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：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：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：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：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：US20150151848A1

公开(公告)日：2015-06-04

申请号：US14609548

申请日：2015-01-30

Applicant: Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

Inventor： Steven Gagne ,  Rigoberto Rodriguez ,  William L. Siegel ,  John R. Arvin

IPC: B64D41/00 ,  B64D33/08 ,  H02K7/18 ,  B64D33/04

CPC classification number: B64D13/006 ,  B64D13/08 ,  B64D33/04 ,  B64D33/08 ,  B64D41/00 ,  B64D41/007 ,  B64D2013/0614 ,  B64D2013/0674 ,  F02C6/08 ,  F02C7/32 ,  H02K7/1823

Abstract: One embodiment of the present invention is a unique airborne electrical power and thermal management system. Another embodiment is a unique aircraft. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for aircraft and electrical power and thermal management systems. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.

Abstract translation: 本发明的一个实施例是独特的机载电力和热管理系统。 另一个实施例是独特的飞机。 其他实施例包括用于飞机和电力和热管理系统的装置，系统，装置，硬件，方法和组合。 本申请的其它实施例，形式，特征，方面，益处和优点将从本文提供的描述和附图中变得显而易见。