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1. 发明公开

EP3004785A2 MINIGUN WITH IMPROVED BARREL CLAMP 有权
标题翻译： MINIPISTOLE MIT VERBESSERTER LAUFKLEMME
公开(公告)号：EP3004785A2
公开(公告)日：2016-04-13
申请号：EP14832235.7
申请日：2014-06-03
申请人： Profense, LLC
发明人： ROWE, Thomas , O'DONNELL, Arthur
IPC分类号： F41F1/10
CPC分类号： F41A21/487 , F41A13/10 , F41A21/08 , F41A21/34 , F41F1/10
摘要： An improved barrel clamp assembly for a multi-barreled minigun includes a barrel clamp tube having a front end, a rear end, and a plurality of longitudinal openings extending between the front end and the rear end. An impeller is mounted in the barrel clamp tube between the tube front end and the tube rear end. The impeller includes a plurality of impeller blades that are spaced around a periphery of the impeller and that project forward from a rear flange portion of the impeller and the impeller blades define a plurality of air channels. A barrel assembly includes the barrel clamp tube, a flash suppressor mounted to the front end of the barrel clamp tube, and a barrel clamp co liar mounted to the rear end of the barrel clamp tube. The impeller is mounted to the barrel clamp tube between the flash suppressor and the barrel clamp collar.
摘要翻译：一种用于多管式小型机的改进的筒夹组件包括一个筒夹具管，其具有前端，后端和在前端和后端之间延伸的多个纵向开口。在管前端和管后端之间的筒形夹管中安装有叶轮。叶轮包括多个叶轮叶片，其围绕叶轮的周边间隔开，并且从叶轮的后凸缘部向前突出并且叶轮叶片限定多个空气通道。枪管组件包括枪管夹紧管，安装到枪管夹管的前端的闪光抑制器以及安装到枪管钳管的后端的枪管钳夹。叶轮安装在闪光抑制器和筒夹夹环之间的筒夹管上。

2. 发明公开

EP2337940A4 THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：热管理系统
公开(公告)号：EP2337940A4
公开(公告)日：2012-02-29
申请号：EP09815197
申请日：2009-09-17
申请人： ROLLS ROYCE CORP
发明人： JUNOD LARRY ALLEN
IPC分类号： F02K3/00 , F02C3/32 , F02C7/14
CPC分类号： F02C7/14 , F02C3/32 , F02K1/825 , F05D2260/601 , F41A13/10 , F41H13/0043 , Y02T50/675

3. 发明公开

EP2337940A1 THERMAL MANAGEMENT SYSTEM 审中-公开
标题翻译：热管理系统
公开(公告)号：EP2337940A1
公开(公告)日：2011-06-29
申请号：EP09815197.0
申请日：2009-09-17
申请人： Rolls-Royce Corporation
发明人： JUNOD, Larry, Allen
IPC分类号： F02K3/00
CPC分类号： F02C7/14 , F02C3/32 , F02K1/825 , F05D2260/601 , F41A13/10 , F41H13/0043 , Y02T50/675
摘要： In one embodiment a gas turbine engine is disclosed having a heat exchanger at least partially disposed in a bypass duct. In one form the gas turbine engine is a high bypass ratio engine. The heat exchanger may be coupled with a directed energy weapon to provide coolant flow and regulate the temperature of the directed energy weapon. Other devices may also be coupled with the heat exchanger, either as an alternative to in addition to the directed energy weapon.

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