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公开(公告)号：US10882598B2
公开(公告)日：2021-01-05
申请号：US15951539
申请日：2018-04-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , Brent Chadwick Ross
Abstract: Embodiments are directed to systems and methods for a sliding door in a pressurized aircraft. In one embodiment, an aircraft comprises a fuselage having a door opening, and a door configured to slide into the door opening from within the fuselage, the door held in a closed position in the door opening by excess air pressure within the fuselage during operation of the aircraft.
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公开(公告)号：US10549854B2
公开(公告)日：2020-02-04
申请号：US15082839
申请日：2016-03-28
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , Steven W. Kihara
Abstract: An aircraft has a wing and at least a portion of a hoist system disposed within the wing. A method of hoisting an item includes disposing at least a portion of a hoist system within a wing of an aircraft and extending a cable of the hoist system through an access hole of an exterior wall of the wing.
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公开(公告)号：US10266252B2
公开(公告)日：2019-04-23
申请号：US15269862
申请日：2016-09-19
Applicant: Bell Helicopter Textron Inc.
Inventor： Adam Bryant Anderson , Steven Ray Ivans , Jeremy Robert Chavez
Abstract: A pylon assembly for a tiltrotor aircraft includes a rotor assembly operable to rotate between a generally vertical orientation, in a VTOL flight mode, and a generally horizontal orientation, in a forward flight mode, and having an intermediate orientation therebetween, in a conversion flight mode. The rotor assembly includes a proprotor operable to produce a slipstream. A wing extension, positioned outboard of the rotor assembly, has a minimal dimension and an outboard end. A winglet is coupled to the outboard end of the wing extension and has a minimal dimension. The wing extension and the winglet are operable to rotate generally with the rotor assembly such that the minimal dimensions of the wing extension and the winglet remain in the slipstream of the proprotor.
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公开(公告)号：US20180251230A1
公开(公告)日：2018-09-06
申请号：US15913789
申请日：2018-03-06
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , James R. Williamson , Levi Bilbrey
IPC: B64D43/00 , G06T19/00 , G06F3/01 , G01C23/00 , G08G5/00 , B64C13/18 , B64C13/22 , A42B3/04 , A42B3/22 , A42B3/30
Abstract: The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.
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公开(公告)号：US10822108B2
公开(公告)日：2020-11-03
申请号：US15913789
申请日：2018-03-06
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , James R. Williamson , Levi Bilbrey
IPC: B64D43/00 , A42B3/30 , G06F3/01 , G01C23/00 , G08G5/00 , B64C13/18 , B64C13/22 , A42B3/04 , A42B3/22 , G06T19/00 , G02B27/01 , B64D11/06 , B64C13/04 , B64C1/06 , B64C1/18 , B64C1/40 , B64C13/10 , B64D11/00 , G06F3/044
Abstract: The present disclosure achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present disclosure includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.
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Patent Agency Ranking
公开(公告)号：US20190375506A1
公开(公告)日：2019-12-12
申请号：US16004159
申请日：2018-06-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , Brent Chadwick Ross
IPC: B64D7/06
Abstract: Embodiments are directed to an aircraft, such as a tiltrotor, having an internal payload storage area. A rotatable deployment system is mounted within the payload storage area. The rotatable deployment system comprises a frame that is configured to rotate between a stowed position and a deployment position. Two extendible arms are attached to the frame, wherein each extendible arm is configured to move in opposite directions between a retracted position and a plurality of extended positions. Each extendible arm has a fixed end and a moving end. A payload mounting point on each moving end. The payload mounting point allows a payload to pan and tilt in azimuth and elevation.
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公开(公告)号：US20190315448A1
公开(公告)日：2019-10-17
申请号：US15951539
申请日：2018-04-12
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , Brent Chadwick Ross
Abstract: Embodiments are directed to systems and methods for a sliding door in a pressurized aircraft. In one embodiment, an aircraft comprises a fuselage having a door opening, and a door configured to slide into the door opening from within the fuselage, the door held in a closed position in the door opening by excess air pressure within the fuselage during operation of the aircraft.
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公开(公告)号：US10793275B2
公开(公告)日：2020-10-06
申请号：US16004159
申请日：2018-06-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Jeremy Robert Chavez , Brent Chadwick Ross
Abstract: Embodiments are directed to an aircraft, such as a tiltrotor, having an internal payload storage area. A rotatable deployment system is mounted within the payload storage area. The rotatable deployment system comprises a frame that is configured to rotate between a stowed position and a deployment position. Two extendible arms are attached to the frame, wherein each extendible arm is configured to move in opposite directions between a retracted position and a plurality of extended positions. Each extendible arm has a fixed end and a moving end. A payload mounting point on each moving end. The payload mounting point allows a payload to pan and tilt in azimuth and elevation.
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公开(公告)号：US20200023946A1
公开(公告)日：2020-01-23
申请号：US16297617
申请日：2019-03-09
Applicant: Bell Helicopter Textron Inc.
Inventor： Adam Bryant Anderson , Steven Ray Ivans , Jeremy Robert Chavez
Abstract: A pylon assembly for a tiltrotor aircraft includes a rotor assembly rotatably coupled to a fixed pylon and operable to rotate between a vertical takeoff and landing orientation and a forward flight orientation. The rotor assembly includes a proprotor operable to produce a slipstream. A wing extension is rotatably disposed to the outboard end of the fixed pylon such that the rotor assembly and the wing extension are separated by at least a portion of the fixed pylon. The wing extension has a forward edge and an outboard end. A winglet is coupled to the outboard end of the wing extension and has a forward edge. The wing extension and the winglet are configured to rotate in synchrony with the rotor assembly such that the forward edges of the wing extension and the winglet remain in the slipstream of the proprotor.
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公开(公告)号：US20170316712A1
公开(公告)日：2017-11-02
申请号：US15375292
申请日：2016-12-12
Applicant: Bell Helicopter Textron, Inc.
Inventor： Steven Wayne Kihara , Jeremy Robert Chavez
Abstract: A control and simulation system (CSS) has a flight system configured to selectively provide flight mode of operation of an aircraft and a simulation system configured to selectively provide a simulation mode of operating the aircraft.
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