公开(公告)号：US4971272A

公开(公告)日：1990-11-20

申请号：US373969

申请日：1989-06-29

申请人： Joan M. Gudridge ,  Clement A. Senatro ,  Wieslaw A. Chlus

发明人： Joan M. Gudridge ,  Clement A. Senatro ,  Wieslaw A. Chlus

IPC分类号： F02C9/28 ,  F16L3/12 ,  F16L3/137

CPC分类号： F16L3/137 ,  Y10T24/141

摘要： A support structure 10 for positioning a conduit 12 for various environments including that of an aircraft gas turbine engine is disclosed. Various construction details are developed for the support structure which facilitate assembly of portions of the support structure. The support structure includes a clamp assembly 18 and a clip 22 for orienting the clamp assembly in the proper direction. Orientation of the clamp assembly is facilitated by features of the clip. These features include a pair of tabs 32, 34 which face each other from either side of the clamp assembly. In one detailed embodiment, the clamp includes a laterally extending tab 92 to block the channel formed between the pair of longitudinally extending tabs.

摘要翻译： 公开了一种用于定位用于包括飞机燃气涡轮发动机的各种环境的管道12的支撑结构10。 开发了用于支撑结构的各种构造细节，其有利于组装支撑结构的部分。 支撑结构包括用于使夹具组件沿正确方向定向的夹具组件18和夹子22。 夹子组件的方向由夹具的特征促进。 这些特征包括从夹具组件的任一侧彼此面对的一对翼片32,34。 在一个详细的实施例中，夹具包括横向延伸的突片92，以阻挡形成在一对纵向延伸突片之间的通道。