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：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：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：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.