IP-Coster | WO2024116085 | CREEP RESISTANT MISSILE CANISTER COVER SYSTEM

Country	Stages	Total
China	Filing, Examination, Granting	1878
EPO	Filing, Examination, Granting	8143
Japan	Filing, Examination, Granting	1899
South Korea	Filing, Examination, Granting	1491
USA	Filing, Examination, Granting	4740

Abstract[English] This invention relates to a cover system for missile canisters that, in addition to functioning as a missile launch system, enables the transportation and storage of the missile in a protected manner from the external environment. This cover system consists of two cover parts: the frangible cover part (3) and the deployable cover part (2), which are mounted on the end of the canister (1). The frangible cover part (3) is easily broken by the sudden pressure increase that occurs in the canister (1) as a result of the missile firing, and thus ensures that the missile moves out of the canister (1) without any damage. The deployable cover part (2) has support interfaces (11) that increase the resistance of the frangible cover part (3), which is subjected to creep under the influence of pressure load under storage conditions in the canister (1), against the creep effect and plastic deformation. There is a cover locking mechanism on the deployable cover part (2) that ensures that the cover (2) is kept in the closed position to ensure the sealing of the canister under storage conditions. The deployable cover part (2) also has a drive mechanism that enables the cover (2) to be opened during the launch of the missile and a cover positioning mechanism that ensures that the cover (2) is kept in the open position.[French] La présente invention concerne un système de couvercle pour des cartouches de missile qui, en plus de fonctionner en tant que système de lancement de missile, permet le transport et le stockage du missile d'une manière protégée de l'environnement externe. Ce système de couvercle est constitué de deux parties couvercles : la partie couvercle frangible (3) et la partie couvercle déployable (2), qui sont montées sur l'extrémité de la cartouche (1). La partie couvercle frangible (3) est facilement rompue par l'augmentation de pression soudaine qui se produit dans la cartouche (1) à la suite de la mise à feu du missile et garantit ainsi que le missile se déplace hors de la cartouche (1) sans aucun dommage. La partie couvercle déployable (2) présente des interfaces de support (11) qui augmentent la résistance de la partie couvercle frangible (3), qui est soumise à un fluage sous l'influence d'une charge de pression dans des conditions de stockage dans la cartouche (1), à l'effet de fluage et à la déformation plastique. Il existe un mécanisme de verrouillage de couvercle sur la partie couvercle déployable (2) qui garantit que le couvercle (2) est maintenu dans la position fermée pour assurer l'étanchéité de la cartouche dans des conditions de stockage. La partie couvercle déployable (2) comporte également un mécanisme d'entraînement qui permet au couvercle (2) d'être ouvert pendant le lancement du missile et un mécanisme de positionnement de couvercle qui garantit que le couvercle (2) est maintenu dans la position ouverte.

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Recordal of a Change of the Applicant's Name/Address	Change of Applicant's Name and Address *
Type of Assignment	The Standard Agent's Assignment *
Applicant's Legal Status	Legal Entity *
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Entry into National Phase under	Chapter II *
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Patent Delivery	Send the Letters Patent by Courier *
Translation

WO2024116085 - CREEP RESISTANT MISSILE CANISTER COVER SYSTEM

Quotation for National Phase entry

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