CNIPA.AI
검색으로 돌아가기
기록

DETERMINING THE COMPATIBILITY OF AIRSIDE INFRASTRUCTURE FOR AN AIRCRAFT

발명심사 중
2조회수
21청구항 · 3 독립항
§ Ⅰ

개요

발명자

Girish Naik; Evanicio C. Costa

IPC 분류

G8G 5/

CPC 분류

G8G5/21G8G5/50G8G5/55

Assessing compatibility of airport infrastructure with an aircraft model design is provided. The method comprises retrieving information about features of an airport from an airport infrastructure database and calculating, through triangulation, distances between the features of the airport. A rationale for regulatory design requirements for the features of the airport is determined. An assessment is generated based on the distances between the features, dimensions of the aircraft model, and the rationale for the regulatory requirements. The assessment identifies areas of the airport that can accommodate the aircraft model and any areas of the airport that cannot. A map of the airport is dynamically displayed in a user interface with visual indications of the areas of the airport that can accommodate the aircraft model and the areas of the airport that cannot accommodate the aircraft model to guide movement of an aircraft of the aircraft model.

원문 (중국어)

Assessing compatibility of airport infrastructure with an aircraft model design is provided. The method comprises retrieving information about features of an airport from an airport infrastructure database and calculating, through triangulation, distances between the features of the airport. A rationale for regulatory design requirements for the features of the airport is determined. An assessment is generated based on the distances between the features, dimensions of the aircraft model, and the rationale for the regulatory requirements. The assessment identifies areas of the airport that can accommodate the aircraft model and any areas of the airport that cannot. A map of the airport is dynamically displayed in a user interface with visual indications of the areas of the airport that can accommodate the aircraft model and the areas of the airport that cannot accommodate the aircraft model to guide movement of an aircraft of the aircraft model.