To provide systems and methods for enhancing takeoff performance by displaying symbology representing an initial pitch angle target that optimizes a payload that can be carried by an airplane.SOLUTION: An optimum initial pitch angle at rotation during takeoff is determined which is associated with an optimum ratio of the takeoff safety speed to the stall speed that satisfies a specific set of climb/obstacle constraints. Targeting this optimum initial pitch angle allows selection of the maximum takeoff gross weight that corresponds to the optimum takeoff safety speed/stall speed ratio.SELECTED DRAWING: None

    【課題】航空機によって運ぶことができるペイロードの量を最適化する初期ピッチ角ターゲットを表すシンボル体系を表示することによって離陸性能を向上させるためのシステム及び方法を提供する。【解決手段】特定の組の上昇/障害物制約を満たす離陸安全速度対失速速度の最適な比率に関連する離陸中の回転時の最適初期ピッチ角を決定する。この最適初期ピッチ角をターゲットにすることにより、最適離陸安全速度/失速速度比率に対応する最大離陸総重量が選択可能になる。【選択図】なし


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    Title :

    OPTIMIZING CLIMB PERFORMANCE DURING TAKEOFF USING VARIABLE INITIAL PITCH ANGLE TARGET


    Additional title:

    可変初期ピッチ角ターゲットを使用した離陸中の上昇性能の最適化


    Contributors:

    Publication date :

    2019-10-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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