公开(公告)号：US20160185436A1

公开(公告)日：2016-06-30

申请号：US14293250

申请日：2014-06-02

申请人： Bell Helicopter Textron Inc.

发明人： John R. Wittmaak, JR. ,  Philip J. Hannan ,  Maxx S. Lucas ,  Chandrashekhar Tiwari

IPC分类号： B64C1/06 ,  B64C27/04

CPC分类号： B64C1/06 ,  B64C27/006 ,  B64C27/04 ,  B64D45/00 ,  B64D2045/0095

摘要： In some embodiments, an aircraft includes a structural assembly, a skin, and a snubber. The structural assembly comprises a first rigid element and a second rigid element. The first and second rigid elements are separated from each over by a void. The skin is disposed proximate to the structural assembly and adjacent to the void such that the skin would deflect into the void in response to an impact force received by the skin. The snubber is disposed in the void between the first and second rigid elements and positioned such that, when the skin deflects in response to the impact force, the skin contacts the snubber and the snubber reduces further deflection of the skin into the void.

摘要翻译： 在一些实施例中，飞行器包括结构组件，皮肤和缓冲器。 结构组件包括第一刚性元件和第二刚性元件。 第一和第二刚性元件由空隙分隔开。 皮肤靠近结构组件设置并且邻近空隙，使得皮肤响应于由皮肤接收的冲击力而偏转到空隙中。 缓冲器设置在第一刚性元件和第二刚性元件之间的空隙中并且定位成使得当皮肤响应于冲击力而偏转时，皮肤接触缓冲器，并且缓冲器减少皮肤进一步进入空隙的偏转。

公开(公告)号：US20140145035A1

公开(公告)日：2014-05-29

申请号：US13689743

申请日：2012-11-29

申请人： The Boeing Company

发明人： Kelly L. Boren

IPC分类号： B64D45/00 ,  B64D1/00

CPC分类号： B64D1/18 ,  A01M29/12 ,  B64D1/16 ,  B64D45/00 ,  B64D2045/0095

摘要： An aircraft comprises an aircraft body, and apparatus, carried by the body, for discharging a persistent vapor of bird repellant into an elevated airspace.

摘要翻译： 一架飞机包括飞行器主体和由身体携带的装置，用于将悬浮剂的持续蒸气排放到升高的空域。

公开(公告)号：US08528317B2

公开(公告)日：2013-09-10

申请号：US12859806

申请日：2010-08-20

申请人： Valerio Gerez ,  Claude Alain Mazur

发明人： Valerio Gerez ,  Claude Alain Mazur

IPC分类号： F02K9/38 ,  B64D33/02

CPC分类号： G07C5/0891 ,  B64D45/00 ,  B64D2033/022 ,  B64D2045/0095 ,  F01D21/003 ,  F01D21/04 ,  F02C7/05 ,  F02C7/057

摘要： A method and a system for detecting the ingestion of an object by an aircraft turbine engine during a mission is disclosed. The method includes: acquiring during the mission digital images of the operating fan of the turbine engine, these images being acquired at an acquisition frequency proportional to the speed of rotation of the fan and to the number of blades of the fan; identifying the different phases of the mission of the aircraft for each phase of the mission; comparing the images of the fan with at least one reference image corresponding to sound operation of the fan; and, if necessary, identifying each abnormal image of the fan which differs from the corresponding reference image, the identification of an abnormal image of the fan corresponding to the crossing of an alert level for detecting the ingestion of an object by the turbine engine.

摘要翻译： 公开了一种用于在任务期间检测由飞行器涡轮发动机摄入物体的方法和系统。 该方法包括：在任务期间获取涡轮发动机的操作风扇的数字图像，以与风扇的旋转速度和风扇的叶片数成比例的采集频率获取这些图像; 确定飞行任务每个阶段的飞行任务的不同阶段; 将风扇的图像与对应于风扇的声音操作的至少一个参考图像进行比较; 并且如果需要，识别与相应的参考图像不同的风扇的异常图像，识别与用于检测涡轮发动机摄入的物体的警报水平的交叉相对应的风扇的异常图像。

公开(公告)号：US20170099827A1

公开(公告)日：2017-04-13

申请号：US15287811

申请日：2016-10-07

申请人： Lite Enterprises Inc.

发明人： Donald Ronning

IPC分类号： A01M29/10 ,  H05B33/08

CPC分类号： A01M29/10 ,  B64D45/00 ,  B64D47/02 ,  B64D2045/0095 ,  H05B33/086

摘要： Wildlife deterrence methods and systems use mono-colored light within a sensitivity range of a short-wavelength-sensitive (SWS) photoreceptor of a species to be deterred, such as an avian species. The mono-colored light may be generated by one or more high brightness mono-colored light emitting diodes (LEDs) and may be within 25 nm of a peak absorption wavelength of the SWS photoreceptor of the species. The mono-colored light is directed to a deterrence area with an intensity sufficient to cause at least a temporary disruption of visual perception in the species to induce an augmented behavioral response in the species resulting in avoidance of the deterrence area. The mono-colored light may also be generated as intermittent pulses having a duration sufficient to keep a pupil of an eye of the species in a continuous unstable state to prevent light adaption by the species.

