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公开(公告)号：US09096325B2
公开(公告)日：2015-08-04
申请号：US14082615
申请日：2013-11-18
Applicant: Bell Helicopter Textron Inc.
Inventor： Erik Oltheten , James M. McCollough , Peter F. Scheidler , Jeffery S. Greenwood
CPC classification number: B64D31/14 , B64D31/04 , B64D31/06 , F02C9/42 , F05D2220/329 , Y02T50/671
Abstract: According to one embodiment, a method of managing pilot and copilot control of engine power in an aircraft includes receiving, from a first pilot input device, a first signal representative of a pilot selection of an increase power position or a decrease power position and receiving, from a second pilot input device, a second signal representative of a pilot selection of an increase power position or a decrease power position. One of the first signal and the second signal is prioritized. An aircraft engine is then instructed to change power output based on the prioritized signal.
Abstract translation: 根据一个实施例，一种管理飞行器中的发动机功率的先导和副驾驶控制的方法包括从第一导频输入装置接收代表增加功率位置或减小功率位置的飞行员选择的第一信号， 来自第二导频输入装置的代表增加功率位置或减小功率位置的导频选择的第二信号。 第一个信号和第二个信号之一被优先排列。 然后指示飞机发动机基于优先化信号来改变功率输出。
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公开(公告)号：US08918234B2
公开(公告)日：2014-12-23
申请号：US13715277
申请日：2012-12-14
Applicant: Bell Helicopter Textron Inc.
Inventor： Charles E. Covington , Bradley Regnier , Robert Worsham , Troy S. Caudill , Thomas E. Archer, II , James M. McCollough
Abstract: According to one embodiment, a landing point indication system includes an image provider, a rotorcraft position provider, a pilot image generation system, and a display device. The image provider is operable to provide a visual representation of an area underneath a rotorcraft. The rotorcraft position provider is operable to provide information indicating a position of the rotorcraft. The pilot image generation system is operable to generate a supplemented visual representation. The supplemented visual representation includes the visual representation of the area underneath the aircraft and information indicating a position of the rotorcraft relative to the visual representation. The display device is operable to display the supplemented visual representation within the rotorcraft.
Abstract translation: 根据一个实施例，着陆点指示系统包括图像提供器，旋翼航空器位置提供器，导频图像生成系统和显示设备。 图像提供者可操作地提供旋翼飞机下面的区域的视觉表示。 旋翼航空器位置提供器可操作以提供指示旋翼航空器的位置的信息。 导频图像生成系统可操作以产生补充的视觉表示。 补充的视觉表示包括飞机下面的区域的视觉表示和指示旋翼航空器相对于视觉表示的位置的信息。 显示装置可操作以在旋翼航空器内显示补充的视觉表示。
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公开(公告)号：US09879824B2
公开(公告)日：2018-01-30
申请号：US13863126
申请日：2013-04-15
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： James M. McCollough , Ryan T. Ehinger , Troy Bunch
CPC classification number: F16N29/00 , B64C27/00 , B64D45/00 , G01M13/04 , G01N33/2858 , G01N33/2888
Abstract: A system and method to detect non-ferrous debris from a non-ferrous roller bearing element. The system includes a trap in fluid communication with a lubrication fluid of the non-ferrous bearing and a sensor operably associate with the trap. The method includes trapping the non-ferrous material debris in the lubrication fluid with the trap and triggering the sensor upon detection of the non-ferrous material debris trapped within the trap.
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公开(公告)号：US20150142215A1
公开(公告)日：2015-05-21
申请号：US14082615
申请日：2013-11-18
Applicant: Bell Helicopter Textron Inc.
Inventor： Erik Oltheten , James M. McCollough , Peter F. Scheidler , Jeffrey S. Greenwood
CPC classification number: B64D31/14 , B64D31/04 , B64D31/06 , F02C9/42 , F05D2220/329 , Y02T50/671
Abstract: According to one embodiment, a method of managing pilot and copilot control of engine power in an aircraft includes receiving, from a first pilot input device, a first signal representative of a pilot selection of an increase power position or a decrease power position and receiving, from a second pilot input device, a second signal representative of a pilot selection of an increase power position or a decrease power position. One of the first signal and the second signal is prioritized. An aircraft engine is then instructed to change power output based on the prioritized signal.
