发明名称 Radial sonobuoy launcher
摘要 A radial sonobuoy launch system comprising a clam-shell launch tube and method for launching a sonobuoy. The clam-shell launch tube radially releases a sonobuoy and the clam-shell launch tube is reloaded during flight. The sonobuoys are pneumatically ejected about parallel to the airstream. A pressure boundary structure, having a door and a gate, maintains cabin pressure during reloading and launching. Support arms and drive arms evenly distribute the ejection accelerations from the firing mechanism and guide the trajectory of the sonobuoy during release. A clam-shell launch tube is capable of launching a multitude of differently sized sonobuoys.
申请公布号 US6679454(B2) 申请公布日期 2004.01.20
申请号 US20020123823 申请日期 2002.04.15
申请人 THE BOEING COMPANY 发明人 OLSEN MARK L.;PITZER JON W.
分类号 B64C1/22;B64D1/10;B64D1/12;B64D9/00;F41A9/27;F41A9/73;F41F3/06;(IPC1-7):B64D1/02 主分类号 B64C1/22
代理机构 代理人
主权项
地址