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1. (WO2012118994) FAULT TOLERANT CONTROL SYSTEM FOR DISTRIBUTED MICRO-THRUSTERS
Latest bibliographic data on file with the International Bureau   

Pub. No.: WO/2012/118994 International Application No.: PCT/US2012/027324
Publication Date: 07.09.2012 International Filing Date: 01.03.2012
IPC:
F02K 3/08 (2006.01) ,F02K 7/00 (2006.01) ,F23R 3/42 (2006.01) ,F23R 3/60 (2006.01)
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
K
JET-PROPULSION PLANTS
3
Plants including a gas turbine driving a compressor or a ducted fan
08
with supplementary heating of the working fluid; Control thereof
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
K
JET-PROPULSION PLANTS
7
Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
23
COMBUSTION APPARATUS; COMBUSTION PROCESSES
R
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
3
Continuous combustion chambers using liquid or gaseous fuel
42
characterised by the arrangement or form of the flame tubes or combustion chambers
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
23
COMBUSTION APPARATUS; COMBUSTION PROCESSES
R
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
3
Continuous combustion chambers using liquid or gaseous fuel
42
characterised by the arrangement or form of the flame tubes or combustion chambers
60
Support structures; Attaching or mounting means
Applicants: SANCHEZ, Jason D.[US/US]; US (UsOnly)
GARBUZ, Piotr A.[UA/US]; US (UsOnly)
ZONENBERG, Andrew D.[US/US]; US (UsOnly)
GAME CHANGERS, LLC[US/US]; 41 East 31st Street New York, NY 10016, US (AllExceptUS)
Inventors: SANCHEZ, Jason D.; US
GARBUZ, Piotr A.; US
ZONENBERG, Andrew D.; US
Agent: WIELAND, Charles F., III; Buchanan Ingersoll & Rooney PC P.O. Box 1404 Alexandria, VA 22313-1404, US
Priority Data:
61/448,62102.03.2011US
Title (EN) FAULT TOLERANT CONTROL SYSTEM FOR DISTRIBUTED MICRO-THRUSTERS
(FR) SYSTÈME DE COMMANDE À TOLÉRANCE DE DÉFAILLANCES DESTINÉ À DES MICROPROPULSEURS RÉPARTIS
Abstract:
(EN) A control system for controlling the operation of a plurality of micro thrusters arranged in a plurality of parallel horizontal rows and a plurality of parallel vertical columns, the control system requires a power source, a first plurality of power lines connected to the power source and coupled to at least one micro thruster of the plurality of micro thrusters in a horizontal row of the plurality of parallel horizontal rows, a second plurality of power lines connected to the power source and coupled to at least one micro thruster of the plurality of micro thrusters in a vertical column of the plurality of parallel vertical columns, and a control unit coupled to the power source to control activation of the first plurality of power lines and activation of the second plurality of power lines.
(FR) Cette invention se rapporte à un système de commande destiné à commander le fonctionnement d'une pluralité de micropropulseurs agencés en une pluralité de rangées horizontales parallèles et en une pluralité de colonnes verticales parallèles, le système de commande nécessitant une source de puissance, une première pluralité de lignes de puissance connectées à la source de puissance et couplées à un micropropulseur au moins de la pluralité de micropropulseurs dans une rangée horizontale de la pluralité de rangées horizontales parallèles, une seconde pluralité de lignes de puissance connectées à la source de puissance et couplées à un micropropulseur au moins de la pluralité de micropropulseurs dans une colonne verticale de la pluralité de colonnes verticales parallèles et une unité de commande couplée à la source de puissance de façon à commander l'activation de la première pluralité de lignes de puissance et l'activation de la seconde pluralité de lignes de puissance.
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, 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, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, MD, 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, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)