Method and device for optimizing a takeoff procedure of an aircraft
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
G06F-019/00
G01C-023/00
출원번호
US-0872264
(2010-08-31)
등록번호
US-8527119
(2013-09-03)
우선권정보
FR-09 04202 (2009-09-04)
발명자
/ 주소
Chaptal, Jérôme
Torres Calderon, Rosa Maria
출원인 / 주소
Airbus Operations (SAS)
대리인 / 주소
Novak Druce Connolly Bove + Quigg LLP
인용정보
피인용 횟수 :
2인용 특허 :
15
초록
An optimization method and device for a take-off procedure of an aircraft. The device (1) comprising means (2, 10) for determining optimum values for take-off parameters and adapting them for the actual take-off conditions.
대표청구항▼
1. A method for optimizing a take-off procedure of an aircraft, wherein the take-off procedure comprises a plurality of take-off parameters, the method comprising: receiving, via a processor on-board the aircraft, a plurality of reference take-off conditions, wherein each of the plurality of referen
1. A method for optimizing a take-off procedure of an aircraft, wherein the take-off procedure comprises a plurality of take-off parameters, the method comprising: receiving, via a processor on-board the aircraft, a plurality of reference take-off conditions, wherein each of the plurality of reference take-off conditions are input by an operator of the aircraft;determining, via a processor on-board the aircraft, a plurality of sets, wherein each of the plurality of sets comprises at least one of the plurality of reference take-off conditions and a plurality of take-off criteria for the aircraft;receiving, via a processor on-board the aircraft, a cost for each take-off criteria in each of the plurality of sets;creating, via a processor on-board the aircraft, a selected set from the plurality of sets, wherein the selected set minimizes a total cost associated with the selected set, wherein the total cost is a sum of the cost for each take-off criteria in each of the plurality of sets;receiving, via a processor on-board the aircraft, a plurality of actual take-off conditions, wherein each of the plurality of reference take-off conditions are input by the operator of the aircraft immediately prior to a take-off procedure, such that the plurality of actual take-off conditions represent current take-off conditions and may be the same as or different from the plurality of reference take-off conditions;converting, via a processor on-board the aircraft, the selected set into an optimum set comprising a plurality of optimized take-off parameters, wherein each optimized take off parameter is given by the expression: X=Xref+dXref/dp(p−pref)wherein Xref represents a member of the selected set,wherein pref represents a reference take-off condition,wherein p represents an actual take-off condition;defining a take-off procedure based on the optimum set; andimplementing the take-off procedure upon take-off. 2. The method according to claim 1, wherein each of the plurality of optimized take-off parameters are selected from the group consisting of a take-off speed, a thrust reducing altitude, an intermediate thrust speed, an acceleration altitude, an intermediate speed, and an altitude indicating an end of a take-off procedure. 3. The method according to claim 1, wherein each of the plurality of reference take-off conditions are selected from the group consisting of an airport characteristic, a pilot-selected aircraft characteristic, a condition imposed by air control authorities. 4. The method according to claim 1, wherein each of the plurality of take-off criteria are selected from the group consisting of a pollutant emission under a predetermined altitude, noise at a predetermined distance of a runway used for take-off, an average noise around an airport, an acoustic footprint at ground level, a use duration of a take-off speed, an ascent duration up to an ascent end, and a quantity of fuel consumed.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (15)
Gonser John M. (Albuquerque NM) Kominek Richard J. (Albuquerque NM), Apparatus and method for controlling an optimizing aircraft performance calculator to achieve time-constrained navigatio.
Lebrun Jean-Louis (Antony FRX) Pont Patrick (Paris FRX), Method and device for guiding an aerodyne on a runway, particularly during the taxiing phase preceding take off.
Lemoult, Frederic; Demortier, Jean-Pierre; Pitard, Fabien; Betouret, Damien; Marani, Frederic; Lacaze, Isabelle; De Menorval, Jean-Louis; Marchand, Gael; Ott, Adrien; Wachenheim, Maxime, Method for detecting an error in input of one of the takeoff parameters into a flight management system.
Michal, Benedicte; Pitard, Fabien; Demortier, Jean-Pierre; Charbonnier, Christine; Lacaze, Isabelle; Marchand, Gael; Le Duigou, Christine; Cayrou, Jerome; Blondin, Vincent; Lemoult, Frederic, Process for verifying the coherence between aircraft take-off parameters and an available runway length.
Duggan, David S.; Felio, David A.; Pate, Billy B.; Longhi, Vince R.; Petersen, Jerry L.; Bergee, Mark J., Unmanned aerial vehicle take-off and landing systems.
Johnson, Steve; Ishihara, Yasuo; Conner, Kevin J, Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing.
Gurusamy, Saravanakumar; Karmakar, Nirupam; Malviya, Pramod Kumar; Krishnamurthy, Prithvi, System and method of displaying airspeed information for an aircraft.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.