公开(公告)号：US20210300543A1

公开(公告)日：2021-09-30

申请号：US17225342

申请日：2021-04-08

Applicant: BOOM TECHNOLOGY, INC.

Inventor： Nathaniel Blake Scholl ,  Joseph Ray Wilding ,  Joshua Krall ,  Andrew P. Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D27/18 ,  B64C1/14 ,  B64D27/20 ,  B64D13/06 ,  B64D33/04 ,  B64D33/02 ,  B64D11/06 ,  B64D13/08 ,  B64D27/10 ,  B64D43/00

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.

公开(公告)号：US20210300544A1

公开(公告)日：2021-09-30

申请号：US17225359

申请日：2021-04-08

Applicant: BOOM TECHNOLOGY, INC.

Inventor： Nathaniel Blake Scholl ,  Joseph Ray Wilding ,  Joshua Krall ,  Andrew P. Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D27/18 ,  B64C1/14 ,  B64D27/20 ,  B64D13/06 ,  B64D33/04 ,  B64D33/02 ,  B64D11/06 ,  B64D13/08 ,  B64D27/10 ,  B64D43/00

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.

公开(公告)号：US20180134382A1

公开(公告)日：2018-05-17

申请号：US15811327

申请日：2017-11-13

Applicant: Boom Technology, Inc.

Inventor： Nathaniel Blake Scholl ,  Joe Wilding ,  Josh Krall ,  Andy Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D13/08 ,  B64D43/00 ,  B64D11/06

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.

公开(公告)号：US20240132221A1

公开(公告)日：2024-04-25

申请号：US18493186

申请日：2023-10-23

Applicant: Boom Technology, Inc.

Inventor： Nathaniel Blake Scholl

IPC: B64D27/16 ,  B64C15/14 ,  B64C30/00 ,  F02C7/32 ,  F02K3/04

CPC classification number: B64D27/16 ,  B64C15/14 ,  B64C30/00 ,  F02C7/32 ,  F02K3/04

Abstract: An aircraft propulsion system having a variable airflow capture area is provided. The propulsion system includes a main propulsion source and an auxiliary propulsion source. In a first mode, the auxiliary propulsion source is stowed within an aerodynamic profile of the aircraft, and the main propulsion source provides all of the propulsion force for powering flight of the aircraft. In a second mode, the auxiliary propulsion source is deployed to augment the airflow capture area of the main propulsion source and increase an overall airflow capture area of the propulsion system. In the second mode, the auxiliary power source is operated by power extracted from the main propulsion source. The main propulsion source may include one or more low bypass ratio engines. The auxiliary power source may include one or more auxiliary thrust fans coupled at a plurality of locations on the aircraft.

公开(公告)号：US20240228048A9

公开(公告)日：2024-07-11

申请号：US18493186

申请日：2023-10-24

Applicant: Boom Technology, Inc.

Inventor： Nathaniel Blake Scholl

IPC: B64D27/16 ,  B64C15/14 ,  B64C30/00 ,  F02C7/32 ,  F02K3/04

CPC classification number: B64D27/16 ,  B64C15/14 ,  B64C30/00 ,  F02C7/32 ,  F02K3/04

Abstract: An aircraft propulsion system having a variable airflow capture area is provided. The propulsion system includes a main propulsion source and an auxiliary propulsion source. In a first mode, the auxiliary propulsion source is stowed within an aerodynamic profile of the aircraft, and the main propulsion source provides all of the propulsion force for powering flight of the aircraft. In a second mode, the auxiliary propulsion source is deployed to augment the airflow capture area of the main propulsion source and increase an overall airflow capture area of the propulsion system. In the second mode, the auxiliary power source is operated by power extracted from the main propulsion source. The main propulsion source may include one or more low bypass ratio engines. The auxiliary power source may include one or more auxiliary thrust fans coupled at a plurality of locations on the aircraft.

公开(公告)号：US20210300542A1

公开(公告)日：2021-09-30

申请号：US17225315

申请日：2021-04-08

Applicant: BOOM TECHNOLOGY, INC.

Inventor： Nathaniel Blake Scholl ,  Joseph Ray Wilding ,  Joshua Krall ,  Andrew P. Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D27/18 ,  B64C1/14 ,  B64D27/20 ,  B64D13/06 ,  B64D33/04 ,  B64D33/02 ,  B64D11/06 ,  B64D13/08 ,  B64D27/10 ,  B64D43/00

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.

公开(公告)号：US20210139142A1

公开(公告)日：2021-05-13

申请号：US16998238

申请日：2020-08-20

Applicant: BOOM TECHNOLOGY, INC.

Inventor： Nathaniel Blake Scholl ,  Joseph Ray Wilding ,  Joshua Krall ,  Andrew P. Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D27/18 ,  B64C1/14 ,  B64D27/20 ,  B64D13/06 ,  B64D33/04 ,  B64D33/02 ,  B64D11/06 ,  B64D13/08 ,  B64D27/10 ,  B64D43/00

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.

公开(公告)号：US10793266B2

公开(公告)日：2020-10-06

申请号：US15811327

申请日：2017-11-13

Applicant: Boom Technology, Inc.

Inventor： Nathaniel Blake Scholl ,  Joseph Ray Wilding ,  Joshua Krall ,  Andrew P. Berryann ,  Michael Reid

IPC: B64C30/00 ,  B64D13/08 ,  B64D43/00 ,  B64D11/06 ,  B64D27/18 ,  B64C1/14 ,  B64D27/20 ,  B64D13/06 ,  B64D33/04 ,  B64D33/02 ,  B64D27/10 ,  B64D27/16

Abstract: Commercial supersonic aircraft and associated systems and methods. A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between 20 and 60 passengers, a delta wing mounted to the fuselage, and a propulsion system carried by at least one of the wing and the fuselage, the propulsion system including a plurality of engines, at least one variable-geometry inlet, and at least one variable-geometry nozzle.