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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/188 ; 244/186 ; 364/430|
|우선권정보||FR-0342181 (1976-11-12); FR-0030703 (1977-10-12)|
|발명자 / 주소||
|출원인 / 주소||
|인용정보||피인용 횟수 : 10 인용 특허 : 2|
A method for controlling the decelerated approach of an aerodyne on radio-alignment generally referred to as “glide,”in particular for the purpose of reducing its fuel consumption and reducing the noise, mainly in the final stage of the approach, by approaching the glide at high speed, initiating the descent according to the glide angle, also at high speed then beginning a decelerated phase in order to reach a predetermined speed V sel+k, k being generally equal to 10 knots, on reaching a predetermined altitude, hF, and then passing progessively from the...
A method of controlling the decelerated approach of an aircraft on glide radioalignment, said aircraft having equipment comprising at least one landing gear which can take the positions gear retracted and gear down, at least one control surface such as a flap which can take at least three positions, flap in final position for landing, flap at one notch from the final position for landing, and flap at two notches from the final position for landing, and a throttle having a slow position, comprising the following steps: (a) approaching the capture of glide...