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公开(公告)号：US09248759B2
公开(公告)日：2016-02-02
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.
IPC: B64D11/06 , B60N2/06 , B60N2/14 , B60N2/07 , B64D43/00 , B60N2/075 , B60N2/08 , B60N2/24 , B60N2/01 , B60N2/04
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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公开(公告)号：US09899980B2
公开(公告)日：2018-02-20
申请号：US15426085
申请日：2017-02-07
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Thomas W. Brooks , David Steinhoff , Ottis Lynn Morgan
CPC classification number: H03G7/004 , B64D47/00 , H03G3/32 , H04R3/00 , H04R2430/01 , H04R2499/13
Abstract: A method of controlling an audio system includes generating a situation response model for a situation parameter, determining a situation parameter value, and at least one of (1) providing an audio system output as a function of the situation response model and the situation parameter value and (2) receiving an audio system input as a function of the situation response model and the situation parameter value.
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公开(公告)号：US09676476B2
公开(公告)日：2017-06-13
申请号：US14589548
申请日：2015-01-05
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , William A. Amante
CPC classification number: B64C25/52 , B64C2025/325
Abstract: A lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a structure coupling mechanism; wherein the body prevents friction-related damage to the structure. Another lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material selected from the group consisting of: a polyamide or polyimide impregnated carbon fiber layup, a peek or PEI injection mold with carbon fiber, compression molded carbon fiber or fiberglass, a resin infusion with carbon fiber preform fabric, a fiber reinforced thermoset, acetal resin, machined acetal or thermoplastic, thermosetting plastic, or a metal-matrix composite; wherein the body prevents friction-related damage to a structure. Another lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a shear-bearing mechanism; wherein the shear-bearing mechanism directs shear forces away from the body; and wherein the body prevents friction-related damage to the structure.
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公开(公告)号：US20140374534A1
公开(公告)日：2014-12-25
申请号：US13925008
申请日：2013-06-24
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Carlos A. Fenny
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 rudder system, and an anti-torque control system. 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. The anti-torque control system is operable to receive a request to change an amount of anti-torque force applied to the body, compare a rotorcraft performance parameter to a threshold value, instruct one of the anti-torque rotor system or the anti-torque rudder system to change the amount of the first force if the rotorcraft performance parameter is less than the threshold value, and, if the rotorcraft performance parameter is greater than the threshold value, instruct the other of the anti-torque rotor system or the anti-torque rudder system to change the amount of the second force.
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，抗扭矩舵系统和抗扭矩控制系统。 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。 抗扭矩控制系统可操作以接收改变施加到车身的抗扭矩力的量的请求，将旋翼航空器的性能参数与阈值进行比较，指示抗扭矩转子系统或抗扭矩 方向舵系统，如果旋翼航空器的性能参数小于阈值，则改变第一力的量，并且如果旋翼航空器的性能参数大于阈值，则指示另一个抗扭矩转子系统或抗扭矩转子系统， 扭矩舵系统改变第二力的量。
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公开(公告)号：US20140233759A1
公开(公告)日：2014-08-21
申请号：US13771535
申请日：2013-02-20
Applicant: BELL HELICOPTER TEXTRON INC.
Inventor： James M. McCollough , Tom Brooks , David Steinhoff , Lynn Morgan
IPC: H03G3/20
CPC classification number: H03G7/004 , B64D47/00 , H03G3/32 , H04R3/00 , H04R2430/01 , H04R2499/13
Abstract: A method of controlling an audio system includes generating a situation response model for a situation parameter, determining a situation parameter value, and at least one of (1) providing an audio system output as a function of the situation response model and the situation parameter value and (2) receiving an audio system input as a function of the situation response model and the situation parameter value.
