KR KR20250032049A

VERTICAL TAKEOFF and Landing AIRCRAFT SURFACE TENSION compensation SYSTEM

Abstract

A non-transitory machine-readable medium storing instructions that, when executed by one or more processors, perform operations including: obtaining one or more surface tension measurements of a surface by using a computer system and one or more surface tension sensors; determining, by the computer system, a repulsive force to an aircraft using the one or more surface tension measurements and a weight of the aircraft; and causing, by the computer system, one or more engines included in the aircraft to generate a propulsive force based on the determined repulsive force.

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Bibliographic data via the European Patent Office's Open Patent Services (DOCDB) . Republished here for research and prior-art review. This page is not legal advice, and its presence in our index says nothing about the validity or enforceability of the document. For the Indian legal position (status, oppositions, renewals), see InPASS.