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1. (WO2019002925) SYSTEM AND METHOD FOR CONTROLLING A TAKEOFF THRUST
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Pub. No.: WO/2019/002925 International Application No.: PCT/IB2017/053985
Publication Date: 03.01.2019 International Filing Date: 30.06.2017
IPC:
B64D 31/06 (2006.01) ,F02C 9/28 (2006.01) ,G05D 1/00 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
31
Power plant control; Arrangement thereof
02
Initiating means
06
actuated automatically
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
C
GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
9
Controlling gas-turbine plants; Controlling fuel supply in air-breathing jet-propulsion plants
26
Control of fuel supply
28
Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
G PHYSICS
05
CONTROLLING; REGULATING
D
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1
Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
Applicants:
C SERIES AIRCRAFT MANAGING GP INC. [CA/CA]; 13100 Henri-Fabre Boulevard Mirabel, Quebec J7N 3C6, CA
Inventors:
HAMEL, Remi; CA
BOUDREAULT, Joel; CA
DEL CASTILLO, Derik; CA
PEROUT, Eva; CA
MEUNIER, Francis; CA
SPINELLI, Tony; CA
TAMESTIT, Nicolas; CA
LEBEGUE, Olivier; CA
NOUHAUD, Christophe; CA
Agent:
NORTON ROSE FULBRIGHT CANADA LLP/S.E.N.C.R.L., S.R.L.; Suite 2500 1 Place Ville-Marie Montréal, Québec H3B 1R1, CA
Priority Data:
Title (EN) SYSTEM AND METHOD FOR CONTROLLING A TAKEOFF THRUST
(FR) SYSTÈME ET PROCÉDÉ DE COMMANDE D'UNE POUSSÉE AU DÉCOLLAGE
Abstract:
(EN) The present disclosure provides systems and methods for controlling thrust produced at takeoff by at least one engine (114, 116) of an aircraft (100). At least one input signal comprising input data indicative of a speed of the aircraft is received (202). The speed of the aircraft is compared to a first predetermined threshold. Responsive to determining that the speed is below the first threshold, a thrust limit for the at least one engine is determined (204) from the input data and output to the at least one engine a thrust limitation signal for causing the thrust to be limited according to the thrust limit (210).
(FR) La présente invention concerne des systèmes et des procédés de commande de poussée produite au décollage par au moins un moteur (114, 116) d'un aéronef (100). Au moins un signal d'entrée comprenant des données d'entrée indicatives d'une vitesse de l'aéronef est reçu (202). La vitesse de l'aéronef est comparée à un premier seuil prédéterminé. En réponse à la détermination que la vitesse est inférieure au premier seuil, une limite de poussée pour l'au moins un moteur est déterminée (204) à partir des données d'entrée et un signal de limitation de poussée est délivré à l'au moins un moteur pour amener la poussée à être limitée en fonction de la limite de poussée (210).
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Designated States: 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
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (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)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)