公开(公告)号：US09651059B2

公开(公告)日：2017-05-16

申请号：US13728200

申请日：2012-12-27

Applicant: United Technologies Corporation

Inventor： Thomas J. Robertson, Jr. ,  Darin S. Lussier ,  Kirk D. Stackhouse ,  Johan Santana

IPC: F04D29/52 ,  F04D29/02 ,  F01D11/12

CPC classification number: F04D29/526 ,  F01D11/122 ,  F01D11/127 ,  F04D29/023 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2250/283 ,  F05D2300/431 ,  F05D2300/501 ,  F05D2300/50212 ,  Y02T50/672

Abstract: A section of a gas turbine engine includes a case structure and a liner. The liner is attached to the case structure by a compliant adhesive. The adhesive covers at least a portion of the liner surface area, and can have interruptions used to tune the compliance of the adhesive layer.

公开(公告)号：US20140186165A1

公开(公告)日：2014-07-03

申请号：US13728200

申请日：2012-12-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas J. Robertson, JR. ,  Darin S. Lussier ,  Kirk D. Stackhouse ,  Johan Santana

IPC: F04D29/52

CPC classification number: F04D29/526 ,  F01D11/122 ,  F01D11/127 ,  F04D29/023 ,  F05D2220/36 ,  F05D2230/23 ,  F05D2250/283 ,  F05D2300/431 ,  F05D2300/501 ,  F05D2300/50212 ,  Y02T50/672

Abstract: A section of a gas turbine engine includes a case structure and a liner. The liner is attached to the case structure by a compliant adhesive. The adhesive covers at least a portion of the liner surface area, and can have interruptions used to tune the compliance of the adhesive layer.

Abstract translation: 燃气涡轮发动机的一部分包括壳体结构和衬套。 衬里通过柔性粘合剂附接到壳体结构。 粘合剂覆盖衬垫表面积的至少一部分，并且可以具有用于调节粘合剂层的柔顺性的中断。