Abstract translation: 根据一个实施例，一种管理飞行器中的发动机功率的先导和副驾驶控制的方法包括从第一导频输入装置接收代表增加功率位置或减小功率位置的飞行员选择的第一信号， 来自第二导频输入装置的代表增加功率位置或减小功率位置的导频选择的第二信号。 第一个信号和第二个信号之一被优先排列。 然后指示飞机发动机基于优先化信号来改变功率输出。
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公开(公告)号：US08882024B1
公开(公告)日：2014-11-11
申请号：US13924990
申请日：2013-06-24
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Tommie L. Wood
IPC: B64C27/82
CPC classification number: B64C27/82 , B64C2027/8254 , B64C2027/8272
Abstract: According to one embodiment, a rotorcraft includes a main rotor system, an anti-torque rotor system, an anti-torque rotor enhancement system, and an anti-torque rudder system. The anti-torque rotor enhancement system includes an aerodynamic structure having an opening therethrough and a support structure coupling the aerodynamic structure to the body of the rotorcraft such that the opening is positioned proximate to a rotation path of the at least one anti-torque rotor blade. The anti-torque rudder system includes at least one rudder surface operable to provide a second force on the body in the direction of rotation of the at least one main rotor blade.
Abstract translation: 根据一个实施例，旋翼航空器包括主转子系统，抗扭矩转子系统，抗扭矩转子增强系统和抗扭矩舵系统。 抗扭矩转子增强系统包括具有穿过其中的开口的空气动力结构和将空气动力学结构联接到旋转器航空器的主体的支撑结构，使得开口定位成接近至少一个抗扭矩转子叶片的旋转路径 。 防扭矩舵系统包括至少一个方向舵表面，其可操作以在所述主体上沿所述至少一个主转子叶片的旋转方向提供第二力。
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Patent Agency Ranking
公开(公告)号：US20140305740A1
公开(公告)日：2014-10-16
申请号：US13863126
申请日：2013-04-15
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： James M. McCollough , Ryan T. Ehinger , Troy Bunch
CPC classification number: F16N29/00 , B64C27/00 , B64D45/00 , G01M13/04 , G01N33/2858 , G01N33/2888
Abstract: A system and method to detect non-ferrous debris from a non-ferrous roller bearing element. The system includes a trap in fluid communication with a lubrication fluid of the non-ferrous bearing and a sensor operably associate with the trap. The method includes trapping the non-ferrous material debris in the lubrication fluid with the trap and triggering the sensor upon detection of the non-ferrous material debris trapped within the trap.
Abstract translation: 一种从有色金属滚子轴承元件检测有色金属碎屑的系统和方法。 该系统包括与非铁轴承的润滑流体流体连通的捕集器和与捕获器可操作地相关联的传感器。 该方法包括在捕集器中捕获润滑流体中的有色金属碎屑，并且在检测到捕获在捕集阱内的有色金属碎屑时触发传感器。
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公开(公告)号：US20130289804A1
公开(公告)日：2013-10-31
申请号：US13868159
申请日：2013-04-23
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： Charles Eric Covington , Brian E. Tucker , Thomas B. Priest , David A. Platz , James M. McCollough
IPC: B64D45/00
CPC classification number: B64F5/0045 , B64D45/00 , B64F5/60 , G01C23/00 , G05D1/0005
Abstract: The present application relates to a system and method for providing real-time indications of economic impact of aircraft operations to an aircraft operator. The system and method allow the aircraft operator to reduce economic impact during flight of the aircraft. Such an analysis and cue to the aircraft operator allows the operator to make real-time changes during flight to reduce damage of life-limited aircraft components, thereby reducing the economic impact of aircraft operation that is directly associated with maintenance and component replacement. The system and method can also include pre-flight and post-flight analysis methods for reduction of economic impact of flight operations.
