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AIRCRAFT LANDING GEAR SYSTEM

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AIRCRAFT LANDING GEAR SYSTEM

ORDINARY APPLICATION

Published

date

Filed on 4 November 2024

Abstract

ABSTRACT An aircraft landing gear system (100), the system (100) comprising: a body comprising: a plurality of advanced material components configured to withstand fatigue loading conditions; a shock absorption mechanism integrated with the body to dissipate energy efficiently; a monitoring system configured to track stress and fatigue levels in real-time.

Patent Information

Application ID202411084295
Invention FieldMECHANICAL ENGINEERING
Date of Application04/11/2024
Publication Number46/2024

Inventors

NameAddressCountryNationality
KAJOL SABATLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
HARSH RAJLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
HARI NARAYANANLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
ANGSHUMAN BARUAH SHUBHAM AGARWALLOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411IndiaIndia
Dr. RAJEEV KUMARLOVELY 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 a field of aircraft landing gear systems and, more specifically, to an improved landing gear design that addresses fatigue loading conditions to enhance durability and performance.
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] Traditional aircraft landing gear systems are subject to significant fatigue loading conditions due to repetitive takeoff and landing cycles. These conditions often lead to the progressive weakening of structural compon , Claims:1. An aircraft landing gear system (100), the system (100) comprising:
a body comprising:
a plurality of advanced material components configured to withstand fatigue loading conditions;
a shock absorption mechanism integrated with the body to dissipate energy efficiently;
a monitoring system configured to track stress and fatigue levels in real-time.

2. The system (100) as claimed in claim 1, wherein the plurality of advanced material components includes nanocomposites and smart materials.

3. The system (100) as claimed in claim 1, further comprising a predictive maintenance feature that uses data from the monitoring system to predict potential failures and schedule maintenance activities proactively.

Documents

NameDate
202411084295-COMPLETE SPECIFICATION [04-11-2024(online)].pdf04/11/2024
202411084295-DECLARATION OF INVENTORSHIP (FORM 5) [04-11-2024(online)].pdf04/11/2024
202411084295-DRAWINGS [04-11-2024(online)].pdf04/11/2024
202411084295-FIGURE OF ABSTRACT [04-11-2024(online)].pdf04/11/2024
202411084295-FORM 1 [04-11-2024(online)].pdf04/11/2024
202411084295-FORM-9 [04-11-2024(online)].pdf04/11/2024
202411084295-POWER OF AUTHORITY [04-11-2024(online)].pdf04/11/2024
202411084295-PROOF OF RIGHT [04-11-2024(online)].pdf04/11/2024
202411084295-REQUEST FOR EARLY PUBLICATION(FORM-9) [04-11-2024(online)].pdf04/11/2024

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