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81. 发明授权

US08886372B2 Flight deck touch-sensitive hardware controls 有权
标题翻译：飞行甲板触摸屏硬件控制
公开(公告)号：US08886372B2
公开(公告)日：2014-11-11
申请号：US13606082
申请日：2012-09-07
申请人： Mark Ivan Nikolic , Stephen Minarsch
发明人： Mark Ivan Nikolic , Stephen Minarsch
IPC分类号： B64C13/04 , G08B21/00 , G06F3/00 , G01C23/00
CPC分类号： G06F3/0416 , G01C23/00 , G01C23/005 , G05D1/00 , G06F3/00 , G06F3/0488
摘要： Touch or proximity sensors are integrated into control devices such as knobs, dials or wheels incorporated in a user control panel. A control output processor detects whether any of the sensors are outputting signals indicating that a control device is being touched (or nearly touched) by a user. The control output processor causes an associated display area to be highlighted or otherwise modified on a display screen to indicate to the user which control device is being touched. This feature allows for “no-look” interaction with control panels, and keeps the user's eyes focused on the relevant displays where the control devices produce effects. This allows users to preview and verify that the correct control device is being manipulated prior to taking any (potentially erroneous) control actions.
摘要翻译：触摸或接近传感器集成到控制设备中，例如嵌入用户控制面板中的旋钮，刻度盘或轮。控制输出处理器检测是否有任何传感器正在输出指示控制设备被用户触摸（或几乎被触摸）的信号。控制输出处理器使相关联的显示区域在显示屏幕上被突出显示或以其他方式修改，以向用户指示正在触摸哪个控制装置。该功能允许与控制面板进行“无外观”交互，并将用户的眼睛保持在控制设备产生效果的相关显示器上。这允许用户在采取任何（潜在的错误）控制动作之前，预览和验证正在操纵正确的控制设备。

82. 发明授权

US08870125B2 Trailing edge split flap with pneumatic actuation 有权
标题翻译：具有气动启动功能的后缘分离式皮瓣
公开(公告)号：US08870125B2
公开(公告)日：2014-10-28
申请号：US13187634
申请日：2011-07-21
申请人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
发明人： Michael A. Balzer , Gregory M. Santini , Michael K. Klein
IPC分类号： B64C3/50 , B64C9/16
CPC分类号： B64C9/16 , B64C3/46 , Y02T50/14 , Y02T50/32 , Y02T50/44
摘要： A system for pneumatically actuating a split flap hingedly mounted near or at a trailing edge of an airfoil. The system includes a bladder system disposed between the split flap and the upper surface of the airfoil. The split flap is a small-chord (usually 1-3% of total wing chord) long-span lower panel which separates from the airfoil trailing edge by means of a hinge or a flexible lower skin. Deployment of the split flap is actuated pneumatically by the inflatable bladder system. The split flap may exist at a fixed wing trailing edge, a moving flap trailing edge, or an empennage trailing edge. The pneumatic bladder provides distributed force to extend and retract the split flap. This pneumatic approach eliminates extra drag, reduces cost and weight, and lessens flutter concerns.
摘要翻译：一种用于气动地致动分开的翼片的系统，其铰接地安装在翼型件的后缘附近或其后缘。该系统包括设置在分裂翼片和翼型件的上表面之间的气囊系统。襟翼是一个小和弦（通常是总翼弦的1-3％）长跨度下面板，通过铰链或柔性下皮肤与翼型后缘分离。通过可充气膀胱系统气动地驱动分裂瓣的部署。分裂瓣可以存在于固定的翼缘后缘，移动的翼片后缘或尾翼的后缘。气动气囊提供分布的力以延伸和缩回分裂瓣。这种气动方式消除了额外的阻力，降低了成本和重量，并减轻了颤抖的担忧。