Abstract translation: 本申请涉及一种用于向航空器操作者提供飞机操作的经济影响的实时指示的系统和方法。 该系统和方法允许飞行员在飞机飞行期间减少经济影响。 对航空器操作者的这种分析和提示允许操作者在飞行中进行实时改变以减少对生命限制的飞行器部件的损坏，从而减少与维护和部件更换直接相关的飞机操作的经济影响。 该系统和方法还可以包括飞行前和飞行后分析方法，以减少飞行运行的经济影响。
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公开(公告)号：US09815553B2
公开(公告)日：2017-11-14
申请号：US13932407
申请日：2013-07-01
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Carlos A. Fenny
Abstract: According to some embodiments, a rotorcraft includes a secondary rotor control system located proximate to the empennage of the rotorcraft. The secondary rotor control system includes at least one hydraulic pump and at least one hydraulic actuator. The at least one hydraulic pump is located proximate to the empennage. The at least one hydraulic actuator is located proximate to the empennage and configured to adjust at least one operating characteristic of the at least one secondary rotor blade.
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公开(公告)号：US20150015039A1
公开(公告)日：2015-01-15
申请号：US14498675
申请日：2014-09-26
Applicant: Bell Helicopter Textron Inc.
Inventor： Albert G. Brand , John R. Wittmaak , James M. McCollough , James H. Harse , Richard H. Adams, JR.
CPC classification number: B60N2/0745 , B60N2/01 , B60N2/04 , B60N2/0702 , B60N2/075 , B60N2/08 , B60N2/0875 , B60N2/14 , B60N2/24 , B64D11/0689 , B64D11/0696 , B64D43/00
Abstract: A movable seat assembly for a vehicle comprises a predetermined path having an operational location at a first end and an ingress/egress location at a second end, and a seat that travels along the predetermined path between the operational location and the ingress/egress location, wherein the seat has an operational orientation at the operational location and an ingress/egress seat orientation at the ingress/egress location; the ingress/egress seat orientation being substantially angled relative to the operational seat orientation. Another moveable seat assembly for a vehicle comprises a predetermined path having an operational location at a first end, an ingress/egress location at a second end, and a standby location along the path there between; and a seat that travels along the predetermined path between the operational location, the standby location, and the ingress/egress location; wherein the position of the seat is adjustable at the operational location. Another moveable seat assembly for a vehicle comprises a seat coupled to and moveable along at least one track defining a predetermined path between an operational location and an ingress/egress location.
Abstract translation: 一种用于车辆的可移动座椅组件包括具有在第一端处的操作位置和在第二端处的入口/出口位置的预定路径以及沿着操作位置和入口/出口位置之间的预定路径行进的座椅， 其中所述座椅在所述操作位置处具有操作方向，并且所述入口/出口位置处的入口/出口座椅取向; 入口/出口座椅方向相对于操作座椅方向基本成角度。 用于车辆的另一可移动座椅组件包括具有在第一端处的操作位置，在第二端处的入口/出口位置以及沿着其间的路径的备用位置的预定路径; 以及在操作位置，待机位置和入口/出口位置之间沿着预定路径行进的座位; 其中所述座椅的位置在所述操作位置是可调节的。 用于车辆的另一可移动座椅组件包括座椅，该座椅沿着至少一个轨道连接并可移动，所述轨道在操作位置和入口/出口位置之间限定预定路径。
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20.发明申请公开(公告)号：US20150001337A1
公开(公告)日：2015-01-01
申请号：US13932407
申请日：2013-07-01
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Carlos A. Fenny
Abstract: According to some embodiments, a rotorcraft includes a secondary rotor control system located proximate to the empennage of the rotorcraft. The secondary rotor control system includes at least one hydraulic pump and at least one hydraulic actuator. The at least one hydraulic pump is located proximate to the empennage. The at least one hydraulic actuator is located proximate to the empennage and configured to adjust at least one operating characteristic of the at least one secondary rotor blade.
Abstract translation: 根据一些实施例，旋翼航空器包括位于旋翼航空器的尾翼附近的次级转子控制系统。 次级转子控制系统包括至少一个液压泵和至少一个液压致动器。 至少一个液压泵位于尾翼附近。 所述至少一个液压致动器位于所述尾翼附近并且被构造成调节所述至少一个次级转子叶片的至少一个操作特性。
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