公开(公告)号：US20180244364A1

公开(公告)日：2018-08-30

申请号：US15593607

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C1/06 ,  B64C27/08 ,  B64C29/02 ,  B64C39/06

Abstract: An aircraft capable of vertical takeoff and landing and stationary flight includes a distributed airframe coupled to a modular fuselage. The modular fuselage has a longitudinal axis substantially parallel to a rotational axis of three or more propellers. The modular fuselage includes a rear module substantially disposed within a perimeter of the distributed airframe, a front module removably connected to the rear module and substantially aligned with the longitudinal axis. One or more engines or motors are disposed within or attached to the distributed airframe or fuselage. The three or more propellers are proximate to a leading edge of the distributed airframe, distributed along the distributed airframe, and operably connected to the one or more engines or motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight.

公开(公告)号：US10730624B2

公开(公告)日：2020-08-04

申请号：US15593607

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C39/06 ,  B64C27/08 ,  B64C11/28 ,  B64C27/50 ,  B64C29/00 ,  B64C3/10 ,  B64C27/12 ,  B64D27/24 ,  B64D31/00 ,  B64C29/02 ,  B64C1/06 ,  B64C39/02 ,  B64C1/00 ,  B64D27/02

Abstract: An aircraft capable of vertical takeoff and landing and stationary flight includes a distributed airframe coupled to a modular fuselage. The modular fuselage has a longitudinal axis substantially parallel to a rotational axis of three or more propellers. The modular fuselage includes a rear module substantially disposed within a perimeter of the distributed airframe, a front module removably connected to the rear module and substantially aligned with the longitudinal axis. One or more engines or motors are disposed within or attached to the distributed airframe or fuselage. The three or more propellers are proximate to a leading edge of the distributed airframe, distributed along the distributed airframe, and operably connected to the one or more engines or motors to provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight.

公开(公告)号：USD798795S1

公开(公告)日：2017-10-03

申请号：US29564581

申请日：2016-05-13

Applicant: Bell Helicopter Textron Inc.

Designer： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

公开(公告)号：US10960978B2

公开(公告)日：2021-03-30

申请号：US15593554

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C39/06 ,  B64C29/00 ,  B64C11/28 ,  B64C27/50 ,  B64C3/16 ,  B64C3/10 ,  B64C27/08 ,  B64C27/12 ,  B64D27/24 ,  B64D31/00 ,  B64C29/02 ,  B64C1/06 ,  B64C39/02 ,  B64C39/00 ,  B64C1/00 ,  B64D27/02

Abstract: An aircraft capable of vertical takeoff and landing, stationary flight and forward flight includes a closed wing that provides lift whenever the aircraft is in forward flight, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. One or more engines or motors are disposed within or attached to the closed wing, fuselage or spokes. Three or more propellers are proximate to a leading edge of the closed wing or the one or more spokes, distributed along the closed wing or the one or more spokes, and operably connected to the one or more engines or motors. The propellers provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight, and provide thrust whenever the aircraft is in forward flight.

公开(公告)号：US10737786B2

公开(公告)日：2020-08-11

申请号：US15593575

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C39/06 ,  B64C29/02 ,  B64D27/02 ,  B64C11/28 ,  B64C27/50 ,  B64C29/00 ,  B64C3/10 ,  B64C27/08 ,  B64C27/12 ,  B64D27/24 ,  B64D31/00 ,  B64C1/06 ,  B64C39/02 ,  B64C1/00

Abstract: An aircraft includes a closed wing, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. A plurality of hydraulic or electric motors are disposed within or attached to the closed wing, fuselage or spokes in a distributed configuration. A propeller is proximate to a leading edge of the closed wing or spokes and operably connected to each hydraulic or electric motor. A source of hydraulic or electric power is disposed within or attached to the closed wing, fuselage or spokes and coupled to each hydraulic or electric motor disposed within or attached to the closed wing, fuselage or spokes. A controller is coupled to each hydraulic or electric motor, and one or more processors communicably coupled to each controller that control an operation and speed of the plurality of hydraulic or electric motors.

