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1. (WO2019043645) METHOD AND SYSTEM FOR DETERMINING AN ESTIMATION OF AN ANEMOMETRIC PARAMETER IN AN AIRCRAFT
국제사무국에 기록된 최신 서지정보정보 제출

공개번호: WO/2019/043645 국제출원번호: PCT/IB2018/056680
공개일: 07.03.2019 국제출원일: 31.08.2018
IPC:
G01P 5/00 (2006.01) ,B64C 13/00 (2006.01) ,B64D 43/00 (2006.01) ,G01C 9/00 (2006.01)
G SECTION G — 물리학
01
측정; 시험
P
직선속도, 각속도, 가속도, 감속도 또는 충격의 측정; 운동의 유무; 운동의 방향 지시
5
유체, 예· 공기류의 속도측정 유체에 관련된 물체, 예. 선박의 항공기의 상대속도의 측정
B SECTION B — 처리조작; 운수
64
항공기; 비행; 우주공학
C
비행기; 헬리콥터
13
비행 조종 익면, 양력증가 플랩, 공기 제동 장치 또는 스포일러(Spoiler)를 작동하기 위한 조종계통 또는 전달계통
B SECTION B — 처리조작; 운수
64
항공기; 비행; 우주공학
D
항공기의 장비; 비행복; 패러슈트(parachute 낙하산); 동력 장치 또는 추진 전달 기구의 설비 또는 장치
43
계기의 장비
G SECTION G — 물리학
01
측정; 시험
C
자이로스코프; 진동질량을 가지는 회전-감응 장치 ; 운동질량이 없는 회전-감응 장치; 자이로스코프 효과를 이용한 각속도의 측정
9
경사의 측정, 예. 경사계(clinometers) 또는 수준기에 의한 것
출원인:
THALES CANADA INC. [CA/CA]; 105 Moatfield Drive Toronto, Ontario M3B 0A4, CA
발명자:
CASTANG, Fabien; CA
LOUIS, Xavier; CA
대리인:
FASKEN MARTINEAU DUMOULIN LLP; 800 Place Victoria, Suite 3700 P.O. Box 242, Stock Exchange Tower Montréal, Québec H4Z 1E9, CA
우선권 정보:
62/553,38101.09.2017US
발명의 명칭: (EN) METHOD AND SYSTEM FOR DETERMINING AN ESTIMATION OF AN ANEMOMETRIC PARAMETER IN AN AIRCRAFT
(FR) PROCÉDÉ ET SYSTÈME DE DÉTERMINATION D'UNE ESTIMATION D'UN PARAMÈTRE ANÉMOMÉTRIQUE DANS UN AÉRONEF
요약서:
(EN) A method and a system are disclosed for determining an estimation of an anemometric parameter of an aircraft, the anemometric parameter selected from a group comprising at least one of an angle of attack, a sideslip angle and a calibrated airspeed, the method comprising obtaining an indication of a state of at least one secondary surface of the aircraft; obtaining an indication of a position of a horizontal primary surface; obtaining an estimation of the load applied on a corresponding actuator used for actuating the horizontal primary surface of the aircraft using at least the indication of the position of the horizontal primary surface and the position of the corresponding actuator; accessing at least one lookup table with the indication of the state of the at least one secondary surface of the aircraft, the estimation of the load applied on the corresponding actuator used for actuating the horizontal primary surface of the aircraft, and the position of the corresponding actuator; obtaining a corresponding estimation of the anemometric parameter of the aircraft associated with the horizontal primary surface; providing the corresponding estimation of the anemometric parameter of the aircraft associated with the horizontal primary surface and wherein the at least one lookup table is generated during a learning phase.
(FR) L'invention concerne un procédé et un système de détermination d'une estimation d'un paramètre anémométrique d'un aéronef, le paramètre anémométrique étant choisi parmi un angle d'attaque, un angle de dérapage et/ou une vitesse aérodynamique étalonnée, le procédé comprenant l'obtention d'une indication d'un état d'au moins une surface secondaire de l'aéronef; l'obtention d'une indication d'une position d'une surface primaire horizontale; l'obtention d'une estimation de la charge appliquée sur un actionneur correspondant utilisé pour actionner la surface primaire horizontale de l'aéronef au moins à l'aide de l'indication de la position de la surface primaire horizontale et de la position de l'actionneur correspondant; l'accès à au moins une table de consultation comprenant l'indication de l'état de ladite surface secondaire de l'aéronef, l'estimation de la charge appliquée sur l'actionneur correspondant utilisé pour actionner la surface primaire horizontale de l'aéronef et la position de l'actionneur correspondant; l'obtention d'une estimation correspondante du paramètre anémométrique de l'aéronef associé à la surface primaire horizontale; la fourniture de l'estimation correspondante du paramètre anémométrique de l'aéronef associé à la surface primaire horizontale, ladite table de consultation étant générée pendant une phase d'apprentissage.
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지정국: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
아프리카지역 지식재산권기구(ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
유라시아 특허청(EAPO) (AM, AZ, BY, KG, KZ, RU, TJ, TM)
유럽 특허청(EPO) (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
아프리카 지식재산권기구(OAPI) (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
공개언어: 영어 (EN)
출원언어: 영어 (EN)