{"schema_version":"1.0","canonical_url":"https://patentable.app/patents/US-11479349","patent":{"patent_number":"US-11479349","title":"Tail rotor balancing systems for use on rotorcraft","assignee":null,"inventors":[],"filing_date":"2020-12-01T00:00:00.000Z","publication_date":"2022-10-25T00:00:00.000Z","cpc_codes":["G05D"],"num_claims":14,"abstract":"An electrically distributed yaw control system for a helicopter having a tailboom includes a plurality of tail rotors rotatably coupled to the tailboom and a flight control computer implementing a tail rotor balancing module. The tail rotor balancing module includes a tail rotor balancing monitoring module configured to monitor one or more parameters of the helicopter and identify a first set of one or more tail rotors in the plurality of tail rotors based on the one or more parameters. The tail rotor balancing module also includes a tail rotor balancing command module configured to modify one or more operating parameters of the first set of tail rotors."},"analysis":{"summary":null,"layman_explanation":null,"technical_analysis":null,"business_analysis":null,"faqs":null,"topics":[],"tech_cluster":null},"seo":{"title":"Tail rotor balancing systems for use on rotorcraft","description":"An electrically distributed yaw control system for a helicopter having a tailboom includes a plurality of tail rotors rotatably coupled to the tailboom and a flight control computer implementing a tai","keywords":[]},"attribution":{"source":"Patentable","source_url":"https://patentable.app","canonical_url":"https://patentable.app/patents/US-11479349","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-11479349","citation_suggestion":"Patentable. \"Tail rotor balancing systems for use on rotorcraft\" (US-11479349). https://patentable.app/patents/US-11479349","copyright_holder":"Nomic Interactive Technology LLC"},"links":{"html":"https://patentable.app/patents/US-11479349","json":"https://patentable.app/api/llm-context/US-11479349","site":"https://patentable.app","llms_txt":"https://patentable.app/llms.txt"},"generated_at":"2026-05-31T21:24:26.340Z"}