公开(公告)号：US11668205B2

公开(公告)日：2023-06-06

申请号：US17170230

申请日：2021-02-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jeffrey Guymon ,  Brian Walker ,  Manuel Sandoval

IPC: F01D21/04 ,  F01D25/24 ,  F02C7/22

CPC classification number: F01D21/045 ,  F01D25/24 ,  F05D2220/323 ,  F05D2240/14 ,  F05D2250/191 ,  F05D2250/291

Abstract: A containment system for an engine includes an engine case having an inner perimeter. The containment system includes a containment ring nested within the inner perimeter of the engine case and integrally formed with the engine case along a first interface and a second interface. The containment ring includes a first leg opposite a second leg, and the first interface is defined between the first leg and the engine case. The containment system includes a first plurality of perforations defined at the first interface, and the first leg of the containment ring is frangible along the first plurality of perforations to at least partially release the containment ring to protect the engine case during a containment event.

公开(公告)号：US20220251969A1

公开(公告)日：2022-08-11

申请号：US17170230

申请日：2021-02-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Jeffrey Guymon ,  Brian Walker ,  Manuel Sandoval

IPC: F01D21/04 ,  F01D25/24 ,  F02C7/22

Abstract: A containment system for an engine includes an engine case having an inner perimeter. The containment system includes a containment ring nested within the inner perimeter of the engine case and integrally formed with the engine case along a first interface and a second interface. The containment ring includes a first leg opposite a second leg, and the first interface is defined between the first leg and the engine case. The containment system includes a first plurality of perforations defined at the first interface, and the first leg of the containment ring is frangible along the first plurality of perforations to at least partially release the containment ring to protect the engine case during a containment event.

公开(公告)号：US20210388728A1

公开(公告)日：2021-12-16

申请号：US16900692

申请日：2020-06-12

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Peter Hall ,  Mark Morris ,  Manuel Sandoval ,  Robert Burkhead

IPC: F01D9/04

Abstract: A turbine nozzle for a gas turbine engine includes an outer endwall, and an inner endwall spaced apart from the outer endwall. The turbine nozzle includes at least one airfoil coupled between the inner endwall and the outer endwall, and a compliant joint defined in at least one of the outer endwall and the inner endwall. The compliant joint includes at least one partially-fused seal that is configured to restrict a flow of fluid through the at least one of the outer endwall and the inner endwall and to form a slip-joint above a predetermined threshold stress. The slip-joint is configured to maintain a radial position of the at least one of the outer endwall and the inner endwall.

公开(公告)号：US11421541B2

公开(公告)日：2022-08-23

申请号：US16900692

申请日：2020-06-12

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Peter Hall ,  Mark Morris ,  Manuel Sandoval ,  Robert Burkhead

IPC: F01D9/04 ,  F01D11/00

Abstract: A turbine nozzle for a gas turbine engine includes an outer endwall, and an inner endwall spaced apart from the outer endwall. The turbine nozzle includes at least one airfoil coupled between the inner endwall and the outer endwall, and a compliant joint defined in at least one of the outer endwall and the inner endwall. The compliant joint includes at least one partially-fused seal that is configured to restrict a flow of fluid through the at least one of the outer endwall and the inner endwall and to form a slip-joint above a predetermined threshold stress. The slip-joint is configured to maintain a radial position of the at least one of the outer endwall and the inner endwall.