公开(公告)号：US20160340023A1

公开(公告)日：2016-11-24

申请号：US14718324

申请日：2015-05-21

申请人： EMBRAER S.A.

发明人： Alysson Kennerly COLACITI ,  Leandro Guilherme CRENITE SIMÕES ,  Alexandre Viana FERREIRA ,  Micael Gianini VALLE do CARMO ,  Mário TRICHES, JR. ,  Vinicius Losada GOUVEIA

IPC分类号： B64C7/00 ,  B64C9/18

CPC分类号： B64C7/00 ,  B64C9/18 ,  Y02T50/32

摘要： Flap track fairing systems are split into a forward immovably fixed portion and an aft movable portion. The fixed forward portion is immovably attached to the main wing structure of an aircraft while the movable aft portion is attached either to the movable components of the flap deployment mechanism or to the lower surface of the flap. A separation line between the forward movable portion and the aft fixed portion is provided such that the movable portion does not interfere structurally with the flap fairing structure during a flap extension/retraction cycle. An airflow deflector is positioned near a forward separation edge of the aft fairing portion so as to be positioned within a gap defined between the forward edge of the aft fairing portion and a rearward edge of the forward fairing portion when the flap is in the deployed configuration thereof to thereby deflect airflow away from the interior space of the fairing.

摘要翻译： 挡板整流罩系统分为前进固定部分和后部活动部分。 固定的前部不可移动地附接到飞行器的主翼结构，而可移动的后部附接到翼片展开机构的可移动部件或者附接到翼片的下表面。 前后可动部和后固定部之间的分离线设置成使得可动部在翼片延伸/缩回循环期间不会与翼片整流装置结构地干涉。 当翼片处于展开构型时，气流偏转器位于后整流罩部分的前分离边缘附近，以便定位在后整流罩部分的前边缘和前整流罩部分的后边缘之间的间隙内 从而使气流偏离整流罩的内部空间。

公开(公告)号：US09476533B2

公开(公告)日：2016-10-25

申请号：US14595838

申请日：2015-01-13

申请人： EMBRAER S.A.

发明人： Sideto Futatsugi ,  Francisco Keller Klug ,  André Gasparotti

IPC分类号： F16K47/02 ,  F16L55/033

CPC分类号： F16L55/033 ,  F16L55/041

摘要： Fluid attenuator systems and methods for attenuating fluid ripple waves within a main fluid line (e.g., a main hydraulic fluid line of an aircraft hydraulic system). At least one attenuator branch conduit may be provided in fluid communication with and at substantially a right angle to the main fluid line with a porous material positioned therewithin (e.g., at an open inlet or a closed distal end of the at least one attenuator branch conduit). The porous material may be a metallic or ceramic open-cell foam material. Multiple attenuator branch conduits may be provided with each having a different length as compared to the others. In such embodiments, the porous material may (or may not) be positioned within the different length attenuator branch conduits (e.g., at an open inlet or a closed distal end of respective ones of attenuator branch conduits).

摘要翻译： 用于衰减主流体管线（例如，飞行器液压系统的主液压流体管线）内的流体波纹波的流体衰减器系统和方法。 可以提供至少一个衰减器分支导管，其与主流体管线流体连通并且与主流体管线基本成直角，其中多孔材料定位在其中（例如，在至少一个衰减器分支导管的开放入口或封闭的远端处 ）。 多孔材料可以是金属或陶瓷开孔泡沫材料。 可以提供多个衰减器分支导管，每个衰减器分支导管与其它分支导管的长度不同。 在这种实施例中，多孔材料可以（或可以不）定位在不同长度的衰减器分支导管内（例如，在相应的衰减器分支导管的开放入口或封闭的远端）。

公开(公告)号：US20160244150A1

公开(公告)日：2016-08-25

申请号：US14631423

申请日：2015-02-25

申请人： EMBRAER S.A.

