公开(公告)号：US20230303263A1

公开(公告)日：2023-09-28

申请号：US17702754

申请日：2022-03-23

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: B64D41/00 ,  F02C7/04

CPC classification number: B64D41/007 ,  F02C7/04 ,  F05D2220/10

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US20230303264A1

公开(公告)日：2023-09-28

申请号：US17702755

申请日：2022-03-23

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: B64D41/00 ,  B64D33/08 ,  B64C21/02 ,  F02K7/10

CPC classification number: B64D41/007 ,  B64D33/08 ,  B64C21/02 ,  F02K7/10 ,  F05D2220/34

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US20230358148A1

公开(公告)日：2023-11-09

申请号：US18347383

申请日：2023-07-05

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: F01D15/10 ,  B64D41/00 ,  F01D5/14 ,  F01D11/12 ,  F04D29/18 ,  H02K1/2706 ,  H02K7/18 ,  H02K1/276

CPC classification number: F01D15/10 ,  B64D41/007 ,  F01D5/147 ,  F01D11/122 ,  F04D29/186 ,  H02K1/2706 ,  H02K7/1823 ,  H02K1/276 ,  F05D2220/768 ,  F05D2260/30 ,  F05D2220/34 ,  F05D2260/232 ,  F05D2240/307

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US20230312128A1

公开(公告)日：2023-10-05

申请号：US17702759

申请日：2022-03-23

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: B64D33/08 ,  B64D41/00

CPC classification number: B64D41/007 ,  B64D33/08

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US10443497B2

公开(公告)日：2019-10-15

申请号：US15233402

申请日：2016-08-10

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk

IPC: F02C7/047 ,  F02C3/04 ,  F01D25/02 ,  F02C6/08 ,  F02C7/18

Abstract: A gas turbine engine includes devices, systems, and methods for de-icing using heat of compression and expelling the de-icing medium into a gas flow path of the engine.

公开(公告)号：US11878812B2

公开(公告)日：2024-01-23

申请号：US17702754

申请日：2022-03-23

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: B64D41/00 ,  H02K1/2783 ,  H02K9/22 ,  H02K7/00 ,  F01D15/10 ,  H02K7/08

CPC classification number: B64D41/007 ,  H02K1/2783 ,  H02K7/006 ,  H02K7/08 ,  H02K9/22 ,  F01D15/10

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US11719119B1

公开(公告)日：2023-08-08

申请号：US17702757

申请日：2022-03-23

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk ,  Rigoberto Rodriguez ,  David Locascio

IPC: F01D15/10 ,  F01D5/14 ,  F01D11/12 ,  B64D41/00 ,  F04D29/18 ,  H02K7/18 ,  H02K1/2706 ,  H02K1/276

CPC classification number: F01D15/10 ,  B64D41/007 ,  F01D5/147 ,  F01D11/122 ,  F04D29/186 ,  H02K1/2706 ,  H02K1/276 ,  H02K7/1823 ,  F05D2220/34 ,  F05D2220/768 ,  F05D2240/307 ,  F05D2260/232 ,  F05D2260/30

Abstract: The present disclosure is directed to an aircraft with an accessory system configured to be powered independent of the primary propulsion system by a ram air turbine power system. The ram air turbine power system illustratively includes an accessory generator integrated with a turbine rotor as well as other components so as to manage space claim and offer unique functionality.

公开(公告)号：US20180045116A1

公开(公告)日：2018-02-15

申请号：US15233402

申请日：2016-08-10

Applicant: Rolls-Royce Corporation

Inventor： Peter M. Schenk

IPC: F02C7/047 ,  F02C3/04

CPC classification number: F02C7/047 ,  F01D25/02 ,  F02C3/04 ,  F02C6/08 ,  F02C7/185 ,  F05D2260/205 ,  F05D2260/213 ,  Y02T50/671 ,  Y02T50/676

Abstract: A gas turbine engine includes devices, systems, and methods for de-icing using heat of compression and expelling the de-icing medium into a gas flow path of the engine.