公开(公告)号：FR2649180B1

公开(公告)日：1992-12-31

申请号：FR9008291

申请日：1990-06-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GUDRIDGE JOAN M ,  SENATRO CLEMENT A ,  CHLUS WIESLAW A

IPC: F02C9/28 ,  F16L3/12 ,  F16L3/137 ,  F16L3/123 ,  H02G3/26

Abstract: 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.

公开(公告)号：GB2235491A

公开(公告)日：1991-03-06

申请号：GB9014082

申请日：1990-06-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GUDRIDGE JOAN M ,  SENATRO CLEMENT A ,  CHLUS WIESLAW A

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

Abstract: 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.

公开(公告)号：FR2649180A1

公开(公告)日：1991-01-04

申请号：FR9008291

申请日：1990-06-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GUDRIDGE JOAN M ,  SENATRO CLEMENT A ,  CHLUS WIESLAW A

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

Abstract: 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.

公开(公告)号：GB2235491B

公开(公告)日：1993-04-14

申请号：GB9014082

申请日：1990-06-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GUDRIDGE JOAN M ,  SENATRO CLEMENT A ,  CHLUS WIESLAW A

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

Abstract: 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.