83. 发明授权

US08860234B2 Systems and methods for harvesting vibrational energy from vehicles 有权
标题翻译：从车辆收获振动能的系统和方法
公开(公告)号：US08860234B2
公开(公告)日：2014-10-14
申请号：US12983749
申请日：2011-01-03
申请人： Herbert Hoffman , Eric Hofbeck , Alex Lin
发明人： Herbert Hoffman , Eric Hofbeck , Alex Lin
IPC分类号： F02B63/04 , F03B13/10
CPC分类号： H02N2/188 , B64D41/00 , F03G7/08 , Y02T50/53
摘要： Disclosed are methods, systems and apparatuses for harvesting vibrational energy from vehicles, as well as methods for locating vibrational energy on a vehicle. One harvesting apparatus comprises a vibrational energy harvester coupled to a substantially maximal vibrational displacement node of the structural element of a vehicle, and tuned to a frequency of vibration of the maximal vibrational displacement node. The harvester may be one of a variety of harvesting devices, such as piezoelectric devices. Methods are also provided to locate structural elements which are appropriate for vibrational energy harvesting.
摘要翻译：公开了用于从车辆收获振动能的方法，系统和装置，以及用于在车辆上定位振动能的方法。一种收获装置包括耦合到车辆的结构元件的基本上最大的振动位移节点并被调谐到最大振动位移节点的振动频率的振动能量收集器。收割机可以是各种收获装置之一，例如压电装置。还提供了用于定位适于振动能量收集的结构元件的方法。

84. 发明授权

US08834360B2 Laryngoscope 有权
标题翻译：喉镜
公开(公告)号：US08834360B2
公开(公告)日：2014-09-16
申请号：US13264471
申请日：2010-03-25
申请人： Marko Plevnik , Brian Gough
发明人： Marko Plevnik , Brian Gough
IPC分类号： A61B1/267 , A61B1/00
CPC分类号： A61B1/267 , A61B1/00052 , A61B1/00103
摘要： A laryngoscope comprising a handle, a blade holding element, a releasable blade and releasable attachment means to attach the blade to the blade holding element, and handle and a blade for such a laryngoscope.
摘要翻译：一种喉镜，其包括手柄，刀片保持元件，可释放刀片和将刀片附接到刀片保持元件的可释放附接装置，以及用于这种喉镜的手柄和刀片。

85. 发明授权

US08786467B2 Methods and systems for filtering traffic information for display 有权
标题翻译：用于过滤交通信息进行显示的方法和系统
公开(公告)号：US08786467B2
公开(公告)日：2014-07-22
申请号：US13051146
申请日：2011-03-18
申请人： Samuel T. Clark , Roglenda R. Bowe , Stephen Bernard Ortman , Jean Marie Crane
发明人： Samuel T. Clark , Roglenda R. Bowe , Stephen Bernard Ortman , Jean Marie Crane
IPC分类号： G08G5/00 , G01C21/00 , G06G7/76 , G01S13/00
CPC分类号： G08G5/0078 , G01C23/00 , G08G5/0021 , G08G5/065
摘要： A method and a system for displaying an airport or runway moving map with traffic information on a display screen in the cockpit or flight deck of an aircraft. Symbology representing surface and near-surface aircraft and surface vehicle traffic and associated traffic data are filtered to prevent or limit clutter on the display screen. Traffic symbology is automatically and manually filtered to display only relevant traffic. Traffic data is selectively displayed and displayed as/when relevant or needed. The displayed traffic information may be derived from automatic dependent surveillance-broadcast, traffic information system-broadcast, automatic dependent surveillance-rebroadcast, traffic collision avoidance system or other source.
摘要翻译：一种用于在飞机的驾驶舱或飞行甲板中的显示屏幕上显示具有交通信息的机场或跑道移动地图的方法和系统。表示表面和近地面飞机和地面车辆交通流量及相关交通数据的符号系统被过滤，以防止或限制显示屏幕上的杂波。自动和手动过滤流量符号系统，仅显示相关流量。有选择地显示和显示交通数据，当有关或需要时显示。所显示的交通信息可以从自动依赖监视广播，交通信息系统广播，自动依赖监视转播，交通冲突避免系统或其他来源获得。