发明人： Helio HIRANO ,  Luis Gustavo TRAPP

IPC分类号： B64C11/46

CPC分类号： B64C11/46 ,  B64C5/02 ,  B64C5/06 ,  B64C23/005 ,  B64D27/04 ,  B64D27/10

摘要： Propeller-driven craft (e.g., aircraft) are provided with at least one propulsion system having at least one engine and at least one aerial tractor propeller which generates a propeller propwash airflow when driven by the engine. At least one airfoil is disposed in the propeller propwash airflow of the at least one aerial tractor propeller. The airfoil is contoured and oriented relative to a swirl rotation angle (ω) of the propeller propwash airflow in order to induce a forward force component on the craft in response to the propeller propwash airflow over the at least one airfoil, thus improving the craft's performance and/or reducing fuel consumption.

摘要翻译： 螺旋桨驱动的工艺（例如飞行器）具有至少一个具有至少一个发动机和至少一个空中拖拉机螺旋桨的推进系统，其在由发动机驱动时产生螺旋桨推动气流。 至少一个翼型件设置在至少一个空中拖拉机螺旋桨的螺旋桨推动气流中。 翼型件相对于螺旋桨推流气流的旋转旋转角度（ω）成形和定向，以便响应于至少一个翼型上的螺旋桨推动气流而引起飞行器上的向前力分量，从而提高飞行器的性能 和/或降低燃料消耗。

公开(公告)号：US09327751B2

公开(公告)日：2016-05-03

申请号：US13886575

申请日：2013-05-03

申请人： EMBRAER S.A.

发明人： Lallo Kametada Nou ,  Marcelo Andrey de Albuquerque Bonifacio

IPC分类号： B62B3/04 ,  B64F5/00 ,  B66C1/42

CPC分类号： B62B3/04 ,  B64F5/10 ,  B64F5/50 ,  B66C1/42

摘要： Assemblies and methods for the handling, transporting and/or positioning component parts include a jig assembly for supporting a component part is provided with an elongate spar assembly, a plurality of rib assemblies attached to the spar, and a plurality of tensionable strap assemblies operatively associated with the rib assemblies for capturing and holding the component part against the rib assemblies. The strap assemblies may include a strap ratchet mechanism and a strap, so that operation of the strap ratchet mechanism allows strap slack to be removed thereby tensioning the strap. The jig assembly may be positioned and oriented by suspension cables and a hoist mechanism to allow it to be removably connected to a moveable transport dolly.

摘要翻译： 用于处理，运输和/或定位部件的组件和方法包括用于支撑部件的夹具组件设置有细长的翼梁组件，附接到翼梁的多个肋组件和可操作地相关联的多个可张紧的带组件 其中所述肋组件用于捕获并将所述部件保持抵靠所述肋组件。 带组件可以包括带棘轮机构和带，使得带棘轮机构的操作允许带松弛被去除，从而张紧带。 夹具组件可以通过悬挂电缆和提升机构定位和定向，以允许其可移除地连接到可移动的运输台车。

公开(公告)号：US09284035B2

公开(公告)日：2016-03-15

申请号：US13730809

申请日：2012-12-28

申请人： EMBRAER S.A.

发明人： Danilo Seixas Victorazzo

IPC分类号： B32B37/00 ,  B64C1/12 ,  B29D99/00 ,  B29C70/34 ,  B64C1/06 ,  B64C1/00

CPC分类号： B64C1/064 ,  B29C70/28 ,  B29C70/342 ,  B29C70/44 ,  B29C70/683 ,  B29C70/865 ,  B29D99/001 ,  B29D99/0017 ,  B64C1/061 ,  B64C1/12 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T156/10 ,  Y10T156/1002 ,  Y10T428/2457 ,  Y10T428/24661

摘要： A process for fabricating an integrated panel structures and the structures thereby fabricated are provided with first and second stiffeners positioned on a base skin so that the stiffeners intersect at respective intersecting regions. First and second fiber-reinforced resin-composite overlapping layers are provided on the first and second stiffeners so that at least lateral regions thereof are laminated to a corresponding region of the base skin. The base skin and the overlapping layers may be assembled with the first and second stiffeners to form a panel preform which may then be subjected to curing conditions so as to co-cure all previously uncured components and thereby form an integrated composite panel structure with mutually intersecting first and second stiffeners.

