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62. 发明专利

JPS6121600A Ground access alarm for aircraft 失效
标题翻译：飞机接地信号报警
公开(公告)号：JPS6121600A
公开(公告)日：1986-01-30
申请号：JP13924284
申请日：1984-07-06
申请人： Sundstrand Data Control
发明人： CHIYAARUZU DONARUDO BEITOMAN
IPC分类号： B64D45/04 , G01C5/00 , G01C21/00 , G01C21/20 , G01P3/62 , G05D1/06 , G08G5/02
CPC分类号： G01C5/005 , G01P3/62 , G05D1/0653

63. 发明授权

US09969486B1 Unmanned aerial vehicle heat sensor calibration 有权
公开(公告)号：US09969486B1
公开(公告)日：2018-05-15
申请号：US15188922
申请日：2016-06-21
申请人： Amazon Technologies, Inc.
发明人： Barry James O'Brien , Scott Michael Wilcox , Joshua John Watson
IPC分类号： B64C13/20 , G01J5/52 , G05D1/06 , B64C39/02 , B64D47/08 , G01C25/00 , G01K15/00 , G01K13/00 , G06K9/62
CPC分类号： B64C13/20 , B64C39/022 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/108 , B64C2201/128 , B64C2201/145 , B64D47/08 , G01C25/00 , G01J5/522 , G01K13/00 , G01K15/00 , G05D1/0653 , G06K9/6202 , G06T2207/10024 , G06T2207/10032
摘要： This disclosure describes systems, methods, and apparatus for automating the verification of aerial vehicle sensors as part of a pre-flight, flight departure, in-transit flight, and/or delivery destination calibration verification process. At different stages, aerial vehicle sensors may obtain sensor measurements about objects within an environment, the obtained measurements may be processed to determine information about the object, as presented in the measurements, and the processed information may be compared with the actual information about the object to determine a variation or difference between the information. If the variation is within a tolerance range, the sensor may be auto adjusted and operation of the aerial vehicle may continue. If the variation exceeds a correction range, flight of the aerial vehicle may be aborted and the aerial vehicle routed for a full sensor calibration.

64. 发明授权

US09638526B1 GPS carrier-phase based relative navigation 有权
公开(公告)号：US09638526B1
公开(公告)日：2017-05-02
申请号：US14499800
申请日：2014-09-29
申请人： Rockwell Collins, Inc.
发明人： Vladislav Gavrilets , Patrick Hwang , Gary McGraw
IPC分类号： G01C21/00 , G01C21/20 , G01S19/01 , G05D1/04 , G05D1/08
CPC分类号： G01C21/20 , G01S19/01 , G01S19/43 , G01S19/50 , G05D1/042 , G05D1/0653 , G05D1/0808
摘要： Systems and methods for navigation of a vehicle may carry out one or more operations including, but not limited to: obtaining coordinates of a vector connecting two points in space using carrier phase measurements from global navigation system satellites (GNSS); setting the vector as an intended path of a vehicle; storing carrier phase signals from a GNSS receiver received at a first position of the vehicle; receiving carrier phase signals from a GNSS receiver at a second position of the vehicle; and determining a position of the vehicle relative to the intended path from one or more carrier phase signals received at the second position and one or more stored carrier phase signals received at the first position.

