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公开(公告)号：US20190315494A1
公开(公告)日：2019-10-17
申请号：US16182442
申请日：2018-11-06
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad R. Haugeberg , Bradley D. Linton
Abstract: A device to verify main rotor swashplate positioning includes an inner surface of a first section and a gradient surface of a second section. The gradient surface of the second section may have a plurality of graduation indications. In one implementation, the inner surface of the first section at least partially defines a travel arc that is parallel to and concentric with the inner surface. In such an implementation, the device may be configured to move along the travel arc as it rotates about a collective sleeve to contact a swashplate lug.
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公开(公告)号：US09056675B2
公开(公告)日：2015-06-16
申请号：US13736163
申请日：2013-01-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Travis L. Yates , Bradley D. Linton
CPC classification number: B64C27/56 , B64C13/04 , Y10T74/20612
Abstract: According to one embodiment, a control assembly includes a post, a grip, and a hand rest. The post has a top, a bottom, and a body joining the top to the bottom. The grip is positioned at least partially above the post and is movable along at least one arc. The hand rest is coupled to the top and comprises an upper surface having a profile corresponding to the at least one arc.
Abstract translation: 根据一个实施例，控制组件包括柱，手柄和扶手。 该柱具有顶部，底部和与顶部连接的底部。 手柄至少部分地定位在柱上方并且可沿着至少一个弧移动。 扶手连接到顶部并且包括具有对应于至少一个弧的轮廓的上表面。
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公开(公告)号：US20130209256A1
公开(公告)日：2013-08-15
申请号：US13736147
申请日：2013-01-08
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Travis L. Yates , Bradley D. Linton
IPC: F01D7/00
CPC classification number: F01D7/00 , B64C13/04 , B64C27/56 , B64D43/00 , G05G9/047 , G05G2009/04703
Abstract: According to one embodiment, a control assembly includes a first gimbal and a second gimbal. The first gimbal is rotatable about a first axis of rotation. The first gimbal comprises a first linkage attachment point offset from the first axis of rotation. The second gimbal is rotatably coupled to the first gimbal and rotatable relative to the first gimbal about a second axis of rotation. The second gimbal comprises a second linkage attachment point offset from the second axis of rotation and a control shaft attachment point.
Abstract translation: 根据一个实施例，控制组件包括第一万向架和第二万向架。 第一万向架可围绕第一旋转轴线旋转。 第一万向架包括从第一旋转轴线偏移的第一连杆附接点。 第二万向节可旋转地联接到第一万向架并且围绕第二旋转轴线相对于第一万向节可旋转。 第二万向架包括从第二旋转轴线偏移的第二连杆附接点和控制轴附接点。
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公开(公告)号：US08812177B2
公开(公告)日：2014-08-19
申请号：US13736156
申请日：2013-01-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Travis L. Yates , Bradley D. Linton
IPC: G01C23/00
Abstract: According to one embodiment, an integrated aircraft trim assembly features a shaft, a mechanical stop, a trim motor, a clutch, and a measurement device. The mechanical stop device is operable to at least partially prevent rotation of the shaft outside of an allowable range of motion. The trim motor has an output component in mechanical communication with the shaft. The clutch separates the trim motor from the shaft. The measurement device is proximate to the shaft and operable to measure a position of the shaft and communicate the measured position to a flight control computer operable to change a position of a flight control device.
Abstract translation: 根据一个实施例，集成飞行器装配组件具有轴，机械止动件，调整马达，离合器和测量装置。 机械停止装置可操作以至少部分地防止轴在允许的运动范围之外的旋转。 微调电机具有与轴机械连通的输出部件。 离合器将调整电机与轴分离。 测量装置靠近轴并且可操作以测量轴的位置并将测量位置传递到可操作以改变飞行控制装置的位置的飞行控制计算机。
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公开(公告)号：USD701486S1
公开(公告)日：2014-03-25
申请号：US29447393
申请日：2013-03-03
Applicant: Bell Helicopter Textron Inc.
Designer： Travis L. Yates , Bradley D. Linton , Chad R. Haugeberg
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Patent Agency Ranking
公开(公告)号：USD701161S1
公开(公告)日：2014-03-18
申请号：US29447394
申请日：2013-03-03
Applicant: Bell Helicopter Textron Inc.
Designer： Travis L. Yates , Bradley D. Linton , Chad R. Haugeberg
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公开(公告)号：US11040785B2
公开(公告)日：2021-06-22
申请号：US16183385
申请日：2018-11-07
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad R. Haugeberg , Bradley D. Linton
Abstract: A device to verify tail rotor cross-head positioning is disclosed. The device comprises a first portion and a second portion. The second portion may be adjoined to the first portion and comprises maximum and minimum surfaces configured to determine whether a yoke-measuring surface of a tail rotor yoke may be positioned between respective geometric planes of the maximum and minimum surfaces.
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公开(公告)号：US10967990B2
公开(公告)日：2021-04-06
申请号：US16182442
申请日：2018-11-06
Applicant: Bell Helicopter Textron Inc.
Inventor： Chad R. Haugeberg , Bradley D. Linton
Abstract: A device to verify main rotor swashplate positioning includes an inner surface of a first section and a gradient surface of a second section. The gradient surface of the second section may have a plurality of graduation indications. In one implementation, the inner surface of the first section at least partially defines a travel arc that is parallel to and concentric with the inner surface. In such an implementation, the device may be configured to move along the travel arc as it rotates about a collective sleeve to contact a swashplate lug.
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公开(公告)号：US09067672B2
公开(公告)日：2015-06-30
申请号：US13736135
申请日：2013-01-08
Applicant: Bell Helicopter Textron Inc.
Inventor： Travis L. Yates , Bradley D. Linton , Chad R. Haugeberg
Abstract: According to one embodiment, a control assembly includes a post, a grip, and a shaft. The post has a top, a bottom, and a body joining the top to the bottom. The shaft has a first end coupled proximate to the body below the top and a second end opposite the first end coupled to the grip. The shaft positions at least part of the grip directly over the top of the post.
Abstract translation: 根据一个实施例，控制组件包括柱，手柄和轴。 该柱具有顶部，底部和与顶部连接的底部。 轴具有在顶部下方靠近主体的第一端和与该把手相连的第一端相对的第二端。 轴将夹具的至少一部分直接定位在柱的顶部上方。
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公开(公告)号：USD701485S1
公开(公告)日：2014-03-25
申请号：US29447392
申请日：2013-03-03
Applicant: Bell Helicopter Textron Inc.
Designer： Travis L. Yates , Bradley D. Linton , Chad R. Haugeberg
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