公开(公告)号：US20190185179A1

公开(公告)日：2019-06-20

申请号：US15846783

申请日：2017-12-19

申请人： Bell Helicopter Textron Inc.

发明人： Cheng-Ho Tho ,  Michael Reaugh Smith

IPC分类号： B64D45/00 ,  B64C1/14 ,  B64C1/34

CPC分类号： B64D45/00 ,  B64C1/1484 ,  B64C1/1492 ,  B64C1/34 ,  B64D2045/0095

摘要： An in-flight impact protection system for aircraft. An aircraft having a panel, with a sensor disposed on the aircraft and adapted to transmit a signal and receive a reflection of the signal. A controller coupled to the sensor and adapted to receive the reflection from the sensor to determine whether an object is near the aircraft's panel. An inflation device, which includes a tube member, is coupled to the controller and positioned inside the aircraft, proximate the panel. After determining that the object is near the panel, the controller can activate the inflation device so that the tube member inflates, thereby buttressing at least a portion of the panel. The panel can be a windshield, fuselage member, or other suitable component.

公开(公告)号：US20180002034A1

公开(公告)日：2018-01-04

申请号：US14999817

申请日：2016-07-01

申请人： Maurice A. Khawam

发明人： Maurice A. Khawam

IPC分类号： B64D47/06 ,  F03D80/00 ,  B64C19/00

CPC分类号： B64D47/06 ,  A01M29/10 ,  B64D2045/0095 ,  B64D2203/00 ,  F03D80/10 ,  Y02E10/726

摘要： The present invention is an aircraft lighting system. In particular, the present invention is directed to an aircraft lighting system with light that is directed toward an aircraft's engines to deter bird strikes. The lighting system for a jet-powered aircraft has at least one light mounted on an aircraft fuselage aimed at an engine inlet of an engine nacelle of the aircraft. The illumination from the light comprises ultraviolet light between 300 and 400 nm in wavelength and the light flashes at a pre-determined frequency preferably between 1 and 3 Hz. Additional lights can be mounted on the engine nacelles to illuminate outer engine nacelles. Preferably, the engine of the aircraft also has blades coated in fluorescent or iridescent paint to increase the reflectivity of the blades to further illuminate the blades of the engine. The lighting system preferably automatically illuminates the engine inlets during take-off and descent.

公开(公告)号：US09708030B1

公开(公告)日：2017-07-18

申请号：US13315264

申请日：2011-12-08

申请人： Jonathan W. Gabrys ,  Richard Laverty ,  Babu Meka

发明人： Jonathan W. Gabrys ,  Richard Laverty ,  Babu Meka

IPC分类号： B64C1/00 ,  B63B1/24

CPC分类号： B63B1/244 ,  B64C3/26 ,  B64D45/00 ,  B64D2045/0095

摘要： An impact-energy tolerant method and structures for impact-energy absorption and penetration resistance are disclosed. A body comprising a body end, and a fiber band comprising supplemental attachment sites located between an inner wall and an outer wall of the body end.

公开(公告)号：US09573672B2

公开(公告)日：2017-02-21

申请号：US14417406

申请日：2013-06-20

申请人： AIRBUS OPERATIONS (SAS)

发明人： Francis Dazet

IPC分类号： B64C1/00 ,  B64C3/00 ,  B64C5/00 ,  B64C3/28 ,  B64D45/00

CPC分类号： B64C3/28 ,  B64D45/00 ,  B64D2045/0095

摘要： A device for protecting a front spar structure of a central casing -of an aircraft wing and at least one item of equipment situated in the wing, comprising: a shielding surface extending in front of the front spar of the central casing, from a surface of an intersection between the wing and the fuselage delimited by the root of the wing, transversely to the surface of intersection, to a first rib of the central casing partially surrounding at least one item of equipment; and means -for fixing the shielding surface to the central casing producing an isostatic link.

摘要翻译： 一种用于保护飞机机翼的中心壳体的前翼梁结构和位于机翼中的至少一个设备的装置，包括：从中心壳体的前翼梁的前面延伸的屏蔽表面， 机翼与机翼根部之间的横向于交叉路口表面的机身与机身之间的交点连接至部分围绕至少一件设备的中央壳体的第一肋; 以及用于将屏蔽表面固定到中心壳体的装置，其产生等静压连杆。

公开(公告)号：US20130277499A1

公开(公告)日：2013-10-24

申请号：US13840512

申请日：2013-03-15

申请人： EUROCOPTER

发明人： Luc Lecerf ,  Vincent Moreau ,  Xavier Maraninchi ,  Jean-Charles Sicard

IPC分类号： B64C3/18

CPC分类号： B64C3/185 ,  B64C3/28 ,  B64C5/02 ,  B64C27/04 ,  B64D2045/0095

摘要： An airfoil (10) having a main structure (15) including at least one spar (16) and a front structure (20) forming a leading edge (21), said airfoil (10) having an empty space (25) between said main structure (15) and said front structure (20). The airfoil (10) includes a rigid deflector member (30) in said empty space (25), the deflector member being fastened to the main structure (15), said deflector member (30) having a sharp edge (31) facing towards said front structure (20) in order to deflect an external obstacle impacting against said front structure (20).

