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公开(公告)号：US20200216170A1
公开(公告)日：2020-07-09
申请号：US16733806
申请日：2020-01-03
Applicant: Bell Textron Inc.
Inventor： Steven Loveland , Paul Charles Griffiths , Allen Brittain
Abstract: An aircraft landing gear assembly has a longitudinally elongated frame coupled to a lower portion of a fuselage of an aircraft, the frame being capable of supporting at least a portion of the weight of the aircraft. A fairing encloses substantially all of the frame. An optional integrated step can be carried by the frame, and a longitudinally elongated aperture would be formed in the fairing adjacent the step. The step allows a user to place a foot into the aperture and onto the step. An optional door can cover the aperture, and an optional secondary step can be carried by the door.
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公开(公告)号：US11597492B2
公开(公告)日：2023-03-07
申请号：US16733244
申请日：2020-01-03
Applicant: Bell Textron Inc.
Inventor： Paul Charles Griffiths , Bryan Sugg , Samuel Bryk
Abstract: Systems and methods include providing an aircraft with a fuselage having a sliding door system disposed on at least one side of the fuselage. The sliding door system includes a forward sliding door having an upper slide rail and a lower slide rail, a rearward sliding door having an upper slide rail and a lower slide rail, an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door, a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door, and a plurality of actuators coupled to each of the upper rail and the lower rail and configured to displace and retract the forward sliding door and the rearward sliding door linearly with respect to the fuselage.
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Patent Agency Ranking
公开(公告)号：US20200216160A1
公开(公告)日：2020-07-09
申请号：US16733244
申请日：2020-01-03
Applicant: Bell Textron Inc.
Inventor： Paul Charles Griffiths , Bryan Sugg , Samuel Bryk
Abstract: Systems and methods include providing an aircraft with a fuselage having a sliding door system disposed on at least one side of the fuselage. The sliding door system includes a forward sliding door having an upper slide rail and a lower slide rail, a rearward sliding door having an upper slide rail and a lower slide rail, an upper rail coupled to each of the upper slide rail of the forward sliding door and the upper slide rail of the rearward sliding door, a lower rail coupled to each of the lower slide rail of the forward sliding door and the lower slide rail of the rearward sliding door, and a plurality of actuators coupled to each of the upper rail and the lower rail and configured to displace and retract the forward sliding door and the rearward sliding door linearly with respect to the fuselage.
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公开(公告)号：US20220144406A1
公开(公告)日：2022-05-12
申请号：US17094180
申请日：2020-11-10
Applicant: Bell Textron Inc.
Inventor： Kirk Landon Groninga , Daniel Bryan Robertson , Matthew Edward Louis , Paul Charles Griffiths
Abstract: A vehicle has a pod carrier, a pod rotatably connected to the pod carrier, and an energy attenuating system (EAS) disposed between the pod and the pod carrier to attenuate forces associated with a deflection of the pod relative to the pod carrier. A method of operating an energy attenuating system (EAS) is provided for attenuating energy associated with movement between a pod and a pod carrier. The method includes providing a vehicle having a pod carrier and providing the pod carrier with an EAS configured in an undeflected state.
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公开(公告)号：US20200216161A1
公开(公告)日：2020-07-09
申请号：US16733240
申请日：2020-01-03
Applicant: Bell Textron Inc.
Inventor： Paul Charles Griffiths , Steven Loveland , Allen Brittain
IPC: B64C1/14
Abstract: A modular windshield has a central component and at least one side component. The central component is constructed of polycarbonate and the at least one side component is constructed of acrylic.
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公开(公告)号：US11993360B2
公开(公告)日：2024-05-28
申请号：US17094180
申请日：2020-11-10
Applicant: Bell Textron Inc.
Inventor： Kirk Landon Groninga , Daniel Bryan Robertson , Matthew Edward Louis , Paul Charles Griffiths
CPC classification number: B64C1/062 , B64D9/00 , B64F5/10 , B64C29/0016 , B64D25/00
Abstract: A vehicle has a pod carrier, a pod rotatably connected to the pod carrier, and an energy attenuating system (EAS) disposed between the pod and the pod carrier to attenuate forces associated with a deflection of the pod relative to the pod carrier. A method of operating an energy attenuating system (EAS) is provided for attenuating energy associated with movement between a pod and a pod carrier. The method includes providing a vehicle having a pod carrier and providing the pod carrier with an EAS configured in an undeflected state.
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公开(公告)号：US11352130B2
公开(公告)日：2022-06-07
申请号：US16733806
申请日：2020-01-03
Applicant: Bell Textron Inc.
Inventor： Steven Loveland , Paul Charles Griffiths , Allen Brittain
Abstract: An aircraft landing gear assembly has a longitudinally elongated frame coupled to a lower portion of a fuselage of an aircraft, the frame being capable of supporting at least a portion of the weight of the aircraft. A fairing encloses substantially all of the frame. An optional integrated step can be carried by the frame, and a longitudinally elongated aperture would be formed in the fairing adjacent the step. The step allows a user to place a foot into the aperture and onto the step. An optional door can cover the aperture, and an optional secondary step can be carried by the door.
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