86. 发明授权

US08756037B2 Curved fiber paths for composite laminates 有权
标题翻译：复合层压板的弯曲纤维路径
公开(公告)号：US08756037B2
公开(公告)日：2014-06-17
申请号：US13164701
申请日：2011-06-20
申请人： Mostafa Rassaian , Matthew Todd Grimshaw , Thomas A. Grandine , Matthew Steven Patterson , Adriana Willempje Blom
发明人： Mostafa Rassaian , Matthew Todd Grimshaw , Thomas A. Grandine , Matthew Steven Patterson , Adriana Willempje Blom
IPC分类号： G06F17/50
CPC分类号： G06F17/50 , G06F17/5018 , G06F17/5095
摘要： A computational optimization process uses the variable stiffness performance of composite laminates attributed to steered fiber to guide the design of stream functions describing the fibers to build it. This design process combines a finite element-based analysis tool, failure criteria and geometry optimization to determine steered angles associated with stream functions by an optimization program to meet target performance requirements, e.g., load condition(s), and failure criteria for quasi-static or dynamic events. The fiber angle distribution and thickness buildup are computed based on the stream function. The simulated structure is analyzed using finite element analysis. The disclosed process allows the designer to impose manufacturing constraints such as fiber steering radius.
摘要翻译：计算优化过程使用归因于转向光纤的复合层压板的可变刚度性能来引导描述纤维的流功能的设计来构建它。该设计过程结合了基于有限元的分析工具，故障标准和几何优化，以通过优化程序确定与流功能相关的转向角度，以满足目标性能要求，例如负载条件和准静态故障标准或动态事件。基于流函数计算光纤角度分布和厚度累积。使用有限元分析对模拟结构进行分析。所公开的过程允许设计者施加诸如纤维转向半径的制造约束。

87. 发明授权

US08746616B2 Mid-wing multi-deck airplane 有权
标题翻译：中翼多层飞机
公开(公告)号：US08746616B2
公开(公告)日：2014-06-10
申请号：US13276357
申请日：2011-10-19
申请人： Sergey D. Barmichev , Mithra M. K. V. Sandrithi , Kevin M. Retz
发明人： Sergey D. Barmichev , Mithra M. K. V. Sandrithi , Kevin M. Retz
IPC分类号： B64C25/14 , B64C25/20
CPC分类号： B64D11/06 , B64C1/10 , B64C1/26 , B64C2001/0027 , B64C2001/0045 , B64C2025/125 , Y02T50/12 , Y02T50/46
摘要： An airplane comprises a twin-deck fuselage in which an upper deck support structure is utilized for carry-through of a mid-mount main wing box. The main landing gear of the airplane is mounted to the fuselage and is stowed in a non-pressurized area below the main wing box (enabled due to an optimized wing box geometry). A pressurized passageway/cargo/galley complex separates the main landing gear box and the main wing box. The upper deck is continuous, while the lower deck is separated by the wheel wells into two distinct fore and aft areas (for either cargo or passengers). The airplane further comprises an integrated vertical fin and an aft-extended pressurized deck area for reduced double-deck wetted area. More specifically, the double-deck pressurized fuselage structure is extended to form a blending structure to which a structural box of the vertical fin is attached.
摘要翻译：一架飞机包括一个双层机身，其中上甲板支撑结构用于中档安装的主翼箱的穿通。飞机的主起落架安装在机身上，并存放在主机箱下方的非加压区域（由于优化的机翼箱几何形状而启用）。加压通道/货物/厨房复合体分离主起落架和主翼箱。上甲板是连续的，而下甲板由轮井分隔成两个不同的前后区域（货物或乘客）。飞机还包括集成的垂直翼片和用于减小双层接液面积的后延伸的加压甲板区域。更具体地，双层加压机身结构被延伸以形成连接垂直翅片的结构箱的混合结构。