公开(公告)号：US09534540B2

公开(公告)日：2017-01-03

申请号：US14265388

申请日：2014-04-30

申请人： Jose Antonio Tuero

发明人： Jose Antonio Tuero

IPC分类号： F02C7/057 ,  F02C7/25 ,  B64D25/00 ,  B64D31/06 ,  F02C7/05 ,  B64D45/00

CPC分类号： F02C7/25 ,  B64D25/00 ,  B64D31/06 ,  B64D2045/0095 ,  F02C7/05 ,  F02C7/057 ,  F05D2220/323 ,  F05D2230/80 ,  F05D2270/09 ,  F05D2270/44 ,  F05D2270/805

摘要： An automatic emergency radar and proximity sensor activated protection system that could assist to prevent commercial, private, or military aircraft jet engines from being damaged or destroyed by the installment of a Shielding Blade Assembly which will immediately close when detection of objects such as; birds, debris, or other destructive elements try to enter through the engine intake while the aircraft is in FLIGHT causing the Internal Air Injection Unit (A.I.U.) to supply high volumes of air in order for the engine to stay operational and prevent it from stalling while in FLIGHT.

摘要翻译： 一种自动应急雷达和接近传感器激活的保护系统，可以帮助防止商业，私人或军用飞机喷气发动机被安装的屏蔽刀片组件损坏或破坏，当检测到诸如 鸟类，碎片或其他破坏性元素在飞机飞行时试图通过发动机进气进入，导致内部空气喷射单元（AIU）提供大量的空气，以使发动机保持运行并防止其停止，同时 在飞行中。

公开(公告)号：US09494486B2

公开(公告)日：2016-11-15

申请号：US14007269

申请日：2012-03-15

申请人： Julien Tran ,  Richard Lavignotte

发明人： Julien Tran ,  Richard Lavignotte

IPC分类号： G01M13/00 ,  F01D21/00 ,  F01D21/04 ,  G01N21/88 ,  G01N21/954 ,  B64C5/06 ,  G01N17/00 ,  G01B3/00 ,  B64D45/00 ,  B64C3/14

CPC分类号： G01M13/00 ,  B64C5/06 ,  B64C2003/146 ,  B64D2045/0095 ,  F01D21/003 ,  F01D21/045 ,  F05B2280/6003 ,  F05D2260/80 ,  G01B3/00 ,  G01N17/00 ,  G01N21/8803 ,  G01N21/954 ,  Y02T50/672

摘要： A method for inspecting impacts present on an internal face of a fan casing, the method including: spotting a first impact present on the internal face of the fan casing; delimiting an inspection area containing the first impact; spotting the various impacts present in the delimited inspection area, the various spotted impacts forming a set of impacts to be considered; measuring, for each impact that is to be considered, the depth of length of the impact; for each impact to be considered, determining a harmfulness value, using at least one chart relating the depth and length of each impact to be considered to a level of harmfulness; determining, for the inspection area containing the first impact, a total harmfulness value by adding together the harmfulness level determined for each impact to be considered.

摘要翻译： 一种用于检查存在于风扇壳体的内表面上的冲击的方法，所述方法包括：检测存在于所述风扇壳体的内表面上的第一冲击; 划定包含第一冲击的检查区域; 查明划定的检查区存在的各种影响，各种影响形成一套待考虑的影响; 测量，对于要考虑的每个影响，影响的长度的深度; 为了考虑每一个影响，确定一个有害的价值，使用至少一个将每个影响的深度和长度相关的图表视为有害程度; 对于包含第一冲击的检查区域，通过将要考虑的每个影响确定的有害程度加在一起来确定总危害值。

公开(公告)号：US20160029615A1

公开(公告)日：2016-02-04

申请号：US14885623

申请日：2015-10-16

申请人： Government of the United States, as represented by the Secretary of the Air Force

发明人： Jeffrey M. Newcamp ,  Garrett D. Womack ,  Michael D. Foley ,  Carson B. Fugal

IPC分类号： A01M29/10 ,  B64D45/00 ,  A01M29/16

CPC分类号： A01M29/10 ,  A01M29/16 ,  B64D45/00 ,  B64D2045/0095

摘要： A system for deterring bird strikes on an airborne aircraft is provided. The system includes at least one light configured to project light at optical wavelengths within an avian species optical sensitivity but having low or no observability by pilots. The light is further configured to flash. The system additionally includes at least one audio projection device configured to broadcast alert or predatory calls within avian species auditory capability. The audio projection device is also capable of audio projection in airflow having speeds up to about 250 KIAS.