摘要翻译： 具有主结构（15）的翼型件（10）包括至少一个翼梁（16）和形成前缘（21）的前结构（20），所述翼型件（10）在所述主体 结构（15）和所述前部结构（20）。 机翼（10）在所述空的空间（25）中包括一个刚性偏转构件（30），该导流构件紧固到该主结构（15）上，该导流构件（30）具有一锋利边缘（31） 前部结构（20），以便偏转撞击所述前部结构（20）的外部障碍物。

公开(公告)号：US08528864B2

公开(公告)日：2013-09-10

申请号：US13526080

申请日：2012-06-18

申请人： Rafael Villanueva Montero

发明人： Rafael Villanueva Montero

IPC分类号： B64C1/00

CPC分类号： B64D45/00 ,  B64D2045/0095 ,  F41H5/06

摘要： A protection device includes a flexible laminar body resistant to impacts, arranged separately from the body to be protected and put in the way of the beam of possible trajectories with which a foreign object could impact on the object to be protected, and it includes a plurality of energy absorption elements, provided with device clamping elements over a support structure positioned outside of the beam of possible trajectories, in order for the flexible laminar body to intercept an impact trajectory by the foreign object, resulting in its deformation and the subsequent progressive extension of the energy absorption elements reducing the loads to be supported by the support structure. The protection device is applied to prevent birds or other objects from impacting on sensitive areas of aircraft. The protection device is of a textile nature of reduced weight.

摘要翻译： 保护装置包括抵抗冲击的柔性层状体，与要保护的主体分开布置，并且妨碍异物可能撞击到待保护物体的可能轨迹的波束，并且其包括多个 的能量吸收元件，其在位于可能轨迹的光束外部的支撑结构上设置有装置夹紧元件，以便柔性层流体拦截异物的撞击轨迹，导致其变形和随后的逐渐延伸 能量吸收元件减少由支撑结构支撑的负载。 保护装置用于防止鸟类或其他物体撞击飞机敏感区域。 保护装置具有减轻重量的纺织性质。

公开(公告)号：US08164462B1

公开(公告)日：2012-04-24

申请号：US12544379

申请日：2009-08-20

申请人： Jacqueline Carmela Bose ,  August Richard Bose

发明人： Jacqueline Carmela Bose ,  August Richard Bose

IPC分类号： G08B23/00

CPC分类号： A01M29/18 ,  A01M29/10 ,  A01M31/002 ,  B64D2045/0095

摘要： The geese chasing system includes of a housing encasing a visual signaling capability, sensor, and audio signaling capability. A plurality of housings can be installed upon the nose and wings of an aircraft in order to direct more signaling strength as well as to accommodate larger aircraft. The geese chasing system also include a cockpit alarm that provides a manual override as well as an automated signaling capability.

摘要翻译： 鹅追逐系统包括包围视觉信号能力，传感器和音频信号能力的外壳。 多个壳体可以安装在飞机的鼻翼和翼上，以便引导更多的信号强度以及适应较大的飞行器。 鹅追逐系统还包括提供手动超驰以及自动信令功能的驾驶舱报警器。

公开(公告)号：US20110041474A1

公开(公告)日：2011-02-24

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 ,  F01D25/00 ,  G01M15/00

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

摘要： The invention relates to a method and a system for detecting the ingestion of an object by an aircraft turbine engine during a mission. The method includes the steps of 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 (E10), identifying the different phases of the mission of the aircraft (E40), 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 (E60), 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 (E90).

摘要翻译： 本发明涉及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。 该方法包括以下步骤：在任务期间获取涡轮发动机的操作风扇的数字图像，这些图像以与风扇的旋转速度成比例的获取频率和风扇的叶片数（E10）获取， 对于任务的每个阶段，识别飞机任务的不同阶段（E40），将风扇的图像与对应于风扇的声音操作（E60）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（E90）。

公开(公告)号：US12054283B1

公开(公告)日：2024-08-06

申请号：US18463069

申请日：2023-09-07

申请人： HONEYWELL INTERNATIONAL INC.

发明人： Raghavendra Nagappa ,  Gokul Murugesan ,  Jyotismita Sahoo ,  Senthil Kumar S

IPC分类号： B64D45/00 ,  B64C27/32 ,  F21V7/00 ,  F21V23/02

CPC分类号： B64D45/00 ,  B64C27/32 ,  F21V7/0008 ,  F21V7/0091 ,  F21V23/02 ,  B64D2045/0095

摘要： A lighting system for an aircraft having at least one rotationally mounted propeller assembly that includes hub and a plurality of rotor blades extending radially away from the hub includes a light source and an optical element. The light source is mounted within the hub and is configured, upon being energized, to emit light in a first direction. The optical element is mounted within the hub and is disposed to receive the light emitted by the light source and is configured, upon receipt of the light, to redirect the light radially outward from the hub so that the light reflects off the rotor blades.

公开(公告)号：US20230399123A1

公开(公告)日：2023-12-14

申请号：US17806222

申请日：2022-06-09

申请人： General Electric Company

发明人： Kirti Petkar ,  Sesha Subramanian ,  Nicholas J. Kray

IPC分类号： B64D45/00 ,  B64D47/02 ,  G02B30/56

CPC分类号： B64D45/00 ,  B64D47/02 ,  G02B30/56 ,  B64D2045/0095

摘要： In one aspect, a device for preventing bird strikes to an engine. The device includes a projector mounted on a component of the engine. The projector is positioned to project an image outside of the engine. In another aspect, an engine for an aircraft. The engine includes an engine component and a projector mounted on the engine component. The projector is positioned to project an image outside of the engine.