|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||416/001 ; 416/027 ; 416/028 ; 416/029 ; 416/030 ; 416/036 ; 416/037 ; 416/039 ; 416/040 ; 416/047 ; 416/048 ; 600/602 ; 701/007 ; 701/010 ; 701/099|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 22 인용 특허 : 6|
Method and apparatus for controlling an aircraft engine with a single, manually-operable lever includes structure and function for generating a pilot thrust command from the single lever. A processor is coupled to the single lever and (i) receives the generated pilot thrust command, (ii) receives a plurality of detected ambient air flight conditions, (iii) receives a plurality of detected engine performance parameters, (iv) determines first and second engine control commands based on the received pilot thrust command, the detected ambient air flight cond...
[ What is claimed is:] [18.] A method of controlling an aircraft engine with a single lever power controller, comprising the steps of:generating an engine thrust command with the single lever;detecting ambient air flight conditions;concurrently determining an engine rotation command and an engine load command based on the generated thrust command, the detected ambient air flight conditions, and a predetermined maximum thrust efficiency value for the detected ambient air flight conditions and thrust command; andconcurrently outputting first and second con...