WIPO logo
Mobile | Deutsch | Español | Français | 日本語 | 한국어 | Português | Русский | 中文 | العربية |
PATENTSCOPE

Search International and National Patent Collections
World Intellectual Property Organization
Search
 
Browse
 
Translate
 
Options
 
News
 
Login
 
Help
 
Machine translation
1. (WO2011014271) METHODS AND APPARATUS FOR A TANDEM DIVERT AND ATTITUDE CONTROL SYSTEM
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2011/014271    International Application No.:    PCT/US2010/028162
Publication Date: 03.02.2011 International Filing Date: 22.03.2010
IPC:
F42B 10/66 (2006.01)
Applicants: RAYTHEON COMPANY [US/US]; 870 Winter Street Waltham, Massachusetts 02451-1449 (US) (For All Designated States Except US).
PAGLIARA, Philip, W. [US/US]; (US) (For US Only).
LEAL, Michael, A. [US/US]; (US) (For US Only).
JENIA, Justin, C. [US/US]; (US) (For US Only).
DALBELLO, Teryn [US/US]; (US) (For US Only).
HITNER, John, M. [US/US]; (US) (For US Only)
Inventors: PAGLIARA, Philip, W.; (US).
LEAL, Michael, A.; (US).
JENIA, Justin, C.; (US).
DALBELLO, Teryn; (US).
HITNER, John, M.; (US)
Agent: GIFFORD, Eric A.; Law Offices of Eric A. Gifford 11770 E. Calle del Valle Tucson, Arizona 85749 (US)
Priority Data:
61/229,899 30.07.2009 US
12/696,395 29.01.2010 US
Title (EN) METHODS AND APPARATUS FOR A TANDEM DIVERT AND ATTITUDE CONTROL SYSTEM
(FR) PROCÉDÉS ET APPAREIL POUR UN SYSTÈME EN TANDEM DE DÉROUTAGE ET DE CONTRÔLE D'ATTITUDE
Abstract: front page image
(EN)An aeronautical vehicle (100) includes at least one set of tandem divert thrusters (111, 122) incorporated into the body. Each set of tandem divert thrusters includes a first divert thruster (111) and a second divert thruster (122), each configured to provide substantially equal thrust forces at substantially the same time and in substantially opposite directions such that the moment reference point (205) lies between the first and second divert thrusters.
(FR)L'invention concerne un véhicule aéronautique (100) comprenant au moins un ensemble de propulseurs de déroutage en tandem (111, 122) incorporés dans le corps. Chaque ensemble de propulseurs de déroutage en tandem comprend un premier propulseur de déroutage (111) et un second propulseur de déroutage (122), chacun configuré pour fournir des forces de propulsion sensiblement égales sensiblement au même moment et dans des directions sensiblement opposées, de telle manière que le point de référence du moment (205) se trouve entre le premier et le second propulseur de déroutage.
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, RO, RS, RU, 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 (BW, GH, GM, KE, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (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, 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)