Abstract translation: 控制音频系统的方法包括：生成状况参数的状况响应模型，确定情况参数值，以及（1）根据状况响应模型和状况参数值提供音频系统输出中的至少一个 和（2）接收作为状况响应模型和状况参数值的函数的音频系统输入。
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Patent Agency Ranking
公开(公告)号：US20140081484A1
公开(公告)日：2014-03-20
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
IPC: G08G5/02
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：US20170149402A1
公开(公告)日：2017-05-25
申请号：US15426085
申请日：2017-02-07
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Tom Brooks , David Steinhoff , Lynn Morgan
CPC classification number: H03G7/004 , B64D47/00 , H03G3/32 , H04R3/00 , H04R2430/01 , H04R2499/13
Abstract: A method of controlling an audio system includes generating a situation response model for a situation parameter, determining a situation parameter value, and at least one of (1) providing an audio system output as a function of the situation response model and the situation parameter value and (2) receiving an audio system input as a function of the situation response model and the situation parameter value.
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公开(公告)号：US09584086B2
公开(公告)日：2017-02-28
申请号：US13771535
申请日：2013-02-20
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , Tom Brooks , David Steinhoff , Lynn Morgan
CPC classification number: H03G7/004 , B64D47/00 , H03G3/32 , H04R3/00 , H04R2430/01 , H04R2499/13
Abstract: A method of controlling an audio system includes generating a situation response model for a situation parameter, determining a situation parameter value, and at least one of (1) providing an audio system output as a function of the situation response model and the situation parameter value and (2) receiving an audio system input as a function of the situation response model and the situation parameter value.
Abstract translation: 控制音频系统的方法包括：生成状况参数的状况响应模型，确定情况参数值，以及（1）根据状况响应模型和状况参数值提供音频系统输出中的至少一个 和（2）接收作为状况响应模型和状况参数值的函数的音频系统输入。
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公开(公告)号：US20150336661A1
公开(公告)日：2015-11-26
申请号：US14589548
申请日：2015-01-05
Applicant: Bell Helicopter Textron Inc.
Inventor： James M. McCollough , William A. Amante
IPC: B64C25/52
CPC classification number: B64C25/52 , B64C2025/325
Abstract: A lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a structure coupling mechanism; wherein the body prevents friction-related damage to the structure. Another lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material selected from the group consisting of: a polyamide or polyimide impregnated carbon fiber layup, a peek or PEI injection mold with carbon fiber, compression molded carbon fiber or fiberglass, a resin infusion with carbon fiber preform fabric, a fiber reinforced thermoset, acetal resin, machined acetal or thermoplastic, thermosetting plastic, or a metal-matrix composite; wherein the body prevents friction-related damage to a structure. Another lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a shear-bearing mechanism; wherein the shear-bearing mechanism directs shear forces away from the body; and wherein the body prevents friction-related damage to the structure.
Abstract translation: 一种轻质滑靴组件包括耐磨，非金属或部分金属材料的主体; 和结构联结机构; 其中所述主体防止与所述结构的摩擦相关的损坏。 另一个轻质的滑靴组件包括耐磨，非金属或部分金属材料的主体，其选自：聚酰胺或聚酰亚胺浸渍的碳纤维叠层，具有碳纤维的偷窥或PEI注射模具，压缩模制的碳纤维或 玻璃纤维，具有碳纤维预成型织物的树脂浸渍，纤维增强热固性树脂，缩醛树脂，加工缩醛或热塑性塑料，热固性塑料或金属基质复合材料; 其中所述主体防止与结构的摩擦相关的损坏。 另一个轻质的滑靴组件包括耐磨，非金属或部分金属材料的主体; 和剪切承载机构; 其中所述剪切承载机构将剪切力引导离开所述主体; 并且其中所述主体防止与所述结构的摩擦相关的损坏。
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公开(公告)号：US09156567B2
公开(公告)日：2015-10-13
申请号：US14338944
申请日：2014-07-23
Applicant: Bell Helicopter Textron Inc.
Inventor： Charles Eric Covington , Brian E. Tucker , Thomas B. Priest , David A. Platz , James M. McCollough
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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