PROBLEM TO BE SOLVED: To provide an aircraft stall protection system that calculates two different maximum angles of attack and limits an aircraft angle of attack to the at least two different maximum angles of attack at different times.SOLUTION: An aircraft stall protection system and method include calculating a first angle of attack and a second angle of attack based on aircraft configuration and environmental conditions. The first angle of attack is greater than the second angle of attack. The system and method limit an actual aircraft angle of attack to the first angle of attack for a predetermined period of time and thereafter the system and method limit the actual aircraft angle of attack to the second angle of attack. The system and method allow an operator or pilot of an aircraft to extract maximum performance from the aircraft relating to a specific set of flight conditions, without the risk of stalling or the risk of remaining in a high drag state for a long period of time. This system and method are suitable for use together with a stall warning system.SELECTED DRAWING: Figure 1

    【課題】2つの異なる最大迎角を計算し、異なる時点で航空機迎角を少なくとも2つの異なる最大迎角に制限する航空機失速保護システムを提供する。【解決手段】航空機失速保護システム及び方法は、航空機構成及び環境条件に基づいて第1の迎角及び第2の迎角を計算することを含む。なお、第1の迎角は、第2の迎角を上回る。システム及び方法は、所定の期間にわたって実際の航空機迎角を第1の迎角に制限し、その後、システム及び方法は、実際の航空機迎角を第2の迎角に制限する。システム及び方法は、航空機のオペレータ又はパイロットが、失速のリスク又は長期間にわたって高抗力状態にあり続けるリスクなしに特定の組の飛行条件に関して航空機から最大性能を引き出すことを可能にする。このシステム及び方法は、失速警報システムと共に使用するのに適している。【選択図】図1


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    Title :

    AIRCRAFT STALL PROTECTION SYSTEM


    Additional title:

    航空機失速保護システム


    Contributors:

    Publication date :

    2017-03-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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