摘要翻译： 提供了一种用于阻止飞机上的鸟击的系统。 该系统包括至少一个配置成在鸟类光学灵敏度内投射光的波长的光，但是由飞行员具有低或不可观察的光。 光进一步配置为闪光。 该系统还包括至少一个音频投影设备，其被配置为在禽类物种听觉能力内广播警报或掠夺性呼叫。 音频投影设备还能够在高达约250KIAS的气流中进行音频投影。

公开(公告)号：US20140020485A1

公开(公告)日：2014-01-23

申请号：US14007269

申请日：2012-03-15

申请人： Julien Tran ,  Richard Lavignotte

发明人： Julien Tran ,  Richard Lavignotte

IPC分类号： G01M13/00

CPC分类号： G01M13/00 ,  B64C5/06 ,  B64C2003/146 ,  B64D2045/0095 ,  F01D21/003 ,  F01D21/045 ,  F05B2280/6003 ,  F05D2260/80 ,  G01B3/00 ,  G01N17/00 ,  G01N21/8803 ,  G01N21/954 ,  Y02T50/672

摘要： A method for inspecting impacts present on an internal face of a fan casing, the method including: spotting a first impact present on the internal face of the fan casing; delimiting an inspection area containing the first impact; spotting the various impacts present in the delimited inspection area, the various spotted impacts forming a set of impacts to be considered; measuring, for each impact that is to be considered, the depth of length of the impact; for each impact to be considered, determining a harmfulness value, using at least one chart relating the depth and length of each impact to be considered to a level of harmfulness; determining, for the inspection area containing the first impact, a total harmfulness value by adding together the harmfulness level determined for each impact to be considered.

摘要翻译： 一种用于检查存在于风扇壳体的内表面上的冲击的方法，所述方法包括：检测存在于所述风扇壳体的内表面上的第一冲击; 划定包含第一冲击的检查区域; 查明划定的检查区存在的各种影响，各种影响形成一套待考虑的影响; 测量，对于要考虑的每个影响，影响的长度的深度; 为了考虑每一个影响，确定一个有害的价值，使用至少一个将每个影响的深度和长度相关的图表视为有害程度; 对于包含第一冲击的检查区域，通过将要考虑的每个影响确定的有害程度加在一起来确定总危害值。

公开(公告)号：US08616144B2

公开(公告)日：2013-12-31

申请号：US13173822

申请日：2011-06-30

申请人： Aharon Yifrach

发明人： Aharon Yifrach

IPC分类号： A01M29/32 ,  A01M29/00

CPC分类号： A01M31/002 ,  A01M29/32 ,  B64D45/00 ,  B64D2045/0095

摘要： A system for reducing damage by birds to an airplane, the system including: (a) a detector mounted on the airplane, operable to detect a bird in a vicinity of the airplane and to generate detection information indicative of motion of the bird; (b) a processor, connected to the detector, configured to analyze the detection information and to selectively trigger activation of a jetting system that is mounted on the airplane in response to a result of the analysis; and (c) the jetting system, operable to jet a high pressure jet onto a bird.

摘要翻译： 一种用于减少鸟类对飞机的伤害的系统，所述系统包括：（a）安装在飞机上的检测器，可操作以检测飞机附近的鸟类并产生指示鸟的运动的检测信息; （b）连接到所述检测器的处理器，被配置为分析所述检测信息并且响应于所述分析的结果而选择性地触发安装在所述飞机上的喷射系统的激活; 和（c）喷射系统，可操作以将高压射流喷射到鸟上。

公开(公告)号：US20130320103A1

公开(公告)日：2013-12-05

申请号：US13487415

申请日：2012-06-04

申请人： ZAMIR MARGALIT

发明人： ZAMIR MARGALIT

IPC分类号： B05B1/14

CPC分类号： B64D45/00 ,  B64D2045/0095

摘要： A foreign object damage protection system comprises a sensor for detecting a foreign object, a fluid in a reservoir, a means for dispensing the fluid, the means for dispensing the fluid in communication with the reservoir, and a control unit, whereby when the sensor detects a foreign object, the control unit causes fluid to be dispensed from the reservoir through the means for dispensing and towards the foreign object. The sensor is attachable to one or more locations on an aircraft, such as a wing, nose, windshield, fuselage or tail. The sensor can be a radar sensor, weather radar sensor, weather radar sensor modified to detect objects at short ranges, infra-red sensor, forward-looking infrared sensor, a light detection and ranging sensor, motion sensor, thermal sensor, or video sensor. The system provides a way to protect an aircraft from striking foreign objects, such as birds, in the path of the aircraft.

摘要翻译： 异物损坏保护系统包括用于检测异物的传感器，储存器中的流体，用于分配流体的装置，用于分配与储存器连通的流体的装置以及控制单元，由此当传感器检测到 异物，控制单元通过用于分配的装置并且朝向异物从储存器分配流体。 传感器可附接到飞机上的一个或多个位置，例如机翼，鼻子，挡风玻璃，机身或尾部。 传感器可以是雷达传感器，天气雷达传感器，气象雷达传感器，用于检测短距离物体，红外传感器，前瞻性红外传感器，光检测和测距传感器，运动传感器，热传感器或视频传感器 。 该系统提供了一种保护飞机在飞机路径上不受外来物体（如鸟类）的打击的方法。