公开(公告)号：US12025026B2

公开(公告)日：2024-07-02

申请号：US18365118

申请日：2023-08-03

Applicant: Honeywell International Inc.

Inventor： Richard David Conner ,  Ryan Cox ,  Josef Merki ,  Brian Larsen

IPC: F01D5/10 ,  F01D5/02 ,  F01D5/03 ,  F01D5/14 ,  F03D1/06 ,  F03D9/32

CPC classification number: F01D5/10 ,  F01D5/022 ,  F01D5/03 ,  F01D5/143 ,  F03D1/0633 ,  F03D9/32 ,  F05B2220/31 ,  F05B2240/33 ,  F05B2240/923 ,  F05B2250/14 ,  F05B2250/141 ,  F05D2240/24

Abstract: A ram air turbine rotor comprises at least one intra-flow path shroud structure coupled between rotor blades, along a radial position between a support disc and an outer rim. The shroud structure includes shroud sectors each coupled between a respective pair of blades. The sectors each include a first edge adjacent to leading edges of the respective pair of blades, the first edge including a first curved segment, and a second edge adjacent to trailing edges of the respective pair of blades, the second edge including a second curved segment. The curved segments are each partially defined by a respective ellipse having a semi-major axis and a semi-minor axis. The semi-major axis is a portion of a spanwise distance between the respective pair of blades. The semi-minor axis is a portion of an axial distance between the leading edge of one blade and the trailing edge of an adjacent blade.

公开(公告)号：US20240093609A1

公开(公告)日：2024-03-21

申请号：US18365118

申请日：2023-08-03

Applicant: Honeywell International Inc.

Inventor： Richard David Conner ,  Ryan Cox ,  Josef Merki ,  Brian Larsen

IPC: F01D5/10 ,  F01D5/02 ,  F01D5/03 ,  F01D5/14 ,  F03D1/06 ,  F03D9/32

CPC classification number: F01D5/10 ,  F01D5/022 ,  F01D5/03 ,  F01D5/143 ,  F03D1/0633 ,  F03D9/32 ,  F05B2220/31 ,  F05B2240/33 ,  F05B2240/923 ,  F05B2250/14 ,  F05B2250/141 ,  F05D2240/24

Abstract: A ram air turbine rotor comprises at least one intra-flow path shroud structure coupled between rotor blades, along a radial position between a support disc and an outer rim. The shroud structure includes shroud sectors each coupled between a respective pair of blades. The sectors each include a first edge adjacent to leading edges of the respective pair of blades, the first edge including a first curved segment, and a second edge adjacent to trailing edges of the respective pair of blades, the second edge including a second curved segment. The curved segments are each partially defined by a respective ellipse having a semi-major axis and a semi-minor axis. The semi-major axis is a portion of a spanwise distance between the respective pair of blades. The semi-minor axis is a portion of an axial distance between the leading edge of one blade and the trailing edge of an adjacent blade.

公开(公告)号：US11767760B2

公开(公告)日：2023-09-26

申请号：US17089564

申请日：2020-11-04

Applicant: Honeywell International Inc.

Inventor： Richard David Conner ,  Ryan Cox ,  Josef Merki ,  Brian Larsen

IPC: F01D5/10 ,  F01D5/14 ,  F03D1/06 ,  F03D9/32 ,  F01D5/03 ,  F01D5/02

CPC classification number: F01D5/10 ,  F01D5/022 ,  F01D5/03 ,  F01D5/143 ,  F03D1/0633 ,  F03D9/32 ,  F05B2220/31 ,  F05B2240/33 ,  F05B2240/923 ,  F05B2250/14 ,  F05B2250/141 ,  F05D2240/24

Abstract: A ram air turbine rotor comprises at least one intra-flow path shroud structure coupled between rotor blades, along a radial position between a support disc and an outer rim. The shroud structure includes shroud sectors each coupled between a respective pair of blades. The sectors each include a first edge adjacent to leading edges of the respective pair of blades, the first edge including a first curved segment, and a second edge adjacent to trailing edges of the respective pair of blades, the second edge including a second curved segment. The curved segments are each partially defined by a respective ellipse having a semi-major axis and a semi-minor axis. The semi-major axis is a portion of a spanwise distance between the respective pair of blades. The semi-minor axis is a portion of an axial distance between the leading edge of one blade and the trailing edge of an adjacent blade.

公开(公告)号：US20220135242A1

公开(公告)日：2022-05-05

申请号：US17089564

申请日：2020-11-04

Applicant: Honeywell International Inc.

Inventor： Richard David Conner ,  Ryan Cox ,  Josef Merki ,  Brian Larsen

IPC: B64D41/00 ,  F01D5/14

Abstract: A ram air turbine rotor comprises at least one intra-flow path shroud structure coupled between rotor blades, along a radial position between a support disc and an outer rim. The shroud structure includes shroud sectors each coupled between a respective pair of blades. The sectors each include a first edge adjacent to leading edges of the respective pair of blades, the first edge including a first curved segment, and a second edge adjacent to trailing edges of the respective pair of blades, the second edge including a second curved segment. The curved segments are each partially defined by a respective ellipse having a semi-major axis and a semi-minor axis. The semi-major axis is a portion of a spanwise distance between the respective pair of blades. The semi-minor axis is a portion of an axial distance between the leading edge of one blade and the trailing edge of an adjacent blade.