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公开(公告)号：US11541987B2
公开(公告)日：2023-01-03
申请号：US16544117
申请日：2019-08-19
Applicant: Bell Textron Inc.
Inventor： Martin Landry
Abstract: An embodiment is an aircraft, including at least a fuselage, a tail rotatably coupled to the fuselage, the tail coupled at an aft of the fuselage, and a tail actuator coupled to the fuselage and the tail, the tail actuator to transition the tail between an extended position and a retracted position.
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公开(公告)号：US20220177134A1
公开(公告)日：2022-06-09
申请号：US17111224
申请日：2020-12-03
Applicant: Bell Textron Inc.
Inventor： Martin Landry
Abstract: An exemplary integrated battery cargo platform includes a housing having an exterior surface and a structural strength to support cargo for transit on a top surface, a battery enclosed in the housing with power contacts exposed at the exterior surface.
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Patent Agency Ranking
公开(公告)号：US20220169374A1
公开(公告)日：2022-06-02
申请号：US17106514
申请日：2020-11-30
Applicant: Bell Textron Inc.
Inventor： Martin Landry
Abstract: An exemplary anti-torque system for a rotorcraft includes a fan located inside of a channel that extends inside of a fuselage from an inlet proximate a forward end of the tail boom to an outlet at an aft end of the tail boom, the outlet is oriented to direct airflow from the channel onto a rudder coupled to a trailing edge of a vertical stabilizer.
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公开(公告)号：US11981452B2
公开(公告)日：2024-05-14
申请号：US17111224
申请日：2020-12-03
Applicant: Bell Textron Inc.
Inventor： Martin Landry
IPC: B64F1/22 , B64C39/02 , B64D9/00 , B64D27/24 , B64F1/00 , B65D19/00 , B65D19/38 , G01G19/52 , B64C29/00 , B64U50/19 , B64U101/60
CPC classification number: B64D9/00 , B64C39/024 , B64D27/24 , B65D19/0016 , B65D19/38 , G01G19/52 , B64C29/0016 , B64U50/19 , B64U2101/60 , H01M2220/20
Abstract: An exemplary integrated battery cargo platform includes a housing having an exterior surface and a structural strength to support cargo for transit on a top surface, a battery enclosed in the housing with power contacts exposed at the exterior surface.
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公开(公告)号：US11267564B2
公开(公告)日：2022-03-08
申请号：US16659829
申请日：2019-10-22
Applicant: Bell Textron Inc.
Inventor： Martin Landry , Mathieu Beland , Maxime Lapalme
Abstract: An aircraft includes a fuselage, and a wing extending from the fuselage along a spanwise axis. A section of the wing is rotatable about the spanwise axis. A ducted fan is mounted to the section of the wing. The ducted fan has a hub configured to be drivingly engaged by an engine. The hub is rotatable about a fan axis. Blades protrude from the hub between roots mounted to the hub and tips radially spaced from the hub. A duct circumferentially extends about the fan axis and is mounted to the tips of the blades to rotate with the blades about the fan axis. The section of the wing and the ducted fan are rotatable about the spanwise axis between a hover mode in which the fan axis is substantially perpendicular to a ground, and an aircraft mode in which the fan axis is substantially parallel to the ground.
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公开(公告)号：US11584522B2
公开(公告)日：2023-02-21
申请号：US17106514
申请日：2020-11-30
Applicant: Bell Textron Inc.
Inventor： Martin Landry
Abstract: An exemplary anti-torque system for a rotorcraft includes a fan located inside of a channel that extends inside of a fuselage from an inlet proximate a forward end of the tail boom to an outlet at an aft end of the tail boom, the outlet is oriented to direct airflow from the channel onto a rudder coupled to a trailing edge of a vertical stabilizer.
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公开(公告)号：US20210053670A1
公开(公告)日：2021-02-25
申请号：US16544117
申请日：2019-08-19
Applicant: Bell Textron Inc.
Inventor： Martin Landry
Abstract: An embodiment is an aircraft, including at least a fuselage, a tail rotatably coupled to the fuselage, the tail coupled at an aft of the fuselage, and a tail actuator coupled to the fuselage and the tail, the tail actuator to transition the tail between an extended position and a retracted position.
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