65. 发明申请

US20160349759A1 TAKEOFF/LANDING TOUCHDOWN PROTECTION MANAGEMENT SYSTEM 有权
标题翻译： TAKEOFF / LANDING TOUCHDOWN保护管理系统
公开(公告)号：US20160349759A1
公开(公告)日：2016-12-01
申请号：US15168324
申请日：2016-05-31
申请人： TEXTRON INNNOVATIONS INC.
发明人： SHYHPYNG JACK SHUE
IPC分类号： G05D1/06 , B64D45/00 , B64C13/50
CPC分类号： B64C13/04 , B64C13/16 , B64C13/503 , B64C25/001 , B64C25/34 , B64C27/57 , B64C2025/325 , B64D45/00 , G05D1/0653 , G05D1/0669 , G05D1/0676 , G05D1/0858
摘要： An air/ground contact logic management system for use with fly-by-wire control systems in an aircraft. The system includes a first sensor configured to provide an output signal to determine when the aircraft is in a transition region. A logic management system is in communication with the first sensor and is configured to receive and process the output signal and classify a mode of the aircraft. A controller receives signal data from the logic management system and communicates with a control axis actuator to regulate a level of control authority provided to a pilot. The control authority is individually regulated within each integrator as a result of the individual landing gear states.
摘要翻译：一种用于飞行器中的线控控制系统的空气/地面接触逻辑管理系统。该系统包括被配置为提供输出信号以确定飞行器何时处于过渡区域中的第一传感器。逻辑管理系统与第一传感器通信并被配置为接收和处理输出信号并对飞行器的模式进行分类。控制器从逻辑管理系统接收信号数据，并与控制轴致动器进行通信，以调节提供给飞行员的控制权限级别。由于个别起落架状态，控制权由各个集成商单独监管。

66. 发明申请

US20150266590A1 SHORT LANDING WARNING 有权
标题翻译：短路警告
公开(公告)号：US20150266590A1
公开(公告)日：2015-09-24
申请号：US14218672
申请日：2014-03-18
申请人： The Boeing Company
发明人： Mark Hall Henderson
IPC分类号： B64D45/04
CPC分类号： B64D45/04 , B64D45/08 , G05D1/0607 , G05D1/0653 , G05D1/0676 , G08G5/0047 , G08G5/04 , G08G5/045
摘要： A method can include determining that an aircraft is on approach to a runway. The method can include determining a flight path vector (FPV) location of the aircraft based at least in part on a projected landing location with respect to the runway and determining a current airspeed of the aircraft. The method can also include performing at least one of the following: issuing a landing short alert to a pilot of the aircraft if the FPV location is at or before the runway threshold, issuing an airspeed caution alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is below a landing short envelope, and determining not to issue an alert if the FPV location is between the runway threshold and the target runway location and if the current airspeed is at or above the landing short envelope.
摘要翻译：一种方法可以包括确定飞机正在接近跑道。该方法可以包括至少部分地基于相对于跑道的预计着陆位置来确定飞行器的飞行路线向量（FPV）位置，并确定飞机的当前空速。该方法还可以包括执行以下中的至少一个：如果FPV位置在跑道阈值之前或之前，向飞机的飞行员发出着陆短警报，如果FPV位置在跑道阈值之间，则发出空速警告警报目标跑道位置以及当前空速是否低于着陆短信号，并且如果FPV位置在跑道阈值和目标跑道位置之间以及当前空速是否在着陆短路之上或之上，则确定不发出警报信封。

67. 发明申请

US20130092791A1 METHOD FOR A NOISE ABATEMENT PROCEDURE FOR AN AIRCRAFT 审中-公开
标题翻译：航空器噪声消除程序的方法
公开(公告)号：US20130092791A1
公开(公告)日：2013-04-18
申请号：US13276007
申请日：2011-10-18
申请人： Michael John Bakker , Joachim Karl Ulf Hochwarth , Sean Edward Flanary
发明人： Michael John Bakker , Joachim Karl Ulf Hochwarth , Sean Edward Flanary
IPC分类号： G05D1/00 , G10K11/00
CPC分类号： G05D1/0653 , G08G5/006
摘要： A method of reducing noise from an aircraft in a noise abatement zone during flight of the aircraft includes determining where the flight path of the aircraft will intersect the noise abatement zone and then operating the aircraft in a quieter manner when the aircraft is within the noise abatement zone.
摘要翻译：一种在飞行器飞行期间减少噪声消除区域中的飞机噪声的方法包括确定飞行器的飞行路径在噪声消减区域将与哪里相交，然后当飞行器处于噪声消除范围内时以更安静的方式操作飞行器区。