88. 发明授权

US08740139B1 Leading edge snag for exposed propeller engine installation 有权
标题翻译：暴露螺旋桨发动机安装的前沿障碍
公开(公告)号：US08740139B1
公开(公告)日：2014-06-03
申请号：US13453218
申请日：2012-04-23
申请人： Marcus A. Dunavan
发明人： Marcus A. Dunavan
IPC分类号： B64D27/00
CPC分类号： B64D27/12 , B64C3/10 , B64D2027/005 , Y02T50/12 , Y02T50/44 , Y02T50/66
摘要： An airplane powered by exposed propeller engines has a swept wing configuration comprising a leading edge snag coincident with the exposed propeller engine mount. The portion of the leading edge disposed inboard of the exposed propeller engine is offset in an aftwise direction relative to the outboard portion of the leading edge. As a result of this construction, the point of closest approach of the blades of the exposed propeller engines is moved aft, allowing for a more compact engine installation.
摘要翻译：由暴露的螺旋桨发动机驱动的飞机具有包括与暴露的螺旋桨发动机支架重合的前缘狭槽的扫掠翼结构。设置在暴露的螺旋桨发动机内侧的前缘的部分相对于前缘的外侧部分沿前后方向偏移。作为这种结构的结果，暴露的螺旋桨发动机的叶片的最接近的点被移动到后面，允许更紧凑的发动机安装。

89. 发明授权

US08630790B1 Systems and methods for amalgamating flight information 有权
标题翻译：合并航班信息的系统和方法
公开(公告)号：US08630790B1
公开(公告)日：2014-01-14
申请号：US13251406
申请日：2011-10-03
申请人： Louis J. Bailey , Ryan D. Hale
发明人： Louis J. Bailey , Ryan D. Hale
IPC分类号： G06F19/00
CPC分类号： G08G5/0039 , G08G5/0013
摘要： Systems and methods for receiving flight messages relating to a particular flight from multiple sources and processing information in those flight messages to create a single representation of an updated current and intended trajectory of such flight. Preferably, the system comprises one or more processors for performing the following operations: determining which flight message is the most recent; determining which flight messages are relevant; authenticating and processing proposed updates; and merging information contained in the flight messages to create a single representation of one or both of current or intended flight information.
摘要翻译：用于从多个源接收与特定飞行有关的飞行消息的系统和方法，并且处理那些飞行消息中的信息以创建这种飞行的更新的当前和预期轨迹的单个表示。优选地，该系统包括用于执行以下操作的一个或多个处理器：确定哪个飞行消息是最近的; 确定哪些航班信息是相关的; 认证和处理提出的更新; 并且合并包含在飞行消息中的信息以创建当前或预期航班信息中的一个或两个的单个表示。

90. 发明授权

US08622350B1 Compound leading edge device for aircraft 有权
标题翻译：复合的飞机前沿装置
公开(公告)号：US08622350B1
公开(公告)日：2014-01-07
申请号：US13295131
申请日：2011-11-14
申请人： Robert Hoffenberg
发明人： Robert Hoffenberg
IPC分类号： B64C3/50
CPC分类号： B64C9/26 , Y02T50/32
摘要： A small secondary leading edge device, called a compound Krueger vane, works in parallel with a primary device (e.g., a Krueger flap) to delay flow separation on an aircraft wing. The compound Krueger vane is deployed behind a gapped Krueger flap to turn flow ahead of the wing attachment region on the underside of the wing. The compound Krueger vane turns flow that moves forward from the wing lower surface attachment region toward the leading edge of the wing, thereby delaying flow separation on the aircraft wing.
摘要翻译：称为复合Krueger叶片的小型二次前缘装置与主要装置（例如Krueger翼片）平行地工作，以延迟飞机机翼上的流动分离。复合Krueger叶片部署在间隙的Krueger翼片后面，使其在机翼下侧的翼连接区域前方流动。复合式克鲁格叶片使翼片下表面附着区向前移动，从而延缓飞机机翼上的流动分离。

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