|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/00 G01C-023/00 B64D-043/00|
|미국특허분류(USC)||701/003; 701/033.9; 244/017.11; 340/946; 340/973|
|우선권정보||FR-11 00936 (2011-03-30)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 11|
A method of assisting the piloting of an aircraft (1) comprising a first rotor (5) having a plurality of first blades (6) with a first variable collective pitch, and a second rotor (7) having a plurality of second blades (8) with a second variable collective pitch. According to the method, a computer determines a power limit curve (70) and displays said limit curve (70) in a diagram (60) to inform the pilot of the first and second collective pitch margins available before reaching the limits of at least one operating rating of the power plant of the airc...
1. A method of assisting the piloting of an aircraft comprising a first rotor having a plurality of first blades with a first variable collective pitch, and a second rotor having a plurality of second blades with a second variable collective pitch, said aircraft having a power plant provided with at least one engine operating in a plurality of ratings, said power plant being monitored by a computer via a plurality of predetermined monitoring parameters, wherein said computer: determines the current first and second collective pitches at each instant, and...