68. 发明授权

US08265807B2 Automatic takeoff and landing apparatus for aircraft, and methods for performing an automatic takeoff and an automatic landing of an aircraft 有权
标题翻译：用于飞机的自动起飞和着陆装置，以及执行飞行器的自动起飞和自动着陆的方法
公开(公告)号：US08265807B2
公开(公告)日：2012-09-11
申请号：US12954244
申请日：2010-11-24
申请人： Akihiro Yamane , Mitsuru Kono , Takahiro Kumamoto
发明人： Akihiro Yamane , Mitsuru Kono , Takahiro Kumamoto
IPC分类号： G06G7/70 , G05D1/04 , G05D1/08 , G05D1/10
CPC分类号： G05D1/0653 , B64C13/18
摘要： An automatic takeoff and landing apparatus for an aircraft for realizing a takeoff run and performing an ascending flight of the aircraft up to a target altitude at takeoff; and for realizing an approaching flight and performing a landing run of the aircraft at landing.
摘要翻译：一种飞机自动起飞和着陆装置，用于实现起飞运行并执行飞行器的升降飞行高达起飞目标高度; 并实现着陆飞行，并着陆着陆飞机着陆。

69. 发明授权

US08141823B2 Method for vertical takeoff from and landing on inclined surfaces 有权
标题翻译：在倾斜表面垂直起飞和着陆的方法
公开(公告)号：US08141823B2
公开(公告)日：2012-03-27
申请号：US12949410
申请日：2010-11-18
申请人： David C. Hursig , Steven D. Martinez
发明人： David C. Hursig , Steven D. Martinez
IPC分类号： G05D1/08
CPC分类号： B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/088 , B64C2201/108 , B64C2201/162 , B64D45/04 , G05D1/0653 , G05D1/0858
摘要： Takeoff and landing modes are added to a flight control system of a Vertical Take-Off and Landing (VTOL) Unmanned Air Vehicle (UAV). The takeoff and landing modes use data available to the flight control system and the VTOL UAV's existing control surfaces and throttle control. As a result, the VTOL UAV can takeoff from and land on inclined surfaces without the use of landing gear mechanisms designed to level the UAV on the inclined surfaces.
摘要翻译：起飞和着陆（VTOL）无人机（UAV）的飞行控制系统增加起飞和着陆模式。起飞和着陆模式使用可用于飞行控制系统和VTOL无人机现有控制面和节气门控制的数据。因此，VTOL无人机可以在倾斜的表面上起飞和着陆，而不需要使用设计成在倾斜表面上对无人机进行平坦化的起落架机构。

70. 发明授权

US07997528B2 Reducing runway requirement for aircraft 有权
标题翻译：降低飞机的跑道要求
公开(公告)号：US07997528B2
公开(公告)日：2011-08-16
申请号：US11653729
申请日：2007-01-16
申请人： James D. Lang
发明人： James D. Lang
IPC分类号： B64C19/00
CPC分类号： B64C23/06 , B64C19/00 , G05D1/0653 , Y02T50/162
摘要： Runway length requirement for take-off and landing of an aircraft is reduced by taking advantage of dynamic lift overshoot, and in some cases, dynamic stall. In take-off and landing, the angle of attack is rapidly increased so that the lift coefficient exceeds the maximum predicted by the steady flow lift curve. By increasing the angle of attack at an appropriate rate, the increased lift coefficient can be maintained, without loss of control, until the aircraft touches down in the case of a landing, or until the aircraft can begin a normal climb, in the case of take-off. A low aspect ratio lifting body is preferred because of its more gradual stall behavior, and the potential to use dynamic stall for further deceleration before touchdown. Vortex fences can be oscillated to delay the onset of stall, and, in cruise, to energize the boundary-layer and reduce drag and/or control roll and/or yaw.
摘要翻译：通过利用动力升降过冲减少飞机起飞和降落的跑道长度要求，在某些情况下，动态停止。起飞和着陆时，攻角迅速增加，使得升力系数超过稳定流量提升曲线预测的最大值。通过以适当的速率增加迎角，可以保持增加的升力系数，而不会失控，直到在着陆的情况下飞机接触下来，或直到飞机开始正常爬升为止脱掉。低纵横比提升体是优选的，因为它具有更加缓慢的失速行为，以及在达阵之前使用动态失速进一步减速的可能性。涡流围栏可以振荡以延迟失速的开始，并且在巡航中，激励边界层并减少拖动和/或控制滚动和/或偏航。

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