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公开(公告)号：US20230067093A1
公开(公告)日：2023-03-02
申请号：US17410442
申请日：2021-08-24
Applicant: Bell Textron Inc.
Inventor： Andrew Maresh , Kyle Cravener
Abstract: Disclosed is a blade lock assembly, which may include a drag brace coupled to a fold crank assembly and to a rotary wing blade and may further include an actuator assembly configured to be coupled to a rotary wing cuff. The actuator assembly may include an actuator pin housing, an actuation pin at least partially sheathed by the actuator pin housing, and an actuator configured to extend and retract the actuation pin away from and toward the actuator pin housing.
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公开(公告)号：US10994837B1
公开(公告)日：2021-05-04
申请号：US16655855
申请日：2019-10-17
Applicant: Bell Textron Inc.
Inventor： Kyle Thomas Cravener , Andrew Maresh , Mark Adam Wiinikka
Abstract: An exemplary pitch lock for a tiltrotor aircraft to enable and disable a pitching degree of freedom of a rotor blade assembly includes a first tab coupled to a blade stop assembly, the first tab having a first ramp surface, a second tab coupled to a blade cuff, the second tab having a second ramp surface, a hasp having a central opening to receive the first and the second tab and rollers rotatably coupled to the hasp on opposite sides of the central opening, where the rollers engage the first and second ramp surfaces and retain the first and the second tabs in the central opening.
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公开(公告)号：US12162594B2
公开(公告)日：2024-12-10
申请号：US17410442
申请日：2021-08-24
Applicant: Bell Textron Inc.
Inventor： Andrew Maresh , Kyle Cravener
Abstract: Disclosed is a blade lock assembly, which may include a drag brace coupled to a fold crank assembly and to a rotary wing blade and may further include an actuator assembly configured to be coupled to a rotary wing cuff. The actuator assembly may include an actuator pin housing, an actuation pin at least partially sheathed by the actuator pin housing, and an actuator configured to extend and retract the actuation pin away from and toward the actuator pin housing.
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公开(公告)号：US11535370B2
公开(公告)日：2022-12-27
申请号：US16599471
申请日：2019-10-11
Applicant: Bell Textron Inc.
Inventor： Kyle Thomas Cravener , Andrew Maresh
Abstract: An exemplary blade lock for a tiltrotor aircraft to enable and disable a folding degree of freedom and a pitching degree of freedom of a rotor blade assembly includes a link pivotally connected to a lever and a bellcrank, where the link is in a center position when the lever is in a locked position disabling the folding degree of freedom and the lever is secured in the locked position when the link is positioned in an over-center position.
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Patent Agency Ranking
公开(公告)号：US11059566B2
公开(公告)日：2021-07-13
申请号：US16590618
申请日：2019-10-02
Applicant: Bell Textron Inc.
Inventor： Christopher Edward Foskey , Andrew Maresh
Abstract: An exemplary proprotor blade assembly includes a structural skin extending spanwise from a root to a tip and along a chord from leading edge to a trailing edge and a structural core positioned inside of the structural skin, the structural skin comprising hex-shaped structures oriented normal to the structural skin.
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公开(公告)号：US10526068B2
公开(公告)日：2020-01-07
申请号：US15428687
申请日：2017-02-09
Applicant: Bell Textron Inc.
Inventor： Troy Cyril Schank , Carlos Alexander Fenny , Andrew Maresh , Chyau-Song Tzeng
Abstract: A mechanism for transitioning a tiltrotor aircraft between rotary and non rotary flight modes. The mechanism includes a gimbal lock positioned about a mast that is operable to selectively enable and disable a gimballing degree of freedom of a rotor assembly relative to the mast. A blade stop assembly, positioned about the mast, includes a plurality of arms having a radially contracted orientation and a radially extended orientation. A blade lock assembly is operably associated with each rotor blade assembly. Each blade lock assembly is operable to selectively enable and disable a folding degree of freedom and a pitching degree of freedom of the respective rotor blade assembly. A swash plate is operable to change the pitch of the rotor blade assemblies in the rotary flight mode and fold the rotor blade assemblies in the non rotary flight mode.
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公开(公告)号：US11142300B2
公开(公告)日：2021-10-12
申请号：US16655400
申请日：2019-10-17
Applicant: Bell Textron Inc.
Inventor： Kyle Thomas Cravener , Andrew Maresh , Chyausong Tzeng
Abstract: An exemplary length adjustable link includes a tube having an internal bore and internal surface, a first rod end having a first shaft disposed in a first end of the internal bore, a second rod end having a second shaft disposed in a second end of the internal bore, and a member threadably connecting the first rod end to the second rod end.
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公开(公告)号：US11052993B2
公开(公告)日：2021-07-06
申请号：US16599483
申请日：2019-10-11
Applicant: Bell Textron Inc.
Inventor： Kyle Thomas Cravener , Christopher Edward Foskey , Andrew Maresh
IPC: B64C27/57 , F16F3/02 , B64C11/28 , B64C29/00 , B64C27/80 , B64C27/605 , B64C11/38 , B64C27/59 , B64C11/32 , B64C27/64
Abstract: An exemplary spring-loaded link for an aircraft including a spring interposed between a first and a second rod, the spring, when compressed, urging the first rod and the second rod away from each other.
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公开(公告)号：US11814153B2
公开(公告)日：2023-11-14
申请号：US17552052
申请日：2021-12-15
Applicant: Bell Textron Inc.
Inventor： Kyle Thomas Cravener , Andrew Maresh , Jonathan Andrew Knoll
CPC classification number: B64C11/28 , B64C11/04 , B64C27/28 , B64C29/0033
Abstract: A system for retaining a folded proprotor blade in flight. The system includes a mounting plate, a first arm coupled to the mounting plate at an acute angle relative to the mounting plate, and a first deformable pad affixed to the first arm and adapted to contact the folded proprotor blade.
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