摘要翻译： 一种用于制造集成的面板结构和由此制造的结构的方法设置有位于基底皮肤上的第一和第二加强件，使得加强件在相应的交叉区域相交。 第一和第二纤维增强树脂复合重叠层设置在第一和第二加强件上，使得至少其横向区域层压到基底皮肤的相应区域上。 基础皮肤和重叠层可以与第一和第二加强件组装以形成面板预成型件，然后可以对其进行固化条件，以便共同固化所有先前未固化的组分，从而形成具有相互交叉的整合的复合面板结构 第一和第二加强筋。

公开(公告)号：US20160019808A1

公开(公告)日：2016-01-21

申请号：US14741175

申请日：2015-06-16

申请人： Embraer S.A.

发明人： Nilson Emanuel Bezerra CHAVEZ ,  Guilherme DE MIRANDA CARA ,  Nelson Jose Issa DE MACEDO

IPC分类号： G09B9/30 ,  G09B9/24 ,  G09B5/06

摘要： A system and method for training an aircraft pilot employs a station that delivers training lessons in the form of output and also receives input data from the trainee. An apparatus comprising a computational system is capable of displaying content from different types of media, including virtual reality, augmented reality, and variations. A mixed reality environment interacts with a human being, simulating the response of real objects, and also provides necessary information to achieve Learning Objectives for a specific part of training. A register or record of the interactions is used for evaluation.

摘要翻译： 用于训练飞行员飞行员的系统和方法使用以输出形式提供训练课程的站，并且还从受训者接收输入数据。 包括计算系统的装置能够显示来自不同类型的媒体的内容，包括虚拟现实，增强现实和变化。 混合现实环境与人类相互作用，模拟真实物体的反应，并提供必要的信息来实现特定部分培训的学习目标。 交互的记录或记录用于评估。

公开(公告)号：US20150369723A1

公开(公告)日：2015-12-24

申请号：US14309484

申请日：2014-06-19

申请人： Embraer S.A.

发明人： Paulo Anchieta DA SILVA ,  Fernando DOTTA ,  Ricardo Pinheiro RULLI

IPC分类号： G01N21/17 ,  B05D5/00 ,  B05C9/10 ,  B05C11/10 ,  G01N29/09 ,  G01N27/02

CPC分类号： G01N21/17 ,  B05C9/10 ,  B05C11/1015 ,  B05D5/005 ,  B29C73/22 ,  G01N27/02 ,  G01N29/043 ,  G01N29/09 ,  G01N29/348 ,  G01N2291/0258 ,  G01N2291/2694 ,  G06F19/00 ,  G06Q50/22

摘要： An integrated system and method to acquire the health state of a structure identifying the presence of damage, and to self-repair the damage in the considered structure. A sensor network installed in the structure is interrogated by a dedicated hardware for damage detection. In case of damage is detected by the sensor network in the structure, the sensor network is triggered and generates harmonic excitation in the structure. Due to the excitation, the natural frequency of vascular microtubes and/or capsules presented in the structure is reached, promoting their disruption. The vascular microtubes and/or capsules disruption along the damage releases the healing compound, repairing the damaged portion of the structure.

摘要翻译： 一种用于获取识别损伤存在的结构的健康状况的综合系统和方法，并且在所考虑的结构中自我修复损伤。 安装在结构中的传感器网络由用于损坏检测的专用硬件询问。 在结构中传感器网络检测到损坏的情况下，传感器网络被触发并在结构中产生谐波激励。 由于激发，达到在结构中呈现的血管微管和/或胶囊的固有频率，促进它们的破坏。 沿损伤的血管微管和/或胶囊破裂释放愈合化合物，修复结构受损部分。

公开(公告)号：US09194174B2

公开(公告)日：2015-11-24

申请号：US13729416

申请日：2012-12-28

申请人： EMBRAER S.A.

发明人： Aroldo Pontes ,  Danilo Seixas Victorazzo ,  Douglas Carrari Firmino ,  Erich Robert Schaay ,  Fabiano Lobato ,  Flavio Yoiti Sasaki ,  Sidney Osses Nunes ,  Silvio Luiz Francisco Osorio

IPC分类号： H05F3/00 ,  E06B5/10 ,  B64C3/34 ,  B64D37/32 ,  B64C1/14

CPC分类号： E06B5/10 ,  B64C1/1446 ,  B64C3/34 ,  B64D37/32

摘要： There is disclosed a structural arrangement (10) for an access window (30) to a fuel tank (20) with composite coating (40), this structural arrangement (10) comprising an external lid (11) associated to the access window (30) by fastening means (12), the structural arrangement (10) for an access window (30) to a fuel tank (20) with composite coating (40) further comprising a continuous metal frame (31) disposed on an internal portion of the fuel tank (20), fastened to the composite coating (40) internally and perimetrally circumventing the access window (30), the continuous metal frame (31) being cooperative with the external lid (11) in the conduction of an electric current.

