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. (WO2011141527) GUIDED MUNITION PROTECTED BY AN AERODYNAMIC CAP
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2011/141527    International Application No.:    PCT/EP2011/057648
Publication Date: 17.11.2011 International Filing Date: 11.05.2011
IPC:
F42B 10/46 (2006.01)
Applicants: TDA ARMEMENTS S.A.S [FR/FR]; Route d'Ardon F-45240 La Ferté-Saint-Aubin (FR) (For All Designated States Except US).
COHE, Patrick [FR/FR]; (FR) (For US Only).
MOREAU, Fabien [FR/FR]; (FR) (For US Only)
Inventors: COHE, Patrick; (FR).
MOREAU, Fabien; (FR)
Agent: LUCAS, Laurent; MARKS & CLERK France Immeuble Visium 22, avenue Aristide Briand F-94117 Arcueil Cedex (FR)
Priority Data:
10/02024 12.05.2010 FR
Title (EN) GUIDED MUNITION PROTECTED BY AN AERODYNAMIC CAP
(FR) MUNITION GUIDEE PROTEGEE PAR UNE COIFFE AERODYNAMIQUE
Abstract: front page image
(EN)The invention relates to guided munitions intended to destroy a target after at least a flight phase followed by a target approach phase. The munition comprises a munition body (10) of cylindrical shape with longitudinal axis ZZ' having, at a front end Eav of the munition which is the end intended to be directed towards the target, a front body (14) comprising an optic (26) of a device that guides said munition onto the target, a cap (20) for protecting the optic, secured to the munition body (10), characterized in that the protective cap (20) comprises at least one recess (60, 120) containing a pyrotechnic device (130, 132, 183, 184) intended to destroy said protective cap (20) to free the optic and make the munition guidance device operational during the target approach phase. Application: steered or guided munitions such as those of the rocket or projectile type, or missiles.
(FR)L'invention concerne les munitions pilotées destinée à détruire une cible après au moins une phase de vol suive d'une phase d'approche de la cible. La munition comporte un corps de munition (10) de forme cylindrique d'axe longitudinal ZZ' ayant, du côté d'une extrémité avant Eav de la munition destinée à être dirigée vers la cible, un corps avant (14) comportant une optique (26) d'un dispositif de guidage de ladite munition vers la cible, une coiffe (20) de protection de l'optique, solidaire du corps de munition (10) caractérisée en ce que la coiffe (20) de protection comporte au moins un évidement (60, 120) ayant un artifice pyrotechnique (130, 132, 183, 184) destiné à détruire ladite coiffe (20) de protection pour libérer l'optique et rendre opérationnel le dispositif de guidage de la munition lors de la phase d'approche de la cible. Application : munitions pilotées ou guidées telles que celles de type roquette ou projectile ou les missiles.
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, LR, 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 (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: French (FR)
Filing Language: French (FR)