公开(公告)号：US20150053193A1

公开(公告)日：2015-02-26

申请号：US13972201

申请日：2013-08-21

Applicant: Raytheon Company

Inventor： James A. Pruett ,  Purnachandra R. Gogineni ,  Zachary Williamson

IPC: F41B11/70

CPC classification number: F41B11/73 ,  F41B11/80 ,  F41F7/00

Abstract: A launcher includes a pusher that has parts that move relative to one another to provide desired forces or accelerations to corresponding parts of an object to be launched. Pressurized gasses are used to move the pusher to eject the object from the launcher. The parts of the pusher engage the different parts of the object to account for differences in shape and/or orientation of the parts of the objects, and to provide desired accelerations to the object parts. The pusher parts may include a piston or diaphragm that moves relative to an outer annular part of the pusher. The piston or diaphragm may press against a warhead explosive or other payload of a missile, with the outer part pressing against a fuselage or casing of the missile, in which the payload is mounted. Use of the pusher with multiple parts minimizes stresses between the object parts.

Abstract translation: 发射器包括推动器，其具有相对于彼此移动的部件，以向要发射的对象的相应部分提供期望的力或加速度。 加压气体用于移动推动器以从发射器弹出物体。 推动器的部件接合对象的不同部分以解决对象部件的形状和/或取向的差异，并且为对象部件提供期望的加速度。 推动器部件可以包括相对于推动器的外部环形部分移动的活塞或隔膜。 活塞或隔膜可以压靠导弹的弹头爆炸物或其他有效载荷，外部部件压靠导弹的机身或套管，有效载荷安装在该机身上。 使用具有多个部件的推动器可以最大限度地减少对象部件之间的应力。

公开(公告)号：US09587922B2

公开(公告)日：2017-03-07

申请号：US13861684

申请日：2013-04-12

Applicant: Raytheon Company

Inventor： Michael G. Kalifa ,  Zachary Williamson

IPC: F42B14/06 ,  F42B10/14 ,  F42B10/64

CPC classification number: F42B14/064 ,  F42B10/14 ,  F42B10/64

Abstract: A ballistic sabot for adapting a payload to a launch device is disclosed. The ballistic sabot can include a support structure configured to be releasably coupled to a payload and to operably interface with a launch device. The launch device can be operable to launch the payload and the support structure on a ballistic trajectory. The support structure can be configured to retain and travel with the payload along the ballistic trajectory substantially beyond the launch device prior to release and separation from the payload.

Abstract translation: 公开了一种用于将有效载荷适配到发射装置的弹道式装置。 弹道防盗器可以包括被配置为可释放地联接到有效载荷并且与发射装置可操作地连接的支撑结构。 发射装置可以用于在弹道轨迹上发射有效载荷和支撑结构。 支撑结构可以被配置为在释放和分离有效载荷之前沿着弹道轨迹保持和行进有效载荷基本上超出发射装置。

公开(公告)号：US20160102953A1

公开(公告)日：2016-04-14

申请号：US13861684

申请日：2013-04-12

Applicant: Raytheon Company

Inventor： Michael G. Kalifa ,  Zachary Williamson

IPC: F42B14/06

CPC classification number: F42B14/064 ,  F42B10/14 ,  F42B10/64

Abstract: A ballistic sabot for adapting a payload to a launch device is disclosed. The ballistic sabot can include a support structure configured to be releasably coupled to a payload and to operably interface with a launch device. The launch device can be operable to launch the payload and the support structure on a ballistic trajectory. The support structure can be configured to retain and travel with the payload along the ballistic trajectory substantially beyond the launch device prior to release and separation from the payload.

Abstract translation: 公开了一种用于将有效载荷适配到发射装置的弹道式装置。 弹道防盗器可以包括被配置为可释放地联接到有效载荷并且与发射装置可操作地连接的支撑结构。 发射装置可以用于在弹道轨迹上发射有效载荷和支撑结构。 支撑结构可以被配置为在释放和分离有效载荷之前沿着弹道轨迹保持和行进有效载荷基本上超出发射装置。

公开(公告)号：US09360270B2

公开(公告)日：2016-06-07

申请号：US13972201

申请日：2013-08-21

Applicant: Raytheon Company

Inventor： James A. Pruett ,  Purnachandra R. Gogineni ,  Zachary Williamson

IPC: F41F7/00 ,  F41B11/73 ,  F41B11/80

CPC classification number: F41B11/73 ,  F41B11/80 ,  F41F7/00

Abstract: A launcher includes a pusher that has parts that move relative to one another to provide desired forces or accelerations to corresponding parts of an object to be launched. Pressurized gasses are used to move the pusher to eject the object from the launcher. The parts of the pusher engage the different parts of the object to account for differences in shape and/or orientation of the parts of the objects, and to provide desired accelerations to the object parts. The pusher parts may include a piston or diaphragm that moves relative to an outer annular part of the pusher. The piston or diaphragm may press against a warhead explosive or other payload of a missile, with the outer part pressing against a fuselage or casing of the missile, in which the payload is mounted. Use of the pusher with multiple parts minimizes stresses between the object parts.

Abstract translation: 发射器包括推动器，其具有相对于彼此移动的部件，以向要发射的对象的相应部分提供期望的力或加速度。 加压气体用于移动推动器以从发射器弹出物体。 推动器的部件接合对象的不同部分以解决对象部件的形状和/或取向的差异，并且为对象部件提供期望的加速度。 推动器部件可以包括相对于推动器的外部环形部分移动的活塞或隔膜。 活塞或隔膜可以压靠导弹的弹头爆炸物或其他有效载荷，外部部件压靠导弹的机身或套管，有效载荷安装在该机身上。 使用具有多个部件的推动器可以最大限度地减少对象部件之间的应力。