicants

NameAddressCountryNationality
LOVELY PROFESSIONAL UNIVERSITYJALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia

Specification

Description:FIELD OF THE DISCLOSURE
[0001] This invention generally relates to the field of Structural Health Monitoring (SHM) and in particular relates to a method for utilizing advanced sensing technologies and data analysis techniques to assess the integrity and safety of aerospace structures.
BACKGROUND
[0002] The subject matter discussed in the background section should not be assumed to be prior art merely as a result of its mention in the background section. Similarly, a problem mentioned in the background section or associated with the subject matter of the background section should not be assumed to have been previously recognized in the prior art. The subject matter in the background section merely represents different approaches, which in and of themselves may also correspond to implementations of the claimed technology.
[0003] The increasing demand for sustainable practices in various industries has led to a heightened interest in environmentally friendly solvents. Traditional solvents, often derived from , Claims:WE CLAIM:
1. A method (100) for enhancing aviation safety through Structural Health Monitoring (SHM) of aircraft components, the method comprising the steps of:
deploying a plurality of sensors on critical structural components of an aircraft, wherein the sensors are selected from the group consisting of strain gauges, accelerometers, fiber optic sensors, and piezoelectric sensors;
continuously collecting real-time data from the deployed sensors regarding structural integrity and operational conditions of the aircraft components during flight;
processing the collected data using advanced signal processing algorithms to identify potential damage or degradation in the aircraft components;
utilizing a damage propagation model, including the Arrhenius equation, to predict the remaining useful life of the aircraft components based on the processed data; and
generating maintenance recommendations based on the predicted remaining useful life to facilitate condition-based maintenance of the aircraft components.
2. Th

Documents

NameDate
202411087608-COMPLETE SPECIFICATION [13-11-2024(online)].pdf13/11/2024
202411087608-DECLARATION OF INVENTORSHIP (FORM 5) [13-11-2024(online)].pdf13/11/2024
202411087608-DRAWINGS [13-11-2024(online)].pdf13/11/2024
202411087608-FIGURE OF ABSTRACT [13-11-2024(online)].pdf13/11/2024
202411087608-FORM 1 [13-11-2024(online)].pdf13/11/2024
202411087608-FORM-9 [13-11-2024(online)].pdf13/11/2024
202411087608-POWER OF AUTHORITY [13-11-2024(online)].pdf13/11/2024
202411087608-PROOF OF RIGHT [13-11-2024(online)].pdf13/11/2024
202411087608-REQUEST FOR EARLY PUBLICATION(FORM-9) [13-11-2024(online)].pdf13/11/2024

footer-service

By continuing past this page, you agree to our Terms of Service,Cookie PolicyPrivacy Policy  and  Refund Policy  © - Uber9 Business Process Services Private Limited. All rights reserved.

Uber9 Business Process Services Private Limited, CIN - U74900TN2014PTC098414, GSTIN - 33AABCU7650C1ZM, Registered Office Address - F-97, Newry Shreya Apartments Anna Nagar East, Chennai, Tamil Nadu 600102, India.

Please note that we are a facilitating platform enabling access to reliable professionals. We are not a law firm and do not provide legal services ourselves. The information on this website is for the purpose of knowledge only and should not be relied upon as legal advice or opinion.