公开(公告)号：US10676183B2

公开(公告)日：2020-06-09

申请号：US15593521

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C27/50 ,  B64C11/28 ,  B64C39/06 ,  B64C29/00 ,  B64C3/10 ,  B64C27/08 ,  B64C27/12 ,  B64D27/24 ,  B64D31/00 ,  B64C29/02 ,  B64C1/06 ,  B64C39/02 ,  B64C1/00 ,  B64D27/02

Abstract: A rotor blade rotation system includes two or more rotor blades, each rotor blade in mechanical communication with a hub and pivotable about an axis of rotation, a bearing plate comprising a rotating portion and a non-rotating portion, a fold linkage coupled to the rotating portion of the bearing plate and in mechanical communication with the rotor blade, and an actuator coupled to the non-rotating portion of the bearing plate and operable to reposition the bearing plate from a first position to a second position such that the folding links pivot the rotor blades from a deployed position to a forward folded position.

公开(公告)号：US20180244376A1

公开(公告)日：2018-08-30

申请号：US15593575

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C27/08 ,  B64C11/28 ,  B64C29/02 ,  B64C39/02 ,  B64C39/06 ,  B64D27/24

Abstract: An aircraft includes a closed wing, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. A plurality of hydraulic or electric motors are disposed within or attached to the closed wing, fuselage or spokes in a distributed configuration. A propeller is proximate to a leading edge of the closed wing or spokes and operably connected to each hydraulic or electric motor. A source of hydraulic or electric power is disposed within or attached to the closed wing, fuselage or spokes and coupled to each hydraulic or electric motor disposed within or attached to the closed wing, fuselage or spokes. A controller is coupled to each hydraulic or electric motor, and one or more processors communicably coupled to each controller that control an operation and speed of the plurality of hydraulic or electric motors.

公开(公告)号：USD798794S1

公开(公告)日：2017-10-03

申请号：US29564548

申请日：2016-05-13

Applicant: Bell Helicopter Textron Inc.

Designer： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

公开(公告)号：US20180244381A1

公开(公告)日：2018-08-30

申请号：US15593554

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C29/02 ,  B64C39/06

CPC classification number: B64C29/02 ,  B64C1/068 ,  B64C3/10 ,  B64C11/28 ,  B64C27/08 ,  B64C27/12 ,  B64C27/50 ,  B64C29/0025 ,  B64C39/024 ,  B64C39/06 ,  B64C39/062 ,  B64C2001/0045 ,  B64D27/24 ,  B64D31/00 ,  B64D2027/026

Abstract: An aircraft capable of vertical takeoff and landing, stationary flight and forward flight includes a closed wing that provides lift whenever the aircraft is in forward flight, a fuselage at least partially disposed within a perimeter of the closed wing, and one or more spokes coupling the closed wing to the fuselage. One or more engines or motors are disposed within or attached to the closed wing, fuselage or spokes. Three or more propellers are proximate to a leading edge of the closed wing or the one or more spokes, distributed along the closed wing or the one or more spokes, and operably connected to the one or more engines or motors. The propellers provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight, and provide thrust whenever the aircraft is in forward flight.

公开(公告)号：US20180186445A1

公开(公告)日：2018-07-05

申请号：US15593521

申请日：2017-05-12

Applicant: Bell Helicopter Textron Inc.

Inventor： Carlos Alexander Fenny ,  Rohn Lee Olson ,  Andrew James Zahasky

IPC: B64C11/28 ,  B64C29/00 ,  B64C39/06

Abstract: A rotor blade rotation system includes two or more rotor blades, each rotor blade in mechanical communication with a hub and pivotable about an axis of rotation, a bearing plate comprising a rotating portion and a non-rotating portion, a fold linkage coupled to the rotating portion of the bearing plate and in mechanical communication with the rotor blade, and an actuator coupled to the non-rotating portion of the bearing plate and operable to reposition the bearing plate from a first position to a second position such that the folding links pivot the rotor blades from a deployed position to a forward folded position.