摘要翻译： 公开了一种用于具有复合涂层（40）的燃料箱（20）的进入窗（30）的结构布置（10），该结构布置（10）包括与进入窗（30）相关联的外盖（11） ）通过紧固装置（12），用于具有复合涂层（40）的燃料箱（20）的进入窗（30）的结构装置（10）还包括连接金属框架（31） 燃料箱（20），其在内部被紧固到复合涂层（40）并围绕所述进入窗（30）周向地缠绕，所述连续金属框架（31）与外部盖（11）协调以传导电流。

公开(公告)号：US09033277B2

公开(公告)日：2015-05-19

申请号：US13682607

申请日：2012-11-20

申请人： EMBRAER S.A.

发明人： Marcelo Berthoud

IPC分类号： B64C1/14 ,  E05D13/00

CPC分类号： B64C1/1407 ,  E05D13/123

摘要： A counterbalance mechanism for counterbalancing weight of a bottom-hinged door (such as a clamshell-type airstair door of an aircraft) includes an operator handle, a hoist rod pivotally connected at one end to the operator handle and at an opposite end thereof to the door near a bottom region thereof. A force accumulator assembly is provided which includes a force biasing member which accumulates and dissipates a bias force when opening and closing the door, respectively, to provide mechanical counterbalance to the weight of the door. A bellcrank assembly operatively connects the operator handle to the force accumulator. In such a manner, weight counterbalancing of the door is achieved.

摘要翻译： 用于平衡底部铰链门（例如飞机的蛤壳式开井机门）的重量的平衡机构包括操作者手柄，一端枢转地连接到操作者手柄并且在其相对端与 靠近其底部区域的门。 提供了一种力蓄能器组件，其包括力偏压构件，其分别在打开和关闭门时累积并消散偏压力，以向门的重量提供机械平衡。 曲拐组件将操作者手柄操作地连接到力蓄能器。 以这种方式，实现了门的重量平衡。

公开(公告)号：US20150016129A1

公开(公告)日：2015-01-15

申请号：US14259929

申请日：2014-04-23

申请人： EMBRAER S.A.

发明人： Bruno Kimura CASTANHA ,  Fernando Henrique DA SILVA ,  Celso Aparecido Cruz GUEIROS ,  Jay BEEVER ,  Oliver Turci DE CAMARGO ,  Joshua REA ,  Rainer ZIERER

IPC分类号： A62B25/00 ,  A62B18/02 ,  B64D47/02 ,  A62B7/14

CPC分类号： A62B25/005 ,  A62B7/14 ,  A62B18/02 ,  B64D11/00 ,  B64D47/02 ,  B64D2011/0038 ,  B64D2011/0053 ,  B64D2013/003

摘要： Passenger interface units include individual passenger modules having co-located controls for passenger comfort and entertainment systems. The modules will include a glass panel having front and rear surfaces, a structural support panel bonded to the rear surface of the glass panel and a light-emitting unit supported by the support panel behind the rear surface of the glass panel. The rear surface of the glass panel may include an opaque printed coating layer having at least one unpainted region that is transparent to visible light emitted by the light-emitting unit thereby allowing the visible light to be transmitted through the glass panel and visible at the front surface thereof.

摘要翻译： 乘客接口单元包括具有用于乘客舒适和娱乐系统的共同控制的个人乘客模块。 模块将包括具有前表面和后表面的玻璃面板，结合到玻璃面板的后表面的结构支撑面板和由玻璃面板背面后面的支撑面板支撑的发光单元。 玻璃面板的后表面可以包括不透明的印刷涂层，其具有对由发光单元发射的可见光透明的至少一个未涂漆区域，从而允许可见光透过玻璃面板并在前面可见 表面。