PROBLEM TO BE SOLVED: To provide systems and methods to leverage aircraft performance and flight efficiency for noise abatement during a departure phase.SOLUTION: Systems and methods are described for dynamically generating flight departure profiles that are in compliance with aircraft emission limits. The emission limits may include noise abatement limits. The flight departure profiles may be generated on a flight by flight basis, and/or may be based on then-current conditions such as wind speed, wind direction, and ambient temperature.
【課題】出発段階中に騒音削減のために航空機性能及び飛行効率を活用するためのシステム及び方法を提供する。【解決手段】航空機排出量制限に準拠する飛行出発プロファイルを動的に生成するためのシステム及び方法が記載される。排出量制限は騒音削減制限を含んでもよい。飛行出発プロファイルは、飛行毎に生成されてもよく、及び/又は、風速、風向、及び、周囲温度などのその当時の状態に基づいていてもよい。【選択図】図1
AIRCRAFT DEPARTURE PROFILE GENERATION COMPLIANT WITH NOISE ABATEMENT LIMITS
騒音削減制限に準拠した航空機出発プロファイル生成
2016-01-12
Patent
Elektronische Ressource
Japanisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS |
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