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    • 1. 发明申请
    • Anti-missile defense suite
    • 反导弹防御套件
    • US20060249009A1
    • 2006-11-09
    • US10560767
    • 2004-06-10
    • Eugene Rubin
    • Eugene Rubin
    • B64D1/04F41F5/00
    • B64D7/00F41H11/02F41J2/02F41J9/10
    • A system and method for an aircraft (10) that provides an IR decoy (12) for an incoming missile (18) to track instead of an engine (14) of the aircraft (10) is disclosed. The IR decoy (12) is deployed during or just after take off, and prior to landing to provide a signature (16) for any incoming missile (18). The IR decoy (12) provides a heat source (16) that has a higher radiant intensity than the hottest heat source on the aircraft (10), which is typically the engine (14), thereby providing a more attractive heat source for the missile (18). In another embodiment, a warning system (20) for an aircraft (10) detects an incoming missile (18), and deploys IR decoy (12) and creates an engine mask (22) by injecting an additive into the exhaust stream of the engine (14), thereby obscuring the radiation emanating from the engine (14).
    • 公开了一种用于飞行器(10)的系统和方法,其为进入的导弹(18)提供用于跟踪而不是飞行器(10)的发动机(14)的IR诱饵(12)。 IR诱饵(12)在起飞期间或之后部署,并在着陆前为任何进入的导弹(18)提供签名(16)。 IR诱饵(12)提供了具有比飞行器(10)上最热的热源(其通常是发动机(14))更高的辐射强度的热源(16),从而为导弹提供更有吸引力的热源 (18)。 在另一个实施例中,用于飞行器(10)的警告系统(20)检测进入的导弹(18),并且部署IR诱饵(12)并且通过将添加剂注入发动机的排气流中来产生发动机罩(22) (14),从而遮蔽从发动机(14)发出的辐射。