{"schema_version":"1.0","canonical_url":"https://patentable.app/patents/US-9836575","patent":{"patent_number":"US-9836575","title":"Method of design and manufacturing of aircraft structural object","assignee":null,"inventors":[],"filing_date":"2016-02-26T00:00:00.000Z","publication_date":"2017-12-05T00:00:00.000Z","cpc_codes":["G06F","G06F","G06F","G06F"],"num_claims":5,"abstract":"According to one implementation, a method of making design information of an aircraft structural object, executed by a computer, includes: setting at least one parameter as a variable for an optimization calculation which minimizes a weight of the structural object composing an aircraft; setting at least one allowable range for at least a strength of the structural object corresponding to the at least one parameter; and calculating an optimal value of the weight of the structural object and a value of the at least one parameter by the optimization calculation. The at least one parameter expresses the design information of the structural object. The at least one allowable range is set as at least one constraint condition of the optimization calculation. The value of the at least one parameter corresponds to the optimal value and meets the at least one allowable range."},"analysis":{"summary":null,"layman_explanation":null,"technical_analysis":null,"business_analysis":null,"faqs":null,"topics":[],"tech_cluster":null},"seo":{"title":"Method of design and manufacturing of aircraft structural object","description":"According to one implementation, a method of making design information of an aircraft structural object, executed by a computer, includes: setting at least one parameter as a variable for an optimizat","keywords":[]},"attribution":{"source":"Patentable","source_url":"https://patentable.app","canonical_url":"https://patentable.app/patents/US-9836575","license":"CC-BY-4.0-like","license_terms":"AI-generated analysis on this page (summary, layman_explanation, technical_analysis, business_analysis, faqs) may be reused with attribution and a visible link back to the canonical URL above. Patent abstracts, claims, and bibliographic data are USPTO public domain.","required_link":"https://patentable.app/patents/US-9836575","citation_suggestion":"Patentable. \"Method of design and manufacturing of aircraft structural object\" (US-9836575). https://patentable.app/patents/US-9836575","copyright_holder":"Nomic Interactive Technology LLC"},"links":{"html":"https://patentable.app/patents/US-9836575","json":"https://patentable.app/api/llm-context/US-9836575","site":"https://patentable.app","llms_txt":"https://patentable.app/llms.txt"},"generated_at":"2026-06-06T08:36:26.627Z"}