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AIRCRAFT LANDING GEAR SYSTEM
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Abstract
Information
Inventors
Applicants
Specification
Documents
ORDINARY APPLICATION
Published
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 ID | 202411084295 |
Invention Field | MECHANICAL ENGINEERING |
Date of Application | 04/11/2024 |
Publication Number | 46/2024 |
Inventors
Name | Address | Country | Nationality |
---|---|---|---|
KAJOL SABAT | LOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
HARSH RAJ | LOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
HARI NARAYANAN | LOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
ANGSHUMAN BARUAH SHUBHAM AGARWAL | LOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
Dr. RAJEEV KUMAR | LOVELY PROFESSIONAL UNIVERSITY, JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
Applicants
Name | Address | Country | Nationality |
---|---|---|---|
LOVELY PROFESSIONAL UNIVERSITY | JALANDHAR-DELHI, G.T. ROAD, PHAGWARA, PUNJAB (INDIA) -144411 | India | India |
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
Name | Date |
---|---|
202411084295-COMPLETE SPECIFICATION [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-DECLARATION OF INVENTORSHIP (FORM 5) [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-DRAWINGS [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-FIGURE OF ABSTRACT [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-FORM 1 [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-FORM-9 [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-POWER OF AUTHORITY [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-PROOF OF RIGHT [04-11-2024(online)].pdf | 04/11/2024 |
202411084295-REQUEST FOR EARLY PUBLICATION(FORM-9) [04-11-2024(online)].pdf | 04/11/2024 |
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